EFTA00277580.pdf

• e US Department MAJOR REPAIR AND ALTERATION Of Transportation Federal (Airframe, Powerplant, Propeller, or Appliance) Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification So- r5DO- 1 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions a d disposition of this form. This report is required bylaw (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for ea such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-100 Serial No. 20115 _ Nationality and Registration Mark USA N908JE 2. Owner Name (As shown on registration certificate) J.E.G.E, Inc. = N om Only 3. For FAA Use .. ..• • . OCT Tor, data identified here' pties atoverthInes reqiiFements is approved described aircraft, subject ntorrnity ,uthe dram 43, se 43.7. with applicable for the above I by a person 5 (-1 --f5V 0 — i T Date Sign of Inspector 4. Unit Identificati 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE •VI NICS DIVISION U.S. Certificated Mechanic Radio Class 1,2,3 Limited Airframe Foreign Certificated Mechanic Certificated Repair Station 0 Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date . :,7fr/ C?-7---46 '&/-g_. <71, 0C)Z Signature of Authorized lndi .d4,31) ,/ eeZ Steve Ouellette ( 9/W_ 7. Approval for Return to Service Pursuant to the authority given personsRecified Federal Aviation Administration and is below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the APPROVED O REJECTED BY FAA Flt. Standards Inspector Manufacturer inspectfon Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group -b, Date of Approval or Rejection Der-0,57 _ ,,ao 6 Certificate or Designation No. SD4R514M Signatur ____ 0: thorized I idu d Ouellette ..______ Steve l FAA Form 337 (12-88) EFTA00277580 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the work performect 1•1908JE under Banyan Air Service; Avionics Division work order #71301 completed on a2s/a6 A. Installed ari AirCell Iridium ST-3100 P/N 400-10680-001 and removed a previously installed AirCell AGT.01 P/N 900001-2. Minor wiring changes were made at the mating connector IAW installation manual P/N 800-10680 Rev. B dated June 2005. B. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapterg,'Options,3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 2, paragraphs 24 & 25 and the aircraft's maintenance manual. . 111W: C A functional test of the .ab6e/Aniprrient has been performed FAR25.1309 and FAR25 .1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. The weight change is negligible. the equipment list was updated to reflect this change. E. Instructions for continued airworthiness is attached.. END K Additional Sheets are Attached EFTA00277581 Instruction for Continued Airworthiness for AirCell ST 3100 Aircraft Subscriber Equipment System Installed on Boeing 727-100 N908JE S/N 20115 Revision O. Dated: 9/17/2006 EFTA00277582 • APPLICATION REVISIONS . DESC. NEXT ASSY USED ON REV DESCRIPTION DATE APPROVED ST 3100 ASE SYSTEM BARON 95-B55 A BASELINE RELEASE 2002-10-16 K. FRANTZ B SEE DCN 00179 2002-10-25 K. FRANTZ ._,.... ALL SHEETS CARRY THE SAME REVISION LETTER UNLESS OTHERWISE SPECIFIED DIMENSIONING & TOLERANCING bkW ASME Y14.5M-1994 DIMENSIONS ARE IN INCHES STANDARD TOLERANCES: x = ±. .1 )(X= ± .02 )(XX= ± .010 e . AirCell, Inc. no d 1172 Century Drive ..._.7 Suite 280, Building B Louisville, CO 80027 APPROVED DATE INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ST 3100 ASE SYSTEM PREPARED BY K. FRANTZ YEAR-M O-DA 2002-10-16 MECH DESIGN Z. HOH YEAR-MO-DA 2002-10-16 ELEC DESIGN B. SOUKUP YEAR-M O-DA 2002-10-16 TECH SUPPORT B. NIELSON YEAR-MO-DA 2002-10-16 SYSTEMS K. FRANTZ --\ YEAR-MO-DA 2002-10-16 ENGINEERING J. POLSON YEAR-MO-DA 2002-10-16 SIZE A - CAGE CODE 1NO67 DRAWING NUMBER . 820-10680-001 REV B FILE FORMAT: Microsoft Word 2000 SCALE: NONE WEIGHT: NA SH 1 of 8 FILENAME: 820-10680-001-B.doc • S a • • a a S S 699-10077: A-SIZE SPEC TEMPLATE.DOC EFTA00277584 p p p p p p p. 9 p p p p p ) ) TABLE OF CONTENTS 1 GENERAL INFORMATION 3 1.1 SCOPE OF THIS DOCUMENT 3 1.2 TECHNICAL SUPPORT CONTACT INFORMATION 3 1.3 • GENERAL. NOTES 3 1.4 ADVISORIES 4 2 SYSTEM DESCRIPTION 4 2.1 TOP LEVEL SYSTEM CONFIGURATION 1 "4 2.2 OPERATION OF THE SYSTEM 6 OPERATIONAL TIME LIMITS AND SCHEDULED MAINTENANCE 7 4 UNSCHEDULED MAINTENANCE 7 4.1 TROUBLESHOOTING PROCEDURE 7 5 AIRWORTHINESS LIMITATIONS 7 FIGURES AND TABLES Table 2.1-1 System Component Definition 5 Figure 2.1-1 Block Diagram of ST 3100 ASE System 6 • AirCell, Inc. SIZE CAGE CODE DRAWING NUMBER REV e 1172 Century Drive A 1NQ67 820-10680-001 B Suite 280, Building B FILE FORMAT: Microsoft Word 2000 SH 2 of 8 Louisville, CO 80027 FILE NAME: 820.10680-001-B.doc 699.10077: A-SIZE SPEC TEMPLATE.DOC EFTA00277586 GENERAL INFORMATION 1.1 SCOPE OF THIS DOCUMENT This manual defines the instructions for continued airworthiness (ICAW) for an AirCell_ 3000 Series Aircraft Subscriber Equipment (ASE) system. The manual is written to demonstrate compliance with FARs 23.1529 and 25.1529. Specifically, this manual defines the instructions for the Model 3100 Satellite Telephone System (ST 3100). This manual is subdivided into sections to support the general operation, inspection and maintenance of the ST 3100 system. Section 1 defines general information for the maintenance and airworthiness of the ASE system. Section 2 provides general information on the configuration and operation of AirCell ASE systems. Section 3 presents a discussion of the scheduled maintenance and operational time limits for the system. Section 4 and Appendix A provide instructions for system operational checks, troubleshooting, unscheduled maintenance and component replacement. Section 5 provides a brief statement addressing airworthiness limitations for the ST 3100 system. 1.2 TECHNICAL SUPPORT CONTACT INFORMATION Technical support for AirCell products is available from 08:00 to 17:00 United States Mountain Time (Time Zone GMT —7 hours) Monday through Friday. The contact information for AirCell Technical Support is as follows: From a landline: Phone (in the US): 1.888.286.9876 (toll free) Phone (outside the US): 001.303.379.0278 (toll call) From an AirCell phone: From an Air Mode/AMPS phone (in the US): 611 (toll free) From a SAT Mode (Iridium) phone (worldwide): 2471 (toll free) Email: customerservice@aircell.com Note: The toll free numbers for AirCell phones will only work for AirCell provided phones and services. 1.3 GENERAL NOTES • All pages in this document carry the same revision level. Revision status is indicated by a letter printed on each page of this manual. • The material in this manual is subject to change. Before planning or performing any installation or maintenance operation, check with AirCell Technical Support to verify that this manual is complete and has the latest revision. • AirCell, Inc. welcomes your comments, suggestions, and corrections concerning this manual. Please include in your correspondence the publication number, equipment part number, page or figure number, and a brief description of any problem or consideration you noted. Please send your comments to: AirCell, Inc. Corporate Publication Coordinator 1172 Century Drive Suite 280, Building B Louisville, Colorado 80027 cpc@aircell.com elf AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE A CAGE CODE 1NC)67 DRAWING NUMBER 820-10680-001 REV B FILE FORMAT: Microsoft Word 2000 I SH 3 of 8 FILE NAME: 820-10680-001-B.doc 699-10077: A-SIZE SPEC TEMPLATE.DOC EFTA00277588 1.4 ADVISORIES WARNING Statements in this section contain critical safety information. Read these statements carefully before installing this unit. WARNING Observe standard safety precautions and wear safety glasses to prevent personal injury while performing maintenance on this unit in the aircraft. WARNING Shut off power before connecting or disconnecting the ST 3100 system, as voltage transients may damage the unit or the interface wiring. WARNING Components or subassemblies found in this unit may contain materials such as beryllium oxide, acids, lithium, radioactive material, mercury, etc. that can be hazardous to your health. If the component enclosure gal is broken, precautions must be taken against personal contact or inhalation in accordance with OSHA requirements 29CFR 1910.1000 or superseding documents. AirCell strongly discourages the opening or disassembly of sealed components. WARRANTY AND CERTIFICATIONS Any alteration of this product voids the FAA or FCC certification and the AirCell warranty. 2 SYSTEM DESCRIPTION The ST 3100 ASE system provides access to a range of two way communication options from an aircraft, including voice and data applications. With the ST 3100 system these services are available when the aircraft is in the air or on the ground. The AirCell satellite mode communications link is provided using the 1600 MHz Iridium LEO (Low Earth Orbit-485 miles altitude) satellite network, which provides coverage from the ground up over the entire surface of the earth. 2.1 TOP LEVEL SYSTEM CONFIGURATION The ST 3100 system consists of a number of primary system components. The heart of the system is the ST 3100 ASE Transceiver, which includes internal electronics to support operation in the Iridium satellite network. Other system components include the externally mounted antenna, a low loss coaxial cable, and various user interfaces including multiple ASE handsets (up to 9), an RS-232 data port, and an audio panel interface. AirCell' AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE CAGE CODE DRAWING NUMBER REV A 1NO67 820-10680-001 B FILE FORMAT: Microsoft Word 2000 SH 4 of 8 FILE NAME: 820-10680-001-B.doc 699-10077: A-SIZE SPEC TEMPLATE.DOC EFTA00277590 The primary components of an ASE system include Line Replaceable Units (LRUs) and AirCell specified assemblies (such as coaxial cables or wiring harnesses) that are manufactured or purchased by the system installer. A list of the LRUs and specified assemblies is provided in Table 2.1-1, and a representative block diagram is provided in Figure 2.1-1 to demonstrate the interconnection of a typical ST 3100 system. For detailed information on the system components, please refer to ST 3100 ASE System installation manual (AirCell document 800-10680), or contact AirCell Technical Support for assistance. Table 2.1-1 System Component Definition System Component Designatio n Description AirCell PN. Approved Alternate(s) AirCell PN of Alternate System Transceiver LRU ST 3100 ASE Transceiver 400-10680-001 none Transceiver :Mounting Tray LRU 3/8 ATR Width Mounting Tray 800007-1 3000 Series Mounting Rails 151-10689-001 System Wiring Harness Specified Assembly 26 wire System Harness NA ASE Handset LRU Flush Mount ASE Handset 400-10001-10X* Standard ASE Handset Portable Coilcord ASE Handset Custom Retractable ASE Handset 400-10035-00X* 400-10015-00X* 400-10019-00X* Satellite ASE Antenna LRU 1600 MHz Satellite ASE Antenna, Patch Style 015-10306-001 1600 MHz Satellite ASE Antenna, Blade Style 015-10683-001 Satellite Channel Coaxial Cable Specified Assembly. Low Loss Coaxial Cable NA (vendor item)" ** "X" designates the color of the ASE handsets. The system coaxial cable is a required item that is not provided by AirCell. The system installer will need to purchase this item from an approved vendor as defined later in this document. (MICA: AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE CAGE CODE DRAWING NUMBER REV A 1NQ67 820-10680-001 B FILE FORMAT: Microsoft Word 2000 I SH 5 of 8 FILE NAME: 820-10680-001-B.doc AAt4r4fAco" 699-1C077:A-SIZE SPEC TEMPLATE.DOC EFTA00277592 • . . . .. : I EFTA00277593 ASE SATELLITE \/ ANTENNA I 0 p I I I I I I I I I I ) ) .44111 .\_ AIRCRAFT FUSELAGE ASE SYSTEM XCVR SAT ANTENNA ID AUX CNCTR NO CONNECTION SYS CNCTR ASE SYS HS CNCTR ASE SYS HS CNCTR 1=1--M120 ASE 5Y5 HS CNCTR D ASE SYS RS232 CNCTR ASE HANDSET CHANNEL ASE HANDSET CHANNEL Mffal ASE HANDSET CHANNEL TO AUDIO PANEL TO RS232 DATA TERMINAL TO AIRCRAFT POWER (2.8 Vdc) AIRCRAFT FUSELAGE Figure 2.1-1 Block Diagram of ST 3100 ASE System Note: Each 'Handset Channel' listed above is capable of supporting up to 3 ASE handsets, making it possible to integrate up to 9 handsets in the ST 3100 system. 2.2 OPERATION OF THE SYSTEM The user interface and operation of the ST 3100 system is designed to be very similar to the operation of a terrestrial cellular or PCS phone. Some key features of the ST 3100 system are as follows: • The system will power up when the avionics master switch for the aircraft is powered on. The AirCell system is always on when the avionics master is powered on. • ' The Satellite mode network provides coverage anywhere on (or above) the surface of the earth with a clear view of the sky in all directions. • To place a call from the system handset, the user must verify that the system is 'in service'. SAT mode calls are typically dialed as international long distance calls (00 + country code + phone number). After dialing, the user must press the " SND " key on the handset, and the phone call will proceed as a typical cellular or PCS call. At the completion of a call, the user may press the " END " key to terminate the call. • The user may receive incoming (ground to air) phone calls depending on the in service condition. The user can answer these calls by pressing the " SND " key on the handset. • Data calls can be made from Air to Ground over the ST system by connecting a Data Terminal Equipment device (such as a PC) to the RS-232 port of the system. The ST system has a built in modem function, so some user setup of the DTE will be required. More detailed operating instructions are provided for this system in the ST 3100 User's manual (AirCell document 810-10680). 6N_j.ri•Celf AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE CAGE CODE DRAWING NUMBER REV A 1NQ67 820-10680-001 B FILE FORMAT: Microsoft Word 2000 SH 6 of 8 FILE NAME: 820-10680-001-B.doc 699-10077: A-SIZE SPEC T EMPLATE.D GC EFTA00277594 3 OPERATIONAL TIME LIMITS AND SCHEDULED MAINTENANCE The ST 3100 system is designed and manufactured to be maintenance free after installation. As a result of this design, there are no operational time limits or periodic maintenance checks or procedures that must be performed for the system. Inspections and/or system verification checks are only required in the event of a system failure (On Condition), as defined in Section 4 of this document. As an option, the system operator may perform a visual inspection of the various system components at the aircraft annual inspection, or other periodic maintenance interval as defined by the aircraft manufacturer. 4 UNSCHEDULED MAINTENANCE The ST 3100 system is designed for "On Condition" maintenance only. In the event of a system failure, the system user/aircraft operator is advised to follow the troubleshooting procedure defined in Appendix A of this manual. After performing the basic procedure, the user will either have returned the system to normal operation, or should contact AirCell technical support for additional guidance. Note that, in the process of performing the troubleshooting procedure, authorized field service personnel are permitted to perform repairs to wiring harnesses, RF cable assemblies, mounting interfaces, or (with prior approval from AirCell Technical Support) to remove and replace any of the primary system Line Replaceable Units (LRUs). AirCell does not, under any circumstances, authorize field repair or subassembly level maintenance on any LRU. Sealed LRUs should always be returned to the AirCell FAA Repair Station for evaluation and repair. 4.1 TROUBLESHOOTING PROCEDURE Appendix A provides a guide to identify simple problems that may be identified and/or resolved with simple field inspection and test processes. It is advised that the procedure in this appendix should be performed before contacting AirCell Technical Support for additional instruction. No specialized tools or equipment are required to perform this procedure. In the event that a step in this procedure is not clear, or the results of a procedure are not conclusive, the test operator should feel free to contact Technical Support for assistance. 5 AIRWORTHINESS LIMITATIONS The AirCell ST 3100 ASE system is a non-critical communications system. In accordance with FAR 23.1529 (with Part 23 Appendix G) and FAR 25.1529 (with Part 25 Appendix H) this system has no Airworthiness Limitations for either Part 23 or Part 25 aircraft. The airworthiness limitations section is FAA approved and specifies maintenance required under Sections 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been approved. A7-frCelf AirCell, Inc. 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE CAGE CODE DRAWING NUMBER REV A 1NQ67 820-10680-001 B FILE FORMAT: Microsoft Word 2000 SH 7 of 8 FILE NAME: 820-10680-001-B.doc uctict)ticccfoC 699-10377: A-SIZE SPEC TEMPLATE.DOC EFTA00277596 'a . . % . . . I EFTA00277597 t.d S • 0 P 9 P p p a a a a Appendix A ST 3100 ASE System Troubleshooting Procedure A tirr AirCell, Inc. kjell 1172 Century Drive Suite 280, Building B Louisville, CO 80027 SIZE A CAGE CODE 1NQ67 DRAWING NUMBER 820-10680-001 B F. FILE FORMAT: Microsoft Word 2000 I SH 8 of 8 FILE NAME: 820-10680-001-B.doc 68410077,S. SPEC TEMPLATE.DOC EFTA00277598 TrCell' Symptom Possible Cause Discussion Verification Step(s) Symptom 1 Power is not available to ASE The handset display should always O Verify that the aircraft power system (master avionics switch) is on. Handset Display is System be illuminated when power is O Verify that the ASE system circuit breaker is closed. not illuminated applied to the ASE transceiver. Because the failure of a handset display is unlikely, a `dead' display O Visually inspect the displays of all installed handsets in the system. If all handsets arc off, proceed to the next bullet in this list. If most handsets are illuminated, but one is not, then proceed to Symptom 2. (One or more suggests that there is a problem with O If all handset displays are dead, the problem is likely in the power system wiring handsets integrated in the input power to the ASE system. before the ASE transceiver. Visually check the system connections and the wiring system, no handset . In the event that the one or more harness leads between the transceiver and the aircraft power system. Repair or displays are handset display(s) are not reconnect any obvious problems. illuminated) illuminated, the user/operator should verify that aircraft power is on and O If needed, ring out the power lines per the system wiring diagram. Repair any broken wires or rework to match the system wiring diagram. . available to the ASE transceiver. O If this procedure does not resolve the problem, contact AirCell Technical Support for additional guidance. Symptom 2 Handset Display is Bad connection or faulty wiring between handset and In a system with multiple handsets, if some handsets are operating and - O Some ASE systems integrate multiple handsets. If more than one handset is installed on the system, check the display on all handsets. If only one of multiple not illuminated transceiver. some arc not, then it is likely that either the handset is bad or the handsets is not illuminated, then the problem is either a bad handset or in the handset connection/ wiring harness between that handset cradle and the transceiver. wiring between the handset and the O Perform a visual inspection to verify that ail connections are made in accordance (ASE System has or transceiver is faulty. with the system wiring diagram. Correct any obvious problems. multiple handsets, and the displays of most handsets are on, but one handset is not Bad handset O If all system connections are correct, then switch the `dead' handset with a known good handset and retest the system. If the handset is still dead in the new location, then the handset is bad. Contact AirCell Technical Support for repair/replacement instructions. illuminated.). . O If the known good handset is now dead, then the problem is in the system wiring/connections between the handset and the transceiver. Ring out the lines per the system wiring diagram. Specifically check for 9V power and ground leads on the HS power line from the transceiver system connector. Repair any broken wires or rework the system wiring harness to match the wiring diagram. • O If this procedure does not resolve the problem, contact AirCell Technical Support for additional guidance. A-1 ST 3100 ASE System Troubleshooting Procedure 820-10680-001, Rev B Ceti- IC tttik MiLttlettAdt EFTA00277600 ‘4110 46P 4019 -.4m! VaY INV 10, INF 4mY 441,,w 400.4, WINO mi, wut:.‘soilmOlpf wov011OtiOWWW 14104rOVINVOtiOVIOU Symptom Possible Cause • Discussion Verification St,9(s) Symptom 3 Handset Display is illuminated and display indicates no signal for Satellite (SAT) mode. Possible Cause 3A' System antenna does not have Line of Sight (LOS) view to satellite. The ST 3100 transceiver operates in Satellite (SAT) mode. When in coverage the ST system should detect and register for SAT mode service. If the system does not register, then it is likely that either the antenna does not have a LOS to a satellite (3A), or there is a problem with the RF channel in the aircraft (3B). In this condition, it is unlikely that there is a problem with the system transceiver. Verification Test 3A O Verify that the system SAT antenna has a clear LOS to the sky in all directions. A clear LOS is defined to exist when there are no obstructions (such as buildings, trees, vehicles etc) that are higher than 30 degrees above aircraft horizon in any direction. This should never be a problem in flight. • O Use the handset to enter the SAT lock mode (FCN,.3, 3) keys on the handset. The handset will display the word "IRIDIUM" when the SAT mode is locked. O Once the LOS has been established the system should register on the SAT network within 60 seconds. The system is registered when the "NO SVC" indicator is not visible on the handset display. 0 If the "NO SVC" indicator extinguishes, then the SAT mode is engaged, and the problem is resolved. The user may choose to make a test call and verify the • operation the system. 0 If the "NO SVC" indicator stays illuminated, then the system cannot register, and it is likely that there is an installation or equipment problem. Either contact AirCell Technical Support for additional guidance, or proceed to Verification Test 3B. No Satellite mode signal Possible Cause 3B There is a problem with the Satellite RF channel. • • Verification Test 3B O While the aircraft is on the ground, perform a visual inspection of the ASE system satellite antenna. Verify that the antenna is installed to the aircraft fuselage in accordance with the system antenna installation drawings. Verify the mechanical integrity of the antenna, and that the antenna is reasonably free of dirt, oil, ice and other undesired coatings. O Visually inspect the RF satellite channel, including the coaxial connections to the antenna and the system transceiver. Inspect the coaxial connectors to verify that they are connected in accordance with the system wiring diagram, and that they are not damaged. Look for breaks, kinks or other damage to the coaxial cable. 0 The user is authorized to correct installation errors (such as cabling errors), or to repair minor damage (such as broken coaxial connections, damaged coaxial cables, etc). The user is not authorized to open or modify sealed LRUs. O If these steps do not resolve the problem, contact AirCell Technical Support for additional guidance. Other conditions For all other conditions, contact AirCell Technical Support for guidance. • A-2 ST 3100 ASE System Troubleshooting Procedure 820-10680-001, Rev B EFTA00277602 --tt US Department MAJOR REPAIR AND ALTERATION 0f Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FA Use Only Office IdentificatioA (5O-rspo- iq INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing _ Model 727-100 Serial No. 20115 Nationality and Registration Mark USA N908JE 2. Owner Name (As shown on registration certificate) J.E.G.E, Inc. Address (as shown on registration certificate) 103 Foulk Road STE 202 Wilmington, DE. 19803-3742 3. For FAA Use Only -,i-c:;;;:.,:•• _ •*4-4 .:, 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE AVIONICS DIVISION 1635 NW 51st Place Ft. Lauderdale, FL 33309 U.S. Certificated Mechanic Radio Cl SD4R514M Class Limited Airframe Foreign Certificated Mechanic El Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) *dentified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date October 10, 2006 Signature of Authorized Indivi Steve Ouellette c.- ---- 7. Approval for Return to Service Pursuant to the authority given persons s• • cified below, Federal Aviation Administration and is e. APPROVED the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the O REJECTED BY FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection October 10, 2006 Certificate or Designation No. SD4R514M Signature of orized Ind* - I Steve Ouellette FAA Form 337 (12-88) EFTA00277604 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) The purpose of this 337 is for the work performed on N908JE under BanYan Air Service; Avionics Division work order #71301 completed on October 4, 2006. A. Installed an AirCell Iridium Antenna P/N S67-1575-109 in accordance with DER Services drawing number 2006-173-1 approved per FAA form 8130-3 signed by Robert Belgau DERT designation number DERT-510024-CE. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapter 11, sections 3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 3, paragraphs 43 & 44 and the aircraft's maintenance manual. A log book entry and equipment list was generated to reflect the above installation. The weight change is negligible. the equipment list was updated to reflect this change. Instructions for Continued Airworthiness is "on condition only." END Additional Sheets are Attached EFTA00277605 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE October 07, 2006 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL 727-31 TYPE (A irPlane. Radio, Helicopter, etc) Airplane NAME OF APPLICANT Banyan Air Services LIST OF DATA IDENTIFICATION TITLE DER Services Drawing: 2006-173-1 _ Rev. I/R -i.'...- *-::-i:Dtd. 27-Sep-06 END END • Iridium Antenna END END END Effectivity: S/N: 20115, T/N: N908JE Installation STA 515 - BTWN S-2R & END END END END END_ _ _ _ _ _ ___ 98-11-03 RI. Certification to FAR 25.571, may be required. Per Advisory Circular 25.1529-1 Repairs on Transport Category Airplanes, of the structure must be performed before of the above listed data are approved design data and is not installation approval. info) aircraft model and serial number listed Approved structural analysis on file Services, Inc. office in Birmingham Serial No. 20115 S-3R . END_ END Note: This aircraft is effected fatigue evaluation Continued Airworthiness and fatigue Notes: by AD of structure of Structural evaluation . only for more valid for the based on FAA FL. or DER 727.-31 Damage - tolerance and Instructions for; the damage tolerance 4/11/2003. . herein. This approval below at DER Services office AL. 1) The structural aspects is only for the engineering (Ref. 8110.45 8/30/02 2) This approval is 3) This approval is in Ft. Lauderdale, Model No. PURPOSE Approve data for low profile antenna installation (structural aspects only, Static Analysis) OF DATA APPLICABLE REQUIREMENTS (LIST SPECIFIC SECTIONS) CAR 4b.200, 4b.201, 4b.202, 4b.260, 4b301, 4b302, 4b303, 4b.306 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I (We) Therefore pi Approve these data SIGNATURES) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Robert J. Belgau DERT-510024-CE Structures — , FAA FORM 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. F2006-173 EFTA00277606 8 7 6 5 4 3 2 1 D C -o B A GENERAL NOTES: 1. FABRICATE PART(s) AS SHOWN. 2. BEFORE INSTALLATION OF DOUBLER, ROLL TO MATCH AIRCRAFT MOLD LINE RADIUS. 3. BREAK ALL SHARP EDGES .0201.030 R. 4. TREAT ALL REWORKED AREAS USING ALODINE 1201S (PER MIL-C-5541, CLASS 1A) AND TVVO (2) COATS OF EPDXY POLYAMIDE PRIMER (PER MIL-P-233377, TYPE I). 5. FINISH ALUMINUM PARTS USING ALODINE 1201S AND TWO (2) COATS OF EPDXY PRIMER. 6. MAINTAIN MINIMUM 2D + 1/16" EDGE DISTANCE FOR ALL FASTENERS ON DETAILS; MINIMUM 2D EDGE DISTANCE ON ASSEMBLY. 7, ALL FASTENERS ARE TO BE INSTALLED IN TRANSITION-FIT HOLES. HOLE TOLERANCE PER NAS618. 8. ALL FASTENER LENGTHS ARE TO BE VERIFIED FOR TOLERANCE PRIOR TO INSTALLATION. 9. INSTALL ALL PARTS AND THREADED FASTENERS WET USING PR1436G TYPE III SEALANT ON ALL FAYING SURFACES. 10. RESTORE ORIGINAL FINISH PER B727 M.M. 51-21. 11. PROTECT REWORKED AREA AGAINST CORROSION PER B727 SRM, CHAPTER 51-10-2. 12. REFERENCE 8727 S.R.M, CHAPTER 51-30 FOR FASTENER REMOVAL AND INSTALLATION PROCEDURES. S - 3R STA 510 13. REINSTALL ALL ADJACENT STRUCTURE REMOVED TO FACILITATE ANTENNA INSTALLATION. 14. BEAD SEAL ANTENNA WITH PRC 1422 SEALENT. 15. REVISE AIRCRAFT RECORDS TO REFLECT INSTALLATION. STA 515.00 S - 2R EXISTING BONDED STRAPS (REF) DESCRIPTION DATE APPROVED I/R INITIAL RELEASE 09-27-2006 EXISTING FUSELAGE SKIN (REF) NAS 1097AD4 - 2 FASTENER CODES ITEM DESCRIPTION K LU K itj NASI097AD4 (TY'P 50 PLS) x 64510428AD 3 (TYP 8 PLS) x STA 520 50 COUNTERSUNK RIVET OPL 8 RIVET - NUTPLATE MS20426AD3- 2 QPL 4 4 SCREW MS24694C55 OPL 3 4 NUTPLATE NAS 1 473A3 QPL 2 1 1 1 DOUBLER - INTERNAL L1 CPS-IRIDIUM ANTENNA 567- 1575-109 0.050" 2024-T3 00 -A -250/5 QPL QPL ITEM QTY NAME PART NUMBER MATERIAL MIL-SPEC VENDOR Ports List CRAVING CREATED FCN, BANYAN AIR SERVICE CRAVING SIZE, B DATE APPROVED 09-27-2006 lJ DER SERVICES 2100 kV 6.311 STREET, Suitt C-I09, FT. LAITIRDAI.E rl. =9. (9509TI.3B32, FAX(954)971-3059 nes date Is provided as • CONFIDENTIAL AND PRIVILEGED 00C(JMENTOebecin BANYAN AIR SERVICE & DER 5•M ass. My oN use of raproductco *afoul the expnrssed tten coneare of DER Sareloatbaxpassly latedcius. My M4064 of 0is docurnerd incluctify INN not Potted IS) rasldabon In pen riOsoul send.n consent ci DER Son nee Is expressly Portirkeen. This aporovei Es Pew] upon AN. mod sr-esti@ ID DER Servicsrs torn BANYAN AIR SERVICE al So. Offs of nsporl corrphillon. My iddlaccial data Mich Osamu reale:is. may mull b afnenftn; 0r COnctoslco(s) expressed haneln UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN INCHES UNSPECIFIED TOLERANCE FRACTIONS ANGLES DECIMALS DRAVN BTU W.D.OLIVERI CHECKED BY' R.J.BELGAU STRESS BY' W.D.OLIVERI ±1/32 .15 MACH. .2 FORMED .X ± .1 .XX t .03 .XXX_ t .010 APPROVED BY. R.J.BELGAU 8 7 5 4 3 TITLE IRIDIUM ANTENNA INSTALLATION STA 515 - BTWN S-2R & S-3R A/C Typr BOEING T'G 2006-173-1 N.A. REV I/R Nod No ' 727-31 TAIL No. r N908JE PROJ 2006-173 -SCALE. SERIAL No 20115 STRL INSTL SHEET 1 OF 3 2 1 D C 4- B A EFTA00277608 8 7 6 5 4 3 2 STA 510 EXISTING FUSELAGE SKIN (REF) VIEW LOOKING UP SOME STRUCTURE REMOVED FOR CLARITY 01.00 CONNECTOR CUTOUT IN SKIN STA 520 IRIDIUM ANTENNA INSTALLATION @ STA 515.00 - BTWN S-2R & S-3R EXISTING BONDED STRAPS (REF) EXISTING BONDED STRAPS (REF) TN. deer b prose.. as • COW IDENTIX. AND PFUYILED0ED DOCUMENT between BANYAN AIR SERVICE DER SerrIces. My Other use or (spend ucton ecnotrt De esOreesslawrInen mos. of DER SessIcse N.sweaty MPMM. My ndsyse of Pis Ovarrent bOumrq (bvl rot ernlletl b) qv...Jon b pert with. written consent of DER Se.. M -Drew lortedden. T. *pus.* Is based v.n dab ft.., sessiebb lo DER Sen.. Rom BANYAN AIR SERVICE al be SIR ot report corrode., My ...Ye/ dale. eh. becomes rear.. may row. In •^r•ran5 eye con:Susie*/ bIreesedb... 4 4 EXISTING BONDED STRAPS (REF) EXISTING FUSELAGE SKIN (REF) SECTION A-A D C 4- DER SERVICES ,'),`." 2006-173-1 2700 N.W. 62/10 STREET, 6us C-109, FT. LAUDERDALE. R 33XS. (554) 571.3832. FAX (M.) . 7 14.0 B SIZE DRAWN BY, W.D.OLIVERI REV UR SERIAL No. . 20115 SCALE 3= 4 SWET 2 OF 3 8 I 7 I 6 5 4 3 2 B A EFTA00277610 8 7 6 5 4 3 2 1 - 0 B 01.62 FASTENER PATTERN (TYP 6 PLS) 00.20 ANTENNA MOUNT HOLE (TYP 4 PLS) 01.00 CONNECTOR CUTOUT ITEM 2 / DOUBLER FABRICATION USE NUTPLATE AS PATTERN FOR RIVET HOLES. (TYP 8 PLS) R 0.25 4.50 0 0 0 0 0 (TYP 4 PLS) 4.13 0 0 0 3.66 O O O 3.19 3.19 O o 2.72 -0 0 0 ( 0 o o o 2.24 Ck O o 1.78 0 1.38 o O ED O o 0 O 1.29 O 0.84 O O O O O O 0 0.38 O 0.00 o CO tO CI O W. to Cl CD CO 1O cn O CO LO C') O cr) t•- e ill CO N CO CD 0, cO CV CO O o o o cNi N (vi ri 4 4 4 4- B A A This data le ortroldid ae • CONFIDENTIAL AND PRA/ILEDDED DOCUMENT betetern BANYAN AiR SERVICE DERE...Mon. Any caw, ow or reproduction without the eapreesed rattan oznunt of DER BeMc.e4 expreeffy forbidden. Any mg.*. of AN 6:.O...nt I:Coelho (but not United quotation in pert without written coreenl of DER Serelpe b eefe...fY forbidden. Thts *pommel Is bawl upon date mad. sysliftes to DER Sonia. eon BANYAN AIR SERVILE el Ow erne of 1900 etelpfli3on. Any edditionei date. which becomes eveiletie, rney refue tr. emending tne oonclusicn(s) freereased herein. DER SERVICES NQG 2006-173-1 2700 N.W. 132.3 STREET. &Ate C-I09, FT. LAUDERDALE. FL. 11309. (p 6e) 971-3832. FAX (964)971-3059 SIZE ERAVN BY. REV W.D.OLIVERI l/R SERIAL No. .2O 1 1 5 SCALE 0.5 = 1 S ET 3 C.F 3 8 7 6 5 fi 4 3 2 EFTA00277612 • , C US Department MAJOR REPAIR AND ALTERATION Of Transportation Federal (Airframe, Powerplant, Propeller, or Appliance) Aviation Administration Form Approved OMB No. 2120-0020 For FA Use Only Office Identification SO- (3 DO -17 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-100 Serial No. 20155 Nationality and Registration Mark USA N908JE 2. Owner Name (As shown on registration certificate) J.E.G.E. Inc. Address (as shown on registration certificate) 103 Foulk Road, Ste 202 Wilmington, DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE AVIONICS DIVISION 1635 NW 51st Place Ft. Lauderdale, FL 33309 U.S. Certificated Mechanic Radio C SD4R514M Class Limited Airframe Foreign Certificated Mechanic 0 Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 8 November 2004 Signature of Authoriz_e_ii.i l icyl . 7 .2; /d -‘,/ e Steve Ouellette 7. Approval for Return to Service Pursuant to the authority Federal Aviation Administration given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the and is II APPROVED II REJECTED BY FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 19 November 2004 Certificate or Designation No. SD4R514M Signature of _---) _ Authorized Individual Steve Ouellette C FAA Form 337 (12-88) EFTA00277614 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the FAA approval of the new flight manual supplement on N908JE under Banyan Air Servive, Avionics Division work order #68062. A. Removed existing TDR-94 transponders P/N 622-9210-003 and routed to the manufacture for upgrade to P/N 6252-9210-007 to provide flight ID. System ground and flight checked good. B. The weight & balance is not affected and equipment list was updated. C. Instructions for continued airworthiness are "on condition only". END K Additional Sheets are Attached G' fin Og(10.b ffL, EFTA00277615 ' . 0 ••--- . -I US Department MAJOR REPAIR AND ALTERATION Of Transportation Federal (Airframe, Powerplant, Propeller, or Appliance) Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification 5a — r 51)6-1 7 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions a disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-100 Serial No. 20115 Nationality and Registration Mark USA N908JE 2. Owner Name (As shown on registration certificate) J.E.G.E, Inc. - Address (as shown on registration certificate) 103 Foulk Road STE 202 Wilmington, DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE AVIONICS DIVISION 1635 NW 51st Place Ft. Lauderdale, FL 33309 U.S. Certificated Mechanic M Radio C SD4R514 lass 1,2,3 Limited Airframe Foreign Certificated Mechanic a Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. . Date 7 . 1/6/1•1/9e-:-/ a 4:2 C7 (71 Signature of Authori 4i .s.Jualit ‘C Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given personsirfi ci ed below, the Federal Aviation Administration and is APPROVED unit identified in item 4 was inspected in the manner prescribed by the Administrator of the • REJECTED BY FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection / / r Ahi/6Arc e__c72O) C Certificate or Designation No. SD4R5 14M Signature o d Indivi Steve Ouellette FAA Form 337 (12-88) EFTA00277616 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the work performed on N908JE under Banyan Air Service, Avionics Division work order #68062. A. Installed a Universal Avionics Systems Corp. Terrain Avoidance and Warning System in accordance with SIP Technical Services, Inc. data list 7280-DL-001-501, Rev. H dated December 2002 or later. (STC# ST09951SC) B. The above installation was performed in accordance with AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapter 11, sections 3-17, AC43.13-2A Chapter 1, AC43.13-2A Chapter 2, paragraphs 24, 25, and 28, AC25-23 and the aircraft's maintenance manual. C. A functional test of the above equipment has been performed FAR25.1309 and FAR25 1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. A weight & balance was calculated. An FAA approved flight manual supplement provided with the above STC, Document No. 7280-FM-001, dated December 13, 2002 or later E. Instructions for continued airworthiness provided by SIP Technical Services Report No. 7280-ICA-001 Rev. F dated June 6, 2002. END *Ay K Additional Sheets are Attached EFTA00277617 pniteb tutes jArrirriCn Prpartrrttnt of Zrartsportation - grbrral czAfliatinn cAbmirtistration , upialentenial `Tuve Certificate t.471 teinh.fe ST09951SC e°rl teak 1,:s,tezeti/o . SIP Technical Services, Inc. 10107 McAllister Freeway San Antonio, TX 78216 cu.-44,1 dead; ejange art de; *//ze tleJe 7y r1.4 a‘e.it,72/<cikelled/f bre dindal4vzs rz./sticevu‘4.-ivz.s . dercAr ens .yieceAdife., ,eevinee4s de izievz-c-vakeaeJis "e9ece.:vnuva.4.t ei4:7tr."/ 4b c/a; Civil Air Refez44iva.s. 6isr:;th2aigivekcl n'iv0cale A3WE ,d&zZe.- Boeing .A6esehi.• 727-100 Series .gesc. , 04"evz c>4.F1//ze Wiazife. - Installation of a Universal Avionics Systems Corporation Terrain Awareness and Warning System in accordance with SIP Technical Services, Data List 7280-DL-001-501, Revision H, dated December 5, 2002, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Document Number 7280-FM-001, dated December 13, 2002, or later FAA approved revision is required. eindg7cyzeit a..s.• Compatibility of this design change with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. ce,-10cate and14 6:- .111/2/2O/66.iip ektet tcs/ficiza 9ga Jarre feei .1‘.4.3/2eze, reecch geeicv , a te..rmZaaleiva eizhr c3 cae.e<av:se e...ilae°4‘ede;/ dt; .../ge/z71.44e:stkzkv, €/° ev -a, '._/gotallevt.AeGitzikeafinciliark. :gale e3:rev/i&alei -vz, .• August 02, 2001 Lale 9/4,sa.z/ue ..December 13, 2002 :2ale rez,...uaed; gale ez,,vezaeAl.• (Sign ture) ces Co er, Spe ial Ce cation Office South4vest Region (Title) Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA Form 8110-2(10-68) Page 1 of 2 This certificate may be transferred in accordance with FAR 2I.47. EFTA00277618 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-100 WITH UNIVERSAL AVIONICS SYSTEMS CORPORATION DUAL MULTISENSOR UNS-ID+ FLIGHT MANAGEMENT SYSTEMS REG #. N908.TE SERIAL #. 20115 M This supplement must be attached to the FAA Approved Airplane Flight Manual when the Universal Avionics System Corporation UNS-1D+ Flight Mana•ement System (FMS) is .in§talled in accordance with field approved 337 dated 1Voll (2200 )4' . The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement; consult the basic Airplane Flight Manual. FAA APPROVED Gary Justice Principal Avionics Inspector Federal Aviation Administration Flight Standards District Office #17 Ft. Lauderdale, FL 33315 Date: NOV 8 2004 Rev. 0 '.'Pl‘ge 1 of 9 EFTA00277620 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 Table of Contents Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 SECTION PAGE GENERAL 3 LIMITATIONS 3 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 3 PERFORMANCE 6 Revision 0 All Date: NOV 8 2004 RECORD OF REVISIONS Pages Description Initial Release Rev. 0 Approved . NOV 8 71104 Pige 2 of 9 EFTA00277621 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 SECTION 1- GENERAL 1. INSTALLATION DESCRIPTION. Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 The Universal Avionics Systems Corporation dual FMS's use inputs from their integral GPS Receivers, Navigation Receivers and DME Transceivers to provide a blended position for navigation. Each FMS contains an internal TSO C129a GPS sensor (GNSS 2400), which is cross-wired to the other FMS such that both systems have GPS 1 and GPS 2 data as inputs. The FMS's receive air data parameters from an Air Data Computer. A Data Transfer Unit (DTU100) is used to load periodic navigation data base updates via zip disks. The systems provide navigation and steering data to the flight director/autopilot system. Refer to the appropriate Operator's Manuals as applicable. The FMS's contain software SCN 802/902 which provides capability for point-to-point navigation, as well as SIDs, STARs, holding patterns and GPS approaches. These SCN's comply with requirements of TSOs C115b and C129a Class Al when interfaced to the internal GPS sensors which are TSO C129a Class Al/B1/C1 certified The UNS- 1D+ FMS may contain either a GLONASS sensor or a GPS sensor, depending on hardware configuration. Lateral and Vertical deviations are provided for En Route, Terminal Area and Approach operations, including GPS overlay approaches. Approaches may be FCS coupled both laterally and vertically. Multi-Mission search patterns are available with SCN 902. 2. LATERAL NAVIGATION APPROVALS. Provided the FMS multi-sensor navigation system is receiving usable signals, it has been demonstrated capable of and has been shown to meet the accuracy specifications of: VFR/IFR En Route domestic, Terminal and Instrument Approach (LOC, BC, GPS and GPS-overlay NDB, VOR, VOR-DME and RNAV) operations within the U.S.National Airspace System using the WGS-84 coordinate reference datum in accordance with the criteria of Advisory Circular AC 20-130A and AC 25-15. Satellite navigation data is based upon use of only the Global Positioning System (GPS) operated by the United States. Additionally, Russian GLONASS satellites provide increased accuracy but are not used for integrity or Receiver Autonomous Integrity Monitoring (RAIM) calculations or predictions. The dual FMS installation with dual internal GPS sensors, as installed, complies with the requirements of FAA Notice 8110.60 for GPS primary means of Class II navigation in oceanic and remote airspace (including NAT MNPS in accordance with AC 120-33 and 91-49), when used in conjunction with the Universal Flight Planning Program, PN 10751 with SCN 24.0 or later FAA approved version. This does not constitute an operational approval. Date: NOV 8 2004 Rev. 0 Page 3 of 9 EFTA00277622 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 SECTION I — GENERAL (cont.) Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 RNP- Approvals The dual multi-senSor FMS installation integrates dual GPS sensors and complies with equipage and accuracy requirements of FAA Order 8400.12A paragraph 12b(4), for operations in RNP-10 airspace. This does not constitute an operational approval. This installation also complies with equipage and accuracy requirements of AC 90- 96 paragraph 7b(1), 7d(3)(a) 2, 7d(3)(e) for BRNAV (RNP-5) when operating in Class I airspace, without time limits. The table details time limitations placed on RNP-10 and BRNAV operations with minimum sensors in NAV mode. Sensors Available RNP-10 Limitations RPN-5 (BRNAV) Limitations minimum dual FMS's required) (minimum single FMS required 1 GPS only N/A No time limitation when used in Conjunction with UFP VOR/DME only N/A No time limitation DME/DME only N/A No time limitation 3. VERTICAL NAVIGATION APPROVAL The dual Flight Management Systems, as installed, meet the requirements for VFR/IFR En Route, Terminal Area and Approach VNAV operations in accordance with the criteria of AC 20-129 and AC 90-97, paragraph 7.a (2). SECTION II - LIMITATIONS 1. The FMS Operator's Manual, Report Nos. 2423sv802/902 Dated 9/16/03 (or later revision) must be available to the flight crew whenever navigation is predicated upon the use of the Universal Avionics Flight Management System. 2. The system must utilize software version SCN 802/902.X, where X represents FAA approved minor changes. 4. IFR En Route and Terminal navigation are prohibited unless the pilot verifies the currency of the database or verifies each selected Waypoint for accuracy by reference to current approved data. Date: NOV 8 2004 Rev. 0 Page 4 of 9 EFTA00277623 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 SECTION 11-- LIMITATIONS (cont.) Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 4. Instrument approaches must be accomplished in accordance with approved instrument approach procedures that are retrieved from the FMS database. The FMS database must incorporate the current update cycle. a. Instrument approaches must be conducted in the Approach-mode, and GPS Integrity monitoring (when using GPS for approach guidance) must be available at the Final - Approach Fix, as indicated to the pilot by the 'GPS INTEG' amber annunciator being off. b. When an alternate airport is required by the applicable operating rules, it must be served by an approach based on other than GPS navigation, the aircraft must have operational equipment capable of using that navigation aid, and the required navigation aid must be operational. c. GPS can only be used for approach guidance if the reference coordinate datum system for the approach is WGS-84 or NAD 83. d. GPS will remain selected for all GPS approaches and any approach with a "G" suffix to the approach identifier in the navigation database. GPS will be deselected for any pilot-defined VOR or VOR/DME" RNAV approaches. e. Pilot-defined IFR approaches must be defined using Waypoint coordinates from FMS's navigation data base. f. The FMS's are approved for pilot-defined VFR approaches as a VFR pilot aid only. NOTE: All sensors remain selected for VFR approaches. 5. When operating in other than oceanic and remote regions, the aircraft must have other approved navigation equipment installed and operating appropriate for the route of flight. 6. Displayed FMS navigation p'arameters are referenced to Magnetic North, and operation of the aircraft is limited to latitudes between N730and S600, unless magnetic variation is manually entered by the flight crew. 7. When using VNAV, the Altimeter on each pilot's panel must be used as the altitude reference for all operations. 8. ' Fuel display parameters are advisory only and do not replace primary fuel quantity or fuel flow gauges for fuel load and range planning. SECTION III - EMERGENCY PROCEDURES NO CHANGE TO AFM. Date: NCV 8 2004 Rev. 0 Page 5 of 9 EFTA00277624 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 SECTION IIIA - ABNORMAL PROCEDURES 1. If 'GPS RAIM' becomes unavailable (as indicated by a Message and `GPS INTEG' (amber annunciation), continue navigating using the GPS equipment or revert to an alternate means of navigation appropriate to the route and phase of flight, as necessary. When continuing to use GPS navigation, position should be verified every fifteen minutes using another IFR-approved navigation system. 2. Should an FMS system component fail, in most cases the CDU will go blank or the 'FMS MSG' light will flash. Depressing the MSG key will display the Message Page, which will indicate the component which has failed. 3. If sensor information is intermittent or lost, utilize remaining operational navigation equipment as required. 3. The FMS and associated components are protected by the following circuit breakers: C/B Name Amps Location Bus FMS No. 1 5 Pilot 28VDC Avionics Bus No. 1 (Triple-Fed) FMS No. 2 5 Copilot 28VDC Avionics Bus No. 2 (L GEN) FMS DTU 1 Pilot 28VDC Avionics Bus No. 1 (Triple-Fed) SECTION IV - NORMAL PROCEDURES 1. OPERATION Normal operating procedures are outlined in the FMS Operator's Manual, Report No. 2423sv802/902. 2. NAVIGATION DATABASE VERIFICATION. After power-on self tests have been completed, the INITIALIZATION page will appear. The term `NAV DATABASE EXPIRES' followed by a date will be displayed. If the actual date is later than that which is displayed, the FMS will notify the pilot with a 'DATABASE EXPIRED'-message. Refer to the Operator's Manual for navigation database update instructions. 3. SYSTEM ANNUNCIATORS Each FMS has the following annunciations presented on the Universal Electronic Flight Instrument (EFI) displays (refer to the EFI Operator's Manual, as applicable) : MSG Illuminates and flashes in conjunction with the CDU to indicate a message is to be acknowledged on the MESSAGE page. SXTK Illuminates to indicate that selected crosstrack is active. FHDG Illuminates to indicate that the FMS is in Heading sub-mode. APPR Illuminates to indicate that an Approach has been activated. GPS INTEG Illuminates to indicate GPS Integrity is outside of the allowable limit for phase of flight (2.0nm En Route, 1.0 nm Terminal and Approach transition, and 0.3 nm Final Approach segment). Date: NOV 8 2004 Rev. 0 Page 6 of 9 EFTA00277625 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 SECTION IV - NORMAL PROCEDURES (cont) 4. AIRCRAFT INTEGRATION a. Universal Avionics EFI display of FMS information Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 1) FMS information is displayed on the Universal Electronic Flight Instrument (EFI) displays. The associated EFI Control Panel provides control of each display. See the appropriate Operator's Manual, as applicable, for each EFI display system. 2) Lateral deviation display scaling meets with requirements of TSO C129a and AC 20-130A (5.0 nm full scale for En Route, 1.0 nm for Terminal operations, and 0.3 nm for Approach operations). 3) b. En Route and Terminal Area Flight Control System Operation 1) With `FMS'-mode selected by using the EFI Control Panel, the respective FMS information can be presented as Flight Director steering commands by pressing the [NAV] button of the FCP-65 Flight Control Panel. 2) With reasonable navigation data being displayed, the steering information can be Autopilot-coupled, to the pilot's or copilot's Flight Director system, by pressing the 'AP ENGAGE' - button on the APP-65A Autopilot Control Panel. c. Approach Operations NOTE: ILS approaches can be retrieved from the Jeppesen database and linked to the flight plan, but cannot be armed or activated as FMS approaches. The FMS can be used to provide navigation up to the final approach course, at which point the EFI must be changed to display raw ILS data which can be coupled to the Flight Control System (FCS). NOTE: GPS will remain selected for GPS and GPS-overlay approved approaches from the navigation database, as well as pilot-defined VFR approaches. Refer to Operator's Manual, Section V, Approach Procedures. Date: NOV 8 2004 Rev. 0 Page 7 of 9 EFTA00277626 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 SECTION IV - NORMAL PROCEDURES (cont) c. Approach Operations (cont.) Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 LOC, B/C, GPS, NDB, RNAV, VOR, VOR/DME, and VFR approaches may be linked into the flight plan and then laterally and vertically coupled to the FCS as follows: 1) Approach Transition: When an entire approach transition (e.g., procedure turn, DME arc, etc.) is to be flown, first arm the approach on the FMS (ARM APPR). If the FMS is not armed manually it will arm automatically at 30nm from the airport. With the desired DIRECT TO or FROM/TO Waypoints selected, or the desired FMS Heading selected with INTERCEPT ACTIVE, select FCS `NAV'- mode by pressing the [NAV] button of the appropriate FCP-65 Flight Control Panel. When the FMS has automatically activated the approach, denoted by the 'APPR' annunciator displayed in the associated EFI display, press the [APPR] button of the Flight Control Panel. When the FCS has captured the "APPR" — mode, a white "VNAV" will appear on the PFD and a white VN on the ADI signifying the 'arming" of the VNAV mode. The "VNAV" and "VN" annunciation will turn to green in color when the FCS has captured the VNAV glideslope. See the EFI operator's manual for specific display annunciations. Continue monitoring both lateral and vertical deviations throughout the duration of the approach. If required, initiate 'Missed Approach Procedures' as described in the Universal Avionics Operator's Manual. 2) Heading Vectors: If given heading vectors by ATC to the final approach course, manually activate the approach on FMS NAV page 1/3. The FMS will enter the "FHDG" mode, the EFI display will now display final approach course data, and the INTERCEPT prompt on Nav page 1/3 will be active. When cleared to intercept final, press the "INTERCEPT "line select key to intercept final. Ensure that commanded heading mode is canceled. Select [APPR] on the FCS Flight Control Panel to capture and track the final approach lateral and vertical information. NOTE: Guidance is provided to the runway threshold or missed approach point. It is the pilot's responsibility to level out at MDA if the runway environment is not in sight. Date: NOV 8 2004 Rev. 0 '' 'Page 8 of 9 EFTA00277627 Banyan Air Service Avionics Division 1635 NW 51st Place Ft. Lauderdale, FL 33309 SECTION IV - NORMAL PROCEDURES (cont) Flight Manual Supplement UNS-1D+ FMS N908JE BOEING 20115 3) Press the APP-65A Autopilot Control Panel [AP ENG]-button to couple the AP to the selected FD. The Autopilot will track pseudo-Localizer and pseudo-Glideslope signals from the FMS. b. Advanced Approach Operations 1) Advanced approaches may be identified in the data base by the prefix "A" to the approach listed in the "ARRIVAL" page and in the navigation data base They are characterized by course changes on the final approach segment of greater than 6 degrees and/or having multiple flight path angles. To avoid excessive deviations from course and flight path, these approaches may need to be flown in FCS [NAV] mode until on the final leg of the approach. Select FCS [APPR] sequencing the final waypoint to engage vertically. c. Vertical Navigation 1) Vertical Navigation (VNAV) information is displayed on the EFI display and is available for enroute, terminal or approach descents. Pitch steering commands for enroute and terminal VNAV operations are not provided to the Flight Control System. SECTION V - PERFORMANCE DATA NO CHANGE TO AFM. Date: NOV 8 2004 Rev. 0 Page 9 of 9 EFTA00277628 . • • 0 . US Department MAJOR REPAIR AND ALTERATION Of Transportation (Airframe, Powerplant, Propeller, or ApplianCe) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only i Office Identification • - 1- • •• , INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and -,I disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such- violation (Section 901 Federal Aviation Act of 1958). - —1 O. Aircraft Make Boeing Model ; , 727-100 i Serial No. 20115 Nationality and Registration Mark USA N908JE . 2. Owner Name (As shown on registration certificate) J.E.G.E, Inc. - Address (as shown on registration certificate) 103 Foulk Road STE 202 Wilmington, DE. 19803-3742 3. For FAA Use Only Tri't data identified h plies airworthines n..quirements is described aircraft. subj conformity lutorized In FAR 43, s on 43.7. OCT 11 7004 d-e/ is FM the applicable tot the by a above person 5 0 - r-.5 DO- 1 . - Inspector Date nature 4. Unit Identifi atio 5. Type ry- Unit Make Model Serial No. Repair Alteration •• ••.i • ,..• AIRFRAME (As described in Item 1 above) -s.-4. POWERPLANT .i t---,-• PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE AVIONICS DIVISION 1635 NW 51st Place Ft. Lauderdale, FL 33309 U.S. Certificated Mechanic Radio Class 1,2,3 —.... Limited Airframe Foreign Certificated Mechanic Certificated Repair Station r Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date /fA//44/16eW paC3 O Signature of Authori c di ' lual Ouellette — Steve , 7. Approval for Return to Service • Pursuant to the authority given persons specified below, Federal Aviation Administration and is APPROVED the unit identified in item 4 was inspected in the manner prescribed by the Administrator of thil.. REJECTED _ I BY FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) ..... FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection /9 A/47/ 106e2C_c:7,.: Certificate or Designation No. SD4R514M Signature of Aut • d Indio' . . Steve Ouellete ----_ —. FAA Form 337 (12-88) EFTA00277630 NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be . .compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. i• f rr. Description of Work Accomplished • (lf more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the work performed on N908JE under Banyan Air Service, Avionics Division work order #68062. A. Installed an Artex ELT406-2HM per Artex installation document number 570-5000, Rev. A, dated 12/10/02 mounted in unpressurized aft compartment. The antenna is mounted in the aft tail section. A remote switch is mounted in cockpit in the copilot's insrtument panel. An aural activation monitor is mount within the vacinity of the ELT per the installation document listed above. 1 f. r • L. I • .; B. The above installation Aidsi3e&efe,din.iccofdanceX4h. AC43.13-1B, Chapter 7, sections 1-5, AC43.13-1B Chapter 11, sections 3-17,AC43.13 -2A ChApter 1, AC43.13-2A Chapter 2, paragraphs 24, 25, and 213,7AZ,431172A7Chapter 3; paragraph 38 and the aircraft's maintenance manual. C. A functional test of the above equipment has been performed FAR25.1309 and FAR25 .1431 for proper operation and did not adversely affect any other aircraft systems. An electrical load analysis was conducted and it was confirmed that this installation would not exceed 80% of the generator output. D. A log book entry and equipment list was generated to reflect the above installation. No Weight and balance was generated as the aircraft was weighed. E. Instructions for continued airworthiness is a battery due time change. This due date is reflected on the log book entry. Annual inspection is required per FAR 91-207 (d). END 0 Additional Sheets are Attached EFTA00277631 0 US Department MAJOR REPAIR AND ALTERATION Of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only .. Office Identification . - - _ INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and •disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such, ,' violation (Section 901 Federal Aviation Act of 1958). . 11. Aircraft Make Boeing Model 727-100 Serial No. 20155 Nationality and Registration Mark USA N908JE 2. Owner Name (As shown on registration certificate) J.E.G.E. Inc. Address (as shown on registration certificate) 103 Foulk Road, Ste 202 Wilmington, DE. 19803-3742 - 3. For FAA Use Only NOV Tr': data identified herei complies the applicable ainvorthines rLquicements d is approv for the above described aircraft, sub' conformity s n by a person authorized in FAR 43, s on 43.7. 8 2004 Ter, . , ., e) — f-S720 --/ 7 . Date Startatura FAA Inspector - 4. Unit Identificat 0 5. Type Unit Make Model Serial No. Repair Alteration . , AIRFRAME (As described in Item 1 above) POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. BANYAN AIR SERVICE AVIONICS DIVISION 1635 NW 51st Place Ft. Lauderdale, FL 33309 U.S. Certificated Mechanic Radio C SD4R514M Class Limited Airframe Foreign Certificated Mechanic Certificated Repair Station 0 Manufacturer , D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and . correct to the best of my knowledge. Date 5 ). A /0,-/e-A1,46-2 ,,, e (-1 V Signature of Au .er Indivi , Steve Ouellette 7. Approval for Return to Service Pursuant to the authority given personsAoecified below, Federal Aviation Administration and is x APPROVED the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the III REJECTED BY FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection n X/1/ - - o 76)- Certificate or Designation No. SD4R514M Signature of Authorized Indivi ual Steve Ouellette 1 -7 — FAA Form 337 (12-88) • EFTA00277632 NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 0. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) The purpose of this 337 is for the FAA approval of the new flight manual supplement on N908JE under Banyan Air Servive, Avionics Division work order #68062. A. Removed existing UNS-1D Flight Management System (FMS) control display/computer units and routed to the manufacture for upgrade to UNS-1D+. Reinstalled UNS-1D+ FMS CDU computers. System ground checked good. B. A flight manual supplement has been generated, approved and incorportated into the existing flight manual. A weight & balance and equipment list update are not required. END • • •v-inc .q)4:11 A'A4 tit3O 0 Additional Sheets are Attached EFTA00277633 NOV. NV. 8. 2004 9:50AM PYKA AEROSPACE NO. 2146 P. 3 Doc. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 TAWS System AFM Supplement for Boeing 727-100 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT UNIVERSAL AVIONICS TERRAIN AWARENESS WARNING SYSTEM (TAWS) AIRPLANE MAKE: BOEING AIRPLANE MODEL: 727-100 AIRPLANE SERIAL NO.: A/yog-j-t--- REGISTRATION NO.: c90 /A-5— This supplement must be attached to the FAA Approved Airplane Flight Manual when the airplane is modified by the installation of a Universal Avionics Terrain Awareness Warning System (TAWS) in accordance with FAA STC number ST09951SC. The information contained herein supplements or supersedes the basic Airplane Flight Manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this document, consult the basic Airplane Flight Manual. APPROVED: S. Frances Cox, Manager Special Certification Office Federal Aviation Administration Ft. Worth, Texas 76193-0190 DATE: October 25, 2004 Page 1 of 9 EFTA00277634 NOY. 8. 2004 9:50AM PYKA AEROSPACE NO. 2146 P. 4 Doc. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc 10107 McAllister Freeway San Antonio, TX 78216 LOG OF REVISIONS TAWS System AFM Supplement for Boeing 727-100 REV, DESCRIPTION REVISED PAGES APPRD. BY DATE IR New supplement All S. Frances Cox 12-13-2002 A Allow use of CDU or MFD display. Format and editorial corrections throughout. All See cover page 10.25.2004 FAA APPROVED Date: October 25, 2004 Page 2 of 9 EFTA00277636 • 1 tat EFTA00277637 NOV. 8. 2004 9:51AM PYKA AEROSPACE NO. 2146 P. 5 Dot. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 TABLE OF CONTENTS SECTION PAGE SECTION I - GENERAL 4 SECTION II - LIMITATIONS 4 SECTION III — NORMAL PROCEDURES 5 1. Operation 5 2. Cold Temperature Operations 5 3. Systems Test 5 4. Pop-Up Terrain Display 6 5. System Annunciators 7 SECTION IV - EMERGENCY/ABNORMAL PROCEDURES 9 EMERGENCY PROCEDURES 9 ABNORMAL PROCEDURES 9 1. Circuit Breakers 9 2. Use of TERR INHIBIT switch 9 3. Response to TAWS Warnings 9 4. Response to Glideslope Deviation Alerts 9 5. Use of Flap Override Switch 10 ff CTION V - PERFORMANCE 10 SECTION VI - WEIGHT AND BALANCE 10 TAWS System AFM Supplement for Boeing 727-100 FAA APPROVED Date: October 25, 2004 Page 3 of EFTA00277638 , NOV. 8. 2004 9:51AM PYKA AEROSPACE Na 2146 P. 6 Doc. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 TAWS System AFM Supplement for Boeing 727-100 SECTION 1 — GENERAL This Supplement provides general information for the Enhanced Ground Proximity Warning System installation. The aircraft is equipped with a Universal Avionics TAWS system. The system uses inputs from the air data computer No. I, navigation receiver No. 1, radio altimeter, and the Universal Avionics UNS-1 Flight Management System (FMS) , and an internal terrain database to provide basic GPWS alerts and terrain alerts The TAWS alerts provide the crew with aural and visual indications of possible inadvertent flight into terrain. TAWS alerts are generated if one or a combination of the airplane's: 1) vertical speed, 2) rate of closure to terrain, 3) accumulated altitude loss, 4) airspeed, flap and /or gear configurations or 5) glideslope deviation is unsafe given the airplane's radar altitude and phase of flight. Terrain alerts are generated by comparing aircraft position and altitude to the EGPWS terrain database. This system also provides "Flight Plan Look Ahead" terrain alerts and warnings by comparing the FMS flight plan to the terrain database SECTION II - LIMITATIONS The TAWS display will be used for situational awareness only. Navigation must not be predicated upon the use of the TAWS. The 3-1) view provides no attitude information. To avoid giving unwanted terrain alerts, the TAWS terrain alerts must be inhibited by pressing the TERR INHIB switch when landing at airports that are not included in the airport database or when landing at an airport other than the airport in the FMS flight plan. Deviation from Air Traffic Control Clearances is authorized to the extent necessary to comply with TAWS warning. The use of terrain awareness warning and terrain display function is prohibited during QFE operations. The current local altimeter setting must be entered in the pilot's altimeter for proper terrain alerting. The TAWS database and alerting algorithms do not account for man made obstructions FAA APPROVED Date: October 25, 2004 Page 4 of 9 EFTA00277640 NOV. 8.2004 9:51AM PYKA AEROSPACE NO. 2146 P. 7 Doc. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 TAWS System AFM Supplement for Boeing 727-100 SECTION III — NORMAL PROCEDURES 1. Operation All aircraft crew interface is conducted through the Universal Avionics display, either multi- function display (MFD) or FMS control display unit (CDU), and system annunciator switches. TAWS terrain information may be presented on either an MFD or a CDU. The TAWS requires inputs from the following systems; radio altimeter, air data computer, VHF navigation receiver, FMS, gear position and flap position. 2. Cold Temperature Operations TAWS uses barb-corrected altitude as the reference for Forwared Looking Terrain Alerts (FLTA). TAWS does NOT compensate the baro altitude input for non-standard temperature lapse rates that may be encountered in extreme cold conditions, causing degraded FLTA operation. Basic ground proximity warning modes (1 through 6), as well as Premature Descent Alert (PDA), are radio altitude based and not affected. In extreme cold conditions, the aircraft will be operating at a lower altitude than indicated, thus resulting in TAWS alerts being delayed or missing. The color-banding on the TAWS display will be offset by the cold temperature altitude error. When operating into and out of airports where cold temperatures exist, the crew should be aware of the difference between the indicated baro altitude and the true altitude and the effect this has on FLTA and the terrain display. To determine the effect on FLTA warnings consult the Airman's Information Manual Chapter 7 paragraphs 7-2-3d and 7-2-3e. 3. System Tests BUILT IN TEST TAWS has a Built-In-Test (BIT) function which includes Power-Up Self Tests, Initiated Tests and Continuous Tests. Where there has been degradation in capabilities that result in TAWS being unavailable, BIT annunciates the fact to the flight crew via a GPWS FAIL or TERR 1NOP Lamp. PRE-FLIGHT TESTS A TAWS Self Test should be conducted prior to each flight. Momentarily press the GPWS TEST annunciator. The following indications confirm proper TAWS operation: PULL-UP Annunciator Illuminated TERR Annunciator Illuminated BELOW G/S Annunciator Illuminated G/S INHIBIT Annunciator Illuminated TERR INHIBIT Annunciator Illuminated FAA APPROVED Date: October 25, 2004 Page 5 of 9 EFTA00277642 C. 2.;04 is PYKA NO. 2146 P. 8 Doe. No. 7280-1, . 1, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727.100 10107 McAllister Freeway San Antonio, TX 78216 SECTION III - NORMAL PROCEDURES(Continued) GPWS FAIL Annunciator GPWS TEST Annunciator Illuminated Illuminated TAWS Terrain Display Test Image (Colored Bars) Aurel Annunciations "TERRAIN, TERRAIN" "PULL UP, PULL UP" "DON'T SINK" "SINK RATE" "GLIDESLOPE" "TOO LOW TERRAIN" "TOO LOW GEAR" "TOO LOW FLAPS" "FIVE HUNDRED" Once the test is complete, TAWS will reboot. During this time the GPWS FAIL and TERR INOP annunciators will remain lit and a TAWS FAIL message will be generated on the MFD until the system is operational. (approx one min) NOTE: As a result of pressing the GPWS TEST annunciator again within five seconds of initiating this test, the test will cancel and the TAWS computer will continue to operate without rebooting. 4. Pop-Up Terrain Display In the event of terrain alert, the map view of the TAWS display will "pop-up" on the MFD or CDU. Pressing any function key on the display will remove the pop-up and revert to the selected display function. Prospective terrain conflicts are depicted by a star shaped Terrain Threat Symbol. Both Warnings and Cautions are annunciated with this symbol. Terrain warnings are a flashing red symbol while Terrain cautions are depicted by a flashing yellow symbol. Terrain threats along the flight plan are depicted by a white symbol and represent the predicted first point of conflict between the flight plan and terrain RED threat "stars" on the TAWS display indicate a Terrain Alert (30-second warning). YELLOW threat "stars" on the TAWS display indicate a Terrain Caution(60-second warning) FAA APPROVED Date: October 25, 2004 Page 6 of 9 EFTA00277644 _ "••••• ••••• EFTA00277645 NOV. 8. 2004 9:52AM PYKA AEROSPACE NO. 2146—P. 9" Doc. No. 7280-FM-001, Rev A TAWS System Issue 092401 AFM Supplement for S.I.P. Technical Services Inc. Boeing 727-100 10107 McAllister Freeway San Antonio, TX 78216 SECTION 1.1 1 PROCEDURES Continued WHITE advisory alert " stars" on the TAWS display indicate a flight plan terrain conflict These alerts are annunciated by a "star" on the display shortly after a VNAV altitude is entered into the flight plan or when a procedure (STAR or approach) containing altitudes is linked to the flight plan. Flight plan terrain advisories do not require immediate action but indicate that adhering to the flight plan as entered will cause a future terrain alert. Waypoints and altitudes should be checked for accuracy. 5. System Annunciators The following system annunciators are provided for the system; A. PULL UP Red PULL UP annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates whenever TAWS has detected terrain in the aircraft's immediate flight path. The annunciator will remain illuminated until the terrain has been cleared. Aural annunciations of "TERRAIN, TERRAIN, PULL UP" or "PULL UP, PULL UP" are also provided whenever the red PULL UP annunciator illuminates. B. BELOW GS Amber BELOW GS annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates on approach whenever the TAWS has detected that the aircraft is at least 1.3 dots below the glideslope. This annunciator remains illuminated until the aircraft has returned to within less than one dot of the glideslope. Aural warnings of "GLIDESLOPE-GLIDESLOPE-GLIDESLOPE" sound until the aircraft has returned to within less than one dot below the glidepath. The aural annunciation may be canceled by pressing the BELOW GS armunciator/switch. However, the BELOW GS annunciators will remain illuminated. If the aircraft goes below the glideslope after the aural warning and light annunciation has gone out, the light and aural warning will again sound. C. GPWS FAIL Amber GPWS FAIL annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates if the TAWS has failed. FAA APPROVED Date; October 25, 2004 Page 7 of 9 EFTA00277646 NOY. 8. 2004 9:53AM PYKA AEROSPACE N0. 2146 P. 10 Doc. No. 7280-FM-001, Rev A Issue 092401 S.I.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 SECTION UI - NORMAL PROCEDURES (Continuedi D. GPWS TEST TAWS System AFM Supplement for Boeing 727-100 GPWS TEST switches are located on the Captain's and First Officer's instrument panel shared with the GPWS FAIL annunciator. This switch is utilized to perform a self-test of the TAWS system. E. TERR Amber TERR annunciators are located on the Captain's and First Officer's instrument panel. The "TERRAIN, TERRAIN" aural warning paired with a visual alert is indication of reduced terrain clearance. F. TERR INOP Amber TERR INOP annunciators are located on the Captain's and First Officer's instrument panel. This annunciator illuminates when the terrain function is inhibited by TERR INHIB switch, terrain database is invalid or failed, terrain alert function is inoperative due to hardware failure or lack of a required input such as position or altitude. G. TERR INHIB Blue TERR INHIB annunciator/switch is located on the Captain's instrument panel adjacent to the TERR INOP annunicator. This annunciator/switch is illuminated white visible only when the TERR DRIB is active. FAA APPROVED Date: October 25, 2004 Page 8 of 9 EFTA00277648 NOV. 8.2004 9:53AM PYKA AEROSPACE -NO. 2146—P. 11' Doc. No. 7280-FM-001, Rev A Issue 092401 S.1.P. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 SECTION IV - EMERGENCY/ABNORMAL PROCEDURES EMERGENCY PROCEDURES No change to basic Airplane Flight Manual ABNORMAL PROCEDURES 1. Circuit Breakers The TAWS system is protected by the following tip-five circuit breakers: NAME GPWS TAWS System AFM Supplement for Boeing 727-100 LOCATION AMPS BUS P-18 5 28 VDC Ess. 2. Use of TERR INHIB switch. The Terrain Awareness Display inhibit switch (TERR INHIB) must be placed in the INHIB position in the following conditions: 1-Whenever the FMS in the Dead Reckoning (DR) mode 2-Within 15 nm of approach or landing at an airport not contained in the TAWS database. NOTE: When an off airport landing is required the FLTA and PDA functions should be inhibited by activation of the TERR INHIB switch. 3. Response to TAWS Warnings When an aural `TERRAIN, TERRAIN, PULL UP" or a red PULL UP warning light annunciates, execute a positive pull up maneuver, apply maximum rated thrust, and ascend to at least the best climb angle until the warning ceases. Notify ATC if action requires deviation of ATC cleared flight plan. When an aural "CAUTION TERRAIN", "TOO LOW TERRAIN," "SINKRATE" SINK," "TOO LOW FLAPS" or `TOO LOW GEAR" caution annunciates, initiate corrective action to remove the cause of the warning. 4. Response to Glideslope Deviation Alerts When the BELOW GS annunciator illuminates and an aural "GLIDESLOPE" annunciation alert occurs, initiate corrective action to fly the airplane back to the glideslope centerline. To inhibit the "GLIDESLOPE" annunciation on back course approaches, select the BELOW GS warning light/switch. The glideslope inhibit function is only available below 2000 ft AOL when the BELOW GS annunciator illuminates. FAA APPROVED Date: October 25, 2004 Page 9 of 9 EFTA00277650 NOV. 8. 2004 9:53AM PYKA AEROSPACE NO. 2146—P. 12 Doc. No. 7280-FM-001, Rev A Issue 092401 S.LP. Technical Services Inc. 10107 McAllister Freeway San Antonio, TX 78216 TAWS System AFM Supplement for Boeing 727-100 SECTION IV - EMERGENCY/ABNORMAL PROCEDURES (Continued) 5. Use of Flap Override Switch When landing with less than normal flaps, the FLAP OVERRIDE switch should be usesd to prevent the 'TOO LOW FLAPS" aurel annunciation, SECTION V - PERFORMANCE No change to basic Airplane Flight Manual. SECTION VI - WEIGHT AND B4LANCE Refer to applicable weight and balance document. FAA APPROVED Date: October 25, 2004 Page 10 of 9 EFTA00277652 MAJOR REPAIR AND ALTERATION US Department 01 transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use On y Office Identification _ 50-r-37,0- r7 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-.1 (or subsequent revision thereof) for instruc • ns and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC Address (As shown on registration certificate) 103 FOULK RD STE 202 WILMINGTON DE 19803-3742 3. For FAA Use Only 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS EYKR782D AIRFRAME 1,3. RADIO 1,2,3. LIMITED A/F & ENG. Foreign Certified Mechanic X ---, Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and desc . ed on tti reverse o attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Ra ulation4 and that th information ) furnished herein is true and correct to the best of my knowledge. \ \ Date 6/12/02 Signature of Authorized Individual ' Christopher Houseworth. Inspector. \ i• \ _, I 7. Approval for Return to Service Pursuant Administrator BY, to the authority given of the Federal Aviation persons specified below, the unit Administration and is identified in item 4 was inspected in the manndr pr cribed by the 0 REJECTED ,..., CI APPROVED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 6/12/02 • Certificate or Designation No. EYKR782D Signature of Authorized Individual .- C.. - . John K. Urso. Inspector. -- ' & 6 1 FAA Form 337 (12-88) EFTA00277654 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) N908JE, BOEING 727-31, S/N 20115, W.O. 18046 REFERENCE F.A.A. FORM 337 DATED 7/2/01 INSTALLING A UNIVERSAL AVIONICS CORP. UNS-ID FLIGHT MANAGEMENT SYSTEMS (FMS) WITH INTEGRAL GPS SENSORS. RECONFIGURED AIRCRAFT WIRING TO PROVIDE V-NAV DISPLAY INFORMATION ONLY, FROM THE EXISTING # I AND # 2 UNS-ID FLIGHT MANAGEMENT SYSTEMS. THIS MODIFICATION AS ACCOMPLISHED PER THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY F.A.A. FROM 8110-3 RESPECTIVELY: WIRING DRAWINGS: • B727-16236-410, REV A, DATED 4/16/02, SHEETS 1 THRU 5, TITLED - NO. 1 FLIGHT MANAGEMENT SYSTEM. • B727-I6236-411, REV A, DATED 4/16/02, SHEETS 1 THRU 5, TITLED - NO. 2 FLIGHT MANAGEMENT SYSTEM. REFERENCE F.A.A. FORM 8110-3 DATED 4/19/02 BY SYSTEMS AND EQUIPMENT DER NO. DERT510087-NM. ACCOMPLISHED OPERATIONAL CHECKS PER UNIVERSAL AVIONICS CORP. RETURN TO SERVICE MAINTENANCE AND CHECKOUT PROCEDURES MANUAL NO. 34-60-21, DATED 19 MARCH 2001 WITH NO DISCREPANCIES NOTED. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 1 OF 5, DATED 06/19/2001, WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE REQUIRED F.A.A. APPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236-100, REV A, SHEETS 1 THRU 9, DATED 5/8/02 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END K Additional Sheets Are Attached -A- U.S. G. P.O 1990-761-753 EFTA00277655 'f Apr-19-02 08:08A N J Curran 352 243 1011 P_O2 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE April 19, 2002 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio. Helicopter. etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-410, Revision A, dated April 16, 2002 B727-16236-411, Revision A, dated April 16, 2002 NO. 1 FLIGHT MANAGEMENT SYSTEM NO. 2 FLIGHT MANAGEMENT SYSTEM PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) CFR TITLE 14, CHAPTER 1, SUBCHAPTER C FAR 25.581 (a)(b)(1) FAR 25.1329 (h) FAR 25.1529 FAR 25.869 (a)(4) FAR 25.1351 (a) FAR 25.1581 (a)(b)(d) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c)(d)(e) FAR 25.1309 (a)(b)(c)(d)(e)(g) FAR 26.1381 (a)(b) FAR 25.1322 (b)(c) FAR 25.1431 (al(b)(c) CERTIFICATION - under authority vcsted by direction data limed above and on attached shirts numbered NONE have tithe Administrator and to accordance with conditions and Limitations or appointment under Part 18.1 or the Federal Aviation Regulations. been examined in accordance with established procedures and found to comply with applicable requirements or the Federal Aviation these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Rezulations. II Recommend approval of I (We) Therefore El Approve these data (Systems SIGNATUR . 0 DESIGN ED NGIN ' REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) ‘44661--- DERT-510087-NM Systems & Equipment Nor an J. an FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME: SC-727-FMS-REVA.DOC EFTA00277656 lot • I EFTA00277657 Jet Aviation Associates Ltd. Bldg. 1515 Perimeter Rd. Palm Beach Int'l Airport West Palm Beach, FL 33406 FAA CRS EYKR782D Document No. B727-16236-100 AFM Supplement to The Boeing Company 727-31 Serial No. 20115 FAA Form 337 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-31 REGISTRATION NO.: N908JE SERIAL NO.: 20115 WITH DUAL UNIVERSAL AVIONICS FLIGHT MANAGEMENT SYSTEMS (UNS1-D) INSTALLED This supplement must be attached to the FAA approved Airplane Flight Manual when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VOR/DME from the Collins No. 1 and No. 2 VOR/DME systems in accordance with manufacture's Installation and Checkout Manual No. 34-60-09, Rev. 2, dated August 15, 1997 or later approved revision and FAA Form 337, dated June 26, 2001. The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult the appropriate basic Airplane Flight Manual. FAA Approved: iriz Federal Aviation Administration Flight Standard District Office - 17 1050 Lee Wagener Blvd. Ft. Lauderdale, Florida 33315 FAA Approved Date: June 21, 2001 Revision A, Dated: 5/ Page 1 of 9 EFTA00277658 MAJOR REPAIR AND ALTERATION US Dopartment . of Transportation ‘ (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation • Administration Form Approved OMB No. 2120-0020 For FAA Use Only OffiQeldentificatjon, 7 SDU7 .604 6s 3 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMITED EYKR782D 1,3. 1,2,3. ENG. -Foreign Certified Mechanic ---, X Certificated Repair Station Manufacturer A/F & D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 1/14/02 Signature of Authorized Individual , ,i John K. Urso. Inspector. x,I.Z.-- L/C-6 -- , 7. Approval for Return to Sery Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 Was inspected in the manner prescribed by the K REJECTED Cs APPROVED FM Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 1/14/02 Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance. 11-V. FAA Form 337 (12-88) EFTA00277660 NOTICE Weisht.andtalanca Or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all prev7ous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, S/N 20115, N9081E,'W/O 17454. ACCOMPLISHED AN ALTERATION TO THE CABIN INTERIOR FURNISHING ARRANGEMENT PREVIOUSLY INSTALLED UNDER PAGE AVJET STC SA3137SO, DATED 1/17/92, BY REMOVING THE FOLLOWING INTERIOR FURNISHINGS: DESCRIPTION POSITION P/N S/N F.S. R/H O/B AFT FACING SEAT. FORWARD SALON 303413-2 4350 401.94 R/H 1/B AFT FACING SEAT. FORWARD SALON 303413-10 4351 401.94 FORWARD R/H TABLE AND PEDESTAL FORWARD SALON A727-2531-001 NSN 438.50 UH AFT FACING SEAT CENTER LOUNGE 303413-1 4354 732.00 COFFEE TABLE AND PEDESTAL CENTER LOUNGE 727-2535-003 NSN 772.50 THIS ALTERATION WAS ACCOMPLISHED PER JET AVIATION DRAWING B727-17454-200, REV IR, DATED 1/2/02, SHEETS I & 2, TITLED - MINOR DEVIATION TO STC SA3137SO, THE LIMITED 727-100 GENERAL ARRANGEMENT. REFERENCE F.A.A. FORM 8110 DATED 1/6/02 BY STRUCTURES D.E.R. NO. DERT-810028-NE. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES REQUIRED FOR THIS ALTERATION. END K Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277661 MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, or Appliance) of Transportation Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification dift ---( 1 INSTRUCTIONS Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N908JE 2. Owner Name (As shown on registration certificate) JEGE Inc. Address (As shown on registration certificate) 103 Foulk RD STE 202 Wilmington, DE 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) X POWERPLANT PROPELLER APPLIANCE Type 1 / 1 1 _ Manufacturer 61 Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Gary K Palmer 6 Hyacinth Lane Holbrook, NY 11741 X U.S. Certified Mechanic #84544584AP Foreign Certified Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 08/01/01 _ Signature of Authorized Gary K Palmer Individual 7. Approval for Return to Service Pursuant Administrator BY to the authority given of the Federal Aviation persons specified below, the unit Administration and is identified in item 4 was inspected in the manner prescribed by the 0 REJECTED ►4, APPROVED FAA Flt. Standards Inspector Manufacturer X Inspection Authorization Other (Specify) FAA Designee Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 08/01/01 Certificate or Designation No. 84544584IA Signature of Authorized Individual _. Gary K Palmer FAA Form 337 (12-88) EFTA00277662 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. Li B. Description of Work Accomplished (If more space is required, attach additional sheets, identify with aircraft nationality and registration mark and date work accomplished.) Fireblocked and upholstered existing, one (1) cabin single chair (Erda SIN 4359) in Townsend: Leather Lambskin Paris Alligator Embossed/Tipped Gold/Black, leather and two (2) cabin chairs (Erda S/N 4357 and 4358) in Clarence House: 10379B1S-37 Velours Mohair, fabric. D.E.R. Identification 62326-01. Fireblocked and upholstered existing, two (2) cabin single chair (Erda SIN 4360 and 4361) in Old World Weavers: Edmond Petit FMPOO 10004 Zoom, fabric. D.E.R. identification 64318-01. Fireblocked and upholstered existing, one (1) cabin single seat (Erda S/N 4354) and one (1) three section divan (Dettmers S/N 520, 521, and 522) in Geltman Ind.: Tiburon Tweed, fabric and one (1) divan (Dettmer SIN 516) in Clarence House: 10379BIS-37 Velours Mohair, fabric. D.E.R. Identification 65624-01. Fireblocked and upholstered existing six (6) single cabin seats (Erda S/N 4350, 4351, 4352, 4353, 4355, 4356), one (1) LH forward sidefacing divan (Dettmers S/N 517), and two (2) 3-place reclining divans (Dettmers S/N 518 and 519) in Old Weavers: EA81340013 Alfa Check, fabric and ETS J. Tassin S.A.: Mastic #19075, leather. D.E.R. Identification 66059- 01. All materials meet FAR 25.853(a) Appendix F, Part l(a)(1)(ii). Aircraft seat cushions have been fireblocked as per the requirements of FAR 25.853(c) Appendix F, Part II, Amendment 25 - 83. Results of sample burn tests are documented on S.A.I.'s Test Plan #7428, #7617, #7722, and #7759 and on attached DER approved 8110-3, Identification 62326-01, 64318-01, 65624-01, and 66059-01. Seat cushions have been tagged as being in compliance with the applicable regulatory requirements. Aircraft seatbelts were sent to Aircraft Belts, Inc. Repair Station YB1R632K for rewebbing, work order number 0046395 and reinstalled on the seats and divans. Replaced 19 each P.L. Porter SLO2300-28 seat recline Hydrolok and 6 each P.L. Porter SLO2300-21 divan recline Hydrolok. Hydroloks were replaced using standard interior practices. Installed Erda Hydro Legrest P/N 302617-3 and mechanical control single P/N MC15-36 on two (2) cabin single seats Erda seat S/N 4360 and 4361 in accordance with Erda drawing 302617 Rev B. Attached: FAA approved Townsend: Leather Lambskin Paris Alligator Embossed/Tipped Gold/Black, feather and Clarence House: 10379BIS-37 Velours Mohair, fabric. Test Plan #7428, form FAA 8110-3 dated 04/16/01, Judy Boggs, DERY-405020-CE. Identification 62326-01. Attached: FAA approved Old World Weavers: Edmond Petit FMPOO 10004 Zoom, fabric. D.E.R. Identification 64318-01. Test Plan #7617, form FAA 8110-3 dated 06/20/01, Judy Johnson, DERY-405020-CE. identification 64318-01. Attached: FAA approved Geltman Ind.: Tiburon Tweed, fabric and Clarence House: 10379B1S-37 Velours Mohair, fabric. Test Plan #7722, form FAA 8110-3 dated 07/12/01, Donna J. Parrish, DERY-410100-CE. Identification 65624-01. Attached: FAA approved Old World Weavers: EA81340013 Alfa Check, fabric and ETS J. Tassin S.A.: Mastic #19075, leather. Test Plan #7759, form FAA 8110-3 dated 07/24/01, Donna J. Parrish, DERY-410100-CE. Identification 66059-01. Attached: Aircraft Belts, Inc.: Certification/Packing List, work order number 0046395 consisting of 11 sheets. Attached: FAA form 8130-3 from P.L. Porter Controls, Inc.: SLO2300-21 and SLO2300-28 Hydrolocs tracking number 7723, 6751, 7176, 6759, 9495, 7367, 7368, and 9292. Pertinent data on file at International Jet Interiors, Inc. under W.O.#: 01119. Customer to install seats and divans in aircraft. Log entry has been made. END DI Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277663 (jv C - . MAJOR REPAIR AND ALTERATION U.S. Dc.-partinalt of (Airframe, Powerplant, Propeller, or Appliance) Transportation Federal Aviation Administration s ... Form Approved OMB No. 2120-0020 For FAA Use Only : Office Identification tlae) F5 De - t f--"--(--_ INSTRUCTIONS: Print or tspe all entries. See FAR 43.9, FAR 43 Appendix B , and AC43.9-1 (or subsequent revision thereof for instructions and disposition of this form. This report is required' by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed S1,900 for each such violation (Section 901 Federal Asia tion Act of 1958). . . i. Aircraft • Make Boeing . Model 727-31 • Serial No.201 15 ' Nationality and Registration Mark N908JE . 2. Owner . Name (As shown . TEGR INC_ on registration certificate). . Addri s (as shown, on registration certifikmte) . 103 FOULKRD STE 202 - WILMINGTON DE. 19803-3742 _ 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration ' AIRFRAME — above) )O - (As described in item 1 ^ . POWERPLANT • s PROPELLER . . APPLIANCE Type . . . Manufacturer 6. Conformity Statement A Agency's Name and- Address B Kind of Agency - C. Certificate:No. - TIMCO Lake City Municipal Airport Lake City, FL 32025 . U.S_CertificatxxiModianic ' DU4R141M Foreign Certificated- Mechanic X Certificated Repair Station .. . Manufacturer . ' D. I certify that accordance with- the repair and/or alteration ill, tiv-rnPnts of Part 43 of made to the units the U.S. Federal -on-the informatices been made in the best of my knowlees identified in item-4 4 •e, and described Aviation Regulaticess andthatthe restat. oraltaeiuencut. hereto have furnished herein. istrue and ccarectto , Date August 1, 2001 . Signature of Authorized Individnal Owen H. Pritchard II I. Approval- for Return- To-Sery cc Pursuant Administrator BY to the authority given persons of the Feclizal Aviatioa specified below, the unit identified Administration and is El APPROVED in item 4 was inspected in the manner prescribed by the D REJECTED FAA Flt.. Standards Inspector Manufacturer Inspection Authorization , Other (Specify! . FAA Designee X Repair Station - • Person- Approved by Transport Canada .. Aim() • .....4. Group - Data of Approval or Rejection August 1, 2001 Certificate or Designation Na • DU4R141M ' Signatu c • 1 / L. Palm Authorized Ind' y • ual 0 IIIIIP, On FAA Form 337 (12-88) EFTA00277664 NOTICE • Weight andbalance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued con fomity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is-required, attach additional sheets. Identify with aircraft nationality and registration mark and data work*Cornpleted_) BOEING SIN 20115 REG. NO. N908JE Page 1 August 1, 2001 The following major repairs were accomplished: NR# 27754 Repaired delaminated R/H Mid Flap Trailing Edge wedge by removing the delaminated section and fabricating and installing a new T/E wedge and strips IAW TIMCO REO-L00464 dated 7/17/01 FAA Form 8110-3 approved by DER Richard C. Saltivan DER # DERT-405157-CE dated June 19, 2001. NR# 27918 Repaired the delaminated and corroded Left Hand Inboard Mid Flap bottom upper Rock-shield panel by removing Rock-shield and corrosion, treated and primed area to be bonded,. impregnated fiberglass overlays as required, applied conductive coating and installed panel IAW B727 SRM 5-7-50-2, 51-40-8, MM 51-20-0 & SB 727-32-247 R1 dated June 5, 1981. SUMMARY 1. All work accomplished IAW Boeing SRM, TIMCO REO, FAA Form 8110-3 and Service Bulletin. 2. Records of all work accomplished is on file at this repair station under work order 185003. 3. Aircraft Weight and Balance updated accordingly. end Ei Additional Sheets Are Attached *- U.S. GOVERNMEqF PRLNTLVG OFFICE: 1992-769-012160157 EFTA00277665 (tt'' • MAJOR REPAIR AND ALTERATION US Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC Address (As shown on registration certificate) 103 FOULK RD STE 202 WILMINGTON DE 19803-3742 3. For FAA Use Only ino data identified herein with described aircraft, subject try aPPlovad, linverthines requirements J Ufilterini 3' s 431. i i the applicabl: brthte person :above by 1 7- SO —rD ,e)- Date , ire A Inspector 4. Unit Identifica 99) 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type ' Manufacturer ... 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMITED EYKR782D 1,3. 1,2,3. ENG. Foreign Certified Mechanic x Certificated Repair Station Manufacturer AfF & D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date -71WO / Signature of Authorized Individ I John K. Urso. Inspector. C.- ,a441 --- 7. Approval for Return to Servl Pursuant Administrator BY to the authority given of the Federal Aviation persons specified below, the unit Administration and is identified in item 4 was inspected in the manner prescribed by the a APPROVED M REJECTED Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Ap royal or Rejection p 7/2 1—/&/ Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance FAA Form 337 (12-88) EFTA00277666 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) AIRCRAFT: BOEING, TYPE: 727-31, S/N 20115, DATE: 06/14/2001, W.O. 16236, PAGE 1 OF 2 INSTALLED A SINGLE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY SYSTEM (TSO C113). THIS MODIFICATION WAS COMPLETED USING JET AVIATION DRAWING NO. B727-16236-270, ARGUS 5000 C/E MOVING MAP DISPLAY, REV. A, DATED 06/19/01. REFERENCE FAA FORM 8110-3, DATED 6/20/01, BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM. THE EXISTING LASERTRAK WIRING WAS RE-BUSSED DUE TO RELOCATION OF LASERTRAK C.D.I. THIS MODIFICATION WAS COMPLETED USING JET AVIATION DRAWING NO. 34-61-32-1, LAZERTRAK SYSTEM MODIFICATION, REV IR, DATED 5/24/01. THE STRUCTURAL INSTALLATION OF THE ARGUS:5(104/GFAMDVAIO MAP,DISPLAY nsum AND THE RELOCATION OF THE LASERTRAK C.D.I. WAS COMPLETED USING JgTANTIM , 1'413119ff,ING:N9:1372-7-1p31V-i1270, ARGUS 5000/CE MOVING MAP EQUIPMENT INSTALLATION, REV. IR, DATED 05d9'/OrREff itEN r 41,0,-5115AIED 06/03/2001, BY STRUCTURES DER NO. DERT-810028-NE. 7110 A can, &A — THE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY IS A PICTORIAL NAVIGATION INSTRUMENT, WHICH PROVIDES VISUAL REFERENCE OF AIRCRAFT POSITION RELATIVE TO LANDING FACILITIES, NAVIGATIONAL AIDS AND SPECIAL USE AIRSPACE. THE ARGUS 5000/CE RECEIVES GEODETIC POSITION AND OTHER NAVIGATION INFORMATION FROM THE NO. 1 UNS-ID FMS THROUGH AN EVENTIDE AVIONICS ARINC 419/429 ADAPTER UNIT AND THE AIRCRAFT'S NO. 3 HONEYWELL "LASERREF' INERTIAL REFERENCE SENSOR (IRS) DIRECTIONAL HEADING SYSTEM WHICH, PROVIDES MAP GRAPHICS AND BEARING ORIENTATION. THE FOLLOWING SWITCHES ARE LOCATED ON P16 FORWARD CONTROL STAND, BELOW THE ARGUS 5000/CE MOVING MAP DISPLAY: ARGUS INFO MOMENTARILY DEPRESSING THE ARGUS INFO ILLUMINATED (BLUE) SWITCH BRINGS UP INFORMATION ABOUT MAP OBJECTS ON THE ARGUS 5000/CE MOVING MAP DISPLAY. IF THE ARGUS INFO SWITCH IS PUSHED IN FOR 1 SECOND, THE ARGUS 5000/CE WILL RETURN TO THE MAP DISPLAY IN THE SAME MODE AND AT THE SAME RANGE SET, WHEN INFO WAS ENTERED. ARGUS SEL MOMENTARILY DEPRESSING THE ARGUS SEL ILLUMINATED (BLUE) SWITCH CYCI RS THE ARGUS 5000/CE DISPLAY THROUGH THE VARIOUS MAP OBJECTS. ARGUS TEST MOMENTARILY DEPRESS THE ARGUS TEST SWITCH TO ENABLE DISPLAY SIMULATION TEST. THE ARGUS 5000/CE MOVING MAP DISPLAY IS APPROVED FOR IFR ENROUTE NAVIGATION ONLY WHEN RECEIVING NAVIGATION INFORMATION FROM AN IFR APPROVED GPS, LORAN, OR OTHER LONG-RANGE NAVIGATION SYSTEM. THE ARGUS 5000/CE DATABASE MUST BE CURRENT (NOT EXPIRED). THE ARGUS 5000/CE IS APPROVED FOR USE AS A SUPPLEMENTAL NAVIGATION DISPLAY FOR VFR AND IFR OPERATIONS BUT IS LIMITED TO THE APPROVAL OF THE LORAN C OR GPS NAVIGATION SYSTEM. THE ARGUS 5000/CE MOVING MAP DISPLAY HAS BEEN SHOWN TO MEET THE CRITERIA OF FAA rso-c113, AIRBORNE MULTIPURPOSE ELECTRONIC DISPLAYS, AND HAS BEEN PREVIOUSLY INSTALLED UNDER EVENTIDE INC. FAA APPROVED STC SA0054NY, IN AN AIRCRAFT AND MEETS THE FAA REQUIREMENTS FOR OPERATION IN THE AIRCRAFT DURING INSTRUMENT FLIGHT AND CAN BE USED AS A REQUIRED INSTRUMENT. THE NEW EQUIPMENT AND. ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER EVENTIDE AVIONICS INSTALLATION MANUAL NO. 5003, REVISION 03.07, DATED JULY 10, 1995 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-I6236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. 1S] Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277667 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) AIRCRAFT: BOEING, TYPE: 727-31, SIN 20115, DATE: 06/1442001, W.O. 16236, PAGE 2 OF 2 AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER 11, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED IAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS OUTLINED IN EVENTIDE AVIONICS DRAWING NO. 14O003, REV. B, DATED JUNE JUNE 4, 1999, AND STATES THAT THE ARGUS 5000/CE MOVING MAP DISPLAY SYSTEM IS "ON CONDITION". THE REQUIRED F.A.A. ARPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236-I01, REV IR, PAGES 1 THRU 6 DATED JiJ lie 2 00 I HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END K Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277668 . AI as EFTA00277669 • Jet Aviation Associates Ltd. Bldg. 1515 Perimeter Rd. Palm Beach Int'l Airport West Palm Beach, FL 33406 FAA CRS EYKR782D Document No. B727-16236-101 AFM Supplement to The Boeing Company 727-31 Serial No. 20115 FAA Form 337 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-31 REGISTRATION NO.: N908JE SERIAL NO.: 20115 WITH A. SINGLE EVENTIDE AVIONICS ARGUS 5000/CE MOVING MAP DISPLAY This supplement must be attached to the FAA approved Airplane Flight Manual when the airplane is modified by the installation of a single Eventide Avionics Argus 5000/CE Moving Map Display receiving navigation inputs from the No. 1 UNS-1D Flight Management System (FMS) in accordance with manufacture's Installation Manual No_ 50 3 Revision 03.07, dated July 10, 1995 or later approved revision and FAA Form 337, dated "7/ 7 O/ 1 The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult the appropriate basic Airplane Flight Manual. FAA Approved: Federal Aviation Administration Flight Standard District Office - 17 1050 Lee Wagener Blvd. Ft. Lauderdale, Florida 33315 FAA Approved Date: JUN 2 1 2001 Page 1 of 6 EFTA00277670 O-01 08:53 Jet Aviation ,Jun -20-01 08:03A N 3 Curran 352 243 1011 P-02 P _ 02 C DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAI. AVIATION REGULATIONS DATI:. 06/20/2001 • •I AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. • 727-31 TYPE (Alt-Mane. Radio. Helicopter. etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-270, Revision A, dated 06/19101 ARGUS 5000/CE MOVING MAP DISPLAY • PURPOSE OF DATA In support of major alteration to.Boe-ing 727-31, serial number 20115, registration number N905.1E. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.869 (a)(4) FAR 25.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1529 FAR 25.1309 (a)(b)(g) FAR 25.1581 (a)(b)(d) FAR 25.1351 (a) FAR 26.1357 (a)(c) CERTIFICATION -'Witt ratthont• .vault by ain-criaa Isla loud obwre AuK1006 al/talked OK'd, ..00t Iscrrsi 'WINE of tart- AitagigolfiltOr slid it, WroidliaCe 1.101 tau:gime, aid tiviii.O•As of tippAix1Ann I grfttles, Fan ISJ if the Finlitral Ariati.• Kepis hods, hare bora tisairrid no stionti.or ...III, ntsobik lord prolletturn and hoad no cn..pty will. applicable mtikeoph-xti ei Ow I edc.1 .4.'114. these data & Equipment Aspects. Desi/a Approval Only. Does Plot ('osassita he Installation Approval) Rtptatanwl a Recommend approval of I (We) Therefore L] Approve these ties (Systems SI GNATILIKEIS) N El) ENG) NG REPRESENTATIVEISI DESIGNATION NOM BER(SI CLANSIFIE •rtnhts €40---- DERT-510087-NM Systems & Equipment an — FAA Form 8110-3 n i-70) SUPERSETWC PREVIOUS EDITION CiPO 9O1-613 FLLENAIME: SC-127-NCINGMAP_ADOC EFTA00277672 k 4 71& . JEF NIf/R11-10111 JET AVIATION ASSOCIATES, LTD 1515 PERIMETER ROAD PALM BEACH INT'L AIRPORT WEST PALM BEACH, FLORIDA 334O6-1493 561-233-7262 FAX 561 -233-7279 CRS-EYKR782O MODIFICATIO\ DAWING PROPRIETARY NOTES Ths drcrwlng contoins specifications and/or data. technical materiel, proprietary designs and information that ere the sate property of JET AVIATION ASSOCIATES. LTD. to be held and treated by its recipient on o confidential basis and is not to be shown or disclosed to any unauthorized organization or person without the written authorization of JET AVtATION ASSOCIATES. LTD. TITLE: LASERTRAK SYSTEM MODIFICATION PAGE: 1 OF 1 DWG NO.: 34-61-32-1 REASON: RE-BUSS LASERTRAK INSTRUMENT LIGHTING FROM CENTER PANEL TO CAPTAINS INSTRUMENT PANEL DUE TO RELOCATION OF INSTRUMENT A NOTES: 1. AIRCRAFT WIRING INSTALLATION CHAPTER 11, SECTIONS 2. ALL WIRE PER MIL 3. ALL SHIELDED WIRE 4. ALL WIRE 20 AWG 5. ALL CIRCUIT BREAKERS 6. ALTERNATE TWISTED TRIPLE TWISTED: • . TWISTED PAIR: 7. LOWER CASE LEITERS 8. THIS MODIFICATION SYSTEM PER THE I REGARDING THE LASERTRAK DWG. 34-61-32. TO THE ORIGINAL ITAPT BRGAIST IND. i H I INSTR LTS{ ci tI rr, i L .A.,__. __...y__. _ _.•\„,.._ LOC: CAPT. INSTR. PANEL rIASERTRAK CDI I I- I H IT ) INSTR LTS { I i I I ...- LOC: CAPT. INSTR. PANEL IAW FM A.C. 43.13-1B, 1, AND 3-20. -W-22759 UNLESS SHIELDED. PER MIL- C-27500TG. UNLESS SPECIFIED OTHERWISE. PER MS36574. WIRE COLORS MAY BE SUBSTITUTED: PRIMARY SUB LASERTRAK PAGE AVJET DWG. 33-11-11 RED (R) WHITE (W) BLUE (B) BLUE (B) YELLOW (Y) ORANGE (0) RED (R) WHITE (W) BLUE (B) BLUE (B) ARE SHOWN UNDERLINED. I.E. ci. DRAWING ONLY CHANGES THE EXISTING WIRING SHOWN, FOR ALL OTHER INFORMATION SYSTEM REFER TO ORIGINAL PAGE THIS MODIFICATION DRAWING SHALL BE ATTACHED PAGE AVJET DRAWING FOR REFERNCE. 09504 20 „T, I-- 20 ill — 019 -20 — — —5 ----018-20---o M • D9315 D9315 1 20 } 09315-9-20 Q SYMBOL AND NUMBER REFERS TO PARTS LIST ITEM NUMBER. A SYMBOL AND NUMBER REFERS TO INSTALLATION NOTES. O SYMBOL AND LETTER REFERS TO LIKE LETTER IN SYMBOL ON THIS DWG. NO. =DC GND GROUND NOTES: { -D> =SHLD GND NEW WIRE WIRE TYPE NOTES: -C> =AC GND --I> =CHASSIS GND REMOVED WIRE EXISTING WIRE (* ) (_ - - -) ( ) /G. SCALE: NONE SER. NO.: 20115 PREPARED BY: G.L. KARR APPROVED BY: T. JARDINE 1 A/C MODEL: 727-100 REG. NO.: N908JE DATE: 05/24/01 DATE: 05/24/01 EFTA00277674 ty DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 3, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter,etc.) Airplane _ NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1270 B727-16236-1331 •• Argus 5000/CE Moving Map Equipment Installation Sht 1-5, Rev IR Aircell Equipment Installation, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions under Part 183 of the Federal Aviation Regulations,data listed above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recommend approval of these data. I ( X Therefore Approve these data. and limitations of appointment 0 have been examined Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) David E. Haralson Jr-;.,:ie. iici-ez.— DERT-810028-N E Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDMON ER01207.doc EFTA00277676 Q-• O MAJOR REPAIR AND ALTERATION US t Departmen of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration F o r m Approved OMB No. 2120-0020 For FAA Use Only Office Identification INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft _ Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC Address (As shown on registration certificate) 103 FOULK RD STE 202 WILMINGTON DE 19803-3742 3. For FAA Use Only crv3 data Identified heroin compile* ainevorthinee requirements is approved described aircraft. Contor -uthorized in FAR 43, s on 43.7. JUN t 1 20P1 , or* the applicable for the above by a person - 1 7 50- SR) Date ginnfett of FAA inspector 4. Un Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer ,,. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMITED EYKR782D 1,3. 1,2,3. Foreign Certified Mechanic x Certificated Repair Station Manufacturer AF &ENG, D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date -7/0 ) . Signature of Authorized Individual /L.- t 35-- John K. Urso. Inspector. eA— 7. Approval for Return to Se ce Pursuant Administrator BY to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is 0 APPROVED K REJECTED Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Appr val r Rejection 9 - . /. Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assuranc .//' FAA Form 337 (12-88) EFTA00277678 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with afl previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) AIRCRAFT: BOEING, TYPE: 727-31, S/N 20115, DATE: 06/14/2001, W.O. 16236, PAGE 1 OF 2 REMOVED THE EXISTING NO. 1 AND 2 HONEYWELL NZ-920 FMS SYSTEMS AND THE DL-900 DATA LOADER UNIT, AND INSTALLED DUAL UNIVERSAL AVIONICS CORP. UNS-ID FLIGHT MANAGEMENT SYSTEMS (FMS) WITH INTEGRAL GPS SENSORS, A UNIVERSAL AVIONICS CORP. RADIO TUNING UNIT (RTU), AND A UNIVERSAL AVIONICS CORP. DTU-100 DATA TRANSFER UNIT (DTU). THIS MODIFICATION WAS COMPLETED USING ita AVIATION DRAWING NO. B727-16236-410, NO. 1 FLIGHT MANAGEMENT SYSTEM, REV IR, DATED 04/10/01 AND B727-16236-411, NO.2 FLIGHT MANAGEMENT SYSTEM, REV. IR, DATED 04/15/01. THE RTU WAS INSTALLED USING JET AVIATION DRAWING NO. B727-16236-293, FLIGHT MANAGEMENT SYSTEM RADIO TUNING UNIT, REV IR, DATED 04/16/01. REFERENCE FAA FORM 8110-3 DATED 05/29/2001 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM. crli Mr" 25,4+ 11,313;i ts:;::, sC r..:•, ,d,3 orb FOi tno ---, ,,Avfnft= 2t Inc dirlartrup11 THE STRUCTURAL INSTALLATION OF EACH FMS, THE DTU;`' irrtintlIT WEItte9y1P4t7TgRy, .IL7T AVIATION DRAWING NO. B727-16236-1410, DUAL FMS W/RTU EQUIPMENT INSTALLATIONS, REV. IR, DATED 05/1'7/91, cg FAA FORM 8110-3, DATED JUNE I, 2001 BY STRUCTURES DER NO. DERT-810028,- ANTENNAS WER AILED USING JET AVIATION DRAWING NO. B727-16236-144I, GPS ANTENNA INSTALLATI REV. A, DATED 05/29/01, REFERENCE FAA FORM 8110- 3, DATED 6/18/01 BY STRUCTURES DER NO. DERT-510024-CE. THE UNS-1D SYSTEMS RECEIVE BARO-CORRECT1ED ALTITUDE AND TAS INFORMATION FROM THE NO. 1 AND NO.2 AIR DATA COMPUTERS RESPECTIVELY, VOR/DME BEARING AND DISTANCE INFORMATION FROM THE NO. I AND NO.2 COLLINS VIR-432 AND DME-442 SYSTEMS, AND CROSS SIDE GPS INFORMATION AS WELL AS EACH UNITS INDEPENDENT GPS SENSOR DATA, FUEL FLOW DATA FROM THE AIRCRAFT FUEL FLOW SYSTEM AND IRS INFORMATION FROM THE EXISTING NO. 1, 2, AND 3 HONEYWELL "LASERREF" SYSTEMS. THE UNS-ID FMS HAS BEEN PREVIOUSLY INSTALLED UNDER UNIVERSAL AVIONICS SYSTEMS CORP. FAA APPROVED STC SA5072NM, IN AN AIRCRAFT AND CERTIFIED FOR VFR AND IFR NAVIGATION WHICH QUALIFIES THIS INSTALLATION AS A "FOLLOW ON" INSTALLATION PER AC 20-130A. THE UNS-1D FMS SYSTEMS HAVE BEEN SHOWN TO MEET ALL OF THE REQUIREMENTS OF AC-20-130A FOR VFR-IFR NAVIGATION ENROUTE, TERMINAL, OVER WATER AND IN REMOTE AREAS, AND FOR NON-PRECISION APPROACHES. THE NO.1 AND 2 FMS SYSTEMS ARE DIGITALLY INTEGRATED TO THE EXISTING HONEYWELL FIVE-TUBE ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS). THE PILOT AND COPILOT'S EFIS SYMBOL GENERATOR'S HAVE HONEYWELL SERVICE BULLETIN A21-2000-028 AND THE MULTI-FUNCTION GENERATOR HAS HONEYWELL SERVICE BULLETIN A21-2000-029 TO INCORPORATE NON-PRECISION GPS SCALING VIA GAMA ARINC 429 LRN INTERFACE WHICH MEETS REQUIREMENTS OF TSO C129A AND AC 20-130A. THE FMS SYSTEMS ARE CROSS-COUPLED TO EITHER THE PILOT OR COPILOT EFIS FOR DISPLAY AND NAVIGATION. THE EFIS CONVERTS THE DIGITAL TO ANALOG OUTPUTS AND PROVIDES ALL LATERAL STEERING TO THE AUTOPILOT AND FLIGHT DIRECTOR SYSTEM. VERTICAL NAVIGATION (VNAV) FROM EITHER FMS SYSTEM IS NOT DISPLAYED OR COUPLED IN THIS INSTALLATION. THE FOLLOWING REQUIRED ANNUNCIATORS FOR THE FMS SYSTEMS ARE DISPLAYED ON THE EFIS DISPLAYS: FMS MSG INDICATES A MESSAGE IS TO BE ACKNOWLEDGED ON THE MSG PAGE. (COLOR: AMBER) LOCATED ON EADI. XTK SELECTED CROSSTRACK IS ACTIVE. (COLOR: CYAN) LOCATED ON EHSI. WPT INDICATES WAYPOINT ALERT TWO MINUTES PRIOR TO WAYPOINT IN EN ROUTE MODE, AND 15 SECONDS PRIOR IN APPROACH MODE. WHEN THIS ANNUNCIATOR FLASHES, IT INDICATES THAT AN UPCOMING VERTICAL FLIGHT PATH ANGLE (FPA) CHANGE IS WITHIN TWO MINUTES. (COLOR: AMBER) LOCATED ON EHSI. APP AN APPROACH HAS BEEN ACTIVATED. (COLOR: CYAN) LOCATED ON EHSI. El Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277679 NOTICE Weight andtalance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. Nk. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) AIRCRAFT: BOEING, TYPE: 727-31, S/N 20115, DATE: 06/14/2001, W.O. 16236, PAGE 2 OF 2. THE FOLLOWING REQUIRED ANNUNCIATORS WERE LOCATED ON THE EXISTING PILOT AND COPILOT'S INSTRUMENT PANEL ADJACENT TO THE EADI UNITS: FMS HDG THE FMS IS IN HEADING SUB-MODE. (COLOR: BLUE) GPS INTEG GPS INTEGRITY IS OUTSIDE OF THE ALLOWABLE LIMIT FOR A PHASE OF FLIGHT (2.0-NM EN ROUTE, 1.0-NM TERMINAL AND APPROACH TRANSITION, AND 0.3-NM FINAL APPROACH SEGMENT). SEE SECTION III, ABNORMAL PROCEDURES. (COLOR: AMBER). THE ADDED ANNUNCIATORS ARE DIMMED AND TESTED USING THE EXISTING PILOT AND COPILOT ANNUNCIATOR COUPLERS. THESE UNITS HAVE BEEN MODIFIED USING JET AVIATION MODIFICATION NO. 33-39-02-1, CAPT. AND F/O ANNUNCIATOR COUPLER MODIFICATION, DATED 04/12/01, REFERENCE FAA FORM 8110-3, DA IED 05/29/2001 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-NM. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER UNIVERSAL AVIONICS CORP. RETURN TO SERVICE MAINTENANCE AND CHECKOUT PROCEDURES MANUAL NO. 34-60-21, DATED 19 MARCH 2001 WITH NO DISCREPANCIES NOTED. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 1 OF 5, DATED 06/19/2001, WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH•12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK, INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER 11, SECTION 4. ELECIRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTAT J.FD IAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLY WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.I3-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS AS REQUIRED BY FAR 25.1529 IS DETAILED IN THE UNIVERSAL AVIONICS CORP. UNS-1D FLIGHT MANAGEMENT SYSTEM TECHNICAL MANUAL NO. 34-60-09, DATED AUG 15/97. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATE6112001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333- CE. THE REQUIRED F.A.A. APPROVED FLIGHT MANUAL SUPPLEMENT DOC NUMBER B727-16236-100, REV IR, SHEETS 1 THRU 9, DATED ne 2-1 i 20 0 I HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END K Additional Sheets Are Attached EFTA00277680 "fr .4 EFTA00277681 Oak Jet Aviation Associates Ltd. BIdg. 1515 Perimeter Rd. Palm Beach Int'l Airport West Palm Beach, FL 33406 FAA CRS EYKR782D Document No. B727-16236-100 AFM Supplement to The Boeing Company 727-31 Serial No. 20115 FAA Form 337 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BOEING 727-31 REGISTRATION NO.: N908JE SERIAL NO.: 20115 WITH DUAL UNIVERSAL AVIONICS FLIGHT MANAGEMENT SYSTEMS (UNS1-D) INSTALLED This supplement must be attached to the FAA approved Airplane Flight Manual when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VOR/DME from the Collins No. 1 and No. 2 VORJDME systems in accordance with manufacture's Installation and Checkout Manual No. ?4-60-09, Rev. 2. dated August 15, 1997 or later approved revision and FAA Form 337, dated- 7/2/0/ 0 The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult the appropriate basic Airplane Flight Manual. FAA Approved: Federal Aviation Administration Flight Standard District Office - 17 1050 Lee Wagener Blvd. Ft. Lauderdale, Florida 33315 JUN 2 1 2001 FAA Approved Date: Page 1 of 9 EFTA00277682 May-29-01 01:59P N 3 Curt-an 352 243 1011 P _ 06 L DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 05129/2001 -, AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane. Radio. Helicopter. etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-293, Initial Release, dated 04/16/01 B727-16236-410, Initial Release, dated 04/10101 B727-16236-411, Initial Release, dated 04/15/01 33-39-02-1, Initial Release, dated 04112/01 FLIGHT MANAGEMENT SYSTEM RADIO TUNING UNIT NO. 1 FLIGHT MANAGEMENT SYSTEM NO. 2 FLIGHT MANAGEMENT SYSTEM CAPT AND F/O ANNUNCIATOR COUPLER MODIFICATION PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N90BJE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1329 (h) FAR 25.1529 FAR 25.869 (a)(4) FAR 25.1351 (a) FAR 25.1581 (a)(b)(d) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c)(d)(e) FAR 25.1309 (a)(b)(c)(d)(e)(g) FAR 25.1381 (a)(b) FAR 25.1322 (b)(c) FAR 25.1431 (a)1131(c) CERTIFICATION - Under authority vested by direction data listed above and on attached sheets 'mothered NONE of the Admiwistrator and in accordance laid. conditions and Ensiles-tows of appoinemeat ander Part I23 of the Federal Awl-mien IRegulatiosts, have been remained in accordance with establistard procedures sod fooad to comply with applicable requirements of the Federal Aviation these data & Equipment Aspetts, Design Approval Only. Does Not Constitute Installation Approral) Regulations. 0 Retommeoil approval of I (We) Therefore El Approve these data (Systems SIGNATURES F D LUG TE GLNEE RETRESENTATIVE(S) DESIGNATION NUMBERIS) CLASSIFICATTON(S) ,Q DERT-510087-NM Systems & Equipment No an J. an 01111 _ 110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME: SC-727-FMS.DOC EFTA00277684 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 1, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION • MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE • B727-16236-1261 B727-16236-1410 • • AT-855/RTA-880 Antenna Installations, Sht.1-7, Rev A • Dual FMS WI RTU Equipment Installations, Sht 1-6, Rev IR Note: - 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 . . . CERTIFICATION - Under authority vested by direction of the Administrator .and in accordance with conditions under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recommend approval of these data. I ('Therefore Approve these data. and limitations of appointment 0 have been examined Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) David E. Haralson .a.are. 14,-.1.-- DERT-810028-NE Structural FAA FOITTI 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01202.cloc EFTA00277686 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 18, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL B727-31 TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Jet Aviation LIST OF DATA IDENTIFICATION TITLE Jet Aviation Engineering Drawing No. B727-16236-1441, Dtd. 5/29/2001, Rev. A END END GPS Antenna Installation Beoing B727-31, N908JE, S/N 20115 END END END END END END END END Note: The certification evaluation of structure. Structural Repairs on Notes: basis of this aircraft includes FAR 25.571 Damage - tolerance and fatigue Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness of Transport Category Airplanes, the damage tolerance and fatigue evaluation of the structure must be performed before 6/18/2002. aspects only of the above listed data are approved is valid for the aircraft model and serial number is based on structural analysis on file at DER Services office in Ft. Lauderdale, FL. No. B727-31 Serial No. 20115 1) The structural herein. 2) This approval listed below 3) This approval corporate Model PURPOSE Approve data for antenna installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS (LIST SPECIFIC SECTIONS) 25301, 25303, 25.305, 25.307, 25.601, 25.603, 25.605, 25.609, 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered been examined in accordance with established procedures and found to comply with applicable requirements of the Aviation Regulations. Recommend approval of these data I (We) Therefore P1 Approve these data and limitations of have Federal SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Robert J. Belgau DERT-510024-CE Structures FAA FORM 8110-3 (11-70) SUPERSEDES PREVIOUS EDITIO N DER SERVICES PROJECT NO. 2001-082 EFTA00277688 a MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, or Appliance) of Transportation Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Ont Office Identification 5-0- FS`DO - i 7 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructi s 9 and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exc ed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type •- Manufacturer ,,, 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMITED EYKR782D 1,3. 1,2,3. ENG, Foreign Certified Mechanic X Certificated Repair Station Manufacturer AIF & D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 7/2/01 • Signature of Authorized Individual John K. Urso. Inspector. 16, U -V 7. Approval for Return to Service k Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 was inspected in the manner prescribed by the K REJECTED C4 APPROVED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assuranc FAA Form 337 (12-88) EFTA00277690 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, SIN 20115, N908JE, W/O 16236. INSTALLED 2 EA NEW GARMIN GPS ANTENNAS P/N 011-00134-00 (TSO C129A). 1 EA AT FUSELAGE STATION 284.8, BL 0.0, AND 1 EA FUSELAGE STATION 934.3 RBL 4.56, PER JET AVIATION DRAWING B727-16236-1413, REV IR, DATED 6/5/01 TITLED - DUAL AUXILIARY GPS ANTENNAS INSTALLATION. REF F.A.A. FORM 8110-3 DATED 6/6/01 BY STRUCTURES D.E.R. NO. DERT-510394- CE. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-IB, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER 11, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SF.I.FCTED AND INSTALLED LAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-IB, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS LAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS CONTAINED IN ENGINEERING REPORT JMER-836, REV IR, DATED 6/10/01. REFERENCE FAA FORM 8110-3 DATED 6/11/01 BY STRUCTURES DER NO. DERT-510394-CE. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END K Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277691 ••• yr 44t.c.c000v..)4 0 AgiA U ri't S • to 002 U.S. DEPARTMENT OF TRANSPORTATION PEDERAL AVIATION ADMINISTRATION STATEMENT OP COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE Tune 6, 2001 • AIRCRAFT OR AIRCRAFT COMPONENT WENTIFICATION MAKE BOEING MODEL NO. 8727-3I TYPE (Airplane. Reif*, Helicopter, etc.) Airplaii NAME OP APPLICANT I ul, ...----A-kl../ViaaalLasicKjares ...., , LIST OP DATA IDENTIFICATION TITLE B727-16236-1413 IR Sheets 1— 3 (6/5/01) END DRAWING — DUAL AUXILIARY GPS ANTENNAS INSTALLATION NOTE: Approval for the structural aspects related to the above design data will be covered by a separate Form 8110-3 which will be issued for the Proof of Structure and will include required inspection items) to ensure Continued Airworthiness . . associated with this modification. END END PURPOSE OF DATA To provide a record of design approval of the above data applicable to B727-31, SIN 20115, Registration No. N90&1E. for manufacturing and confortnity. See NOTE above. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.6601 FAR 25.609 FAR 25.603 FAR 25.611 FAR 25.605 FAR 25.613 CERTIFICATION - Under authority vetted by direction of the Administrator arxi in 2,c,cordanee wick cordidons sad limitations of appointment under part 183 of az Pcderal Aviation Regulatiorn. ellta listed above and on attached slims numbered IVA have been examined in sem-dame with #=011101(4 procodures and found m comply with applicable requirements of !be Federal Aviation Regulations. I * Therefore 0 Recommend approval of these dota X Approve Mete data (Sec NOTE above) siGNATurtr.(s) OF DESIGNATED REPRESENTATIVE(S) DESIGNATION NUNIBMS) CLASSIFICATION(S) DERT - 510394 - CE STRUCTURES Kenneth W. Thompson - FAA 8110.3 (11-70) SUPERSEDES PREVIOUS EDITION sheet 1 of 1 EFTA00277692 • .. U.S. DEPARTMENT OF TRANSPORTATION. - FEDERAL.AVIATION ADMINISTRATION . , STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 11, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BDEilia /172L-31 EURELANE.---IgLAYialisnlAsurdatcda11_, MODEL NO. TYPE (Airplane, Radio, Helicopter, etc.) NAME OF APPLICANT LIST OF DATA IDENTIFICATION TITLE JMER-836 IR Dated 06/10/01 • ENGINEERING REPORT — STRUCTURAL SUBSTANTIATION - DUAL AUXILIARY GPS ANTENNA INSTALLATION ON A BOEING B727-31 AIRCRAFT, S/N 20115 NOTE: The operator of B727-31 aircraft S/N 20115 modified by drawing B727-16236-1413 dated 6/5/01 issued at no revision, is required to incorporate in the Airworthiness Limitations Section of the Instructions for Continued Airworthiness applicable to the existing Maintenance Program, an inspection item at a frequency not to exceed 3700 flights to detect signs of distress (0.25 inch or smaller crack and/or working rivets) common to the GPS antenna installation as detailed in drawing B727-16236-1413. Refer to FAR PART 25 Appendix H and Report JMER-836 IR page 4.1 (CONCLUSIONS) for instructions. PURPOSE OF DATA To provide a record of design approval of the above data as applicable to B727-31 S/N 20115 and to show compliance to the following FAR's: . . APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 FAR 25.307 FAR 25.605 FAR 25.613 FAR 25.303 FAR 25.571 FAR 25.609 FAR 25.625 FAR 25.305 FAR 25.603 FAR 25.611 Chlt111-ICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered N/A have been examined in accordance with I (k) Therefore established . X procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data Approve these data (Structural aspects only) - . SIGNATURE(S) OF DESIGNATED REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 60- 7- DERT - 510394 - CE . STRUCTURES Kenneth W. Thompson .. • FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION sheet 1 of 1 EFTA00277694 .1. 11 EFTA00277695 O f ' MAJOR REPAIR AND ALTERATION OS Deoartrraant 0 Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office identification INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in item 1 above) X POWERPLANT PROPELLER APPLIANCE Type • • _ Manufacturtr \ ,.. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMTIED EYKR782D 1,3. 1,2,3. ENG, Foreign Certified Mechanic x Certificated Repair Station Manufacturer A/F & D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 7/2/01 Signature of Authorized Individu ,6- John K. Urso. Inspector. (1,,,_.,- 7. Approval for Return to Servi Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 was inspected in the manner prescribed by the 0 APPROVED • REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EY1CR782D Signature of Authorized individual Ronald K. Bystrom. Manager Quality Assurance FAA Form 337 (12-88) EFTA00277696 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with 'all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, S/N 20115, N908.1E, W/O 16236. INSTALLED A NEW KGS ELECTRONIC MODEL UC-28-14, 28 VDC TO 14 VDC CONVERTER AND THREE POWER OUTLETS IN THE COCKPIT IN ACCORDANCE WITH KGS ELECTRONIC MODEL UC-28-14 INSTALLATION MANUAL AND ADVISORY CIRCULAR 25-10 (INSTALLATION OF MISCELLANEOUS NON REQUIRED ELECTRICAL EQUIPMENT) USING THE FOLLOWING JET AVIATION DRAWINGS SUBSTANTIATED BY F.A.A. FORM 8110-3 RESPECTIVELY WIRING DRAWING: • B727-16236-352, REV IR, DATED 5/25/01, SHEETS 1 & 2, TITLED - 28-14 VDC CONVERTER WIRING DIAGRAM. REFERENCE F.A.A. FORM 8110-3 DATED 6/7/01 BY SYSTEMS AND EQUIPMENT DER NO. DERT-510087-CE. STRUCTURAL DRAWING: • B727-16236-1352, REV IR, DATED 6/6/01, SHEETS 1 THRU 5, TITLED - 28-14 VDC CONVERTER EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3 DATED 6/10/01 BY STRUCTURES DER NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER KGS ELECTRONIC MODEL UC-28-14 INSTALLATION MANUAL WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/20011 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER 11, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED IAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.I3-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-IB, CHAPTER 10, SECTION 2 AND AC 43.I3-2A, CHAPTER 1 PARAGRAPH 9. THERE IS NO CHANGE TO THE MANUFACTURERS MAINTENANCE FOR CONTINUED AIRWORTHINESS DUE TO THIS MODIFICATION. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END K Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277697 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 06/07/2001 ... AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE " B727-16236-352, Initial Release, dated 05/25/01 B727-16236-580, Initial Release, dated 05/25/01 B727-16236-600, Initial Release, dated 05/25/01 • ---- 28-14 VDC CONVERTER WIRING DIAGRAM CABIN NO. 2 60 Hz SYSTEM SPARE WIRING (PROVISIONS) PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.869 (a)(4) FAR 25.1353 (a)(b) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c) FAR 25.1309 (a)(b)(g) FAR 25.1431 (a)(b)(c) FAR 25. 1322 (b) FAR 25.1529 FAR 25.1351 (a) CERTIFICATION - Under authority vested by direction data listed above and on attached sheets numbered NONE have of the Administrator and in accordance with conditions and limitations of appointment under Part la3 of the Federal Aviation Regulations. been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Regulations. K Recommend approval of I (We) Therefore E3 Approve these data (Systems )• SIGNATURE( ESIGN NGIN REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) - DERT-510087-NM Systems & Equipment - No an an J. ran FAA Foim 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 90I-6I3 FILENAME SC-727-CAB-PWR.DOC EFTA00277698 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 10, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter,etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1352 28-14 VDC Converter Equipment Installation, Sht 1-5, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions under Part 183 of the Federal Aviation Regulations,data listed above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recommend approval of these data. I ( )34 Therefore Approve these data. and limitations of appointment 0 have been examined Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICAT1ON(D Structural David E. Haralson P.,..,,e. 1-4,-.1.-- DERT-810028-NE FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01209.doc EFTA00277700 4 2 MAJOR REPAIR AND ALTERATION US Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification ()— r5D6-i7 7/- INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructs s and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to ex d $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only • 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer \ ,. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMITED EYKR782D 1,3. 1,2,3. ENG. Foreign Certified Mechanic x Certificated Repair Station Manufacturer A/F & D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 7/2/01 Signature of Authorized Individual John K. Urso. Inspector. 7. Approval Approval for Return to Service Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 was ns in the manner prescribed by the lID REJECTED APPROVED FAA Flt. Standards Inspector Manufacturer inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 7/2/01 , Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance. ae " . FAA Form 337 (12-88) EFTA00277702 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with .alf previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, SIN 20115, N908JE, W/O 16236. INSTALLED A UNITRON 60 HZ CONVERTER P/N PS-62-66D AND 26 EA CABIN OUTLETS PER UNITRON 60 HZ CONVERTER INSTALL MANUAL NO. PS-62-66D-6. THIS MODIFICATION WAS ACCOMPLISHED PER THE FOLLOWING JET AVIATION DRAWINGS WHICH ARE SUBSTANTIATED BY F.A.A. FORM 8110-3 RESPECTIVELY WIRING DRAWING: • B727-13236-580, REV IR, DATED 5/25/01, SHEETS 1 THRU 5, TITLED - CABIN NO. 2 60 HZ SYSTEM REFERENCE FAA FORM 8110-3 DATED 6/7/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS: • B727-16236-1580, REV IR, DATED 6/11/01, SHEETS 1 THRU 7, TITLED - CABIN NO. 2 60 HZ EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3, DATED 6/13/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-:1B, CHAPTER 11, SECTION 4. ELECIRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16, ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.I3-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. THERE IS NO CHANGE TO THE MANUFACTURERS MAINTENANCE FOR CONTINUED AIRWORTHINESS DUE TO THIS MODIFICATION. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END K Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277703 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE • 06/07/2001 -.. AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-352, Initial Release, dated 05/25/01 B727-16236-580, Initial Release, dated 05/25/01 B727-16236-600, Initial Release, dated 05/25/01 , 28-14 VDC CONVERTER WIRING DIAGRAM CABIN NO. 2 60 Hz SYSTEM . SPARE WIRING (PROVISIONS) . PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.869 (a)(4) FAR 25.1353 (a)(b) FAR 25.1301 (a)(b)(c)(d) FAR 25.1357 (a)(c) FAR 25.1309 (a)(b)(g) FAR 25.1431 (a)(b)(c) FAR 25. 1322 (b) FAR 25.1529 FAR 25.1351 (a) CERTIFICATION — Under authority voted by direction data listed above and on attached sheets numbered NONE have of the Administrator and in accordance with conditions and limitations of appointment under Part IS3 of the Federal Aviation Regulations. been examined in accordance with established procedures and found to comply with applicable requirements or the Federal Aviation these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Regulations. El Recommend approval of I (We) Therefore 0 Approve these data (Systems siGNA7-0 £SIG G REPRESENTATIVES) DESIGNATION NUMBER(S) CLSSIFICATIONS) 11-ele,--- DERT-510087-NM Systems & Equipment No an J. ran AA Form 8110-3 (11-70) sUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME SC-727-CAB-PWR.DOC EFTA00277704 • DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 13, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter,etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1580 Cabin #2 60 Hz Equipment Installation, Sht 1-7, Rev IR Note: • 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions under Part 183 of the Federal Aviation Regulations,data listed above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recommend approval of these data. I ( X Therefore Approve these data. and limitations of appointment 0 have been examined Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) Structural David E. Haralson 1,-;4Oae. ilicied......--- DERT-810028-N E FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01210.doc EFTA00277706 4k • `V EFTA00277707 No MAJOR REPAIR AND ALTERATION US Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120.0020 For FAA Use O ly Office Identification c0-- r5DO - 1 7 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instr ions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to xceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer ‘,. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMITED EYKR782D 1,3. 1,2,3. ENG, Foreign Certified Mechanic X Certificated Repair Station Manufacturer A/F & D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 7/2/01 . Signature of Authorized Individual John K. Urso. Inspector. r\ 4- 16-'6(----! — 7. Approval for Return to Servige Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 wa inspected in the manner prescribed by the APPROVED III REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EYKR782D ..... Signature of Authorized Individual 1 Ronald K. Bystrom. Manager Quality Assuranc FAA Form 337 (12-88) EFTA00277708 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, S/N 20115, N9083E, W/O 16236. INSTALLED AN AIRCELL ATG.01 FLIGHT PHONE SYSTEM CONSISTING OF AN ANTENNA P/N CI-5000, A TRANSCEIVER P/N 900002-2, and AN ANTENNA MATCHING UNIT P/N 83518, 4 EA HANDSETS P/N 400-10035-001 AND 4 EA HANDSET CRADLES P/N 400-10038-001. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING: • B727-13236-330, REV. IR, DATED 4/30/01, SHEETS 1 THRU 3, TITLED - AIRCELL ATG.01 AIR / GROUND TELEPHONE REFERENCE FAA FORM 8110-3 DATED 5/29/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-1330, REV. A, DATED 5/29/01, SHEETS 1 THRU 4, TITLED - AIRCELL ATG.01 AIR / GROUND TELEPHONE ANTENNA INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 6/18/01, BY STRUCTURAL D.E.R. NO. DERT-510024-CE. • B727-16236-1331, REV. IR, DATED 5/24/01, SHEETS 1 THRU 6, TITLED -AIRCELL EQUIPMENT INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 6/3/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER AIRCELL ATG.01 FLIGHT PHONE SYSTEM INSTALLATION MANUAL REV IR, DATED 6/11/99 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-IB, CHAPTER 12, SECTION 3, PARAGRAPH 12- 37 AND AC 43.13-2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. _ AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.I3-1B, CHAPTER 11, SECTION 4. FT FCTRICAIJELECIRONIC WIRING WAS SELECTED AND INSTALLED IAW AC43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-IB, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-IB SECTION 16. ELECIRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-1B, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. PER THE AIRCELL ATG.01 FLIGHT PHONE SYSTEM MANUAL ALL COMPONENTS ARE CONSIDERED LINE REPLACEABLE UNITS AND DO NOT API-ECT THE MANUFACTURERS INSTRUCTIONS FOR CONTINUING AIRWORTHINESS. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATE6112001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333-CE. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES REQUIRED FOR THIS INSTALLATION. END K Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277709 --M4y-29 - 01 01:59P N J Curran 352 243 1011 P C.) / DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 05129/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane. Radio, Helicopter. etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-330, Initial Release, dated 04/30/01 • - - - • AIRCELL AGT.01 AIR/GROUND TELEPHONE PURPOSE OF DATA In support of major alteration to Boeing 727-31. serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1357 (a)(c) FAR 25.869 (a)(4) FAR 25.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1529 FAR 25.1309 (a)(b)(g) FAR 25.1351 (a) CERTIFICATION - Under sithoriry . eyed by direction data kited ibtwc sad** tinseled sheen niseslweed NONE or tht Administrator and is setordsset will clisdielons and /imitations et" 'pp:amine/se taedtr Tan 113 *fibs Federal Atistis• ;Ululation:4 have bets emainintd in aceordsnce with reublishtel peiscrchirts and Amid to esertrily with applicabh rtquirttnents et the Fedmri Aviation these data & Equipment Aspects. Design Approval Only, DIM Not Constitute Installation Approval) &Dilations. O Recommend approval of I (We) Therefore 1 Approve these data (Systems SIGNATURE ESIGNA GINEERI PRESENTATIVE(S) DESIGNATION N UM ILERM CLASSIFICATIONS) !at--. DERT-510087-NM Systems & Equipment No n J. C n EFTA00277710 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 18, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL B727-31 TYPE Oftplane, RaSe, Iftlicopra: ac.) Airplane NAME OF APPLICANT Jet Aviation LIST OF DATA 1DEN fIFICALLUN It ILL Jet Aviation Engineering Drawing No. B727-16236-1330, Dtd. 5/29/2001, Rev. A END END Aircell AGT.01 Air/Ground Telephone Antenna Installation Beoing B727-31, N908JE, S/N 20115 END END END END END END END END Note: The certification evaluation of structure. Structural Repairs on tlotes: basis of this aircraft includes FAR 25.571 Damage - tolerance and fatigue Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness of Transport Category Airplanes, the damage tolerance and fatigue evaluation of the structure must be performed before 6/18/2002. aspects only of the above listed data are approved is valid for the aircraft model and serial number is based on structural analysis on file at DER Services office in Ft. Lauderdale, FL. No. B727-31 Serial No. 20115 1) The structural herein. 2) This approval listed below 3) This approval corporate Model PURPOSE Approve data for antenna installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS (LIST SPECIFIC SECTIONS) 25.301, 25.303, 25.305, 25.307, 25.601, 25.603, 25.605, 25.609, 25.613 CF.RTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets number been examined in accordance with established procedures and found to comply with applicable requirements of Aviation Regulations. Recommend approval of these data 1 (y) Therefore Fil Approve these data and Ii • tions of have the ederal SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S) DESIGNATION NUMBERS) CLASSIFICATION(S) Robert J. Belgau 19 0/276415 e.---- -. DEBT-510024-CE Structures FAA FORM 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. 2001-082 EFTA00277712 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 3, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radfo, Helicopter,etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE 8727-16236-1270 B727-16236-1331 . Argus 5000/CE Moving Map Equipment Installation Sht 1-5, Rev IR Aircell Equipment Installation, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority under Part 183 of the Federal Aviation in accordance with established procedures I ( X Therefore vested by direction of the Administrator and in accordance with conditions Regulations,data listed above and on attached sheets numbered and found to comply with applicable requirements of the Federal Recommend approval of these data Approve these data. and limitations of appointment 0 have been examined Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVES) DESIGNATION NUMBER(S) CLASSIFICATION(S) Structural David E. Haralson Pe-,:fe. /4,-d._ DERT-810028-NE FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01207.doc EFTA00277714 DEPARTMCNT OF TRANSPORTATION • . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JUNE 12, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION 'HAKE BOEING MODEL NO. 727-31 TYPE (Airlakoc. Radio, Helicopter, ad) AIRPLANE NAME OF APPLICANT JET AVIATION • LIST OF DATA IDENTIFICATION TITLE. A.T.E. INC. STRUCTURAL REPORT No. ATE6I 12001 BOEING 727-31 S/N 20115, AERO-M SATCOM ANTENNA INSTL., UPPER B.S. 360-390; GPS ANTENNA INSTL., UPPER B.S. 312-328; AIRCELL AGT.01 ANTENNA INSTL., LOWER B.S. 400-420 DAMAGE TOLERANCE ANALYSIS; SR 1-31, REV. (IR) • NOTE; REQUIREDINSPECT1ONS AT'T'ACHED 20115 THESE DATA APPLY ONLY TO BOELNG 727-31 S/N . PURPOSE OF DATA TO APPROVE DATA FOR DAMAGE TOLERANCE ANALYSIS, B-727-3 I S/N 20115 1 APPLICABLE REQUIREMENTS (List spainc cations) . - FAR 25.571 (STRUCTURAL ASPECTS ONLY) • . CERTIFICATION — Under of appointment under Part 183 have authority vested by direction of the Administrator and in accordance with conditions and of the Federal Aviation Regulations, data listed above and on attached sheets numbered been examined in accordance with established procedures and found to comply with applicable Recommend approval of these data Approve these data limitations • . I of l requirements of the Federal Aviation Regulations. I (Ye) Therefore i SIGNATURE(S) OF DESIGNATED ENGINEERING DESIGNATION NUMBER(S) CLASSIFICATIONS) DERT-510333-CE STRUCTURAL • • • • . FAA Form 8110-3 (I t.70) SUPERSEDES PREVIOUS EDMON cro 901.613 EFTA00277716 • •• it EFTA00277717 MAJOR REPAIR AND ALTERATION O us Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Onl Office Identification 5 0— F 5 Do — 17 INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructs s and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to ex red $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 . Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type . Manufacturer ‘,. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LIMITED EYKR782D 1,3. 1,2,3. ENG. Foreign Certified Mechanic x Certificated Repair Station Manufacturer A/F & D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 7/2/01 Signature of Authorized individual John K. Urso. Inspector. laJ-- -- 7. Approval for Return to Service Pursuant Administrator BY to the authority given of the Federal Aviation persons specified below, the unit Administration and is identified in item 4 was _p_ected in the manner prescribed by the U REJECTED APPROVED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance FAA Form 337 (12-88) EFTA00277718 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, S/N 20115, N908JE, W/O 16236. ACCOMPLISHED AN UP-GRADE TO THE EXISTING HONEYWELL WEATHER RADAR SYSTEM FROM PRIMUS 870 TO PRIMUS 880. REMOVED THEl 1 & 2 WC-870 CONTROLLERS P/N 7008471-803 AND INSTALLED WC-880 CONTROLLERS P/N 7008471-405 (TSO C63c), REMOVED THE WU-870 ANTENNA & RECEIVER / TRANSMITTER UNIT P/N 7012640-902 AND INSTALLED NEW WU- 880 ANTENNA & RECEIVER / TRANSMITTER UNIT P/N 7021450-801 (TSO C63c). INSTALLED A HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM CONSISTING OF AN LP-860 PROCESSOR P/N 7011822-904 (TSO C110) AND AN AT-855 ANTENNA PIN 7014062-901 (TSO C110). THE LIGHTNING SENSOR SYSTEM INTERFACES WITH THE PRIMUS 880 RADAR SYSTEM THRU THE # I & 2 WC-880 CONTROLLERS. RELOCATED EXISTING SECURITY SYSTEM ANTENNA P/N DMC57-1 TO THE TOP OF THE RADAR ANTENNA & RECEIVER / TRANSMITTER UNIT. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING: • B727-16236-260, REV. IR, DATED 5/29/01, SHEETS 1& 2, TITLED - WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) REFERENCE FAA FORM 8110-3 DATED 6/7/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. • B727-16236-261, REV. IR, DATED 4/10/01, SHEETS ITHRU 3, TITLED - HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM REFERENCE FAA FORM 8110-3 DATEDS/29/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-1261, REV. A, DATED 5/30/01, SHEETS 1 THRU 7, TITLED - AT-855/RTA-880 ANTENNA INSTALLATIONS REFERENCE F.A.A. FORM 8110-3, DATED 6/1/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. • B727-I6236-1262, REV. IR, DATED 5/21/01, SHEETS 1 & 2, TITLED - LSZ-860 LIGHTNING SENSOR EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3, DATEDS/28/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER HONEYWELL PRIMUS 880 RADAR SYSTEM INSTALLATION MANUAL NO. 34-42-12, REV 3, DATED 2/15/00 AND THE HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM INSTALLATION MANUAL NO. 34-41-50, REV 5, DATED 2/15/01 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO. B727-16236-080, REV IR, DATED 6/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELFCTRICAL LOAD ANALYSIS UPDATE REPORT B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH 43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-IB, CHAPTER 4, SECTIONS I, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.13-1B, CHAPTER 7, SECTIONS 1- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-1B, CHAPTER II, SECTION 4. ELECTRICAIJELECIRONIC WIRING WAS SELECTED AND INSTALLED IAW AC43.13-IB, CHAPTER 11, SECTIONS 5-8, 13, 15, 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURER'S INSTRUCTIONS AND AC43.13-2A, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC43.13-IB, CHAPTER 10, SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. MAINTENANCE FOR CONTINUED AIRWORTHINESS IS CONTAINED IN HONEYWELL PRIMUS 880 RADAR SYSTEM INSTALLATION MANUAL NO. 34-42-12, REV 3, DATED 2/15/00 AND THE HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM INSTALLATION MANUAL NO. 34-41-50, REV 5, DATED 2/15/01. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION K Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277719 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 06/07/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-260, Initial Release, dated 05/29/01 , k... WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) • PURPOSE OF DATA •In support of major alteration to Boeing 727-31, serial number 20115, registration•number N980JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) . FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 25.1316 (b) CERTIFICATION — Under authority vested by direction data Fisted above and on attached sheets numbered NONE have of the Administrator and in accordance with conditions and limitations of appointment ander Part 183 orate Federal Aviation Regulations, been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Regulations. El Recommend approval of I (I.Ve) Therefore X Approve these data (Systems SIGNATU F DESIGN NG INE INC REPRESENTATIVE(S) DESIGNATION NUMBERS) CLASSIF/CAT/ON(S) DERT-510087-NM Systems & Equipment Nor an. J. ran . FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME SC-727-RDRDOC EFTA00277720 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 06/07/2001 r AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE , Boeing • MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION . TITLE B727-16236-260, Initial Release, dated 05/29/01 i.. WEATHER RADAR SYSTEM UPGRADE (PRIMUS 880) PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N980JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) . FAR 25.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 25.1316 (b) CERTIFICATION - Under authority vested by direction data listed above and on attached sheets numbered NONE have of the Administrator and in accordance with conditions and Etnitatimis of appointment under Part I &I of the Federal Aviation Regulations, been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Regulations. K Recommend approval of I (We) Therefore X Approve these data (Systems SIGNATU F DESIGN GINE G REPRESENTATTVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) • DERT-510087-NM Systems & Equipment Nor an J. ran FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901-613 FILENAME: SC-727-REIRDOC EFTA00277722 May-29-01 01:58P N J Curran 41, ••=mowm..1 • :352 2L1-:3 1O11 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, ctc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA IDENTIFICATION TITLE B727-16236-261, Initial Release, dated 04/10/01 - . HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM • PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 26.1357 (a)(c) FAR 25.869 (a)(4) FAR 25.1431 (a)(b)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1529 FAR 25.1309 (a)(b)(g) _ FAR 25.1351 (a) CERTIFICATION - trader authority vested by direction dm) ram' aticre mid *a ttutitrd Skeels sumbered NONE of the Administratsr sad is accordance with cooditivos and limitations of appointment under Parr ILI artist Federal Avisiien Regulations, tune Ices east:sized is setordaset with esiablished procedures sad found to comply with applicable rectoiroueom .f the Fed eTht Avialie • these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Rttoilatlikt- O Recommend approval of I I (We)Therefore 0 Approve these data (Systems SIGNATU FD EN ERING RETRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION'S) —•TED 1 .1 &17- ---..- DERT-510087-NM Systems & Equipment Nor an . urran FAA Form 8110-3 (11.70) SUPERSEDES PREVIOUS EDMON GPO 901-613 FELENAME: SC-727-LTOSNSRDOC EFTA00277724 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 1, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE MODEL NO. TYPE (Airplane. Radio, Helicopter, etc.) NAME OF APPLICANT Boeing 727-31 Airplane Jet Aviation Associates- WPB - LIST OF DATA IDENTIFICATION TIRE B727-16236-1261 AT-855/RTA-880 Antenna Installations, Sht 1-7, Rev A B727-16236-1410 Dual FMS WI RTU Equipment Installations, Sht 1-6, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA . authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.601 25.603 25.605(a) 25.609 25.611 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered 0 have been examined in accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data. I Therefore ' Approve these data. , .. SIGNATURE(S) OF. DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) ,,.:, : CLASSIFICATION(S) •••..'$1,- David E. HaralOn P,-.2(e. ii,,,,z.-I-,' DERT-810028-NE --.7=7 - Structural -.-.4:-. -4, ' ,;:,s:4, . 447 • • :1•,: k• •44,-,44 . • - -• ,c-,"4•.-- • -.. FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01202.doc EFTA00277726 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE May 28, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1262 B727-16236-1342 LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2, Rev IR Aero-M SATCOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561(b)(c) 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recommend approval of these data. I 0,tX Therefore Approve these data. and limitations of appointment 0 have been examined Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) David E. Haralson Pc- t.., re /iced-46-- DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION L ER01205.doc EFTA00277728 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE May 28, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1262 B727-16236-1342 ._ • LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2, Rev IR Aero-M SATOOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561(b)(c) 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation in accordance with established procedures I Therefore by direction of the Administrator and in accordance with conditions Regulations, data listed above and on attached sheets numbered and found to comply with applicable requirements of the Federal Recommend approval of these data. Approve these data. and limitations of appointment 0 have been examined Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) David E. Haralson P.,- e. // ,-1..,.--- DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01205.doc EFTA00277730 00 4 MAJOR REPAIR AND ALTERATION US Department of Transportation (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification 50- fsbo- 17 i INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instruc ' ns and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 . Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 , . 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type Manufacturer \ s. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO EYKR782D 1,3. 1,2,3. ENG, Foreign Certified Mechanic X Certificated Repair Station Manufacturer AJF & _LIMITED D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 7/2/01 • Signature of Authorized Individual John K. Urso. Inspector. 1e---c' 7. Approval for Return to Service Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 w inspected in the manner prescribed by the C.4 APPROVED ■ REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance. FAA Form 337 (12-88) EFTA00277732 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets, identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, S/N 20115, N908.1E, W/O 16236. ACCOMPLISHED A TCAS CHANGE 7 UPGRADE TO THE EXISTING HONEYWELL TCAS II SYSTEM PREVIOUSLY INSTALi.ED UNDER PAGE AVJET CORPORATION STC SA3094SO DATED 8/24/93. REFERENCE F.A.A. FORM 337 DATED 8/25/93. THE TCAS PROCESSOR P/N 4066010-904 WAS MODIFIED TO P/N 4066010-910 (CUSTOMERS UPGRADED UNIT) IN ACCORDANCE WITH TIMCO MASTER DRAWING LIST 01T012L001, REV IR, DATED 5/21/01. REFERENCE F.A.A. FORM 8110-3 DATED 5/21/01 BY SYSTEMS AND EQUIPMENT DER NO.DERT-510239-CE. THE TCAS II CHANGE 7 PROCESSOR WAS INSTALLED AND TESTED IN ACCORDANCE WITH TIMCO ENGINEERING ORDER DOCUMENT 01T012E006, REV IR, DATED 5/21/01 WITH NO DISCREPANCIES. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE AIRCRAFT EQUIPMENT LIST WAS AMENDED AND ENTERED IN THE AIRCRAFT RECORDS. AIRWORTHINESS DIRECTIVE 94-01-04 AMENDMENT 39-8786 IS N/A TO THIS INSTALLATION BY PROCESSOR P/N. THERE IS NO CHANGE TO THE AIRCRAFT WEIGHT AND BALANCE. THERE IS NO CHANGE TO THE AIRCRAFTS MAINTENANCE FOR CONTINUED AIRWORTHINESS REQUIREMENTS DUE TO THIS INSTALLATION. THE REQUIRED F.A.A. APPROVED HONEYWELL INC, TCAS II FLIGHT MANUAL SUPPLEMENT DOCUMENT TCAS-APPS-0294, REV A, DATED 3/21/00 HAS BEEN INSERTED INTO THE AIRCRAFT FLIGHT MANUAL. END K Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277733 communications Aviation Communications & Surveillance Systems 21111 N. 19[11 Avenue Phoenix, AZ 85027-2708 602-436-7070 Fax: 602-436-6899 May 16, 2001 TIMCO 623 Radar Road Greensboro, NC 274 Attn.: Mr. Gregg Stutes Re: Letter of Authorization to use technical data Dear Mr. Stutes, This letter is to authorize TIMCO ("Recipient") to use the following technical data owned by L-3 Communications Corporation — Aviation Communications & Surveillance Systems (L-3) for the limited purpose indicated here below. The technical data subject to this Letter of Authorization (`date) is the L-3 developed data used to apply for the following FAA certifications: Supplemental Type Certificate STC SA4S34NM, as defined by ML4070349, for B727 aircraft. L-3 Authorization to use Data is limited to the following B727 aircraft tail number, namely: • B727 SIN 20115 L-3 Authorization to use Data is granted hereby for the sole purpose to provide the Recipient with technical information for its internal use and engineering review purposes. The Recipient recognizes L-3' s proprietary rights in Data and will limit its disclosure to a need-to-know basis for its employees. The Recipient will not use Data for any other purposes than the internal use and engineering review purpose established for this Authorization. The Recipient will not sell, license, rent, market, transfer, assign, distribute, or otherwise disclose to any third party, exploit or permit any other use of Data. L-3 does not provide any warranty whatsoever on Data, whether express, or implied, or implied by law, including but not limited to merchantability and fitness for any particular purpose_ EFTA00277734 In no event shall L-3 be liable for. • Any direct, incidental, indirect, special or consequential damages including but not limited to loss of use, revenue or profit, even if L-3 has been advised, knew or should have known of the possibility of such damages; or • Damages caused by the Recipient's failure to perform its obligations and responsibilities; or • Claims, demands or aeons against the Recipient by any other party. The term of this Authorization is one (1) calendar year from its date. If during such term L-3 believes that its proprietary rights in Data are being infringed or injured or otherwise are at risk, L-3 reserves the right to terminate Authorization hereunder and, upon notice to Recipient, request the Recipient to discontinue any further use of Data. Upon termination of Authorization hereunder, the Recipient will either destroy or return Data in its possession and notify L-3 that no further use of Data will take place. For any communication concerning this Authorization, please contact F.W. (Bill) Lynch, Certification Engineer: Phone: (602) 436.2421 Fax: (602) 436.6899 E-mail- bill.lynch@L-3com.com PIease, countersign this Letter of Authorization and return it to us as follows: original by mail (with the original signature of your authorized representative); a copy by fax to the undersigned. Thank you for your interest. S E.W. (Bill) L ch Agent for L-3 Communications, ACSS EFTA00277736 United gRatts graica Bepartment of Zransportation—fidtral aviation administration supplemental Zppe Certificate Y .2€21,..e..ezpitt-eur4 43.4ezed-io Page Avjet Corporation 9809 Tradeport Drive Orlando, Florida 32827 A3WE Boeing 727-100 Series 25 Federal Aviation gLi' di'n'94-;& -- ---611 '.6CAanf e': Installation of Provisions only for a Honeywell TCZ-910 TCAS II System in accordance with Page Avjet Master Drawing List MDL-91- 41, Initial Release, dated November 19, 1991, or later FAA approved revisions. /'7m-tat This approval should not be extended to other airplanes of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. zdte7a- ca, irv.e# / Az.n/e/Azzr- rre 44.eziyi.ende44.cw,LW, c14-7724nale z.' -cfa zik,wea &,e.11,214:14,/iy, //it • Cat in e3 ik t9 ‘41:Araidirtiz&im,ilezirte:nc.:Ilran'er-n, October 21, 1991 January 15, 1992 !Lk peZtJa,i: iinei4w./i•r hn Tigue (Signature nager, Atlanta Aircraft Certification Office (Title) Any alteration of this certificate is punishable by a.fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. This certificate may be transferred in accordance with F.-1R 21.47. FAA folua 8110-2 (10-68) EFTA00277738 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE -67'24/0/ AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-100 TYPE (AIRPLANE, RADIO, HEUCOPTER, ETC.) Airplane NAME OF APPLICANT TIMCO LIST OF DATA IDENTIFICATION TITLE TIMCO Master Data List, 01T012L001 Rev IR Dated 5/21/01 - Honeywell TCAS II Change 7 Software Upgrade for a Boeing 727-100 END OF DATA - - - . • PURPOSE OF DATA To document and approve the installation of a TCAS Change 7 in a Boeing 727-100 aircraft. STC SA4834NM is the approval basis for this installation. APPLICABLE REQUIREMENTS (Listspedricsections) FAR 25.1301 (a), (c) v - • CERTIFICATION - Under appointment under Part 183 of have authority vested by direction of the Administrator and in accordance with conditions the Federal Aviation Regulations, data listed above and on attached sheets numbered been examined in accordance with established procedures and found to Regulations approval of these data these data and limitations of comply with applicable requirements of the Federal Aviation 1 ) Therefore 0 Recommend ... Approve SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) • CLASSIFICATION(S) Robert McClellan 14 DERT-510239CE System & Equipment FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION • GPO 901-613 EFTA00277740 TIMCO ENGINEERED SYSTEMS, I.. u, "WO N 5,40 CommY A TITLE: HONEYWELL STC / FAA PROJECT NO.: ENGINEER: P. FERGUS MASTER DATA LIST • TCAS II CHANGE 7 SOFTWARE UPGRADE SA4834NM / 650259 AIRCRAFT TYPE: FORM NO.: EN•0003 DATE: 01/01/00 MDL NO. 01T012L001 REV/DATE: IR / 5/21/01 BOEING 727-100 APPROVAL: ROBERT MCCLELLAN SHEET 1 OF 1 DOCUMENT NUMBER REVISION LTR DATE TITLE SHT 01T012C002 IR 5/21/01 HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE FOR A BOEING 727-100 ISSUED vim 2 2 zttl wool collinot. 1 Th'sda's'Pr'Perv'''PrglIe0V: rTritTa:,','°iTtezierrdsarazix=sovr',d,==sur,Veotr=unThsc=roarnTdV,===.1Ler,:mgte=1,72;ebs=t7V-I"E"'"er""s`e"'In'and Copyright (C) 2000 TIMCO Engineered Systems, Inc. 011.012L0015 Stock No.: 091100108 EFTA00277742 TIMCO ENGINEERED SYSTEMS. !sc. CONFIGURATION DOCUMENT AN AWVI $.13 CO/MWY A TITLE: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE FOR A BOEING 727-100 ENGINEER: P. Fergus APPROVAL: Robert McClellan Form No.: EN-0008 Date: 01/01/00 . CFG NO, 01T012C002 REV/DATE: IR/ 5121/01 SHEET 1 OF 1 I. CONFIGURATION DATA A. APPLICABLE MDL: HONEYWELL TCAS II CHANGE 7 SOFTWARE UPGRADE # 01T012L001 B. EFFECTIVITY ISSUED 2 2 1. BOEING 727-100 SERIAL NO. 20115 MAY 20 C. DESCRIPTION CION.MEta CONTROL 1. THIS INSTALLATION WILL CONSIST OF USING STC SA4834NM AS THE APPROVAL BASIS TO PERFORM THE TCAS CHANGE 7 MODIFICATION TO THE TCAS COMPUTER UNIT, D. DEVIATION FROM PREVIOUSLY APPROVED DATA , 1. NONE Items marked with an asterisk (*) are for manufacturing and certification and will not be supplied. If required, the documents will be sent directly to the customer's certification authority only after TIMCO receives assurance that their confidentiality will be protected. DOCUMENT REVISION NUMBER LTR DATE TITLE SHT 01T012E006 IR 5/21/01 Installation of a Honeywell TCAS II CU with Change 7 in a Boeing 727-100 6 01T012R007 IR 5/21/01 Description and Substantiation of a TCAS II Change 7 Installation 2 'This data Is the properly of. and proprietary to, TIMCO Engineered Systems, Inc, and Is restricted for use by designated persons, firms or corporations with whom contracts have been entered Into. User agrees to Indemnify TIMCO Engineered Systems, Inc. and to hold It hornless against any claim arising by reason of the possession or use thereof. lis unauthorized use and duplication Is prohibited, and it Is protected under an unpublished copyright' Copyright (C) 2000 TIMCO Engineered Systems. Inc. •1 1:1017012 Jet AviattonN0IT012C002S.doc Stock No.: 091100403 EFTA00277744 1 F • e EFTA00277745 TIMCO ENGINEERED SYSTEMS. Pro. AmAwn. SALES Cosawm A ENGINEERING ORDER Form No.: EN•0002 Date: 01/01/00 E.O. TITLE: Installation of a Honeywell TCAS II CU with Change 7 in a Boeing 727-100 E.O. NO.: 01T012E006 AIRCRAFT: Boeing 727-100 REV: IR DATE: 5/21/01 ISSUED MAY 2 2 21101 DOCUMENT. CONTROL. INITIAL RELEASE REVIEWS R Fergus PkEPARE , -,',:- .,,:,.-''.:,! David Thornton tilEtKEtit ii-A:: ::T-f4aV :„ - •• .. :•-,',,,,.., Richard Cunningham ,QA--13gyIE -.. .-:-:,, -----=: s 41;-,,EE,_.;.•-,--,;: - -? Robert McClellan ',_, , Rtiv-E- 1 - : -:•.; -,. ..x...4-,N.-5.-s3,----A,_,-,- --,,,,. ,--44-*: ... . ..,, _........ .. •. ...,...... :•••••• •,-,•:-:.,,.„•,,,i--:•••-,4•:•.-!..--,-_,-,-,...t,„ TIMCO ENGINEERED SYSTEMS, INC. 623 Radar Road Greensboro, North Carolina 27410 Telephone: (336) 668-4410 This data is the property of, and proprietary to. TIMCO Engineered Systems. Inc. and is restricted for use by designated persons, firms or corporations viith whom contracts have been entered Into. User agrees to indemnify TIMCO Engineered Systems, Inc. and to hold it harmless against arty claim arising by reason of the possession or use thereof. Its unauthorized use and duplication is prohibited, and it is protected under art unpublished copyright,' Copyright (C) 2000 TIMCO Engineered Systems. Inc. 01T012E0065 Stock No.: 091100106 EFTA00277746 Honeywell Inc . 21111 North 19th Ave. Phoenix, .AZ 85027 Spec. No. TCAS -APPS- 0294 AFM SUPPLEMENT General TCAS/ACAS Applications FAA APPROVED WHEN EQUIPPED WITH HONEYWELL TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM ( TCAS II ) This supplement must be attached to the FAA Approved Airplane Flight Manual for aircraft that have been modified by installation of the Honeywell Traffic Alert and Collision Avoidance System (TCAS II) in accordance with a Honeywell STC (see SECTION I). The information contained in this document supplements and supersedes the basic manual only in those areas listed. For limitations, procedures, and performance information not contained in this supplement, consult the basic Airplane Flight Manual. FAA APPROVED Manager, Flight Test Branch, ANM-160L Federal Aviation Administration Los Angeles Aircraft Certification Office Tranport Airplane Directorate Date EFTA00277748 r 4.• • EFTA00277749 I 0 MAJOR REPAIR AND ALTERATION US Departmwt of Tran_sportatIon (Airframe, Powerplant, Propeller, or Appliance) Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use O ly Office Identification So- r-sDo- f 7 cik)' INSTRUCTIONS: Print or type all entries. See FAR 43.9 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instreitions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to keed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark U.S.A. N908JE 2. Owner Name (As shown on registration certificate) JEGE INC. Address (As shown on registration certificate) 103 FOULK RD. STE 202 WILMINGTON DE. 19803-3742 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT PROPELLER APPLIANCE Type • • Manufacturer . s. 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. JET AVIATION ASSOCIATES LTD. 1515 PERIMETER RD. WEST PALM BEACH. FL. 33406 U.S. Certified Mechanic CRS AIRFRAME RADIO LTMIT11I2 EYKR782D 1,3. 1,2,3. ENG, Foreign Certified Mechanic ---, x Certificated Repair Station Manufacturer AIF & D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 7/2/01 . Signature of Authorized lndi idual John K. Urso. Inspector. L,,, /C. 7. Approval for Return to Servl Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 w s inspected in the manner prescribed by the CI APPROVED III REJECTED FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Airworthiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EYKR782D Signature of Authorized Individual , Ronald K. Bystrom. Manager Quality Assuranc / FAA Form 337 (12-S8) EFTA00277750 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. • 8. Description of Work Accomplished (if more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplished.) BOEING 727-31, S/N 20115, N908JE, W/O 16236. INSTALLED A UNIVERSAL AVIONICS TT-3000 SERIES AREO-M SATCOM SYSTEM PER UNIVERSAL AVIONICS AIRBORNE SATELLITE TELECOMMUNICATIONS SYSTEM INSTALLATION MANUAL NO. 23-15-02 DATED 3/7/01. SYSTEM CONSISTS OF 2 EA HANDSETS, 1 EA ANTENNA, 1 EA HIGH POWER / LOW NOISE AMP AND THE SATELLITE DATA UNIT. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING: • B727-13236-340, REV. IR, DATED 4/30/01, SHEETS 1 THRU 3, 'I I1LED -1T-3000 AERO-M AIRBORNE SATELLITE TELECOMMUNICATIONS SYSTEM. REFERENCE FAA FORM 8110-3 DATED 5/29/01, BY SYSTEMS & EQUIPMENT D.E.R. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-1340, REV. A, DATED 5/29/01, SHEETS 1 THRU 5, TITLED - AERO-M SATCOM ANTENNA INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 6/18/01, BY STRUCTURAL D.E.R. NO. DERT-510024-CE. • B727-16236-1342, REV. IR, DATED 5/2I/01, SHEETS 1 THRU 7, TITLED - AERO-M SATCOM EQUIPMENT INSTALLATION REFERENCE F.A.A. FORM 8110-3, DATED 5/28/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE. SYSTEM TESTED PER UNIVERSAL AVIONICS INSTALLATION MANUAL FOR TT-3000 SERIES AERO-M, DOCUMENT 23-15-02, DATED 3/7/01 WITH NO DEFECTS NOTED. NOTE: UNIVERSAL AVIONICS SERVICE BULLETIN NUMBER 10101.00-23-2669, BLOCKING OF BREATHING HOJ RS IN SATCOM ANTENNA P/N 10101-00, DATED 7/25/00, WAS INCORPORATED AT ANTENNA INSTALLATION. THIS HAS NO EH.ECT OF THE STRUCTURAL OR MECHANICAL INSTALLATION OF THE ANTENNA. AN EMI TEST, REPORT NO. B727-16236-080, REV IR, DATED 6/19/01 WAS CONDUCTED AND THE INSTAII.FD EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.13-2A, CHAPTER 1, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT B727-16236-041, REV IR, SHEETS 1 THRU 21, DATED 06/11/401 WAS COMPLETED IN ACCORDANCE WITH 43.13-1B, CHAPTER 11, SECTION 3, PARAGRAPH 11-37. AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC 43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4, CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED THE INSTALLATION CONFORM TO AC 43.13-1B, CHAPTER 5, SECTIONS 1 AND 2, CHAPTER 7, SECTIONS 1, 2,4 AND 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURE OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC 43.13-1B, CHAPTER 11, SECTION 4. ELECTRICAL/ELECTRONIC WIRING WAS SELECTED AND INSTALLED IAW AC 43.13-1B, CHAPTER 11, SECTIONS 5-8, 13, 15, 17- 19 AND AC 43.13-2A CHAPTER 2, PARAGRAPHS 21, 22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC 43.13-1B, CHAPTER 11, SECTIONS 9-12. WIRE MARKING COMPLIES WITH SECTION 16. ELEC1RONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURES INSTRUCTIONS AND AC 43.13-2B, CHAPTER 2, PARAGRAPHS 21 THROUGH 26 AND CHAPTER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS MODIFICATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS IAW AC 43.13-1B, CHAFFER 10, SECTION 2 AND AC 43.13-2A, CHAF1ER 1 PARAGRAPH 9. PER THE AERO-M SATCOM INSTALLATION MANUAL ALL COMPONENTS ARE CONSIDERED LINE REPLACEABLE UNITS AND DO NOT Al.PECT THE MANUFACTURERS INSTRUCTIONS FOR CONTINUING AIRWORTHINESS. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATE6112001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333-CE. THERE ARE NO COCKPIT PROCEDURAL CHANGES OR FLIGHT MANUAL SUPPLEMENTS REQUIRED FOR THIS INSTALLATION. END K Additional Sheets Are Attached * U.S. G.P.O 1990-761-753 EFTA00277751 May-29-01 01:58P N 3 Curran 352 243 1011 P _ 02 c DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 05/29/2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc) Airplane NAME OF APPLICANT Jet Aviation Associates West Palm Beach, FL LIST OF DATA • IDENTIFICATION TITLE B727-16236-340, Initial Release, dated 04/30/01 - • TT-3000 SERIES AERO-M AIRBORNE SATELLITE TELECOMMUNICATIONS SYSTEM PURPOSE OF DATA In support of major alteration to Boeing 727-31, serial number 20115, registration number N908JE. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.581 (a)(b)(1) FAR 25.1351 (a) FAR 25.869 (a)(4) FAR 25.1357 (a)(c) FAR 25.1301 (a)(b)(c)(d) FAR 25.1431 (a)(b)(c) FAR 25.1309 (a)(b)(g) FAR 25.1529 FAR 25.1316 (b) CERTIFICATION - Vetter authority vested by direction data ;wed above aid on attached slims numbered NONE of theAdmInblrator and in accordance with conditions and reasitationa of appointment nodes- Part 113 or the Federal Aviatina Revalatiosts. hare been examined in accordance with established procedures and found to coutply with applicable nrelairensenta of the Federal Aviation these data & Equipment Aspects, Design Approval Only, Does Not Constitute Installation Approval) Rscalm:ans. 0 Recommend approval of I (We) Therefore El Approve these data (Systems SIGNATUR FD NA D EN ' ERING REPRESENTAT1VE(S) DESIGNATION NUNIBERIS) CLASSIF1CATIONIS) r Zezee---_ DERT-510087-NM Systems & Equipment No an Jurran oral 8110.3 (11-70) SUPERSEDES PREVIOUS EDITION GPO 901.613 FILENAME: SC-727-SATCOMDOC EFTA00277752 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 18, 2001 _ AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL B727-31 TYPE (Airplane, Radio. Hs! copra, etc) Airplane NAME OF APPLICANT Jet Aviation LIST OF DATA IDIENIIFICA1 ION III LE Jet Aviation Engineering Drawing No. B727-16236-1340, Dtd. 5/29/2001, Rev. A END END Aero-M Satcom Antenna Installation Boeing 727-31 / S/N: 20115 / N908JE END END END END END END END END Note: The certification evaluation of structure. Structural Repairs on Notes: basis of this aircraft includes FAR 25.571 Damage - tolerance and fatigue Per Advisory Circular 25.1529-1 Instructions for Continued Airworthiness of Transport Category Airplanes, the damage tolerance and fatigue evaluation of the structure must be performed before 6/18/2002. aspects only of the above listed data are approved is valid for the aircraft model and serial number is based on structural analysis on file at DER Services office in Ft. Lauderdale, FL. No. B727-31 Serial No. 20115 • - I) The structural herein. 2) This approval listed below 3) This approval corporate Model PURPOSE Approve data for antenna installation (Structures Only) OF DATA APPLICABLE REQUIRMENTS (LIST SPEC.' FIC SECTIONS) 25.301, 25.303, 25.305, 25.307, 25.601, 25.603, 25.605, 25.609, 25.613 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with condition appointment under Part 183 of the Federal.Aviation Regulations, data listed above and on attached sheets numbered been examined In accordance with established procedures and found to comply with applicable requirements of Aviation Regulations. ri Recommend approval of these data I ) Therefore 1,;i1 Approve these data and liml tions of O have the Fe eral SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTIVE(S)DESIGNATION NUMBER(S) CLASSIFICATION(S) Robert J. Belgau .„QA)15 e........................ DERT-510024-CE Structures FAA FORM 81I0-3 (11-70) SUPERSEDES PREVIOUS EDITION DER SERVICES PROJECT NO. 2001-082 EFTA00277754 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE May 28, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) Airplane NAME OF APPLICANT Jet Aviation Associates- WPB LIST OF DATA IDENTIFICATION TITLE B727-16236-1262 B727-16236-1342 LSZ-860 Lighting Sensor Equipment Installation, Sht 1-2, Rev IR Aero-M SATCOM Equipment Installation, Sht 1-7, Rev IR Note: 1. This approval is for structural aspects only. 2. This approval is based on drawing review and inspection. 3. After the alteration, the aircraft must be returned to service by FAA authorized personnel. PURPOSE OF DATA To approve structural aspects of a major alteration to Boeing 727-31, S/N: 20115 APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301 25.303 25.305(a) 25.307(a) 25.321(a) 25.561(b)(c) 25.601 25.603 25.605(a) 25.609 25.611 25.613 25.789 CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered in accordance with established procedures and found to comply with applicable requirements of the Federal Recommend approval of these data. I Therefore Approve these data. and limitations of appointment 0 have been examined Aviation Regulations. SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) David E. Haralson it7,-„,e. 14.....r...._ DERT-810028-NE Structural FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01205.doc EFTA00277756 DEPARTMENT OF TRANSPORTATION • FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JUNE 12, 2001 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 • • - TYPE (A NAME captcr, iroule, it s dio. Heti etc.) AIRPLANE OF APPLICANT JET AVIATION LIST OF DATA WENTIFICAllON T171.-E A.T.E. INC. STRUCTURAL REPORT No. ATE6112001 BOEING 727-31 SIN 20115, AERO-M SATCOM ANTENNA INSTL., UPPER B.S. 360-390; GPS ANTENNA INSTL., UPPER B.S. 312-328; AIRCELL AGT.01 ANTENNA INSTL., LOWER B.S. 400-420 DAMAGE TOLERANCE ANALYSIS; SH. 1-31, REV. (IR) • - - NOTE: REQUIRED INSPECTIONS ATTAQBED . 20115 . THESE DATA APPLY ONLY TO BOERNIG 727-31 S/N . . . PURPOSE OF DATA . . TO APPROVE -DATA FOR DAMAGE TOLERANCE ANALYSIS, B-727-3I S/N 20115 , APPLICABLE REQUIREMENTS (Lis specific sectioas) . - . FAR 25.571 (STRUCTURAL, ASPECTS ONLY) ' . • . CERTIFICATION - Under of appointment under Part 183 have authority vested by direction of the Administrator and in accordance with conditions and of the Federal Aviation Regulations, data listed above and on attached sheets numbered been examined in accordance with established procedures and found to comply with applicable Recommend approval of these data Approve these data limitations • . 1 of 1 requirements ' of the Federal Aviation Regulations. I (Ye) Therefore ,g, SIGNATURES) OF DESIGNATED ENGINEERING DESIGNATION NUMBER(S) CLASSIFICATION(S) /' • t . DERT-5 I 0333-CE STRUCTURAL - . • . • _. FAA Form 8110-3 tit :70) SUPERSEDES PREVIOUS EDMON cro 901-613 EFTA00277758 .14 ii. • 4 • • EFTA00277759 UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND REGISTRATION MARKS N908JE 2 MANUFACTURER AND MODEL BOEING 727-31 3 AIRCRAFT SERIAL NUMBER 20115 4 CATEGORY TRANSPORT 5 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and certifies that, as of the date of issuance, the aircraft to which issued has been inspected and found to conform to the type certificate therefor, to be in condition for safe operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provide by Annex 8 to the Convention of International Civil Aviation, except as noted herein. Exceptions: NONE 6 TERMS AND CONDITIONS Unless sooner surrendered, suspended, airworthiness certificate is effective as lo g as accordance with Parts 21, 43, and 91 of e F United States. DATE OF ISSUANCE R may 17 2001 ed, or a termination date is otherwise established by the Administrator, this e maintenance, prey: ative maintenance, and alterations are performed in • e I Aviation Regul o , as appropriate, and the aircraft is registered in the DESIGNATION NUMBER SO17 Any alteration. reproduction, or misuse of this flute may be punishable by a fine not exceeding 31,000, or imprisonment not exceeding 3 years or both. THIS CERTIFICATE MUST DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) AFS Electronic Forms System -JetForm FormFlow -1211998 EFTA00277760 I UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE I 1 NATIONALITY AND REGISTRATION MARKS N505LS . MANUFACTURER AND MODEL IP. BOEING 727-31 3 AIRCRAFT SERIAL NUMBER 20115 4 CATEGORY TRANSPORT 5. AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and certifies that, as of the date of issuance, the aircraft to which issued has been inspected and found to conform to the type certificate therefor. to be in condition for safe operation. and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation, except as noted herein, Exception 4- NONE 6. TERMS AND CONDITIONS Unless sooner surrendered. suspended, revoked, or a termination date is otherwise established by the Administrator, this airworthiness certificate ts effective as long as the maintenance, preventative maintenance, and alterations are performed in accordance with Parts 21. 43. and91 of the Federal Aviation Regulations. as appropriate, and the aircraft is registered in the United States. DATE OF ISSUANCE R 07-23-90 JAY Any alteration. reproduction, or misuse of this certi years. or both. THIS CERTIFICATE MUST AVIATION REGULATIONS. DESIGNATION NUMBER GLO7 to ma punishable by a fine not exceeding $1.000. or imprisonment not exceeding 3 DIS ED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL FAA Form 8100-2 (8-62) *U.S.G.RO.: 1994-568-762 EFTA00277762 I la r 2, a at SM S '► EFTA00277763 e l MAJOR REPAIR AND ALTERATION U.S. Department of (Airframe, Powerplant, Propeller, or Appliance) Transportation Federal Aviation Adniinistration _ Form Approved O/v1B No. 2120.0020 For FAA Use Only Office Identification - ,zto —./- 9 /0 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B , and AC 43.9-1 (or subsequent revision thereof for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N505LS 2. Owner Name (As shown on registration certificate) NORTHWEST DELAWARE CORP Address (as shown on registration certificate) 1105 N. MARKET ST WILMINGTON DE 19899 3. For FAA Use Only • . 4. Unit Identification . 5. Type Unit Make Model Serial No. . Repair Alteration AIRFRAME - above) — XX (As deieribed in item 1 - - POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B Kind of Agency C. Certificate No. • TIMCO . Lake City Municipal Airport Lake City, FL 32025 U.S. Certificated Mechanic DU4R141M Foreign Certificated Mechanic X Certificated Repair Station Manufacturer ' D. I certify that the repair and/or alteration made to the units identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date August 23, 1999 Signature of Authorized Individual Arthur E. Saylor a' ,4 6?"aft 7. Approval for Return To Sex-vice Pursuant Administrator BY to the authority given persons specified of the Federal Aviation Administration below, the unit identified in item 4 was inspected in the manner prescribed by the REJECTED and is 10 APPROVED • FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station . . Person Approved by Transport Canada Airworthiness Group • Date of Approval or Rejection August 23, 1999 Certificate or Designation No. DU4R141M Signature of Authorized ividual Scott L. Palm FAA Form 337 (12-88) This 337 supersedes 337 dated August 7, 1999 EFTA00277764 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Boeing 727-31 Reg. No. N505LS S/N 20015 August 23, 1999 Page 1 The following major repairs were accomplished: 1. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 56 IAW TIMCO E.O. 99-1190 Rev. I/R dated 12 JUL 99 Approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delmainated skin above #2 engine pylon L/H side at stations 1342.4, 1371.5 and 1387.85 IAW TIMCO E.O. 99-1191 Rev. I/R dated 23 Jul 99 approved per FAA Form 8110-3 by DER D. Joynes DER #DERY-635317-NM dated 21 July 99. 3. 060H1-0027 Repaired cracked and disbonded #2 engine upper skin on aft fairing assembly IAW ROHR Engineering Repair Data Sheet and FAA Form 8110-3 by DER Jeffrey D. Shutrump DER #DERY-605526-NM dated August 3, 1999. SUMMARY 1. All work accomplished IAW TIMCO E.O.'s, ROHR Engineering Repair Data Sheet and FAA Form 8110-3's. 2. Records of all work accomplished is on file at this repair station under work order 060/T-361. end K Additional Sheets Are Attached * U.S. GOVERNMENT PRINTING OFFICE: 1992.169.012/601S7 EFTA00277765 9) MAJOR REPAIR AND ALTERATION U.S. Department of (Airframe, Powerplant, Propeller, or Appliance) Transportation • Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification .---- / ---5 1) —C•C 7X INSTRUCTIONS: Print or type all entries. See FAR 43.9,. FAR 43 Appendix B , and AC 43.9-1 (or subsequent revision thereof for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N505LS 2. Chvner Name (As shown on registration certificate) NORTHWEST DELAWARE CORP Address (as shown on registration certificate) 1105 N. MARKET ST WILMINGTON DE 19899 3. For FAA Use Only • 4. Unit Identification 5. Type' Unit Make Model Serial No. Repair Alteration AIRFRAME above) )O( , (As described in item 1 — POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. TIMCO • Lake City Municipal Airport Lake City, FL 32025 U.S. Certificated Mechanic DU4R141M Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the units identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with requirements of Part 43 of the U.S. Federal Aviation Reguiations and that the information furnished herein is true and correct to the best of my knowledge. Date August 7, 1999 Signature of Authorized Gregory A Christman 4/ i ____- 7. Approval for Return To Service Pursuant Administrator BY to the authority given persons specified of the Federal Aviation Administration below, the unit identified in item 4 was inspected in the aruier prescribed by the El REJECTED and is E3 APPROVED FAA Flt. Standards Inspector Manufacturer . Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Gro Date of Approval or Rejection August 7, 1999 Certificate or Designation No. DU4R141M Signature of Au - ed Individual out L. Palm FAA Form 337 (12-88) EFTA00277766 4 . NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Boeing 727-31 Reg. No. N505LS S/N 20115 August 7, 1999 Page 1 The following major repairs were accomplished: 1. 060N1-0059 Repaired corroded seat track at sta. 662 RBL 45.5 IAW 'HMCO E.O. 99-1190 Rev. UR dated 12 JUL 99 approved per FAA Form 8110-3 by DER Wayne Fink DER #DERT-510117-CE dated July 12, 1999. 2. 060O1-0066 Repaired corroded and delaminated skin above #2 engine pylon L/H side at stations 1342.4, 1371.5 and 1387.85 IAW TIIVICO E.O. 99-1191 Rev. I/R dated 23 Jul 99 approved per FAA form 8110-3 by DER D. Joynes DER #DF.RY-635317-NM dated 21 July 99. 3. 060H1-0027 Repaired cracked and disbonded #2 engine upper skin on aft fairing assembly IAW ROHR Engineering Repair Data Sheetand FAA Form 8110-3 by DER Jefa ey D. Shutrump DER #DERY-605526-NM dated August 3, 1999. SUMMARY 1. All work accomplished TAW 'HMCO E.O.'s , ROHA Engineering Repair Data Sheet and FAA Form 8110-3's. 2. Records of all work accomplished are on file at this repair station under work order 060/T361. end K Additional Sheets Are Attached * U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 EFTA00277767 trul,21 1999, 22:06 PDT MsgNum: CPZ-LRK-99-00014H Page 2 of 2 117/Zr/99 WED 16:06 FAX 9 544 7667 0001 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 1 0 W A I:1 /141 i j 1 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION .__. MAKE Boeing MODEL NO. 727 TYPE (Airplane, Radio, Helicopter. etc.) Airplane NAME OF APPLICANT • Boeing Commercial Airplane Group • LIST OF DATA IDENTIFICATION TITLE . • • • : . . . CPZ-L Mk99-02041;R • Date&•9.1u1•199p- - • - CPZ-1_11. 199-000.061-I • Dated- 12 Jul-1999 . : - : . • CPZ-LRIC--99-0208TR: • -. ' Dated 19 Jul 1'999 • - • :: . _ - . . . ... — , . • Subject Center Engine Support Skin. Panel Corrosion, Delamination . • Requestor: TIMCO (CPZ) for The Limited (LII) Part Number/ Serial Number: 65-17556 Model No.: 727-100 Serial No.: 20115 Basic No.: E2218 Registry No.: NSOOLS Variable No.: E3704 Line No.: 735 • Flight Cycles: 21643 Hours: 31835 . - Service Bulletin /AD: N/A . - - . -., . TIMCO telex with description Of blendout and doubler repairs to corrosion and • -,..i delamination areas at StatiOnSI3713: 1387.85, and 1342.4. - Boeing reply that repairs ar6itiiidniiitiy. tgfaciory with prciviSi0ns. • , — — .. , - . • . •ITMCO telex with-statementthatl4aii: hai been coinpieted fier• disi:iiisition• andreq'tieSi • for 8110-3 form. • • • - • • • ' .. • . - • • • - • - • • .— • • ,.. • : . . • ' . - PURPOSE OF DATA Structural Substantiation of Repair Plan APPLICABLE REQUIREMENTS (List specific section) CAR 4b - - Subpart C: 4b.200 through 4b.202, 4b.270 Subpart D: 46.300 through 4b.304(a), 4b.306(a)&(b) CERTIFICATION - Under of appointment under Part 183 : authority vested by direction of the Administrator and in accordance with.conditions of the Federal Regulations, data listed above and on attached sheets numbered have been examined in accordance with established procedures and found to comply Aviation Regulations. Recommend approval of these data Approve these data and limitations with applicable requirements of the Federil I (We-) Therefore • SIGNATURE(s) OF DESIGNATED ENGIN ING REPRESENTATIVE(s) DESIGNATION NUMBER(s) CLASSIFICATION(s) D. Joy nes ..---1) DERY-635317-NM Structures .....„...—,. FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION Page 1 of 1 EFTA00277768 a I e • EFTA00277769 07/15/99 15:54 FAX 3366651786 • ar•PZEIME.M.FIRM. • TIMCO ENGINEERING -0 LAKE CITY f?)002 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE July 12, 1999 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE ,Boeing MODEL NO. . 727 TYPE (Airplane, Radio, Herrcopler, etc.) Airplane NAME OF APPLICANT TIMCO LIST OF DATA IDENTIFICATION TITLE TIMCO E.O. 99-1190, Rev. I/R. Dated 12 JUL 99 TIMCO REPORT NO. S.A. 99-1190, Rev. l/R. Dated 12 JULY 99 8727; SEAT TRACK: STATION 662, RBL 56 CORROSION BLENDOUT REPAIR. STRESS ANALYSIS; SEAT TRACK CORROSION REPAIR AT STA 663 RBL 54 . END . . NOTES: 1. This approval is for Northwest Delaware aircraft N505LS, S/N 20115 only. PURPOSE OF DATA In support of a Major Repair accomplished on aircraft S/N 20115. This approval is for design and static analysis only and is not installation approval. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.301, 25.305, 25.601, 25.603, 25.605, 25.609 and 25.613. CERTIFICATION - Under authority Part 183 of the Federal Aviation with established procedures and vested by direction of the Administrator Regulations, data listed above and on attached found to comply with applicable requirements approval of those data th ese data and in accordance with conditions and sheets numbered WA have limitations of appointment under been examined In accordance of the Federal Aviation Regulations. IN Recommend I (wile) Therefore O. Approve SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBERS(S) CLASSIFICATION(S) STRUCTURES Wayne Fink DERT-510117-CE 4._------- _....... . __. SUPERSEDES orm - PREVIOUS EDITION ELECTRONIC FORMAT (4-99) EFTA00277770 a In • • EFTA00277771 8- 4: bb YM ;6UF6K 27 FKUUKAM . • •. . . . - " • . • • • • • bl9bH.1.2232;g 2/ 8 — _ U.S. DEPARTMENT OF TRANSPORTATION . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE August 3, 1999 4 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION TYPE (Airplane. Radio, Helicopter, etc.) . Airplane 4 NAME OF APPLICANT Rohr, Inc. MAKE Boeing MODEL NO_ 727 LIST OF DATA IDENTIFICATION _ TITLE EROS CI 036 dated August 3, 1999 41/4-.' • B- Cox Stress Analysis !Doted August 3, 1999 • • ' (Ref. ERDS C1036) Engineering Repair Data Sheet, Definition of discrepancy and repair design for P/N 1/A545300-1 (Aft Skin - Upper Skin Assembly) . Skin Disband VA545300-1 • • . - . PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. APPLICABLE REQUIREMENTS (List specoc sections) (1) FAR 25.301 (1) FAR 25.307(a) (1) FAR 25.605(a) (1) FAR 25.619 (1) FAR 25.303 . (I) FAR 25.601(a) (1) FAR 25.609(a) (1) FAR 25.305(a)(b) (1) FAR 25.603 (1) FAR 25.613(a)-(d) .c • CERTIFICATION — Under authority appointment under Part 183 of the ' NONE have been vested by direction of the Administrator and in accordance with conditions and limitations of Federal Aviation Regulations. data listed above and on attached sheets numbered examined in accordance with established procedures and found to comply with applicable Regulations. 7 Recommend approval of these data EgApprove these data • requirement) of the Federal Aviation I (We) Therefore SIGNATURE(S) OF LJESIUNATED ENGINEERING E ESENTATIvES Off$IGNATION NUMBER(3) CLAS3IFICATION(8) (1) Jeffrey D.Shutrump DERY-605526-NM Structures - . . " FAA Form 81104 (11-70) SUPERSEDES PREVIOUS EDITION (Computer Generated by Rohr, Inc.) EFTA00277772 4 Y a , so • • • EFTA00277773 O0OO MOO ROHR, INC. HaHH 6.50 Lagoon Drive Chub VIr2. Ca ttnta 91910 - Z198 ENGINEERING REPAIR DATA SHEET (EROS) FORM 8110.3 REQUIRED CLASS MAJOR F3 EROS NO. C1036 REV. S.O. NQ N/A REV. PAGE I OF 2 PART NO. VA545300-1 PART SERIAL NO. N/A MODEL V727RE COMPONENT AFT FAIRING -UPPER SKIN ASSY SERVICE I-CURS UNK CUSTOMER THE LIMITED DISCREPANCY: (BE SPECIFIC - PRINT CLEARLY ) ITEM A. The upper skin on the AFT fairing assembly, P/N .VA545300-1, on the #1 Engine position shows a disbanded condition on approximately 50% of the AFT surface, including two crescent shaped cracks on an existing repair (fiberglass?). On this same arevon the lower surface of the panel, an area of material is also missing and filled as above. The lower repair stops before transitioning to pan down of honeycomb. • See page 2 for sketch of location and description. MATERIALS: Upper Skin .032 2024-T3 QQ-A-250/5 Lower Skin .016 2024-0 QQ-A-25015 Heat treated to —T42 per MIL-H-6088 Honeycomb .310-3116-10 (5052) MIL-C-7438 PREPARED BY Don Adams REPAIR: ITEM A. Repair. UPPER SKIN REPAIR 1. Remove discrepant upper skin from assy. Care should be taken not to disbond the lower skin of the assy. 2. Fabricate a new upper skin from .032 gauge 202443 per QQ- A-250/5. 3. Remove lower surface Clad (bonding side). Do not thin below .029. 4. Make sure all remaining "old" adhesive is removed from core. Clean and prep skin (using PAA or Pasa-Jell 1 0 5) and exposed core (using Pasa-Jell 105) on panel. Clean repair area per 727' SRM 51-40-6, Par. G(2) (SRM 51-40-5). 5. Prime bond side of skin and core with BR-127 adhesiVe primer, per manufacturer specifications. 6. Apply two.coats of FM-73 adhesive material, per manufacturer specifications. 7. Bond replacement upper skin to core and lower skin per 727 SRM, 51.40-6, paragraphs E, J & K 8. Perform Post Bond inspection byvisually inspection of periphery for evidence of adhesive bead, and tap test the whole panel for voids. ORIGINAL rearms! when tilts stamp co is to rid ink DATE 8-02-99 AIRWORTHINESS APPROVAL DATE -_? 7 FOR.41 NO. E6687,5 Lz xggrIR! W1 t!ZEZZT696T9 EFTA00277774 OOOO 42OOO ROHR ROHR. INC. &X Lag= Dave Chtia Vida. CAlrfunia 91910-2098 ENGINEERING REPAIR DATA SHEET (ERDS) SUPPLEMENT SHEET RDS NO. C1036 REV. .0. NO. N/A REV. PAGE 2 OF 2 (1;scR6Rirkticy ecivrieiver)) FORM NO. E7983-1 .11tIZ71 (DISPOSITION CONTIUNUED) LOWER SKIN REPAIR 1. Remove existing repair (fiberglass) from discrepant area on lower surface. . 2. Cut filler to size of discrepant area from .016 gauge 2024-13 per QQ-A-25015. 3. Fabricate doubler from .020 gauge 2024-0, per QQ-A- 250/5 to cover filler. Doubler to overlap filler periphery by 1.50 min. Optional to use 2024-T3, no heat treatment required. 4. Form doubler to match lower skin contour per BAC 5300. Heat treat to -T42 per BAC 5602 or MIL-H-6088. Verify hardness per SRM requirements. 5. Inboard and outboard edges of doubler to be tapered to .010 min. Care should be taken so the edges of the doubler land mid spaced between existing assembly fasteners_ 6. Install doubler using steps 3 through 8 above. 7. Install new panel, filler & doubler using BP fasteners to complete assembly. Apply sealant to edge of logo light cut out , and seal all gaps at assembly. 8. Clear Alodine all external clad surfaces per MIL-C-5541, Class 3. ORIGINALl , is in red Ink When this stamp uvrmusr, EFTA00277776 8- 3-99 4:55 PM ;SUPER 27 PROGRAM 6196912232;# 5/ 8 By B. COX DATE 08/02/99 cHK'D1-51)07O) DATE OM ERDS Cl DODD EH= ROHR ROHR, INC. PAGE 1 of 4 TITLE Skin Disbond VA545300-1 Use or disclosure of this information is subject to the restriction on the title page or on the first page of this document Super 27 I. Discrepancy: The outer skin of the upper skin assembly of the aft fairing is disbonded and the aft edge of the outer skin has two cracks. See sketch below from ERDS. I!. Proposed Disposition: Remove the outer skin of the upper skin assembly and bond on a new outer skin using FM 73 adhesive and BR.127..adhesive primer. The cracks at the aft edge have been reported to be along a previous repair that was filled with a fiberglass patch repair. The fiberglass patch will be removed and replaced with a metallic patch and doubler. All metallic materials will be the same as BP materials. III. Static Analysis: The aft fairing is analyzed in section 10 of Reference'. In section 10 of Reference ', the substructure has been analyzed to withstand all the aerodynamic loading without using any of the skin as affective. Therefore, this analysis will only investigate the capability of the adhesive to carry the shear stress to the core conservatively assuming that the skin will carry the aerodynamic loading. strut Stress Analysis (VA-CR1 54 Rev. C) 1,09112 Dui 'MA EFTA00277778 8- 3-99 4:55 PM ;SUPER 27 PROGRAM 6196912232;# 6/ 8 BY B. COX DATE 08/02/99 CHK'D DATE ERDS Cl 036 DODE1 El= ROHR ROHR, INC. PAGE 2 of 4 TITLE Skin Disband VA545300-1 Use or disclosure of this information is suhicet to the restriction on the title page or on the first page oruris document The noted adhesive primer is compatible with the adhesive as shown in the excerpt of MIL-HDBK-337 at the end of this analysis. Conservatively assume all the aerodynamic load is reacted by a 1.0-Inch wide by 30 inches long beam that is simply supported between the fuselage and outboard edge. The core shear stress (f6) is expressed by = V / hb where V is the vertical load being reacted at the supported end h is the centroid distance of the sandwich panel h = t/2 + to/2 b is the beam width From page 10.7 of Reference ', the aerodynamic pressure (P) on the aft fairing Is .5 psi limit (.75 psi ult). Therefore the ultimate vertical load at one end of a simply supported beam is V = .75(30)(1.0)/2 = 11.25 lbs (ult). From VA545300, = .016, t. = .032 and t, = .30. h = .016/2 + .03212 + .30 = .324 in - = V hb = 11.25 / .324(1.0) = 34.7 lbs/in2 From the certification sheet shown at the end of this analysis, the allowable lap shear for the FM 73 adhesive is 6,523 psi at 75° F. Since there is no test data readily available for this adhesive system for core bond, e comparison of this adhesive system will be made to EA9649R (RMS 058). From figure 3.3.2 of Reference 2, aluminum core and face sheet with EA9649R adhesive has an allowable of 220 psi for the BP core configuration. Since the lap shear for the repair adhesive is significantly higher than EA9649R (2,838 psi at 75° F), it is reasonable to assume that 34.7 psi core shear Is acceptable for this adhesive system. The repair at the aft end of the fairing is acceptable by inspection since the aerodynamic load is very little to nil at this location. IV.. Fatigue Analysis: Repair is acceptable for fatigue strength by inspection since the ultimate margin is high and there are no additional stress concentrations compared to the type design. 2 MecheiniU:11 Design Allowables (RHR 85-013) frnreqvo 1-46A- EFTA00277780 • • A • 4 • EFTA00277781 8- 3-99 4:55 PM ;SUPER 27 PROGRAM DODD 6196912232;# 7/ BY B. COX DATE 08/02/99 CIODO PAGE 3 of 4 DATE ROHR ROHR, INC TITLE CHK'D Skin Distxind EROS C1036 VA545300-1 Usc or disclosure of this information -3 subject to Me ie ti Iction on the title page or on the first page of this do:mai/sot ktEleliD331C-337 1 DEsosnlbe.r 1982 I . R PiA- i! i l i 1 1 I e e t 4•- t i t —6 It P V in ti iti. aci I-- la (. II i5 V 4 . la 5 m 1113 g 11 t g 0 Cs l! . --zi • t I g S t, i t ti 5 1 l 4 CC77 Q g cS a r , a v m I- tit - iii _ m , . E 6 14 — c% li 6 s :frt. Set • 0 A r§ E VIE g I IL b . u. rig . LL ag LL DS • _ = > i' = -g .2 I 1 .g " S. -1 i E • 4-4 1%7/1 Ilredi 8 EFTA00277782 8- 3-99 4:55 PM ;SUPER 27 PROGRAM -k 5198912232;# 8/ 8 BY B. COX DATE 08/02/99 CHK'D ERDS C1036 DATE DODO DODO ROHR ROHR, INC. PAGE 4 of 4 TITLE Skin Disband VA545300-1 Use or dIscIosure Of this Intbrinalion Is subject to the restriction on the title page or on tho first paio of this document CytliCFADAE1 ISICIFirstitowl swat Kowa to 0nu*. kfarSAM2107/3 CSR irrrICAT ON. sow TO VIMCO-LARM CITY PA LA O. BOK 1909 M criry PL. 32066 GRIP VIW2O-1M34 arrl TO EIC;iway 30 EAST • gizaxxnx. Mime= 2cluTE 19. BOX 1029 OUR 'OMER IA= CITY • 0023439/001 PT* 32025 WinOWNt OR131&R 598376 Br* BATaijOrriT taBeiBit 2742-13037 * 2742 B EtsweltjuzysT =Km= TOTAL 1* TEL - turrg 5111sSzo 06/17/99 wait • mAntwacTaRBD =maw UM aum.13,1$)9 500.00 DP taTeR OTY so0.00 t TOTAL OT? 500.00 Tas atinTrzse THE sumotrara AT Trbas op EIBIPMENT OONFORK0 TU ALEIFEXCIUMIK rtalaNGS AWD spEciFiCATIOVS NOT= =WC SpEterisratriarg: 1244-A-132 RSV B, TW(-2 TM x =Ms 2 POEM P GROUP 3 llama 21.O8392VS OR FRU= legrra ACCIPTANCe Bi2 PART or TIM Num 3tragensint rYtngst_ unri ARK ORGY TO metuow WXTR ThZ marumcgo AnCE0strva oapkvAER To Imam caRTnnemoN. saa CSC FOR ASsZ8117Was, * AM 2 ism TzsT D A A 75 P LAP MAR 6584. 5552, 61044 6522, 6122 PEI winGtilrr 061, .01, .061 FISF 8 /£ a:ZUMeggrg rormywn t3I1L3 180 453U, 437B, 405.5# 4368, 45t5 PSX tinDOVd Lz Nef 5S;'e 6B-r -g EFTA00277784 A 3 ..t... al.• • ••• I. S. EFTA00277785 .ra I Work Order 43736. , to MAJOR REPAIR AND ALTERATION iv L.,: c • : i, , ,. !Form Approved OMB No. 2120-0020 • 7- - For FAA Use Only . US Department of (Airframe, Powerplant, Propeller or Appliance) - " Transportation Federal Aviation Administration . Office Id ntification ir.07 ' • '; • r" 4 • . INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, 'and AC,43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make • - . - . ' Boeing .ri :-..,;!•=- ', - Model • • ., , :: 1.,..; :11-".1:1V.,' . ',.. ' • ' i ; • 1 , v 1 727-31 '' Serial No. " S. , •:. • • • 20115 Nationality and Registration Mark • , . • • . .N505LS 2. Owner Name (As shown on registration certificate) I . ' ' ; • i Northwest Delaware Corporation . . . , . .. Address (As shown on registration certificate) • — •• • • .. • • 4 • 1105 N Market St . 1 ' Wilmington, DE 19899 : ' 3. For FAA Use Only 'The data identified herein complies with the applicable airworthiness requirements and is approved only for the above described aircraft, ,,,, , , .. • subject to conformity inspection by a person authorized in FAR 43, se Lion ' . : . , . 43.7 . 2 z ../ _Zieee GL-CMH FSDO , . ate . . .i •i i attire of FAA Ins ecter esus Zubia • Unit Identification 5. Type Unit Make •• ' Model • • . •• l . Serial No. • - • ,. „ .• . Repair . • Alteration AIRFRAME • • % (As described n item 1 above) , ., 1 I. . • . •• , • 'v• . • , ". ..... .;• i ,:, •I ,li -, r -: r •:•1• •,• ::. i ,: • • • ' . .• X POWERPLANT . , • • . , . 4 • 1 • .••• , it i •i • . . ••• .0. "1. • .1 • . . a. ••• • :6 • •'' ' " t I • • s +'•;i•..••. • • • . . ' ' -. • I PROPELLER . - 5 .,. . Z I ‘, 4 )4" .g • '•`.. I ' .' i let; •qtr. ••• . :1 • .:" ‘:' ' • ••••rvzr;• ;* ' ' • I S : !I' •• . APPLIANCE Type • •,, - • . . • . - I' ' Manufacturer 6. Conformity Statement A. Agency's Name and Address . B. Kind of Agency C. Certificate No. ElectroSonics . . „ . ... 4391 International Gateway Port Columbus International Airport Columbus, OHIO 43219 U. S. Certificated Mechanic Repair Station AEI R005K, Radio Class 1,2 & 3; Instrument Class 3, Accessory Class 3 Limited Altimeter Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U. S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date ' April 28, 1999 Signature of Authorized Indiv• -- _, -• • . - - _ . ., _ • 1 . • • '• ' • . • . i r ..,. ; , ; I • t t • ' - 7. Appro al Ret Service i • - . ' - • • t Pursuant to the authority given persons specified below, th Oriitlid fie in item 4 was inspected in the manner prescribed by the •. Administrator of the Federal Aviation Administration and is. Q APPROVED 0 REJECTED ; ', ..- ! 1 0%,......"• O. BY FAA Flt Standards inspector Manufacturer Inspection Authorization Other (Specify) . : A'Irt‘''..V •. ...N. 1- 1 ' ; ' FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group ,— . ! '1 '1 . I . Date of Approval or Rejection 4 s al -i I - - - - --- , Certificate or Designation No. AE1R005K Signature of Authorized Ind* d al I . 1 : 0 • i • _ ..... • • Q8) EFTA00277786 NOTICE Weight and balance or operating limitation changes shall besentered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. • 8. Description of Work Accomplished (if more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKE/MODEL/DESCRIPTION STATION 622-7293-101 3 Collins VHF-422b Comm C37c, C38c 450.0 2. The following equipment was installed in the aircraft. • PART NUMBER QTY MAKE/MODEL/DESCRIPTION ISO ,j= STATION INSTALLATION DATA • 822-1115-001 3 Collins VHF-422c Comm C37c, C38c 450.0 523-0772719 3. The above work was accomplished IAW FAA Advi'sory Circular AC 43.13-1B, Chapter 11,12 and AC 43.13-2A, Chapters 1, 2. 4. This work has been accomplished under ElectroSonics Work Order 43736. 5. Removed existing Collins VHF-422b corn's to accomplish 8.33Khz modifications Collins S.B.17. Following modification, reinstalled as VHF-422c and performed a complete operational check. 6. A complete test of the installation of the modified units has been conducted to confirm that other aircraft systems are free of interference as a result of this installation. All tests found to be satisfactory. 7. Collins does not specify any new continued airworthiness instructions for the above equipment. The owner/operator should consult the Boeing maintenance manuals for general avionics continued airworthiness requirements. 8. The owner/operator must comply with manufacturer's maintenance instructions to ensure continued airworthiness any time the above equipment is removed and/or repaired and reinstalled. 9. The aircraft Weight and Balance is unchanged and Equipment List has been amended. 10. The aircraft must be loaded IAW the prescribed loading information from the manufacturer. END • 0-1 S-A S-0 C-1 C-2 A-1 FSDO SITFIVED Col IMBOS. OH C-3 C-4 C-5 A-11 A-10 A-9 A-7 0-1 ■ ;,'-1 C2 S-A S-0 C-1 C-2 A-1 ■ 0-2 , . A-2 0-3 . Ss-,..-,Eivro .A-3 - ... '''/A ' — 3 1999 . • 0-4 A5 ,; 0 5 " A • - 0-6 CM FSDO- COI LIMMIS OH 0-7 0-3 S C-3 C-4 -C-5 A-11 A-10 A;9 A-7 Ali K Additional Sheets Are Attached •• , U.S. GPO:1991-0-568-012/40035 EFTA00277787 p.* Work Order 43736. t . - • . • ;. .,, MAJOR REPAIR AND ALTERATION ' i ' ' • '''•• - ' Form Approved . . ',I • OMB No. 2120-0020 • :. ' • For FAA Use Only l•••'''' - - - • US Dopartmant of (Airframe, Powerplant, Propeller or Appliance) ,, • Transportation ._ . 5.. , . .-,..- . . . - , .. ,..*:.,,,.•••,-- Federal Aviation Administration Office Identification Lk,: QL • - - ' GL0 7 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). ' • - , -, ' - . , 5, , • -, • • • 1. Aircraft Make .,i 1' 1P-ti :.?:; Boeing - - Model , , ' 727-31 Serial No. 20115 Nationality and Registration Mark ; • i , , ' - N505LS 2. Owner * Name (As shown on registration certificate) .. Northwest Delaware Corporation . , , , . - Address (As shown on registration certificate) • .* „1105 N Market St • - . :t., • 1 . Wilmington, DE 19899 ' • 3. For FAA Use Only • 1 ,; . 'The data identified herein complies with the applicable airworthiness , . . requirements and is approved only for the above described aircraft, ,•.• ,- . 7 , -.., 7; • . , subject to conformity inspection by a person authorized in FAR 43, section , .::**,'; I. . 43.7 / • I 24' 77 • —,,(//g" GL-CMH FSDO ' Date . ..4 tr , nature of FAA I sp I Jesus Zubia - ' "." ' 4. Unit Identification 5. Type Unit , Make , - ,I.,, , " r - i ' • ''',.'4, . . .t, :. Model .;r:::. -, .Serial No. , Repair Alteration AIRFRAME , .. (As described !I.!' Item 1 above),, ,. :;1. .. .,..:i.., t ,..,, , ., , - i t X , POWERPLANT • ,,. 1! 5, --- • 1 J.,,, it* ' ‘ ' 't I PROPELLER . • I • 1 t s • , ' • 1, • ' r...1 ' • .; .' • . 1:1 . APPLIANCE Type , , . , . . ., ' . • . , • . • -, 1,, • , ' I Manufacturer 6. Conformity Statement A. Agency's Name and Address, ••" B. Kind of Agency . . " — ' i • ' C. Certificate No. • ' ' ' ElectroSonics 4391 International Gateway Port Columbus International Airport Columbus, OHIO 43219 U. S. Certificated Mechanic Repair Station AE1R005K , Radio Class 1,2 & 3; Instrument Class 3, Accessory Class 3 Limited Altimeter Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U. S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date April 28, '1999 Signature of Au orized Indivi i I , • -• ...., , ....... .. .e-- i i , , , , 17..., i , f . i ) 7. Approval or turn o rvice - - Pursuant to the authority given persons specified below, the unit Administrator of the Federal Aviation Administration and is identi •./ in tern 4 was inspected in the manner prescribed by the APPROVED K REJEL ILI) . r q.?1•I --..: C BY FAA Flt Standards Inspector • , Manufacturer t Inspection Authorization Other (Specify) 1...:- t. • -• i • v i • FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group . . I Date of Approval or Rejection i t - ). i -19 Certificate or Designation No. AE1R005K Signa r of Authorized idual ; . , • - . FAA Form 337 (12-88) EFTA00277788 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (if more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 1. The following equipment was removed from the aircraft: .71 Ss, PART NUMBER QTY MAKE/MODELJDESCRIPTION STATION 622-6520-005 2 Collins CTL-22 622-6520-005 '1 Collins CTL-22 2. The following equipment was installed in the aircraft. PART NUMBER QTY MAKE/MODELIDESCRIPTION s .• „ • ; ' , 200.0 259.5 • •'':: i .r; 4 • • INSTALLATION TSO STATION • DATA 822-1120-005 82271120-.005 2 Collins CTL-22c C37c, C38c 200.0 523-0072719 1. Collins CTL-22c .1' ' C37c, C38c, , 259.5 • • .1.„ „. . , . , 3. The above work was accomplished IAW FAA Advisory Circular AC 43.13-1B, Chapter 11,12 and AC 43.13-2A, Chapters 1, 2. , • • 4. This work has been adcomplished under ElectrOSonics Work Order 43736. 5. Removed existing CTL-22 to accomplish the 8.33KHZ spacing modifications Collins S.B. 31. Following modification, reinstalled units'and performed a complete operational check. 6. A complete test of the installation of the modified units lls been conducted to confirm that other aircraft systems are free of interference as a result of this installation. All tests found to be satisfactory. I t i 7. Collins does not specify any new continued airworthiness instructions for the above equipment. The owner/operat0r shoUld consult the Boeing •mairitenanc4 manuals- for general avionics continued airworthiness requirements. i I i t 1 i 8. The owner/operator must comply with manufacturer's maintenance instructions to ensure continued ; airworthiness any time the above equipMent is removed and/or repaired and reinstalled. 9. . The aircraft Weight and Balance is unchanged and Equipment List has been amended. , • .r• ,; .., 10. The aircraft must be loaded TAW the prescribed loading information from the manufacturer. •• 0 0.3 0-4 0,5 04 S-A S-0 C-1 C-2 A-1 A-2 crcrivto , Al l(281999 CMH FSDO C-3 03 , COLUMBUS. OH C-4 C-5 A-11 A-101 A-9 A-3 A-4 A-5 A-7 A-8 END. - •fl" • t It ; 0; • '7 ., •!.C. 0-1 m-i -2 S-A -i.) 6-1 C-2. A-4 0-2 - • . ' - 4 .. . * 1 . • I A.-2 r.ZF.CEIVE'D -• JO 0-3 , ! • :. • •1.iiii,..1.-.3 ' A50.1-0' , 0_5-- ••. • • • - A75 .t-i•IJ ' A 0-6, L. • • 1 • 'MUSKY' ^ • • CORIM•Bliz Oh 0-7 ' C-3 - b=d, c-5 ik:.ii. • ".4-161 i'•9 At7 LL ,......___-_, - 0-8 . • t, . , : tr i • . I • ,-.. .i ,..1.J.:; O Additional Sheets Are Attached , - U.S, GPO:1991-0-568-012/40035 EFTA00277789 MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, or Appliance) of Transportation Federal Aviation Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification .e.y.f4.4 490 ,3- 0 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This form is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N505LS 2. Owner Name (As shown on registration certificate) Northwest Delaware Corp. Address (As shown on registration certificate) 1105 N PA S Wilmingtioh; p 93 i 3. For FAA Use Only AUti 1 0 1098 FAA-DILLAS SW05 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME avoraveswer4*~~~0~4•0 (As described in item 1 above) 410010.41~111001~111~~10•4114111 X X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A Agenciis Name and Address B. Kind of Agency C. Certificate No. Associated Air Center 8201 Lemmon Avenue Dallas, Texas 75220 U.S. Certificated Mechanic TX2R203L Airframe Class 3 & 4 Radio Class 1, 2 & 3 Foreign Certificated Mechanic x Certificated Repair Station Manufacturer D. 1 certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date 814/98 Signature of Authorized Individual >7# 7b4JWA lvd ri' l— 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified Administrator of the Federal Aviation Administration and is F:i in item 4 was inspected in the manner prescribed by the APPROVED K REJECTED BY FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee x Repair Station Person Approved by Transport Canadian Airworthiness Group Date of Approval or Rejection 8/4/98 Certificate or Designation No. TX2R203L Signature of Authorized Individual 7-i7, -.49/ti- A- FAA Form 337 (12-88) EFTA00277790 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Aircraft: Boeing 727-31 Registration #: N505LS Serial #: 20115 Aircraft Total Time: 31,675.6 Aircraft Total Cycles: 21,567 August 4, 1998 The following alteration was accomplished at Associated Air Center, Dallas, Texas under Work Order 1565. 1) Mode "S" Transponder ICAO Code Strapping Change in accordance with AAC Drawing 1565-001 Rev A dated July 28, 1998, 8110-3 approved by D.E.R. SW-997, David A. Kimbrell July 29, 1998. The following repair was accomplished at Associated Air Center, Dallas, Texas under Work Order 1565. 1) Repair - L/H Horizontal Stabilizer Trailing Edge Beam at Elevator Station 156 in accordance with AAC Repair Drawing 1565-002 dated July ---, 1998, 8110-3 approved by D.E.R. SW-810, Robert M. Manashi August 4, 1998. El Additional Sheets Are Attached U.S. GOVERNMENT PRINTING OFFICE 1992-769-012/60157 EFTA00277791 DAK-98-089 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JULY 29, 1998 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPUCANT ASSOCIATED AIR CENTER DALLAS, TEXAS LIST OF DATA IDENTIFICATION TITLE 1565-001 REV. A 07/28/98 MODE S TRANSPONDER ICAO CODE STRAPPING CHANGE • - -••-•• .--- - - ,-. - • . - NOTES : TC DATA SHEET A3WE. ELECTRICAL DESIGN ASPECTS OF THIS THIS APPROVAL APPLICABLE TO B727-31 THIS 8110-3 FORM IS IN SUPPORT OF FAA - --- - .., DATA IS APPROVED. S/N 20115 ONLY. FORM 337. PURPOSE OF DATA TO SUPPORT THE AVIONICS/ELECTRICAL MODIFICATIONS. APPLICABLE REQUIREMENTS (List specific sections) FAR 25.1301(a)(b)(c) CERTIFICATION - Under authority appointment under Part 183 of 0 have vested by direction of the Administrator and in accordance with the Federal Aviation Regulations, data listed above and on attached been examined in accordance with established procedures and found Regulations. approval of these data these data conditions and limitations of sheets numbered to comply with applicable requirements of the Federal Aviation n Recommend I (0) Therefore Approve SI NATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) DAVID A. KIMBRELL ( SW-997 AVIONICS/ELECTRICAL , --- :ni :f1 ; SYSTEMS FAA Form 8110-3 (11-70) SUPERSEDES PREVIOUS Eornont( ( COMPUTER GENERATED) GPO 901-813 EFTA00277792 4 t b .., EFTA00277793 AUG-04-1998 10:39 ASSOC AIR 214 357 2845 214 357 2845 P.O1 (1.3. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE #98421 AUGUST 04, 1999 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOZ.ZNO MODEL NO. 727,-31 . TYPE No.& 'to.. hokopasf. rz) AIRPLANE (N5OOL3) NAME OF APPLICANT ASSOCIATE) AIR Cwt LIST OF DATA IDE1471 !CATION TITLE ASIOCIATED AIR C/D1TER DRAIN O NO. 1565-002 REV . "2R" , DM= O7-29.1933 REPAIR - L/ft HORIZONTAL STABILZEER T/E Tipp= REM - ZZXV STA 136. (SKUT 1, 2 AND 3 07 3) . NOTES: 1. THE STRUCTURAL ASPECTS °NIA or THE ABOVE LISTED DATA X= Abl5A0v2D =Man. Titio NW/WV/Lt. IS TOR TEE IINGINIZZRING D191024 DATA O'NLY. 2. MIS APPROVAL IS VALID armY FOR 8=130 MODEL No. -727-31, AIRcRAPT S/N 2O115 AND Is IssuzD Itt SIMPORT OF A MAJOR =PAIR or THE SUBJECT AIRCRirT. PU - - 468E OF DATA IN SUPPORT or A )0JOR REPAIR ON BONING 14013EL NO. 727-31, AIRCRAFT 3/N 20115. APR_ z REQUIREMENTS pa vials; airasom) CAR 4b.20O (a) , (b) , 4b.201 (a) . (10 . (a) , 4b.202, 4b.3OO, 415.901, db. 302, 413.303, 4b.304 (a) , (b) , 4b-3O6 fa) . 04 , (d) . CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered )0000000(XXXXX00004 have been examined in accordance with establithed pnneadunes and found to COmply with applicable requirements of the Federal Aviation Regulations. 0 Recommend Approval of this data I (W) THEREFORE El Approve these data • Illij=gaityk,uzjite,,AL4,14:rivii-ut'ertl- -v 6ENTATiVE S SIGNATioN NUMBE frY4s 0 .. 0 . ek. A SW-910 STRUCTURES Roam — . • •• .. — • ------ 0 .7Q) aupERSIMes PREvIOUI trirrioN ..J a209314I3 TOTAL P.01 EFTA00277794 UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATiON STANDARD AIRWORTHINESS CERTIFICATE . 1 NATIONALITY AND REGISTRATION MARKS N50SLS 2. MANUFACTURER AND MODEL BOEING 727.--31 3 AIRCRAFT SERIAL NUMBER 20115 4 CATEGORY TRANSPORT 5 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and certifies that. as of the date of issuance. the aircraft to which issued has been inspected and found to conform to the type certificate therefor. to be in condition for safe operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation, except as noted herein. Exceptions: NONE 6 TERMS AND CONDITIONS ,, Unless sooner surrendered. suspended. revoked, or a termination date is otherwise established by the Administrator, this airworthiness certificate is effective as long as the maintenance, preventative maintenance. and alterations are performed in accordance with Parts21. 43, and 91 of the Federal Aviation Regulations. as appropriate, and the aircraft is registered in the United States. DATE OF ISSUANCE R 07--23-90 TATIVE t DESIGNATION NUMBER ____. GLO7 Any alteration, reproduction. or misuse oft C itti e may be punishable by a tine not exceeding S1.000. or imprisonment not exceeding 3 years. or both. THIS CERTIFICATE M ST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) 1 * U.S.G.P.O.: 1994-568-762 EFTA00277796 , .:11, MAJOR REPAIR AND ALTERATION US Department (Airframe, Powerplant, Propeller, of Transportation Federal Aviation Administration or Appliance) Form Approved omeApre or se my Ifo LAS t S 'iAJOc / (A/C_ INSTRUCTIONS: Print or type all and disposition of this form. This form for each such violation (Section 901 entries See FAR 43.9, FAR 43 Appendix (49 U.S.C. 1421). of 1958). B, and AC 43.9-1 (or subsequent revision thereof) for instructions Failure to report can result in a civil penalty not to exceed $1,000 is required by law Federal Aviation Act 1. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N500LS 2. Owner Name (As shown on registration certificate) Northwest Delaware Corp. Address (As shown on registration certificate) 1105 N Market St Wilmington, DE 19899 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in item "I above) sessesseasseareis X X . POWERPLANT PROPELLER APPLIANCE Type - . - Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. -Certificate No.:- • Associated Air Center 8201 Lemmon Avenue Dallas, Texas 75220 U.S. Certificated Mechanic 7- TX2R203L‘i a • Class 3 & 4 • • Foreign Certificated Mechanic x Certificatea Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified have been made in accordance with the requirements of Part 43 of furnished herein is true and correct to the best of my knowledge. in item 4 above and described on the reverse or attachments hereto the U.S. Federal Aviation Regulations and that the information Date 8/2/97 Signatur of Authorized Individual 4fr it-7--,- i 7. Approval for Reyirn Service Pursuant Administrator BY to the authority given persons specified below, the unit identified of the Federal Aviation Administration and is - item 4 was inspected in the manner prescribed by the REJECTED 0 APPROVED K FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Canadian Approved by Transport Airworthiness Group Date of Approval or Rejection 8/2/97 Certificate or Designation No. TX2R203L Signature of uthorized individual .4-169-4-c--- - Orin (12- EFTA00277798 • wo• NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (tf more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Aircraft: Boeing: 727-31 Registration #: N500LS Serial #: 20115 Aircraft Total Time:31,471.2 Aircraft Total Cycles: 21,468 August 2, 1997 The following work was accomplished at Associated Air Center, Dallas, Texas under Work Order 1476. 1) Repair - Airstair Door Actuator Attach Clip in accordance with AAC Repair Drawing 1476-001 IR dated July 16, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 2) Repair - #1 & #3 Pylon Corrosion on Forward Engine Mounts in accordance with AAC Repair Drawing 1476-002 IR dated July 17, 1997, 8110-3 approved by D.E.R. SW- 916, Jim Martin July 22, 1997. 3) Repair - #8 Leading Edge Slat Crack at I/B Slat Guide in accordance with AAC Repair Drawing 1476-003 IR dated July 17, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 4) Repair - Corrosion on R/H Wing Upper Surface at WBL 70.5 Between Str. 1-14 in accordance with AAC Repair Drawing 1476-004 IR dated July 21, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 5) Repair - Floor Beam BS 600. RBL 25 Figure 8 Hole in accordance with AAC Repair Drawing 1476-005 IR dated July 22, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 6) Repair - Aft BB Door Interior Structure Cracked in accordance with AAC Repair Drawing 1476-006 IR dated July 22, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 22, 1997. 7) Repair - Wing to Body Fairing Damaged Dome Nut in accordance with AAC Repair Drawing 1476-007 IR dated July 25, 1997, 8110-3 approved by D.E.R. SW-916, Jim Martin July 25, 1997. 8) Repair of Center Engine Exhaust Nozzle in accordance with Rohr, Inc. Engineering Repair Data Sheet No. C0625 Rev. A dated July 23, 1007, 8110-3 approved by D.E.R.(s) NM-2731, Jeffrey D. Shutrump for Structures, NM-738, Tony Bradlaugh-Dredge for Powerplant and NM-2182, Michael August for Special Administrative July 23, 1997 and AAC Repair Drawing 1476-008 IR dated July 25, 1997, 8110-3 approved by D.E.R. SW- 916, Jim Martin July 25, 1997. SrAdditional Sheets Are Attached U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012/60157 EFTA00277799 * * * * 鬓 * 滿 * * * * * * * * * * * * * * * 崇 * 帐 * * * 兴 * 台 扁 盆 * * 幡 * % * * * * * * * * * * * * * * * * * * * * * * * * * ‘ 卜 。 。 一 窗 N 扒 一 昌 老 … 3 吻 O 。 ’ 参 昱 。 一 ＾ 。 呦 等 参 叻 · 餡 · 阉 · Q 宕 「 ⑩ ＞ 。 a Q 髑 M I 2 品 ＾ 卜 ③ ③ 一 ＾ 芻 冒 一 一 瞩 「 出 g 鬲 I - － 入 內 ＇ 卜 ③ 曲 屆 3 蚪 Q O < ＜ ￡ 篆 ① ◎ 為 「 8 ◎ ◎ 巛 鬲 出 剑 划 瀏 铡 剴 国 吲 刊 荆 蒯 剽 唰 门 回 剑 唰 剧 剡 浏 剑 闪 蜊 ~ ＾ ° 卜 · 2 ·N 場 ＝ ~ ＝ < 晌 － － ° N 蘧 鼋 艺 ① 叻 節 冲 矬 筒 N “ 沏 ⑩ ＂ g 熬 g － 雲 昌 噪 細 Q 訕 － ＜ 叻 闫 ° 。 蚋 z ＂ 鞋 g 鼍 募 … 锣 盛 N ’ 叫 卜 矬 耆 M 釜 扈 占 宸 － 昌 噪 訕 Q 訕 － ＜ 一 M I 卜 g ＂ 蜘 庄 － ⑩ 。 箇 ” ‘ 编 齟 Q 齟 … 忍 EFTA00277800 ARC' 91.1 f. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-0011-- REV. IR 7-16-97 REPAIR - AIRSTAIR DOOR ACTUATOR ATTACH CLIP THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 NSPEC-1-01\ PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Regulations, examined in accordance with established by direction of the Administrator and in accordance data listed above and on attached sheets procedures and found to comply with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered ,/ V X have been requirements of the Federal Aviation Regulations. MI I ( ) Therefore 171 SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATIONS) 7: JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277802 s I a EFTA00277803 AAC-110 IS-1 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-002 REV. IR 7-17-97 REPAIR - # 1 & # 3 PYLON CORROSION ON FWD ENGINE MOUNTS THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSPECTION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Regulations, examined in accordance with established by direction of the Administrator and In accordance data listed above and on attached sheets procedures and found to comply with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered V L7,( oe have been requirements of the Federal Aviation Regulations. I ) Therefore 71 SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 1.7 . 4.' JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277804 • II • ... EFTA00277805 RPC°1-1.1SB U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-003 REV. IR 7-17-97 • REPAIR - # 8 UE SLAT CRACK AT 1/B SLAT GUIDE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 t°41SPFC1-\°N PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 . .303 .307(c) .300 .304 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Regulations, examined in accordance with established by direction of the Administrator and in accordance data listed above and on attached sheets procedures and found to comply with applicable Recommend approval of these data these data with conditions and limitations of appointment numbered Z / pL have been requirements of the Federal Aviation Regulations. 1 J I ) Therefore r-- .Approve SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 7- -7 . e/ JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277806 • . • EFTA00277807 AfIC•91,15. • U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 -TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-004 L✓ REV. IR 7-21-97 • REPAIR CORROSION ON R/H WING UPPER SURFACE AT WBL 70.5 BETWEEN STR. 1 - 14 THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 iNIS?E_CION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 - .303 .307(c) .300 .304 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Regulations, examined in accordance with established by direction of the Administrator and in accordance data listed above and on attached sheets procedures and found to comply with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered 0‹. ("<' have been requirements of the Federal Aviation Regulations. I ) Therefore 71 SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) ,,, JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277808 ..9 • S • • EFTA00277809 Af:IC,.91. ILO U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-005 (. REV. IR 7-22-97 REPORT NO. 1476-005 c- . REV. IR 7-22-97 REPAIR - FLOOR BEAM STA. 600 RBL 25 FIGURE 8 HOLE STRUCTURAL SUBSTANTIATION - REPAIR - FLOOR BEAM STA. 600 RBL 25 FIGURE 8 HOLE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 INSpECTION PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 • .303 .307(c) .300 .304 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Regulations, examined in accordance with established I ) Therefore El by direction of the Administrator and in accordance data listed above and on attached sheets procedures and found to comply with applicable Recommend approval of these data these data with conditions and limitations of appointment numbered Z 0.., have been requirements of the Federal Aviation Regulations. ji-i6Approve SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) JIM MARTIN SW-916 STRUCTURES orm (11-70 PERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277810 i, • • EFTA00277811 iL U.S. DEPARTMENT OF TRANSPORTATION . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/22/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-006 `--- REV. IR 7-22-97 REPORT NO. 1476-006 (V REV. IR 7-22-97 REPAIR - AFT B/B DOOR INTERIOR STRUCTURE CRACKED SRUCTURAL SUBSTANTIATION - REPAIR - AFT B/B DOOR INTERIOR STRUCTURE CRACKED THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 IN R P F CT 1 0 N PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.200 .301 .305 .201 .302 .306 .202 .303 .307(c) .300 .304 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Regulations, examined In accordance with established by direction of the Administrator and in accordance data listed above and on attached sheets procedures and found to comply with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered a/ oe have been requirements of the Federal Aviation Regulations. I Therefore 171 SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 7— e JIM MARTIN SW-916 STRUCTURES • _ FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277812 r • • • EFTA00277813 fiRC>97' U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/25/97 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-007 ,.- REV. IR 7-25-97 ‘-- REPAIR - WING TO BODY FAIRING DAMAGED DOME NUT THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 G 'OC) \ s ‘ s, PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.300 .304 .305 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Regulations, examined in accordance with established by direction of the Administrator and In accordance data listed above and on attached sheets procedures and found to comply with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered ,24" pZ of have been requirements of the Federal Aviation Regulations. I 04 Therefore SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) 57 ,.,,,, JIM MARTIN SW-916 STRUCTURES • FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277814 • • • • EFTA00277815 RAC, crl, ILL . U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE 7/25/97 • AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE BOEING MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) AIRPLANE NAME OF APPLICANT ASSOCIATED AIR CENTER LIST OF DATA IDENTIFICATION TITLE REPAIR DWG. 1476-008 ( - REV. IR 7-25-97 REPAIR - OUTER SKIN NOZZLE CENTER ENGINE THE ABOVE DATA IS APPROVED FOR THE STRUCTURAL DESIGN ASPECT ONLY. FOR AIRCRAFT S/N 20115 JA/Ch L--,(Th ,_, .... PURPOSE OF DATA IN SUPPORT OF REPAIR APPLICABLE REQUIREMENTS (List specific sections) CAR 4b.300 .304 .305 CERTIFICATION - Under authority vested under Part 183 of the Federal Aviation Regulations, examined in accordance with established by direction of the Administrator and In accordance data listed above and on attached sheets procedures and found to comply with applicable Recommend approval of these data Approve these data with conditions and limitations of appointment numbered oe 1/ oc- have been requirements of the Federal Aviation Regulations. I (ye) Therefore i- 1 SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) JIM MARTIN SW-916 STRUCTURES FAA Form 8110-3 (11-70 SUPERSEDES PREVIOUS EDITION) GPO 901-613 EFTA00277816 • 0. • EFTA00277817 JWG 97.084 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE JULY 28, 1997 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727 - 100 TYPE (Au-plane. Radro. Ilelicopier. etc.) Airplane NAME OF APPLICANT Associated Air Center LIST OF DATA IDENTIFICATION TITLE Drawing No. Autopilot Interface Unit Modification W/D. END Note: (1) The above data is approved for the electrical/ electronic and avionics design aspects only. 97 - 2211 - 210  Rev -- Date: 7/28/97 PURPOSE OF DATA To Support Major Alteration on S/N 20115 Only. APPLICABLE REQUIREMENTS (fist specific sections) FAR 25.869(a), 25.1301, 25.1431(c). CERTIFICATION - Under of appointment under Part 183 X X X X X X X X X have been authority vested by direction of the administrator and in accordance with of the Federal Aviation Regulations, data listed above and on attached examined in accordance with established procedures and found to comply Regulations. Recommend approval of these data Approve these data conditions and limitations sheets numbered with applicable requirements of the Federal Aviation I (326) Therefore x SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) DESIGNATION NUMBER(S) CLASSIFICATION(S) SW - 880 Systems & Equipment // John W. Goswick V orm - EFTA00277818 a • . •• • • EFTA00277819 7-23-27 3:12 PM ;SUPER 27 PROGRAM 5125912232;# 2/ 5 U.B. DEPARTMENT OF TRANGPORTATION FEDERAL AVIATION ADMINISTRATION I STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE July 23, 1997 AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE Boeing MODEL NO. 727-31 TYPE (Airplane, Radio, Helicopter, etc.) . Airplane NAME OF APPLICANT Rohr, Inc. LIST OF DATA a------ IDENTIFICATION TITLg • Rohr Inc., ERDS C0825 Revision A dated July 23, 1997 • Engineering Repair Data sheet INSPEU k • _.. PURPOSE OF DATA To submit substantiating data for a repair. This constitutes approval of the repair design only. _____ APPLICABLE REQUIREMENTS (List SpecOo Sections) (1)(3) FAR 25.301 (2)(3) FAR 25.605 (a) (1)(3) FAR 25.303 (2)(3) FAR 25.609 (1)(3) FAR 25.305 (a)(b) ,.. CERTIFICATION — Under authority appointment under Part 153 of NONE have been vested by direction the Federal Aviation Regulations, examined In accordance Regulations. of the Administrator and in accordance with conditions and limitations of aata listed above and on attached sheets numbered with established procedures and found to comply with applicable of these data requirements of the Federal Aviation I (We) Therefore Recommend approval Approve these data 8iGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVES DESIGNATION NUMSER(S) CLASSIFICATION(S) (1) Jeffrey D. Shutrump e -, NM-2731 Structures ,. . v• (2) Tony Bradlaugh-Dredge •-•-‘. NM-738 Powerplant (3) Michael August ".Z -t. NM-2182 Special Administrative _ . --- FAA Form 81104 (11-70) SU RSEDES PREVIOUS EDITION (Computer Generated by Rohr, Inc.) EFTA00277820 • pep 40 EFTA00277821 UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD PiRWORTHINESS CERTIFICATE • I NATIONALITY AND REGISTRATION MARKS N5OOLS 2 MANUFACTURER AND MODEL [ 3 AIRCRAFT SERIAL NUMBER BOEING 727-31 20115 AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and ceatties that. as of the date of issuance. the aircraft to which issued has been inspected and found to conform to the type certificate therefor, to be in condition for safe operation, and has been shown to rp,set the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention oh International Civil Aviation. except as noted herein Exceptions 4 CATEGORY TRANSPORT NONE 6 TEAMS AND CONDITIONS Unless sooner surrendered, suspended, revoked. or a termination date is otherwise established by the Administrator, this airworthiness certificate is effective as long as the maintenance. preventative maintenance, and alterations are performed in accordance with Parts 21.43. and 91 of the Federal Aviation Regulations. as appropriate, and the aircr t is registered in the United States 4111. DATE OF ISSUANCE Replacement) 07-23-90 FAA REPRESENTATIVE LEE H. Till DESIGNATION NUMBER GLO7 Any alteration, reproduction, or misuse of this certificate m. a by e froI exceeding S WO, or impnsonrnent not exceeding3 years. or both. THIS CERTIFICATE MUST BE DISPL THE AIRCRAFT IN ACCORDA CE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) GPO 892-804 EFTA00277822 1 5 ... r a e• .fr 4 ili EFTA00277823 . O - • - MAJOR REPAIR AND ALTERATION . Form Approved OMB No. 2120-0020 For FAA Use Only US Dew titija ca-ortp«vmAl - (Airframe, Powerplant, Propeller, or Appliance) ' Federal Ar iaflon Office dentification -- -P i --7Z--40 ) I u RUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model- 727 —100RE Serial No. 20115 Nationality and Registration Mark N500LS - 2. Owner Name (As shown on registration certificate) NORTHWEST DELAWARE CORPORATION Address (As shown on registration certificate) ggYIA4,DE. 1;899; 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME ....................... (As described in Item 1 above) .................„„,„,..... • X POEFIPLANT PROPELLER APPLIANCE Type Manufacturer • 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. THE LIMITED INC. 4387 INTERNATIONAL GATEWAY COLUMBUS, OHIO 43219 X U.S. Certificated Mechanic IA301541619 Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of Ihe ,. -,Eede rMigion Regulations and that the information furnished herein is true and correct to thei,,beq.of my-knowledge. 1 '•; !.;e: :I .... i„ .3"L Date ii . March 11, 1998 , Signature ' ze-r 1 divi a • Richard K Cady II 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item wa inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is - t APPROVED O JE' TED FAA Fit. Standards Inspector Manufacturer X Inspection Authorization • her (Specify) FAA Designee Repair Station Person Approved by Transport Cana orthiness Group , Date of Approval or Rejection Certificate or Designation No. Si natur of thorized I yid:al • March LI , 1998 IA2185934 . - ,x-e T .W. RITCHIE FAA Form 337 riz-aa) EFTA00277824 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must& compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional.sheets. Identify with aircraft nationality and registration mark and date work completed.) REMOVED THE FOLLOWING EQUIPTMENT; 2EA. HONEYWELL DIGITAL AIR DATA COMPUTERSP/N 7000700--962. INSTALLED THE FOLLOWING EQUIPTMENT: 2 EA. HONEYWELL DIGITAL AIR DATA COMPUTERS P/N 7000700-662 WITH STATIC SOURCE ERROR CORRECTION CURVE INSTALLED IN ACCORDANCE WITH AES DRAWING ,LIST NO. 97-727-500 REV. B, DATED NOVEMBER 3, 1997 PER SUPPLEMENTAL TYPE CERTIFICATE STO9364sc. FAA APPROVED FLIGHT MANUAL SUPPLEMENT, DATED OCTOBER 27, 1997 IS REQUIRED AND INSTALLED ON THIS AIRCRAFT. WEIGHT & BALANCE NEGLIBLE. COPY OF STC ST09364SC AND MASTER DRAWING LIST ATTACHED. CONTINUED MAINTENANCE PRACTICES INCLUDED IN THIS PACKAGE. END El Additional Sheets Are Attached *U.S.GPO:1991-0-568-012140035 EFTA00277825 THE LIMITED UR0859 RECEIVED U.S /Department of Transportation Federal Aviation Administration ti . ... MAJOR (Airframe, REPAIR AND ALTERATION Powerplant, Propeller, or Appliance) Form Apprptypdo OMB p( c 1,01d2-0192196 Irina For FAA Use Only CiffirAPPOALLAS SW05 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil : penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 1958). ..-.,. _ - 1. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality N500LS and Registration Mark 2. Owner Name (As shown on registration certificate) Northwest Delaware Corp Address 1105 Wilmington, (As shown N. on registration Market DE St 19899 certificate) 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME — --- — ----- — ------- -------------(As described in item 1 above)------------ POWERPLANT PRATT & WHITNEY Turbo Fan Engine JT8D-7B P654373 X PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. U.S. Certificated Mechanic Greenwich Air Services - Texas, LP Foreign Certificated Mechanic RAI R445K .. 9311 Reeves Street X Certificated Repair Station Powerplant Class 3 Dallas, Texas 75235 Manufacturer Accessory Class 1,2 and 3 D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date /0 r 3 O --n Sign e f Authorized Individual , 7. Approval r Return To Service Pursuant to the authority given persons specified bel w, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is _ X APPROVED [1 REJECTED BY FAA Flt. Standards inspector Manufacturer Inspection Authorization Other (specify) • FAA Designee x Repair Station Person Approved by Transport Canada Airworthiness Group In ividual Date of Approval or Rejection / or O - 9 4 Certificate or Designation No. Signa f Authorized _3 RAI R445K f-AA Form 337 (12.88) EFTA00277826 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Engine S/N P654373 was removed due to "SERVICE BULLETIN COMPLIANCE." • Engine was disasembled, inspected, repaired as required in accordance with Pratt & Whitney JT8D Engine Manual (P/N 481672), and Greenwich Specialized Unit Repair Workscope which are data approved by the Administrator. Inspected/reinstalled Combustion Chamber Outer Case P/N 542155, S/N 243, T.T. & T.C. Unknown, in accordance with P&W Alert S/B 6228, Part I and Part II and AD's 87-11-07 & 95-08-15. Ps4/Drain bosses require reinspection within 6000 cycles and at each Engine shop visit. Rear flange requires reinspection within . 12000 cycles and at each Engine shop visit. Case meets inspection requirements of Part III of P&W ASB 6228. Continue timed combustion chambers. Complied with P&W Alert S/B 5729R2 and AD 87-14-01 R1; immersion ultrasonic inspect C2 fan blades. Complied with P&W Alert 6038R5 and AD 94-20-01; corrosion inspect high pressure compressor disks. Complied with Pratt & Whitney Alert S/B 6196R5; #5 bearing seal assembly. Improved oil return & compartment sealing configuration. Complied with P&W Alert S/B 6110 and Alert S/B 6131, AD 94-20-08. This terminates -reinspection requirements for P&W Alert S/B 5913R6, AD 93-06-05. Engine was preserved forshort term storage IAW Pratt & Whitney JTSD Engine Manual (P/N 481672). Engine was subjected to a test run; a post-test borescope inspection was performed and Engine was accepted as serviceable. Engine TT: 32939.0, TC: 22557, TSR 00:00 CSR 0000. Pertinent details of this repair are on file at this Agency under W.O. UR0859 fl ADDITIONAL SHEETS ARE ATTACHED FAA AC 72-4906 EFTA00277827 0 . MAJOR REPAIR AND ALTERATION uSDeporrpent atralwavarxxl (Airframe, Powerplant, Propeller, or Appliance) Filderolita*Mms Aderinharoftn Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification a_FSDO-09 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model B727-31 Serial No. 20115 Nationality and Registration Mark N500LS • 2. Owner Name (As shown on registration certificate) Northwest Delaware Corporation Address (As shown on registration certificate) 1105 N. Market Street Wilmington, DE 19899 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME ......................".......; (As described in Item 1 above) ...............~............~........" X POWERPLANT PROPELLER APPLIANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. ST Mobile Aerospace Engineering, Inc. 2100 9th. Street, Brookley Complex Mobile, AL 36615 U.S. Certificated Mechanic MZAR013L Limited Airframe Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. Date November 25, 1995 Signature of Authorized Individ Clarence Spencer e.r....---- • 7. Approval for Return To Service Pursuant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is NI APPROVED D REJECTED FAA Flt. Standards Inspector Manufacturer inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection November 25, 1995 Certificate or Designation No. MZAR013L Signature of Authorized Individual Christopher J. Hil FAA Form 337 (12.88) EFTA00277828 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration rAust be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) Installed DeVore Aviation Corporation tail flood light installation in engine pylons in accordance with De Vore STC ST09113AC dated 26 May 95. DeVore Top Drawing List #72700003DL Rev "A" dated 5-30-95. Installed Valsan Winglet Modification in Accordance with Valsan Master Drawing List #VA000007, Rev uN" dated 17 April 1995. STC SA5938NM. Aircraft Inboard and Outboard Aft Flaps and Ailerons rigged to endure functionality and conformity. Aircraft weighed after modification. Weight and balance data provided to customer. Aircraft total time = 31,197 hours. Total cycles = 21,345. END K Additional Sheets Are Attached *U.S.GPO:1990-0-588-012/40004 EFTA00277829 FAA AIRCRAFT REGISTRY CAMERA N0. 3 DATE: die/ fr Se— •••• ••••-2. ; • 9.: of y; E «. •1 :4 : • :: . ;I: • f: : . : P • • I •14fiS • ••: m.44. • ;• 4.4. .4 • •4444.4•444 • 0 MAJOR REPAIR AND ALTERATION • uSOtowirrwre or laracianomn (Airframe; Powerplant, Propeller, or Appliance) I said asionse ' isaverawiesies •• . Fc.rm Approved • OMB No. 2120-0020 For FAA Use Only i t5IdenNication 0 _„ 6- 7 revision thereof) for instructions a civil penalty not to exceed 51,000 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 03 Appendix B. and AC43.9-1 (or subsequent and disposition of this form. This report is required by law (49 U.S.C:1421). Failure to report can result in for each such violation (Section 901 Federal Aviation Act of 1958); 1. Aircraft Make • aiE7N6- Model 7.Z7 - - /,‘Z) Serial No. ' c; o d C . • , .. . Nationality and Registr,ation Mark N5 -6,04.5 , a. Owner Name (As shown on iegistratiqn certificate) /vagazder. 44D/4/6 Oieft-P. .. . . Address (.4s shown on registration certificate) te)..an-k -7435 . V/(14),(16few ..7)e: /912)5 3. For FAA Use Only :. • r . • .• . .. _ .• ...::.1 - •&i • ‘ V. '',\ S ce • c • .--7/.:45:: I. %J.: ... ._ , , . , .. . ., • .• ••• • • • 4. Unit Identification _ . 5. 'Type Unit ... • .. . ' ', ••'', Model • - ' /•• . Serial No. -• Repair Alteration AIRFRAME (As : . described in Item 1 above) -.. • _ , POWERPLANT r. . . , • - .-......., . • • '-: . PROPELLER ._ .. . . - ' - • \'. .\• •• -/I:'+IV '..".-'• 'i• • • 1 .•. . - - - APPLIANCE Type e 24-s untgar .' PA) Zia/6 00 - 90c l (.1,OD. 6-) ; 97405'-e°3 e i i > l< Manulpoturer _ b. 6714/ra, 6. 'Conformity Statement A. Agency's Name and Address . B. Kind of A enc • C. Certificate No. --rief Ziliire3 ..tvc_ y3e2 mt. -fink Coi_i,f6tri osielt.o 5132. pi' - , U.S Certificated Mechanic , • 1 -04...))e S-93tZ . Foreign Certificated Mechanic Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the un i(s) identified in item 4 above and described on the reverse or attachments'hereto have been made in accordance with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my kno - - . --- Date . 7/i/9 41 - S natur of orized Indivi - Pu Administrator BY • ••• 7. Approval for Return \o Sonic* suant to the authority given persons specified below• the Loch identifieo'in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and is APPROVED O REJECTED FAA Ft,. Standards Inspector •N . Manufacturer Inspection Authorization (Specify/ . ' .. • FAA Designee Repair Station Person pprov by Transport Cana Airwo hives recap Date of Approval or Rejection /9/9 (1/ Certilicate or Designation No. --.1.14-a ,acci-w Sig lure of uth zed t Individulther . , FAA Fors 337 Ia.'s) • • • 4 : 4. 1 • eft ri if . • • • 4 .1, •i• •.‘ :••• •4 .1 • , • . onor a,. so iwarr•Iina.se,,,,,,iggilia airman Ofifigam • ffs il t ' 4 16* t • • ••• • S. . • . : . • . ' • i : • • N • • t . i. f. 4. ;rt. • • •• • ail2Si • • EFTA00277830 • I J.4.10. i'••:.! . x•,•nk;ilh 1G hill?' c ' Oint,n;T: • "Yanlei, ;;• ;01.•• • f-mt...o'R • "''• CV C. CA NC., rc...1‘J • • • -• now r- j NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. . t Description of Work Accomplished (If more space is required, attach additiOnal sheets. Identify with aircraft nationality and registration mark and date work completed.) .I••• /: .......i • . ... ••. • • •...• of. .!•1 • . . I I ' . • •• -e. • i • neile ... aPee,47›,e-z• To 4 -71v Vo66o/0.-' 4964 . (fien).- a.) "By • ,xletreAcrearver , Nits/ere-a_ ..sla 41°660/6 - 34 i ertir&041-67) npic.c#&,_ 4(4.49-7eme,A./ ..cs 2),Exa-ivr. AI > 9st -o/-041 4.-.. :...._. ,.Sy nrit /6Z-I 3(60 oPetkriernhild/ 04?"-e-20 eloo.Zo/D adNeo. TevZ .?4,-75,> c-1- 41 sie • 4),/, c hi- Vi Er • AV 4-eargrAig ,ec-ve6-.• idg rE73/ 2,4-.4) • ..?,00-6.edsoht , air ,491.4P 90-a -oV Afro. 39 -- 878Lr .. got -6,za- 23(?)..,-erbe -7116- Aril &Al AZ • v3771 V,Lti - e c.c% • 74)40ee,oi_der-77A.?6-. a- am/ of s stn. AD. 4;;,/ riierwr /111-Ahnot -Warsqc re" 477-Xedieb riehtf- lerre;-,c krfirlerc-zdue,. <ale Affigenak_ Av MeroAr oc --- , .. ......; L• . __J .:. , -:... :. • .: • -. 'i . . .. - I. b14•• .lain til'ArtemoD :t - "‘ . ... • - . ee•Yd.rd: bi 4 • 831•1, • • --.. . r .." • •— -••• • -•• • , • • . " • - • • . ' • el r Itei P.,:i .-; :fle ;".::: ; 410 to•lovin erlInlibm1I14: 4i.4150r. -•••.,..:.1..! •- 4:1•..! 4 ki 14e.itil.:;L: td.(E).1i.loeti.tol Sbs In (*ifZ.1'31 GIO‘tine• itbiitt ro.t,iF. , • :. nc,14:71 iC-;:i. Mit :KM brilt 4....41-.. 461:4;•.r.:11•' ,IlbivA ;it i•,•;•, : it 1.I.;.;-•Ilo a')'iL'•13.11•17in.4telsiitiro!,•• -pt;1 milt b'...nnelysi...i.aepi store r• $ r ; g.,.. • • , ' . • . i .: &'.... :/ it \b '1 t 0 JZ6d.erif ci! Jr.:alio.; t)4::. ,:... d zi nir.brv.' 1 • • - • • ............... • ..%•• . ...... m• ••••••• d.;,.•• '''' ' : '"•••• • J., • ..m.....m. •••• A.. I:Mi. . • . ••• • =4 .. . . . • ... I i'a iV i tit il 46 ‘`: i i c ' ; . P. 4t 1-g ?tc l‘ i) ; 14.: ; 7. i • I . k • . . . • • . • . • • ' " raiviDE2O.T.ot; i.: ' • *:•••! 4, . • • • • • c.r!S vc! tiC•dittiz 1(1,1r.ittittrii ,i:tirill Loitz;ttitril otiw 1%. ratili rii !...:•Iiiii,; ,i., Si: : t i. 1.'.. .... ‘.••1:.ki.t.soli:•••.)cli e:norisr;, • .)*'1,:! vinc...0.;44P., Urn Vi. I714;,::‘• "•;..• i i.,:tt Ii0;10:1041,:t,.;11::- nc•it,.:-.6•A ;•7•.p.i..i.:k.",t•IA.10 mlitt!imiltsn. ' v . •.. I) rti3lan t.1 • (tvtior,:t...:-..,•'? ,. . - r . . . . - . ._ ...... (X‘V.11::.1?. iVil:51 • . . . . • I. . ;;.... tt 1: : : !. i < 71'.: L.... 5. t t; i :•:• -• . : , itglli!:10".:, ..1,0a • : 2.*'.11•‘triate-107 •434,,,i1.1.rAZI . 1 . • . • l'• • . : i'diti:dir.47 yd b loi.;';i lc:521.)g! • :- - - • • ' .. • . fIC;Irlc. lif191............ . i...:-. ..‘Octize!..• A Al • • • — . Mdiehriv3r4in lowilm is.e4.9.•,.. , ..._.... • ...•+...•.••••..... • ea .. aft ••••••••••••. .• ••••.••••=••••••••••1 •••••••••dmmini• •••.... ir••••• •••••• •••11,•••••••,.. ••• : , ••••••••7 .7 ...... ' , • • itii iivitini bt..1=0,4 lo 0,Lpap.. eta 1 . - t incl.,01D, . ritri)34,40,y., •:....,vzi.V, ... • • . i , A i i • • .. .., .1.., • , -, t. , • . i• . ..0.,110,. 7., ,r1.:Et...? " • \-,-: -O kddillo I ShilailicA6 Atiecheid .0';•Cr-')Ot • cL,:..477;:. • • :, :. • s,-;,.:..•. .:, . • ... "I: jti fat, • • 'a' •• • • • • I a' • EFTA00277831 FAA AIRCRAFT REGISTRY CAMERA NO. ,3 DATE: -41e/Ife/fY %."7.-:• 4- USDemamment ottranSpa-tationi Federal Aviation AdotinistratiaA • TRANSPORT AIRPLANE DIRECTORATE AIRCRAFT CERTIFICATION SERVICE LOSJANGELES AIRCRAFT CERTIFICATION OFFIC ; (,. (3229 EAST SPRING STREET / LONG BEACH, CALIFORNIA 90806-242S VAR CI 144 Honeywell inc. Air Transport Systems Division ATTN: Mr. F. W. (Bill) Lynch 21111 North 19th Avenue Phoenix, Arizona 85027 References: a) Honeywell letter, dated Feruary 17, 1994 b) Honeywell letter, dated March 1, 1994 Dear Mr. Lynch: ' Approval of an Alternate Means of Compliance " fp response to your letter of March 1, 1994, our review of the data submitted fivsupport of a proposed alternate means .of compliance with paragraph C. of AD 94-01-04 regarding Conversion of Honeywell TCAS II part No. 4066010-901, -90R and -903 (Any Mod) to part No. 4066010-904 (Mos G), has been completed. We concur that method and procedures outlined in your revised Service Sullitin 4066010-34-SW16 Revision 1, dated February 17, 1994 provides an acceptable level of safety in accordance with paragraph C. of AD 94-01-04 Docket No. 93- NM-68-AD; Amendment 39-8786. If there are any further question, please contact Mr. Abby Malmir at (310) 988-5351. Sincerely, ,‘ 7-/f r"—w.-c, - • Alan T. Shinseki Manager, Systems and Equipment Branch Lt.?: • , . • 4. .4, a_ • o • 7, • • F.-; 1 tt • _s=2 --tze;&,,,„6.smru.lua • ‘.. EFTA00277832 T. •MAKT:2131115; ;;„.(4(.1114 110124AST 33114W. TIARanZA,. "i'40 PPIT ;:•INI.751"A • .2.:1317T4A. • 1'.47Utr; °Muni! tatt • 4.1 , . . . Aflinirrlie3-:4(jkls ?./.1 ria3Dre)Ctritni moitctiyA -•• tr;nriTtz:nia.;:.71.. •• ¢. :iii. I f r. •C tr-H IQ ( iS) .1. . •7;4 ;1.110;4 111.1f: •t.Stfija.r.nosNA :; '-;Co'3110;:i• f ••••vivetno!f ;I • •.• r ±rib tioa t r•I ; V:• • •j:• ;. 0 i2 •• C• ••'• -ray • 0`;) s..1100::f. • • t • • TV.4q AO gr 5:00a tau? -Of0600:2W4 11::4N.3ro10 6 :golzssiVriorpiiii)21-415.1 ry thri/cOla0M/Vie-.0103Y214;;69-,,V7Ap cOM. • • . - 3f.lsifun -iec . v !mg Fiu6. ztriu.i.tboini•Ina. Itorifee,pr ;$35:30v.../31-; M0rfIce.):::)c, aiNz-fsc-oluaboA, ;10tio(J.j10--!.4.7-411i) Olt, 1.15 ,‘.1 •dirriEti-NrAz 'i.:}•zi's.;v1 71' • f. • • .. ft Ottieit* •'i$ 4-8a4;;;: ti •••••1'" • • zfff.:15.2.v.2 *i.ert,;%tr,;. EFTA00277833 I FAA AIRCRAFT REGISTRY CAMERA NO. 3 DATE: y1/4y/f5— • ;: 4 • . .4/ ?•:' , . . C • „ ra ' grakehigko& ..1 . • • t ' :••••••• 1.1... • '-'•• • • • • . • • • • eN1 I It/ •/. • . • ,• . AIRWORTHINESS DIRECTiVE FUGHT STANDARDS SERVICE REGULATORY SUPPORT OMSION P.O. BOX 26460 OICLAHOMA a-ne, OKLAHOMA 73125-0460 ; " ' ' • .• . • 't • • • - . • . • . • ' • , • . • • U.S. Depastrberd of Transpottation •, Federal Aviation Administration Th• Icameno te....,en••• Cara Sued by ea Fa A.td.r asatinieteent Si esimmes eel the eieplise• et reimnd flecsiodoaa east a *Plan a skint "sal d ..'" as " air ". ioulloos you Nonni' •441•Ianal Asinswrearts Pao a _it. sCs sod SO Picamlbale gnat fora losallcOm areka Yom •••• •••••caml RS re p.•. , wary tarn Si sistrellIntioli M Alrailla Oat* sp apasame Ilinseraren 01realre ••••••••S •...bomet 3•1.4. 04-01-04 HONEYWELL: Amendment 39-87843. Docket 93-NM-68-AD. Applicability: Traffic Alert and Collision Avoidance System (TCAS) II computer units; part numbers 4066010-901, -902. and -903; as installed on. but not hatted to, the following almlancs. certificated in any category: Airbus Industrie Model A300-4300. A310-200. A310-300. A320-200. and A340 'scales airplanes: Boeing Model .727-100 and -200: 737-100. -200. -300. -400. and -500: 747-100. -200. -300. -400 and 747SP; 757-200; and 767-200 and -300 series airplanes: Cessna Citation Model C550 and C560 series airplanes. and Cessna Citation III and. VII 1 • series airplanes: Canadair Challenger Model CL-600-2B16 and -2Al2 series airplanes: iJ I British Aerospace Model 125-800A: Gulf:stream Model Gil, GLIB. GIII. and GIV series airplanes- Lockheed Model L-1011 series airplanes; McDonnell Douglas Model DC-9-10, -20, -30-, -40, and -50; DC-10-10, -15..30. and -444 ;It s MD-11: and DC-9-80 series alrplazics; and Model MD-88 airplanes: . Dassault AV/S.111On Model Mystcre-Falcon 50 and 900 series airplanes; • Short Brothers Model 503-60 series airplanes; de Havilland Model DHC-8-100 and DHC-7 series airplanes: ' •Ri • '-; I .011 • Fokker Model F27 series airplanes; and Corporate Jets limited Model BAe 125-800A and EiAc 125-1000A series airplanes. A • s' • -1 2.0"4, Compliance: Required as indicated, unless accomplished previously. To prevent collisions or near misses caused by incompatibility between the TCAS II processors and the current air traffic control system. accomplish the {allowing: (a) Before December 31. 1994, accomplLsh the requirements of paragraphs • (aiel ) +and (aX2) of this AD in acconiance with Honctywell Service Bulletin 4066010-34-S*16. -dated December 20, 1993. • ' (1$ Remove existing Honeywell TCAS U computer units, part numbers 4066010-901, -902, and -903, and replace those units with new units that incorporate updated collision avoidance system (CAS) logic, identified as Version 6.04A in Mitre letter F046-L-0069.i, 1 dated September 21, 1993. (2) Modify the computer surveillance logic on Honeywell TCAS U computer united r.t. part numbers 4068010-901, -902, and -903, to ensure that these units accommodate Mode C altitude input of 100-foot Increments and that the system will be tracked and coordinated by Intruding aircraft when the Mode S transponder CA field Ls set at CA.7. • • (b) WPrior. to further -after accomplishing the requirements- of paragrapir (al- of tidal? AD.—revise the Airplane-. Flight Mniiunl (AIM) :AFM- SupiiIement by • either .+ paragraph (bXI) or (bX2) of this AD; (1) Revise the Normal Procedures Section of the AFM to include the aP13ropriate TCAS operating characteristic relative to the modifications required by paragraph (a) of this AD, in accordance with a method approved by the Manager. Los Angeles Aircraft Certification Office (ACO). FAA. Transport Airplane Directorate. Or (2) - Revise the Normal Procedures Section of the AIM. to Include the following! TCAS operating characteristic relative to the modification required by paragraph (a) of this AD. This may be accomplished by Inserting a-copy of this AD in the AFM or AFM Supplement::7 I! ' • • •• • •!• • et: ,. ere_ 4,4, fr • • ,': a,. 4 -• • 41 • • . 1.e :4i .• ' • • • • • • • • -••! ! - . • • • 0' , • , . • .• • . .• •• • 3 • T. . . . 'Ijk• 4.-0: 41'•;•-• • jsr, k.••;.Att4 7‘.• • EFTA00277834 FAA AIRCRAFT REGISTRY CAMERA NO. 3 - DATE: -y/r/i 2 94:0144 'All Resolution Advisory (RA) and Traffic Advisory CM) aural messages am ' • inhibited at a radio altitude of less than 1.100 feet above ground level (AGL) climbing. and less than 900 fed AGL descending t of the corap .' (c) An alterrtattve method of compliance or adjustmen liance time that provides an acceptable level of safety may be used if approved by the Nianager. Los Angeles Aircraft Certification Office (AC01. FAA. Transport Airplane Directorate. Operators shall submit their • requests through an appropriate FAA Principal Avionics. Inspector. who may add comments and then send it to the Maruager. Los Angeles ACO. • . NOTE: Information txtncerning the existence of approved alternative methods of compliance with this AD. if any. may be obtained from the Los Angeles ACO. (d) Special flight permits may be issued In accordance with FAR 21.197 and 21.199 to operate the airplane to a location whore the requirements of this AD can be a.coomplistux:L (e) The replacement and modification shall be done in accordance with Honeywell Service Bulletin 4066010-34-SW16, dated December 20. 1993. This incorporation by reference was approved by the Director of eel Federal Register in accordance with 5 U.S.C. 5.52(a) and 1 CFR Part 51. Copies may be obtained from Honeywell Inc-. Commercial 14-light Systems Group, Ar . Transport Systems Division. P.O. Box 21111. Phoenix. Arizona asoss. Copies may be inspected the FAA. Traiasport Airplane Directorate. 1601 [led Avenue, SW., Renton. Washington: at the FAA. Transport Airplane Directorate. Los Angeles Aircraft Certification Office_ 3229 ,East Spring Street. • Long Beach. California; or at the Office of the Federal Registers 800 North Capitol Street NW.. suite 700. Washington. DC. (f) This amendment becomes effective on February 4. W94. FOR FURTHER INFORMATION CONTACT: ' . .. Abby Nialn Aerospace ErIginCer. Systems and Equipment Branch. AMA-13216. FAA. Transport Airplane Directorate, Los Angeles Aircraft Certification Office, 3229 East Spring Street. Long Beach. California 90806-2425; telephone (310) 988-5-%51; fax (310) 988-5210. Aircraft Flights Date ode No. Aircraft/APU Hours GI GII Gilt GIV NOT APPLICABLE COMPLIED WITH • -• - DEFERRED UNTIL,. - E ABOVE ITEM IS DUE ON LEASE COMPLETE THIS FORM AND SEND IT IN WHEN THE ITEM IS COMPLIED WITHH. . 5 t..it 1 _ :t ; ::::::15.:ir.ii t'.' I.'111.1: L:,l, .“.• v u: .ti—', 1..1:;.! sc. ',.t.:: :1-.;z:-...'„•7, .i:.ti t:.r: 1.1:e'iilii:t2,'.;. Z:5 4.2,,t z .. tr:/5?:.) a JSOlil.Diltritt:1 J)trird f"!. :1••7••11,. ii:).3 . , . t;?7)v; U•1 Vi T.: '..1 -... i>ttioft I. •.); • , ,_Ali f" r. tit 1, cp :341:le 01 troll. :1;g-iFl. Itro .Jr. : 1 silt t• ....Lc.), : • • t •., . , •.- • . : rnr.. . • liwez • tti : ••-oh• +34K Mr?. (*--.11,11 ae: _101.?1:.0:11X.11.9 I CA ,;1117):"1 r.Pikr.t.:1"1::!t-strb r • • f. •t: Cr. 'grit 'to vr it .; ;,• matht• tztt 13•;71-.:tqrtr., •. tv: C:Uq• , a -an Onftilwls EFTA00277835 -FAA AIRCRAFT REGISTRY CAMERA NO. i it/ DATE: /0 -1R-94 • ( •••••• ••••• •1 it .7! 1 r a MAJOR REPAIR AND ALTERATION • Form Approved OMB No. 2120-0020 For FAA Use Only us Department nr frolsooncmcn . (Airframe, Powerplant, Propeller, or Appliance) riderdAriation , - AdrintenstIon (1)ffiC.Alrang.0-15 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make BOEING Model 727-31 Serial No. 20115 Nationality and Registration Mark NSOOLS 2. Owner Name (As shown on registration certificate) NORTHWEST HOLDING CORP. Address (As shown on registration certificate) 1105 N. MARKET STREET WILMINGTON, DE 19899 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item 1 above) X POWERPLANT • N PROPELLER . I. APPLANCE Type Manufacturer 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. PAGE AVJET CORPORATION 9809 TRADEPORT DRIVE ORLANDO, FLORIDA 32827 U.S. Certificated Mechanic 0S4R425M Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the un't(s) identified in item 4 above and described_on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S Federal Avia egulati and t information furnished herein is true and correct to the best of my knowledge. Date Signature of Authorized Indi dual t2. 056-4-17 /996/- • 7. Approval for Return To Service Pt. suer: to the authority given persons specified below, the unit identified in item 4 was' inspected in the manner prescribed by the F...rnrhistrator of the Federal Aviation Administration and is at APPROVED O REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Canada Ai rthiness Group Date of Ap royal o Refection Certificate or . Signatur Aril Authorized ivid 9 Ii-r/ CO g 2 -4 Designatior• No. 0S4R425M Affte/ 709,1) / Ati ti . ...t-C4-7.---7.-. FAA 'Form 3 1t2.88) A • • No ......Viecte •PC e l :ki t 14;: a aA11 1 ttii4Ty "rot. Aff:1,,a frft tP , - Ina Or ;et. •. , • EFTA00277836 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations,to assure continued conformity with the applicable airworthiness requitements. • 8. Description of Work Accomplished . (If more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed:) . . . 1. INSTALLED A DORNE & MARGOLIN EMERGENCY LOCATION TRANSMITTER (ELT) SYSTEM IN ACCORDANCE WITH PAGE AVJET REPORT PR -91-22 REV. A, DATED 8/15/94 AND MDL- 91-02 REV. B, DATED 8/10/94 AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339, DATED AUGUST 16, 1994.. PROVIDED WEIGHT & BALANCE UPDATE. EQUIPMENT LIST UPDATED ACCORDINGLY. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OTHER SYSTEMS. ALL PERTINET DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION 0S4R425M UNDER WORK ORDER 60298, DATED SEPTEMBER 2, 1994. . . . . . . . . . ••• ;:ot ; •• .1 :1; . • • EFTA00277837 e -FAA AIRCRAFT REGISTRY CAMERA N0.3k DATE: /0-/a- *L____ 4".• MAJOR REPAIR AND ALTERATION wspepartnem . of Tronspc- - or . (Airframe, Powerptant, Propeller, or Appliance) fekleterof A;dorkan Adnitrekstration Form Approved OMB No. 2120-0020 For FAA Use Only ittro_ 15 OfficeAtyf INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAB 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality and Registration Mark N500LS Z. Owner Name (As shown on registration certificate) NORTHWEST HOLDING CORP. Address (As shown on registration certificate) . 1105 N. Market Street Wilmington, DE 19899 3. For FAA Use Ority 4. Unit Identification .5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME • .....~..................~..ww.... (As described in Item 1 above) X POWERPLANT PROPELLER ' APPLIANCE Type Manufacturer 6. Conformity Statement C. A. Agency's Name and Address B. Kind of Agency Certificate No. Page Avjet Corporation 9809 Tradeport Drive Orlando, Florida 32827 U.S. Certificated Mechanic OS4R425M Fore.gn Certificated Mechanic Cer,iticaled Repair Station Manufacturer D. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above have been made in accordance with the requirements of Part 43 of the U.S. Federa furnished herein is true and correct to the best of my knciwiedge. er everse or attachments hereto d that the i ation and descri on t Aviatio egulations Date £ SEPT-6496E-2:- 1993/4 7. Approval Signature of Authorized Individ I 06g/ere-L-4 - for Return To Service -3491(C) - by the Pu Administrator BY suant to the authority of the Federal given Aviation X persons specified below, the unit identified in item 4 was inspect in the manner prescribed Administration and is IX APPROVED O REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Person Canada Other (Specify) Authorization Fl" FAA Designee Repair Station Approved by Transport orthiness Group Date of Approval or Rejection 2 SEPT: 9 1/ Certificate or Designation No. OS4R425M Signet of Author d Ind ual al -4y .,Sgy te.___CgotoPtiztrA,1 ) ere—ter:7r EFTA00277838 -FAA AIRCRAFT REGISTRY CAMERA N0.3,V DATE: joria rJyC - NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An altelation must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. • . • . 8.- Inscription of Work Accomplished . (If more space is required,,attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) .- • . 727-31 S/N 20115 N500LS REPAIRED CORROSION ON THE LOWER FORWARD CORNER OF THE AFT CARGO DOOR BEAR STRAP IN ACCORDANCE WITH PAGE AVJET E.O. NO. 53-30- 02838 DATED 8/11/94 AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339/ DATED AUGUST 22, 1994. 2. REPAIRED DOUBLE DRILLED HOLES IN B.S. 940 MOD KIT'BRACKET IN ACCORDANCE WITH PAGE AVJET -E.O. NO. 53-10-02839 DATED 8/10/94 AND APPROVED PER'8110-3 BY DFR MARION SHIN, SO-339 DATED AUGUST 22, • 1994. SUMMARY: 1. ALL PERTINENT DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION OS4R425M TINDER WORK ORDER 60298, DATED • • • • g • • • .• END .. • . • E. - • .t: :•• "P- • '•`- ;•• :de. • ! . r • . • . 1 0 .• I. 4O; • . . • . • k • • - •• • 1:‘'? D Additional Sheets AreAttniched • 4 • ,-•“Iffet•t. .U.S GP0:1991.0-S8&012140035 • EFTA00277839 i -FAA AIRCRAFT REGISTRY CAmFRA N.i. :A/ DATE: 1O-1a- *it fi • ., • z, MAJOR REPAIR AND ALTERATION lis Department cc tronsocconon (Airframe, Powerplant, Propeller, or Appliance) Fedora Aviation Admintoanion Form Approved OMB No. 2120-0020 For FAA Use OTh offiASIOrtESDO INSTRUCTIONS. Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-31 Serial No. 20115 Nationality and Reg .lion Mark 00LS 2. Owner Name (As shown on registration certificate) NORTHWEST HOLDING CORP. Address (t i so_ivn on registration certificate) 5 N. Market Street Wilmington, DE 19899 3. For FAA Use Only 4. Unit identification 5. Type Unit Make Model Serial No. Repair Alteration AIRFRAME (As described in Item I above) ---- X POWERPLANT PROPELLER 1/4 APPLIANCE Type 4 Manufacturer . 6..Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Page Avjet Corporation 9809 Tradeport Drive Orlando, Florida 32827 U.S. Certificated Mechanic OS4R425M Fo-eign Certificated Mechanic • X Certilicated Repair Station Manulecturer D. I certify that the repair and/or alteration made to the un t(s) identified in item 4 above and described have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviatio furnished herein is true and correct to the best of my knowledge. on the reverse or attachments and that the inf hereto . ation t gulatt Date (2, S EPrE/Y)8Et /99 SZ Signature of Authorized Inc:livid ,ial 744a 7. Approval for Return To Service Pu Administrator BY suant to the authority of the Federal given Aviation persons specified below, the unit identified in item 4 was inspected Administration and is ' . g1 APPROVED LI REJECTED in the manner prescribed by the ..._ FAA Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FAA Designee X Repair Station Person Approved by Transport Canada • • orthiness Group Date of Approval or Rejection W 9' Certificate or Designation No. OS4R425M Signal . of Authorize ndivid Ccht; ge-4/ itfin At) ,----> /Wirfi ../A—,---A--; FAA Form 337 it2.ettn • l• • • I -- • • EFTA00277840 - PAA Al.cICRAFT REGISTRY CAMERA ?il DATE; . NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more spaco is required. attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) 727-31 S/N 20115 N500LS 1. RELOCATED ACCESS PANEL FROM B.S. 1183 TO B.S. 1350 LH AND RH BETWEEN STRINGERS S4 TO 57 IN ORDER TO FACILITATE ACCESS FOR FREQUENT INSPECTION TO TERMINAL FITTING IN ACCORDANCE WITH PAGE AVJET E.O- NO. 53-30-02837 DATED 7t'28/94 AND APPROVED PER 8110-3 BY DER MARION SHIN, SO-339 DATED AUGUST 22, 1994. SUMMARY; 1. ALL PERTINENT DETAILS OF WORK ACCOMPLISHED ARE ON FILE AT THIS REPAIR STATION OS4R425M UNDER WORK ORDER 60298, DATED 2.8,EPT934 • --3-END K Additional Shoots Aro Attached • • • • • . ..... . • . — . . . • • - • • . . • • • • • • • • • * U.S.GPO:1 9 91-0-568-01 2/4003 5 EFTA00277841 FAA AIRCRAFT REGISTRY CAMERA NO, DATE: 0-1 93 - 0 MAJOR REPAIR AND ALTERATION Form Approved OMB No. 2120-9020 us Deporrmtt Appliance) For FAA Use Only erifonteconeon (Airframe, Powerplant, Propeller, or Feigned Aylation Administration Office Identification S0-FS00.15 INSTRUCTIONS: Print ortype all entries. See FAR 43.9, FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disp osition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 91 00O for each such violation (Section 901 Federal Aviation Act of 1958). Make Boeing Model 727-31 1.' Aircraft Serial No. 20115 Nationality and Registration Mark NSOOLS 2 Owner Name (As shown on registration certificate) .,. NORTHWEST HOLDING CORP. Address (As shown on registration certificate) 1105 N. Market Street Wilmington, DE 19899 3. For FAA Use Only 4. Unit Identification 5. Type Unit Make I Model Serial No. Repair Alteration AIRFRAME (At described in Item I above) X . POWERPLANT , PROPELLER APPLIANCE Type ' Manufacturer • 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Page Avjet Corporation U.S. Certificated Mechanic 9809 Tradeport Drive Foreign Certificated Mechanic 0S4R425M Orlando, FL 32827 Certificated Repair Station _X Manufacturer D. I certify that the repair and/or alteration made to the un t(s) identified in gem 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and tat the information furnished heroin is true and correct to the best of my knowledge. • Date Signature uth•rized Individual 4 ,, f7/45, -1/ V. 4:09.e.c..v/ • itict.5/1.5 e.7.4.e.u,. 7. A for Rota • Service Pu suant to the authority given persons specified below, the unit, identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is R.) APPROVED O REJECTED FAA Flt. Standards Inspector Manufacturer Inspection Authorization Other (Specify) - BY FAA Designee x Repair Station Person Approved by Transport Canada Ayryrorthiness Group Date of Approval or Rejection r c2S- ? 3 Certificate or Designation No. 0S411425M • SIgnatu e'of Authorized Individual 7 2/CAAin ‘f/ey / .1• go")/e,enwr EFTA00277842 PAA AIRCRAFT REGISTRY CAMERA NO. 1 DATE: //'/- 93 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatibli with all previous alterations to assure continued conformity with the applicable airworthiness requirements. ?f-PLIZI 8. Description of W rk Accomplished ; (If more space is required, attach additional sheets. Identity with aircraft nationality-and registration mark and date work completed.) • B727-31 -N5OOLS I. INSTALLED HONEYWELL TCA8i,II SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3094S0. SUMMARY: 1 AIRCRAFT WEIGHT AND BALANCE UPDATED ACCORDINGLY. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. ALL SYSTEMS INSTALLED OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. • 4. ALL ENGINEERING AND WORK ACCOMPLISHED AT PAGE AVJET C_ORPORATI.ON_ REPAIR STATION UNDER WORK ORDERS 7492, 8112 AND 9301. 5. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. . • • I:0: .".: • ; . . ; .• • , is tlr,ill Ic, : 1"i • •: • . . . • . .„ . i•;.••-gz.:,••••6 f• ..,:,-, • \ - ' • ‘‘ I • .i,:f l t .',!,, • \;:!".::.. ''‘‘. .. . ...ft..... .......:......,. ...!. ... ../...... ......! .: 30....:...a...... --.....-- ......-- .); nth:A I 1'. .. .• ::12.1::4 l'c . • . • :. '...:7 Pi l'n .:),Pil..n. .6 .v i :n • j 1.1 t."-I:el• •I ...•.1 •)r•si sz.:•:-..! ;,:l. • .1.: rn:;..t...; it-p.i.j •,:. '141.2....10./I 1 . 0 .r. Oil is.: 1!-I .t: P. -. ••• 0.!.. .. ..t.k;ft •-...::.,,,•.• ... nt,.41,9:.:t) • • . . !. i i ..: . 2.,,LA.••• ''.. .: '' ‘1% ; • rtNi,.:xlIzi.14,A rioibo.lardi I .. ...);,74 gg.i-• . . ... • I I I,. c.:;.;,.- i,' : d ' . •';'.".i.,.A rtoe'll..li .....k: , ......:.i„f.: ,i,...)...4•; • • ..1 •:. .t.,.:••••:; ct 1: .\ . ,ivt:./i •.: ...::::,,..e.A .. .,....„ ., • . k • M. .' . . • %. i . \ littif..'11:110 i. ..•-.;ri‘t .1 •;%•..•••.71r>.k., 4) ..'‘, l• .;, .. . \. ." . t:'• . . . . . `t . e• • • •‘‘' , `,. i ..... . ''.• . - O •Addllional.Sheiti Are Attiched ...,:2i:-.;..:c!.;.. ; . • . a" ..":•; l d • ' • . • .. • *U.S. GOVERNMENT PRINTING OFFICE: 1892-719-012/60157' EFTA00277843 V. FAA AIRCRAFT REGISTRY CAMERA NO. 5r4DATES P - 4 - 9a • e• - t • . 1 .• • •• • ". .. e•-t • • I r r• • d . • .. . '• • - • 1 • • . .MAJOR REPAIR ANDcr ALTERATION OS Depot imeni ,• ei bcnseorioi.on (Airframe, Powerplanl, Propeller, or Appliance) ' . . ....Aviation Administronon Form Approved OMB No. 2120-0020 For FAA Use Only Office Identilithoysli o is INSTRUCT IONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix Band AC 43.9-1 (or subsequent revision thereof) for instructions and disposition ol this form. This report is required by law (49 U.S.C. 1421). Failure to report can result In a civil penalty not to exceed $1.000 • for each such violation (Section 901 Federel.Aviation Act of 1958). 1. Aircraft Make Boeing Model 727-31 Serial No. , 20115 Nationality and Registration Mark N500LS 2. Owner • Name (As shown on registration certificate) - i= i Northwest Holding Corporation Address (As shown on registration certificate) . • P.O. Box 7138 Wilmington, DE 19803 3. For FAA Use Only ' . _ • • 4. Unit Identification 5. Type Unit Make Model Serial No. Repair • r Alteration • AIRFRAME (As described In Item I above) ' ' • X POWERPLANT PROPELLER . APPLIANCE - 1 ype .r., ‘ i - • - , • Maimlaciui ei 6. Conformity Statement A Agen!.....y's Name mid Address Avje't Couporalion Trade-TWA_ Florida h int ilicieravi .milk). hem, mom: rk it, „woo, rivrem is um: 4 L11.2 9_12_5.+ . B. Kind ol Agency --. C. Certi icate No. • Page 9809 Orlando. D I 'Aoki) !ed..; umrushed • I !hire 3- 1 . - I/ Wive i, arlij lac 32827 - - X U s Certificated Mechanic I . 0S4R425M Furin9it Certificated Mechanic Certificated Repair Station Meintilacturer .. oil...Limon made to the ini i(s) identified in item 4 above arid described on the reverse or attachments-hereto, e with the requiremoids of Part 43 ol the U S Federal Aviation Regulations and that the Information ‘Ollad W the best ol my knowledge. ' • 22 Signature (---- ol Auth i d Individual 4 AMC,4 : 447 .90 --- 7 Pursuant AdillitirSilaWl UY ..... — . to lily at/Viunty Ul the I tide' di ••• ". - I AA I. It Sidnjoids inspector FAA Desynee ii.er A.I.Illuil • • X 7. Aoki:oval for Return To Service tau auirs specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administration and is • El •APPROVED 0 REJECTED MoilltlidditilUI ' Inspection Authorization Other (Specify) • . ' , . _ itemui Station Pelson Approved by Transport Canada Airworthiness Group Date ul Ai provid or illittClivil 2) Luc ' 4( 5 t . OS) Gelilk:Me or Designation No. OS411425M Signature of Authorized Individual .. a_a i 4 dLictzlz - n - . - f s 4 vth g tstrima' "• I" • EFTA00277844 • • FAA AIRCRAFT REGISTRY . • CAMERA ND. 3 AiDATE. // 70 - 9a • • • . . .. • lir.. . • • ". : • • • NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with (he applicable airworthiness requirements. 8. peeccIplion of Accomplished 1 firmara japcali required. attach additional sheets. Identity with aircraft nationality and registration mark and dale work completed.) D727-31 5/N 20115 • N500LS 1. MODIFIED SECOND BATTERY SYSTEM PER PAGE .AVJET CORPORATION- STC SA3092SO, MASTER DRAWING LIST MDL-91-371 REV. A. 2. MODIFIED ED44-805 EFIS PER PAGE-AVJET CORPORATION STC SA3085SO, MASTER DRAWING LIST MDL-91-44, REV. A. 3. MODIFIED FMS-800 FLIGHT MANAGEMENT SYSTEM PER PAGE AVJET CORPORATION STC SA3089S0, MASTER DRAWING LIST MDL-91-43, REV. A (NZ-9112 SOFTWARE). SUMMARY: 1. PROVIDED WEIGHT AND BALANCE UPDATE. 2. EQUIPMENT LIST UPDATED ACCORDINGLY. el 3. ALL SYSTEMS OPS CHECKED AND DO NOT INTERFERE WITH OTHER SYSTEMS. 4. ALL PERTINENT DETAILS,Or% WORK ACCOMPLISHED ARE ON FILE AT PAGE AVJET CORPORATION UNDER WORK ORDER 9286, DATED AUGUST 31, 1992. • END • 0 ••••••••• •• • i • . • • _ . • - - • . . • • - • - , • . ! ! . . : t. • • rt..; A II • • • • ••••• .• ••• • . . . • • I r • '• • • • • • K Additional SheetiAre Attached • • • 411Serirt- OrOnMalal • - • i EFTA00277845 FAA AIRCRAFT ' CAMERA NO. bi DATE: th _ Qom, • t. • . 0 • MAJOR REPAIR AND ALTERATION ' usorpcsimens cr Ircesoorvorm (Airframe, Powerplant, Propeller, or Appliance) redone Aviation ediminisfrotion Form Approved -6020 OMB No. 2120 For FAA Use Only Office IdentWcation 30-f300-15 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR.43 Apkndix B. and AC43.9-1 (or subsequent revision thereof) for instructions and dispoiition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). 1 1. Aircraft I Make Boeing Model 727-31 • Serial-No: Nationality and Registration Mark N500LS 1• 20115 2. Owner Name (As shown on registration certiiicafe). Northwest'Holding Corporation Address (As shown on registration certificate) P.O._ Box 7138 • •• . ' Wilmington, DE 19803'" . 3. For FAA Use Only . si. • . • , ..• , . . 4. Unit Identification 5. Type Unit Make ?. • " Model . * Serial No. Repair • Alteration AIRFRAME • • • ..--- - (As described in Item 1 above) ' X _ . • POWERPLANT • • . " PROPELLER , • - APPLIANCE Type • • , • Manufacturer . 8. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Page Av jet Corporation 9809 Tradeport Drive Orlando/ Florida 32827 U.S. Certilicaled Mechanic OS4R425M. - Foreign Certificated Mechanic X Certificated Repair Station Manufacturer D. I certify that the repair and/or alteration made to the un I(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S Federal Aviation Regulations and that the information - furnished herein is true and correct to the best of my knowledge. Date • 2 Signature • A izer :' idu J O i-f r ) It: 14 Lt, ire (\.) 4- !Return 7. 'Approv To Service Pursuer I to the authority given persons specIlled below. th nit identified in item 4 was inspected in the manner prescribed by the Administi ator of the Federal Aviation Administration and is KI APPROVED O REJECTED FAA Fli Standards Inspector Manufacturer Inspection Authorization Other (Specify) BY FAA Designee X Repair Station Person Approved by Transport Canada Airworthiness Group . Date of Approval or Rejection Zs JAL) i 5 Certificate or Designation No. OS4B425N_ SI enure of Authorized Indi dual . alt() . .hil-U/1) H L-Fr1 nil tqa--- PAA'Form 317 II; net - ••• I EFTA00277846 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. & Description of Work Accomplished • Of more space Is required, attach additional sheets. Identify with aircraft nationality and registration mark end date work completed.) INSTALLED SUNDSTRAND MARK VII WINDSHEAR DETECTION/GROUND PROXIMITY WARNING SYSTEM (GPWS) IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3133SO. ALL WORK ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION AND IS ON FILE UNDER WORK ORDERS 4784 AND 8112. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. 003.4122044. EFTA00277847 FAA AIRCRAFT REGISTRY CAMERA NO. IN DATE: — q 9v2 - 'tar ••• • • ere CO REPAIR AND ALTERATION ..• Form Approved OMB No. 2120-0020 MAJOR USE/ewer:erg For FAA Use Only okinfosnorym (Airframe, Powerplant, Propeller, or Appliance) Federal AvIcalcin Acentrkstratton Office Identification so--Fs110-15 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix El, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51,000 for each such violation (Section 901 Federal Aviation Act of 1958). Make Boeing Model 727-31 1. Aircraft Serial No. 20115_ Nationality and Registration Mark • N500LS • 2. Owner Name (As shown on registration certificate) • Northwest Holding Corporation Address (As shown on registration certificate) • P.O. ! Box 7138—_!... .: Wilmington, DE 19803 3. For FAA Use Only . • C. , ... • . • . . 4. Unit Identification S. Type Unit Make • Model Serial No. Repair Alteration AIRFRAME ' - (As described in Item I above) .- . a X POWERPLANT PROPELLER . % APPLIANCE Type Manufacturer • • • 8. Conformity Statement A. Agency's Name and Audi ess B. Kind of Agency C. Certificate No. • • U S Cerlilicatee Mechanic Page Avjet Corporation Ft:feign Certificated Mechanic :1 ' 9809 Tradeport Drive X Ceitilicated Repair Station OS4R42514 OrlandoL_Florida 32827 Manulacluier D. I certily that the repair and/or alteration made to the un have been made in accordance with the requirements furnished herein is true and cot rect to the best orsity knowledge. t(s) identified in item 4 above and described on the reverse or attachments hereto of Part 43 of the U.S Federal Aviation Regulations and that the information Date • I ?9r? Signature of Authorized Individual i4Afral.5 r. Writ* Jr. 7. A r I for Return To Service Pu suat I to the authority given peMbna specified below, the unit identified in item 4 was inspected In the manner prescribed by the Administrator of the Fedora) Aviation Administration and is 09 APPROVED O REJECTED FAA Fit Standards Inspector Manufacturer Inspection Authorization Other (Specify) i BY FAA Designee X Repair Station . Person Approved by Transport Canada Airworthiness Group Date of Approval or Rejection a0D. 3,ti-r) fici a Certificate or Designation No. QS4R4a5EL Sigr lure of Authorized Individual • it er:.6.4 Ds v11) bi 2.417/472#2 inn rum, 337 I I,girt c- • • II • ir • EFTA00277848 FAA AIRCRAFT ' CAMERA NO. /A./ DATE: 6 ) _q_ • i NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. Desalpilcin-otWolfaccomplished (If more space is required, attach additional sheets. Identity with aircraft nationality and registration mark and date work completed.) 0727 -31, $/N 20115 1: INSTALLED,EXECUTIVE'INTERIOR.IN.ACCORDANCE.WITH.PAGE AVJET CORPO RATION.STC.SA3137S0. 2. INSTALLED HONEYWELL EDZ-805 ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS) IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3085S0. 3. INSTALLED MODE "S" TRANSPONDER IN ACCORDANCE WITH PAGE AVJET CORPORATION' STC SA3095S0. 4. INSTALLED JAMCO SMOKE DETECTORS IN ACCORDANCE WITH PAGE-AVJET CORPORATION STC SA3132S0. 5. INSTALLED DUAL HONEYWELL AA-300 RADIO ALTIMETER SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3087S0. 6. 'INSTALLED HONEYWELL PRIMUS 870 RADAR SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3086S0. 7,. INSTALLED HONEYWELL FMZ-B00 FLIGHT MANAGEMENT SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3089S0. 8. INSTALLED DUAL COLLINS PROLINE II COMMUNICATION AND NAVIGATION SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3090S0. 9.. INSTALLED HONEYWELL TCAS II SYSTEM PROVISIONS IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3094S0. 10. RELOCATED FIRE "T" HANDLES IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3111S0. 11. INSTALLED FAIRCHILD II PARAMETER FLIGHT DATA RECORDER IN ACCORDANCE WITH'PAGE AVJET CORPORATION STC SA3091S0. 12. INSTALLED DUAL 40 AMP HR NICKEL CADMIUM BATTERY SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3092S0. 13. INSTALLED DUAL HONEYWELL ADZ-800 DIGITAL AIR DATA SYSTEM IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3088S0. 14. INSTALLED AES AUTOPILOT INTERFACE UNIT IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3093S0. El Additional Sheets Are Attached • *U.S.OP0:1989 a 803•17t O • EFTA00277849 FAA AIRCRAFT REGISTRY CAMERA NO. At • .DATE:' - PAGE 3 OF 3 - . • . INSTALLED HYDRAULIC ACOUSTICAL FILTER IN ACCORDANCE WITH PAGE AVJET CORPORATION STC SA3136S0. . INSTALLED ESSENTIAL POWER SELECTION SYSTEM IN ACCORDANCE WITH .PAGE AVJET CORPORATION STC SA259(T!:. SUMMARY: 1. AIRCRAFT WEIGHED AND NEW WEIGHT AND BALANCE COMPUTED. 2. .'EQUIPMENT FURNISHING LIST UPDATED ACCORDINGLY. 3. ALL SYSTEMS INSTALLED. OPERATIONALLY CHECKED AND DO NOT INTERFERE WITH ANY OTHER SYSTEMS. 4. ALL WORK ACCOMPLISHED AT PAGE AVJET CORPORATION REPAIR STATION AND IS ON FILE UNDER WORK ORDERS 4784 AND 8112. , . 5. AIRCRAFT. TEST FLOWN BY CUSTOMER AND ALL SYSTEMS CHECKED NORMAL. 6. AIRCRAFT TEST FLOWN BY FAA FLIGHT TEST ACO ATLANTA. ALL SYSTEMS CHECKED NORMAL. ALL WORK ACCOMPLISHED IN ACCORDANCE WITH APPLICABLE DATA. END 0010404411'. 77,77:,.1....4;b, . • EFTA00277850 4. 41wartentwasintemam - • • W Sta . , ~~rt1ZR EFTA00277851 • FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 91 0 ' . • APPLICATION FOR US Derainlent AIRWORTHINESS or Trompoisoico • Federal Motion 500 L-9 CERTIFICATE Admirilownion -,• • . • • INSTRUCTIONS —Print or type. Do not write in shaded areas; these are for FAA use only. Submit original only lo an authorized FAA Representative. II additional space is required. use an attachment. For special flight permils complete SeCtiOns II and VI or VII as applicable. Z t 0 it 1.REGISTRATI immt • N Sb St 2.AIRCRAFT BUILDERS NAME (Make? 'Bo et IQ 6- • e .. 1 3. AIRCRAFT MODEL DESIGNATION -61 '... 3 I . - 4. YR. MFR /96/ r FAA CITING 3 F Vo / o 5 C' cc u .., . — Ma 5. AIRCRAF • a 0 iis- 6. NGINE BUILDER S AME (P.LiAw effint iiimey 7:3ge/ /TEL Dc.CeTIOtria$0 ,17-3 b - c3-19C Carta C OR C53 0 / 6. NUMBER OF ENGINES 9. PROPEL/En BUIL LA S NAME /Maker 4, vi 10. PROPELLER MODEL r cIGNATION 11. AIRCRAFT IS rChecA ii app4seaDiel :4 . A/ 4- iv i IMPORT a APPLICATION IS HEREBY MADE FOR: (Check andfiCable 4lenisl A i X STANDARD AIRWORTHINESS CERTIFICATE !Indicate category) I !NORMAL I [UTILITY I I ACROBATICD1(1 TRANSPORT I [GLIDER I [ BALLOON • B SPECIAL AIRWORTHINESS CERTIFICATE (Chock appropriate ?Semi? 2 . . LIMiTE05, o 'Ai 5 ai PROVISIONAL 1 CLASS I s. Widmer. Clan; q i3 O CLASS W 1 AGRICULTURE AND PEST CONTROL 2 AERIAL SURVEYING 3 AERIAL ADVERTISING cc Z 3 RESTRICTED fIndoCale OporatiONS r 10 be conducted; 4 FOREST; Wildlife conservflione s PATROLLING 6 WEATHER CONTROL 0 r:. < 7 CARRIAGE OF CARGO 0 OTHER (Speedy( 0 7. 1 RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT 3 EXHIBITION cc . W 4 EXPERIMENTAL (Inciter* opersborest to to condo:WO • 4 RACING s CREW TRAINING MKT SURVEY . U • . 0 70 SHOW COMPLIANCE WITH F AR 1 FERRY FLIGHT FOR REPAIRS. ALTERATIONS. MAINTENANCE OR STORAGE SPECIAL FLIGHT PERMIT ihrdicale 2 EVACUATE FROM AREA OF IMPENDING DANGER A A n. e oporet,ort lobo conducted. Wen complete Section VIM VII as 3 OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKEOFF WEIGHT apphcablo On serene sycliN 4 DELIVERING OR EXPORT • r5 I I PRODUCTION FLIGHT TESTING 6 CUSTOMER DEMONSTRATION FLIGHTS C 16 I MULTIPLE AIRWORTHINESS CERTIFICATE (Check ABOVE 'Rest(t led Operation and 'Standard' or • L.noled as turr,cabie r A. REGISTERED OWNER (As shown on certificate of anCiall registration) IF DEALER. CHECK MERE 4 NAME VOVZICOEST" 6 10 4.2)./A)Ce e. d e+c, ADDRESS /may rev Cg - icAwerin, ,a> R, . ti(ne /Ss zfraiku4-(6-- /Foos B. AIRCRAFT CERTIFICATION BASIS (Gncc* anplitable Wachs arid COmpfetv items al indica ect) 1 S p 3 AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE DATA SHEET /Give No and Revision Nal 3 1J ,i4 fr AIRWORTHINESS DIRECTIVES iCtioca;a/ai:esvereabte latest AD No )4 O9O AD s complied with and gar 4) ._ a . C g AIRCRAFT LISTING (Gov pego nontoell ell /O A X,IPPLEQNT AL TYPE CERTIFICATE 1/4 8 l itifri (List number of earn S TC incorpcualoc0 !Twee/ 623./ /990 15 C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS t • 0 CHECK IF RECORDS IN.* COMPLIANCE WITH FAA 91 173 . TOTAL AIRFRAME Nouns . , cs, 94/4./ .. . EXPERIMENTAL ;5504.41 r 'ICI vans 51000 lass VII f; ONLY r -I c I Cale co reneiree4 D. CERTIFICATION — I hobby Cellily ItiAl I III the iegislesed owner (penis agent; til the ariciall deathbed above. mar 1/00 ancial1 Admonish/Ilion an accordance with Suchen 501 cil the Federal Mullion ALI 0119511.atin applicable Federal Avialion RegulattoiLs.tusd airworthy and eligible for the airworthiness ter Oman: rem •' rid .... ... . . . - 4,07— 40. Ttroir-- • is Thal 1110 iegisleted with the Federal *rialto° RIICIall has been inspected and is DATE OF APPLICATION E AND TITLE HUM It % . \ - SIGNAT UR (-c-, 774-4/ 0 , 3 / 990 (di. yl A. THE AIRCRAF I DESCRIBED ABOV I IAS ([LEN INSPECTED A D FOUND AIRWORTHY BY (Conn/few ;h... •••. .oti only if FAR 21.1671( I onseaf nr.thsptcrio AGENCY veRincemot I 4. '" FAR PART 121 OR 127 CERTIFICATE HOLDER (Give Cerrthesto No 1 3- CERTIFICATED MECHANIC (Girt. Cartrircale NO. I — - - - • 6 CERTIFICATED REPAIR STATION (Gat Certificate No 1 • AIRCRAFT MANUFACTURER ;Grre name of font? • — — - t _. . DATE . TITLE .. .... • .. _ SIGNATURE ' .. . . Whets ALL ,ipplicablo blocks in dents A a dB) THE CERTIFICATE REQUESTED A. yawl dial die anciall described in Section I or VII meets retarireinenis for. AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE 1. Z r. 0 B. Insociclion lot a special High: peed under Sect. 'FAA INSFIECTOR . ... ... . • —.. lr-„. AA DESIGNEE ot g vats conducted by. . . . CERTIFICATE HOLDER UNDER: FAR 65 [ _I FAR 121. 127 or 135] 1 FAR 145 g a > c iv ki w c U e ..• DATE **ID DISTRICT OFFICE • . RE A 1, : . DESIGNEE S SIGNATURE F5 .' N rIl ._. __ % 1Vvi D2. ... AI\ FAA INSPECTOR'S SIGNATURE • . . . . : ' .' • 3:71r 'n t;;Palt retir EFTA00277852 FAA AIRCRAFT REGISTRY CAMERA NO..) At DATE: 9 - 27 - 97 *U.S.CPO:1989-241473/90913 • . • ' • PROOON . . . . • .. 1 • Mt SPECIAL FLIGHT PERMIT PURPOSES'OTHER THAN PRODUCTION FLIGHT TEST VI . • • • FLIGHUCTI T TESTING • . . . - . • . .. . . . _ : . . . . .. . . - . .. . . A. MANUFACTURER. S NAME . .. . •• - . .. . _ • - ADDRESS - .. • . , B. PRODUCTION BASIS (Check applicable item) - PRODUCTION CERTIFICATE (Give reduction COW:Cato numbs') TYPE CERTIFICATE ONLY • .. . .. ............ .. APPROVED PRODUCTION INSPECTION SYSTEM C. GIVE QUANTITY OF CERTIFICATES REWIRED FOR OPERATING NEEDS DATE OF APPLICATION NAME AND TITLE (Prop or typo) SIGNATURE A. ' ... • • . DESCRIPTION OF AIRCRAFT REGISTERED OWNER ADDRESS • • s BUILDER (MAW MODEL: SERIAL NUMBER . • "•- ,. . . - • . • REGISTRATION MARK • . B. DESCRIPTION FROM, OF FLIGHT • STONER DEMONSTRATION FLIGHTS l 0 jebeea d abolicabiel • • • ... . .... ,.. ... .. .. .,.. ,... TO • • .. ... . . .. .. .. .. .. . • VIA • . .. . . . . . . . . . . -. • . DEPARTURE DATE . . DURATION C. CREW REQUIRED TO OPERATE THE AIRCRAFT AND ITS EQUIPMENT.: -- \ : • • I PICOT COPILOT NAVIGATOR • OTHER /Speedy/ .13. THE AIRCRAFT DOES NOT MEET THE APPLICABLE AIRWORTHINESS REQUIREMENTS AS FOLLOWS. .. . . . . . . , . . . • ' ' • • . • ". - . • . .' . . ... . .• • • . . _ . .... . . ..,.. _.. _ _ ........ . ....... ..... .. .. . . . . - •- ._ . • '. -.. • ...... : : "- -...‘. '.., CA:: • c •'' • : '` - i . „ . • s `.. -. 5.‘11.2.•,- . V i•-•• .' ..i.*:•• 7:i-: •• • ., • . . . . ..- • .. • .. .. •. . . . . .. I , r- , • . i ; , • • •• -• i . ' • .":•• .... . E. THE FOLLOWING RESTRICTIONS .ARE CONSIDERED NECESSARY FOR SAFE OPERATION ruse effacement ,0 necessary; ; • . . . ! i ; i I . 3 •,..... r" ... • • , . • • • ' - - • . .. -. - ....-....... „..--- - .. . . ...„ .. .. -..... . - -.... . ... . -. • - .. • : 1 I ; s ! ..• r•:•: • c •• • :, • • ,, ., ; . .4. '. I .. ' . . % .. • .: •.'; •:.* • Ir•l"••••: •.* I • .. . , .... , • • . .. : .:.. : ; r.I.V:r.I.• Cr" ? . I Y i • . i I f . 7. t : f.ol a.:. a •c.. ! • :••: i : \ • ._. . .-., . • • i. ..; - • • • • • • • • •• , • • 6 1 • ! • . .. .:i.. . . • .. . • . . - • : • . • f. CERT IFICATION — I hereby certilythell ant the registered owner tor nia agonbollhaerallalssarawslabove.IntIlwaecransregaleravalhan FederalA.O1UP% Adm satiation tn ...v. • accordance with Section 501 of the Fetleral•Avialion, Ad of 1958, and imitable Federal Avestan Regialront and that the Nara Ins been Inspected and is airworthy for Ins high) .. described , . - .. OAT C . [NAME AND TITLE (Thint of typo) SIGNATURE • _ . . . , • • ' . . . . . .. [ VIII. AIRWORTHINESS DOCUMENTATION (FAA use only) A. Operliting Lunations and Markings InVriniPtuinirilelin FAR ' . 91.31 as Applicable ' • • • . ... . . . .. i.. O..Slidstalent of Com o i mily. FAA Form 01304 (05(tath when require**. .- H. FOllfieriiiilifOtihtn!“ Cerhi;Calion. the fritpOri Airafal— . • ... --- •-••.:: • 1 }Aback when toZhatedl • . "`. " 1 - ".%''C t . % • • D. Cimeni Operably Limilolions Attached :• - • ••• l.':_• .1 • C. We. Drawings. Pholographs, etc. (iitlachechen toquiredi•'. ' • • 1 • I. Previous Auwonnin ' Cgicallis FAlit73 - . cadres willi::. (Oligtnal Allacht(11 V D. Current Weight and Balance InlosmatiOn Available in Aircraft . E, Major Repair and Alteration. FAA Forni 337 (Alraeh When iiquoitcli J. Current AnwortAiness nificat I's in Accordencesvah . ... . . . 1 1 FAR :2 11 .. 1 . ) • /Copy inched) V F. This Inspecah Racurded f M . etall Records . , . ; , . • ' ' EFTA00277853 • FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 91 a. 4 Ot.kr", it.'421 ••••• • 0 • : . . • • • • • • • 'a . • . ' ••.' • . . • UNITED STATES OF AMERICA , DEPARTMENT OF TRANSPORTATION—FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE, , 1. NATIONALITY AND 2 MANUFACTURER AND MODEL REGISTRATION MARKS N505C BOEING 727-31 3 AIRCRAFT SERIAL A CATEGORY NUMBER 20115 TRANSPORT s•• • • . . • • •• ' - . • . •• .• • t • „ 1 • • • • • • • ' , • . 5. AUTHORITY AND ETAS S FOR ISSUANCE . • TNsainvorthiness certificate is issued pursuant to inFederal Aviation Act of 1958 and cenif es that. as of the date ol issuance. the •• aircraft to which issued has been inspected and found 10 conform to the type certifteme Therefor, 10 oe in 'condemn for sale • 'r "....•• r • ••• • operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as . . provided by Annex 8 to the Convention el. Iniernabonal Civil Aviation. except as noted here" Exceptions' NONE ' • • • . 6. TERMS AND CONDITIONS • .- • . . . • Unless sooner surrenclerea, suspended. 'evoked. Or a lerthination dale rS °MM.'Se established by the ACImintSlialOr. Ibis '.. ...?.... .. airworthiness certifies', rs effective as long as the maintenance. pievenlative maintenance. and anerabons are performed in ... .,,l accordance with PartS21. 43. and91 of theFederal AviationRegulations. as aPPI le. and the aocran is leg:Ste:ea .ntrieUnitecl ....; . .• , States DATE OF ISSUANCE 7/23/90 DESIGNATION NUMBER , • DAR-41-FS-NM - .•-• • •, • Any alteration. reprOduCliOn. Or M. use of this certificate may be purushableoy ot exc ng if 000 0 imposonmena erCeerbng 3 / , . . •.... years. or both THIS CERTIFICATE MUST .8E DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL I: . .:• • • •• • • AVIATION REGULATIONS. ' . ' • • • . . . . . FAA Form 8100-2 (8-821 0 IP • • • GPO si2•e04 • • - • • • • I. ••• • • • : • , a 9 - • • .. • x. • 7 : • -rm. • • ....N..— •—•••'. EFTA00277854 FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 21 EFTA00277855 Gk • • t 11 • • •• • rr• - • r • • ." • • • • . • . t 4 ' .•• •Ah.: 0A j • • • • . . ..• in , A . . r 0 . . MAJOR REPAIR AND ALTERATION . uS dearnmenr For or TIXISDOefOriOn ' • (Airframe, Powerplant, Propeller, or Appliance) R OI Avicnien OCIOC Act.wwwwwton Form Approved OMB No. 2120-0020 FAA Use Only Office Identification INSTRUCTIONS. Print or type all entries. See FAR 43.9, FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This repot t is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed 51,000 for each such violation (Section 901 Federal AviatiOn Act of 1958). _-, 1. Aircraft Make BOEING Model • . 727-100 Serial No. 20115 ' Nationality and Registration Mark. N505C • 2. Ovine'' Name (As shown on registration certificate) NORTHWEST HOLDING CORPORATION Address (As shown on registration 1409 Foulk Road, Foulkstone Plaza, 'Wilmington, Delaware certificate) P.O. Box 7138 Suite 102 19803 3. For Use Only - _ 4. Unit Identification S. Type Unit Make Model . Serial No. Repair - Alteration AIRFRAME (As described in Item 1 above) X . POWERPLANT V PROPELLER ___ ___ _ ___. _ _____. _____ t{FPLIANCE Type Manufacturer . -- _ 6. Conformity Statement A. Agency's Nanakend Address l B. Kind of Agency C. Certificate No. North American Aircraft U.S. Certificated Mechamc , Airframe Class 4 Rockwell International Corporation I Foreign Cemficated mecnamc Limited Powerplant 2825 E. Avenue P I X I Certificated Repair Station Class 3 Palmdale, Ca. 93550 I Manufacturer NXAR6B8K D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Pal 43,01 the U.S. Federal Aviation Regulations and that-the information furnished herein is true and correct to the best of my knowledge. i :,. / / Date July 20, 1990 I Signature of Authorized Individual I • D. A. Perazzo , /14.- .— T. Approval Col Return To Service . / ,......1,.../ " Pursuant to the authority given -persons specified below, Administrator of the Federal Aviation Administration and f the unit identified in item 4 was inspected in thezmanner prescribed by the is CD APPROVED -L7i REJECTED FAA Fit. Standards 1 Ins P i Manufacturer 1 Inspection Authorization Other (Specify) I • BY FAA Designee 1 x Repair Station Person Approved by Transport Canada Airworthiness Group n Date of APProvai or Rejection July 20, 1990 . 1I Certificate or Designation No. NXAR688K Signature of Authorized Individual • , I • ' U. A. Perazzo' II V t • I— FAA Form 337 • • EFTA00277856 r. _ hr:::1.1 tit .• • -•.; . • . • :, . • t...; ••, , I EFTA00277857 FAA AIRCRAFT REGISTRY CAMERA NO.9 DATE: 9 - 27 - 91 • ti • • 4 • 4." ' • NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. • 8. Description at Work Accomplished (if more space is required, art additional sheets. Identity with aircraft nationality and registration mark and date work completed.) • A. Modified Boeing Model 727-100 , Serial MUmber 20115, in mental type. certificate SA4363NM, amended September 1, T. Valsan-Boeing 727-200 Re-engining Document VA000001, • 15, 1990. . 2. The following drawings and engineering Orders (EWS) aboVe document: NOTE: "VA" denotes Valsan Drawing. a. Chapter 24 ELECTRICAL POWER . VA240000 A • Electrical System Initl. - Strut E.O.: 003A, 101 0240007 E Panel-Load Control Center Modification E.O.: 003A, 004, 005, & 006 b. accordance with supple- 1989 as follows: Revision F, dated January 's • are in addition to the Chapter 28 FUEL SYSTEM INSTALLATION, STRUT VA280001 B Tube Assy - Fuel Strut Feed Thru E.O.: 100 c. Chapter 48 MISC VA481100 A VA481200 C VA481300 C VA481324' NC VA481325 NC, d. Chapter 53 FUSELAGE VA6.30001 8 VA530003 C • VA530004 - NC Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 Frame Assy Sta 1263 E.0.:.101, 103 Fuselage Skin E.O.: 106, 114A, 114, 116 Intercostal Assy - BSTA 1223-to BSTA 1243 W/L244.39 E.0: 106, Intercostal Assy - BSTA 1223 to BSTA 1243 W/L234.06 E.O: 105 STRUCTURE Ballast Weight Installation E.O: 100, 102 Ballast Weight, Support Structure Assy. E.O.: 002,100 Ballast Weight Instl. STA 312 - 360 E.O.: 002, 100 e. Chapter 54 NACELLES & PYLONS VA543000• C Main Strut Assy (Sh. 1, 2, & 5) E.O.: 003 -VA543100 D Firewaii Rib, Side Engine E.O: 36A, 003A f.' Chapter 71 POWER PLANT, VA710000 NC Power Plant Instl. - Engine Pod V727RE E.O.: 002, 105B, 109, 108, 001A, 104A, 005A, 004, 110, 003, 111, 006A Chapter 73 ENGINE g. FUEL AND CONTROL VA732301 .K Approach Idle Solenoid Wiring Diagram E.O: 002(Rev L), . 002 (Rev. M), 003(Rev. M) VA732303 0 Relay Instl. - Approach Idle Solenoid E:0.:. 103, 003, 100B VA732304 0 Switch/IND Light Instl - Approach Idle E.O.: 002, VA732310 A Switch Instl. - Nose Gear Position Approach Idle £.0.: 103 VA732315 NC Relay Instl. Pilots Overhead Panel E.O.: 100, 002, 101 - h. Chapter 76 ENGINE CONTROL VA760000 A Engine Controls Instl. - Strut E.O.: 00ZA VA760014. A Drum Instl. - Eng. Controls E.O.: 100, 101 VA760015 A Bracket Assy - Pulley ESTA 100 E.O.: 105 (1§ Additional Sheets Are Attached • U.S. GP0,1989.0-663. 11 EFTA00277858 FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 91 EFTA00277859 FAA AIRCRAFT REGISTRY CAMERA NO2 A' DATE: 9 - 27 - 9/ P. k• . - r DESCRIPTION OF WORK ACCOMPLISHED 1ContinuedY Serial No. 20115 .Chapter.77.ENGINE INDICATING VA771005 NC Indicator:Engine,?ressu're Ratio EPR, E.O.: 001 Chapter 78 ENGINE VA780000 B VA783010 E VA78301I- F, VA783013 D - VA783017 J VA783024 B VA783028 A VA783101 C. 'Chapter 91 CUARTS• VA910002 ' A VA910008 NC EXHAUST , • a . • Engine Strut Controls Instl. Fit Deck -Indicator Ihstl. T/R'Sys': E.O.: 003, 004 Thrust Reverser System Wiring Diagram E.O.: 002 (Rev. G) Support Bracket Assy - T/R Control Valve•R/S E.O.: 100 (Rev. E. Placardi E.O.: 007, 008 Relay Instl. - Thrust Reverser Control E.O.: 003 Mixer, Exhaust - Instl. 727E E.0:: 100 No. 2 Engine T/R Wiring Deactiviation E.0.: 002 ° Instl. - Electrical Wire Harness E.O.: 003, 004, 005,006, 007 • Wire List V727RE E.O.: 001, 002, 003 • • , *NEW DRAWINGS ADDED TO MODIFICATION Boeing 727 Service Bulletin 727-53A0171, dated December 14, 1989 SUbject: Fuselage - Station 1182 Pressare Bulkhead web, . Crack Repair and Preventive Modification • • . . , C.. The aircraft empty weight and center of gravity was revised in accordance with Boeing Weight and Balance Manual D6-21100. Weight and Blanace Manual Supplement, VA-CR279 is attached. . . . . D. VA000003, Rev. A, Dated 4-4-90 is equivalent to VA000001, Rev. F, dated 1-15-90. END Sri EFTA00277860 r, FAA AIRCRAFT REGISTRY CAMERA NO3 DATE: 9 - 27 - 97 • EFTA00277861 • FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 27 - 91 pa,5649-tioat i. PERSONNEL ACCOMPLISHING THE CHECK LIST WILL INITIAL EACH ITEM IWTHE APPLICABLE BLOCK FOR PARTS A THROUGH D. N/A BLOCKS NOT APPLICABLE TO A/C BEING WEIGHED. 2. ALL BOTTLES (02CO2, H20) SHOULD BE IN NORMAL OPERATIONAL CONDITION. 3. ANY DEVIATION FROM THIS LIST MUST BE COORDINATED WITH CHIEF INSPECTOR OR HIS DESIGNEE: 4. ON CONIPLErION OF PARTS A THROUGH D THE FOREMAN/LEAD MECHANIC OR ASSIGVED INSPECTOR WILL CHECK & SIGN FORM BE• FORE PROCEEDING WITH WEIGHING. ti9 FLUIDS Checked pV . Checke By 1. FILL ENG. OIL SYSTEMS & TANKS FULL . VI.4-1- 7 k." • 6. LAVATORIES CLEANED & VACUUMED ' Q 2 ALL FUEL TANKS DRAINED USING DRAIN PLUGS WI (H AIRCRAFT LEVEL 4. 0,,,. ...r 50•7. , ALL MAGAZINES, NEWSPAPERS & SEAT BACK . 7< LITERATURE REMOVED ke %43%d • 3. DRINKING di 1e)ASH DRAINED EL WATER TANKS FILLED 1... i - .. B. -PROTECTLVE ENTRY, AISLE & STAIR COVERS REMOVED ' - 1:0 1 ‘i‘ 4. HYDRAULIC SYSTEMS FULL ! • •\ \ • 9. WINDSCREEN STOWAGE EMPTY & CLEAN WV , 5. TOILETS SERVICED TO NORMAL QUANTITY e<74-2;" ..in cr -•• ei • • STOWAGE COMPARTMENTS ON FWD. & AFT. LAV. — . BULKHEADS EMPTY .iitV 6. SEAPLANES: DRAIN HULL & WING FLOATS COMPLETELY le/4yred- r;2- . . 0 CONTROL CABIN . • . _ 1 J . ALL INSTRUMENT PANELS COMPLETE ?:)11iA D. CARGO, LANDING GEAR & POWERPLANT - . • .<, 1 a c 2 ALL MANUALS; CHECKLISTS, LOG BOOKS, FORMS & OTHER WRITTEN MATERIAL REMOVED CO/ 2//f • 1. ENGINE FIRE BOTTLES CHARGED kt b r i •- 3 ' ALL CREW SEATS COMPLETE WITH SEAT BELTS & . HARNESSES INSTALLED 4,er .1//f 2 ALL ENGINES COMPLETE I.E., ACCESSORIES, PLUMBING, ETC. e 4 FLIGHT ENGINEERS TABLE EMPTY & . CLEAN EXCEPT FOR STRETCHER KIT i ALL COWLING & PANELS IN PLACE & SECURED 7..riew,' C. PASSENGER CABIN . X 4. 4 BRAKE AIR BOTTLE CHARGED. ..r.A. ..- 7 • REMOVE ALL ITEMS FROM HATRACKS EXCEPT 1. MEGAPHONES, FIRST AID KIT, MOUNTED OXY. BOTTLES, DEMO OXY. MASK & LIFE VEST IN S. ALL AVIONICS EQUIPMENT INSTALLED -P, • 12 • POUCH 6 FWD, & AFT, CARGO COMPARTMENT EMPTY & CLEANED • SI. 2. ALL PASSENGER SERVICE EQUIPMENT REMOVED FROM GALLEY ' Xis A MAIN OXYGEN SYSTEM SERVICED • 7' FULL 71,4"--a` 7 7 •:' ALL SERVICE EQUIPMENT REMOVED 3. FROM FWD. & AFT. LAVATORIES • a MAIN BATTERY & AUX. BATTERY (IF USED) INSTALLED q...N, ,t.). _ -Not ) _ 4. ALL GALLEY AREAS CLEANED & . VACUUMED • CARGO DOORS & FAIRINGS CLOSED & . a LATCHED .-6-.:--: 5. PASSENGER CABIN CLEANED & VACUUMED nb; &,A) LL TIRES A INFLATED TO OPERATING 10• PRESSURE , ' ce7:: 00-- -9)114-v _AIRCRAFT READY FOR WEIGHING as Ariz alo , Aiil ica4 h ?VERSO% ISO AIM • •••• • • . -•,1/4 EFTA00277862 FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 27 . • , • '• !I ,;•".?.• • • '7. ' . tt• -: ' . i .„ • : ;en,. r.••,;1•:-....c. t 4 -e41-4‘ vrk.:-%peroler.44t4;,*. 4•1w,:‘' •1 ; .0 • -a :; . ; •• ". . ' . • ' •17 •i'.. -••:14.1:1::S. • ." . • '. ••••.:- . . . • • . r '• .r. :.• . .• • • 41 .cr EFTA00277863 I FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - 27 - 91 • AIRCRAFT WEIGHING SCALES: MAKE Eliereeeen ) SERIAL NO. 10(e? -"FIRST WEIGH Nt h MODEL —zwiw awainicmaaTiCOn4041, r.L. • CALIBRATION DATE 5 3 - 9.0 REACTION SCALE READING CORRECTION CALIBRATION CELL DRIFT TARE NET WEIGHT LEFT ML INGge RIGHT "L INGO OS AIL Ya - 4 7 7 3.5 -2o -e0- -62- 1/ 7715-- ligg0 ° - SO ---662- - - iiY75-0 93 `S +1 0 q 3 55- 1 / CIRCLE REACTION USED NET WEIGHT TOTAL 10O1 2T2O SECOND WEIGH REACTION SCALE READING CALIBRATION .CORRECTION CELL DRIFT TARE NET WEIGHT MLG LEFT WING RIGHT MLG WING NOSE/TAIL 11-7 750 -5-O -79- 41 417 9'OO ‘//741.0 +10 -69- -re Ile 120 l 'i3 5- a 6 3 '69' Lt 3 (O 1 / CIRCLE REACTION USED i NET WE GHT TOTAL 1 00/ th CY -5- ST 1. WEIGHING COMPLETED 2. WITNESSED & ACCEPTED Foreman/Lead Mech. Or Inspec 0)1444.4-d ICt4.421,4- Chief Inspector Or Designee NOTE: PART F. AND SUBSEQUENT PARTS TO BE ACCOMPLISHED BY THE QUALITY CONTROL SECTION. NET WEIGHT AVERAGE FIRST WEIGH SECOND WEIGH TOTAL AVERAGE MLG LEFT VVING _ MLG RIGHT WING NOSE/TAIL 117 715- Li F75-0 1-1-355- 91900 q a' Li 20 113425- 956 IS 91 / 7O X72O q 7 Sac ggs-75-- 4t3tho CHECKED BY PAGE 2 OF 3 ' EFTA00277864 FAA AIRCRAFT REGISTRY CAMERA NO.3 4/ DATE: 9 - 27 - 97 . • . . ,,.• . • •, • . . . . .6 4 .6. nl EFTA00277865 FAA AIRCRAFT REGISTRY CAMERA NO3 N DATE: 9 - 27 - 97 11 CIRCLE REACTIONS USED. 2. ENTER AVERAGED NET WEIGHTS FROM PART F. BEW ITEMS NOT ON AIRCRAF ATTACH SUPPLEMENT IF ADDITIONAL SPACE IS REQUIRED TOTAL AS WEIGHED SUB TOTAL ITEMS WEIGHED BUT NOT TO BE INCLUDED IN DEW ATTACH SUPPLEMENT IF ADDITIONAL SPACE IS REQUIRED SUB TOTAL BASIC EMPTY WEIGHT REACTION DATE 7 70 41 360 b 200 in.552,5" CHECKED BY 7-3/, 2. 925., 27 MOMENT 45,4124,6e6.-5- ISC1 PAGE 3 OF 3 EFTA00277866 FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 91 • •••• .•• _ • ._t •• .• E. . • • ••••• • ..• .4, . .. .. If • , c. I • 1 0 i • i ‘1 ‘ ‘ ... • ....gm ...Ob. • 1 ...E..... Z: • . • • . . I 1 ; • • . . • 1 • • • . ',. . • • 1 is . • t .. ••••• ••• • .....•• • •• ••• ..... •••••••• A : • ••• dm ..• ... • k . i • 3 EFTA00277867 • z FAA AIRCRAFT REGISTRY CAMERA NO3 A' DATE: 9 - - 97 • Uan TED STATES OF AMERICA . , • - " ' DEPARTMENT OF TRANSPORTATION.- FEDERAL AVIATION ADMIAISTRATION -SPECIAL AIRWORTHINESS CERTIFICATE A Y C A T E G Op Y / 0 E S i G N A T I ON EXPERIMENTAL •-• , • PURPOSE SHOW COMPLIANCE WITH FAR / MARKET SURVEY :• 1.. , 6-. MANU- , FACTURO NAME N/A 3 ADDRESS . N/A . .. _ C FLIGHT/ FROM • N/A TO N/A D N- 505C SERIAL NO. 20115, ., BUILDER BOEING MODEL 727-31 E DATE OF ISSUANCE 05-01-90 EXPIRY 08-01-90 OPERATING LIMITATIONS DATE 05-01-90 ARE A PART OF THIS CERTIFICATE SIGNATURE qr F REPRE r 'MICHAEL J. SON . i DESIGNATION OR OFFICE NC: . • ' • SEA-MIDO, ANM-108S Any ENFrattOn, reproduction imprisonment not exceeding ACCORDANCE WITH or misuse of this certificate may be punishable by a line not exceeding $1.000 or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN 3 years. FEDERAL APPLICABLE FEDERAL AVIATION REGULATIONS. FAA FORM itiO4 (loam ,•• SEE REVERSE SIDE • t • • : • • • t . ▪ , • , • ' • ▪ . . •••• : • N. • " • . . • . • o , EFTA00277868 FAA AIRCRAFT REGISTRY CAMERA N0.9 N DATE: 9 - Z7 - A This airworthiness certilicate is issued under the authority of the Federal Aviation,Act of 1958' v • and the Federal Aviation Regulations (FAR). • • . '. . B --.• C •—•••••••• O . . . This airworthiness certificate authorizes the manufacturer named on the reverse side to conduct production flight tests, and only production flight tests. of aircraft registered in his name. No person may conduct production flight tests under this certificate: (1) 'Carrying' persons'or property for compensation or hire; and/or (2) Carrying persons notessential to the purpoie of the flight. ; '• ' • .. • 1/4., ...... This airworthiness certificate authorizes the flight specified on the reverse side for,z‘rpose shown in Block A. . • • .. - - ' ( .. ' . . - • . • • • cS,i This airworthiness certificatecertifies that, as of the date of issuance, the aircraft to W. ich issued has been inspected and found to meet the requirements of the applicable FAR. The aircraft does not meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention On International Civil Aviation. No person may operate the aircraft described on the reverse sit (1)except in'accordance with the appliCable FAR and in accordance with conditions and limitation: which may be prescribed by the Administrator as part of this certificate; (2) over any foreign country without the. special permission of that . . . . , country. • . ic • • • - - • . . c E ... Unless sooner surrendered. suspended, or revoked. this airworthiness certificate is effective for the duration and under the conditions prescribed in FAR Part 21. Section 21.181 or.21217. . • - - rsf 1 1.4 EFTA00277869 7 2.Yety FAA AIRCRAFT REGISTRY CAMERA 6,:)..3 iV DATE: 9 - 27 - 97 • 4 sktrir, nos r "'Yr ti •VW ar . " • . . gt. •\ • 1. . • . . • • • • .• • • • •••• . • • • • . 4 • U.S. Department of Transportation Federal Aviation Administration Manufacturing Inspection District. Office 7300 Perimeter -Road South Seattle, WA 98108 May 1, 1990 EXPERIMENTAL -SHOW COMPLIANCE WITH FAR's/MARKET SURVEY MAKE: Boeing . MODEL: 727-31 SERIAL NO. 201157: • REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: 1. No person may operate this aircraft for other than the purpose of Show Compliance with the FAR's and Market Survey to accomplish, the tests outlined in the applicant's program letter dated May 1, 1990 describing compliance with FAR 21.193(d). Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). 2. All flights shall be conducted within the geographical areas described as follows: 1. Western United States of America bounded on the East by the Mississippi River, on the- North by the U.S.A./Canadian border, on the South by the U.S.A./Mexico border, dnd bounded on the West by no more than 200 miles from the West Coast of the United States of America. ! • A 2. Base of operations is Palmdale/Lancaster Airport, i Palmdale, California and secondary base of operation to be Moses Lake Airport, Moses Lake, Washington. 3. The pilot-in-command of aircraft must, as applicable, hold an appropriate category/class rating, have an aircraft type rating, have a flight instructor's log book endorsement or possess a "Letter of Authorization" issued by an FAA General Aviation or Air Carrier Operations Inspector. 4. This aircraft shall not be flown unless it is maintained and opera4-ed in accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. Upon changing between operating purposes of a Multiple Purpose Certificate, the operator shall determine that the aircraft is in a condition appropriate for the purpose intended and has documented that finding in the aircraft log. 6. This aircraft shall contain the placards, markings, etc. required by FAR 91.31. • • EFTA00277870 FAA AIRCRAFT REGISTRY CAMERA NO.3 N DATE: 9 - 27 - 97 EFTA00277871 FAA AIRCRAFT REGISTRY CAMERA N0.3 N DATE: 9 - 27 - 91 • Federal Aviation Administration Manufacturing Inspection District Office Experimental - Show Compliance with FAR's/Market Survey, Cont'd Page 2 of 2 7. The cognizant FAA office must be notified. and their response • received in .writingprior to flying this aircraft after - incorporating a major change.. as defined by FAR'21.93. . 8.• This aircraft approved for day/night VFR/IFR only. '"No operations shall be conducted over densely populated areas or in Congested airways except for takeoffs and landings, and when under.ATC control. :10. No person may be carried in this aircraft during flight unless that person is essential for the purpose of the flight while in the Show Compliance category. 11. This aircraft is prohibited -prom aerobatic flight; that is, an intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved by the cognizant FAA office. 12. If aircraft engipe.or propeller operating limitations are exceeded, an.appropriate entry will be made in the historical records. 13. After the aircraft has been re-engined, the pilot-in-command must make a log book entry stating the aircraft complies with FAR 91.42(a) and FAR 91.42(b). Mic ael J. son Aviation Sa ty Inspector (Mfg) SEA-MIDO, ANM-108S These limitations will expire on August 1, 1990. J1 EFTA00277872 -ti 4: kith- ••• r cs '0. r. • • .7, • ^ .a.•••••:. •• .• • _ EFTA00277873 , .. • • MAJOR REPAIR AND ALTERATION uSDecianrrient of nomoonction (Airframe, Powerplant, Propeller, or Appliance) Peen MiatiOn Administration Form Approved OMB No. 2120-0020 For FAA Use Only Office Identification 7A/y gs ad INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B, and AC43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report le required by law (49 U.S.C. 1421). Failure to report can result in acilejl penalty not to exceed $1,000 for each such violation (Section 901 Federal Aviation Act of 1958). RECEIVE[} FAA Make BOEING Model 727-100 - 2't L-9.0 1. Aircraft Serial No. • 20115 Nationality and Registration Mark jUi N505C 1/14Y 11;[)() 2. Owner Name (As shown on registration certificate) . NORTHWEST HOLDING CORPORATION Address (As shown on registration certificate) -1409 Foulk Road, P.O. Box 7138 Fpulkstone Plaza, Suite 102 Wilmington, "Delaware 19803 3. For FAA Use. Only - • - _ . 4. Unit Identification 5. Type . Unit Make ' Model - Serial No. Repair , . Alteration — . . AIRFRAME . (As in Item 1 above) - X _described • POWERPLANT, - PROPELLER • • - -- .--- - ---- • _ _ ___ APPLIANCE Type Manufacturer • t - - - - • ' 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. North AHL.-ican Aircraft U.S. Certif cated Mechanic Airframe Class 4 Rockwell International Corporation Foreign Cen baited Mechanic LiMited Powerplant 2825 E. Avenue P X Certificated Repo I Station Class 3 Palmdale Ca. 93550 • Manufacturer NXAR688K • D. I certify that the repair and/or alteration made to the un have been made in accordance with the requirements furnished herein is true and correct to the best of my t(s) identified In item 4 above and described on the reverse or attachments hereto of Part 43.of the U.S. Federal Aviation,RegulatIons and that-the infornation knowledge. i / Date • July 20, 1990 Signature of Authorized Individual . D. A. Perazzo kJ 7. Approval for Return To Service j Pu suant to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the , Administrator of the Federal Aviation Administration and is cg. APPROVED :-.7. REJECTED !. FAA Fit. Standards Inspector • I Manufacturer Inspection Authorization Other (Specify) • BY FAA Designee x Repair Station Per I Parson by Transport Approved Canada Airworthiness Group (Th i l Date of Approval or Rejection July 20, 1990 Certificate or Designation No. NXAR688K Signature of Authorized Individual i U. A. Perazzo h . ' . . .. ,..._. i- FAA Form 337 ti y Hsi t, t EFTA00277874 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. - - B. Description of WorteAccornplIshed (It more space is required, attach additional shoots. identify with aircraft nationality and registration mark and date work completed ) A. Modified Boeing Model 727-100 , Serial Number 20115, in accordance with supple- mental type certificate SA4363NM, amended September 1, 1989 as follows: 1. Valsan-Boeing 727-200 Re-engining Document VA000001, Revision F, dated January 15, 1990. 2. The following drawings and engineering orders (E0's) are in addition to the above document:: NOTE: "VA" denotes Valsan Drwing. a. Chapter 24 ELECTRICAL POWER VA240000 A Electrical System Instl. - Strut E.O.: 003A, 101 VA240007 E Panel-Load Control Center Modification E.D.: 003A, 004, 005, & 006 b. Chapter 28 FUEL SYSTEM INSTALLATION, STRUT VA2-80001 B Tube Assy - Fuel Strut Feed Thru E.O.: 100 c. Chapter 48 MISC VA481100 A VA481200 C VA481300 C VA481324 NC VA481325 NC Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 Frame Assy Sta 1263 E.O.: 101, 103 Fuselage Skin E.0.: 106; 114A, 114, 116 Intercostal Assy — BSTA 1223 to BSTA 1243 W/L244.39 E.0: 106 Intercostal Assy - BSTA 1223 to BSTA 1243 W/L234.0b E.0: 105 d. Chapter 53 FUSELAGE STRUCTURE VA530001 B Ballast Weight Installation E.0: 100, 102 VA530003 C Ballast Weight, Support Structure Assy. E.O.: .002,100 VA530004 NC Ballast Weight Instl. STA 312 - 360 E.U.: 002, 100 e. Chapter 54 NACELLES & PYLONS VA543000. C Main Strut Assy (Sh. 1, 2, & 5) E.O.: 003 VA543100 D Firewall Rib, Side Engine E.0: 36A, 003A f. Chapter 71 POWER PLANT VA710000 NC Power Plant Instl. - Engine Pod V727RE E.O.: 002, 105B, 109, 108, 001A, 104A, 005A, 004, 110, 003, l ii, 006A Chapter 73 ENGINE FUEL AND CONTROL VA732301 K Approach Idle Solenoid Wiring Diagram E.0: 002(Rev L), 002 (Rev. M), 003(Rev. M) VA732303 D Relay Instl. - Approach Idle Solenoid E.O.: 103, 003, 100B VA732304 D Switch/IND Light Instl - Approach rdle E.O.: 002, VA732310 A Switch Instl. - Nose Gear Position Approach Idle E.U.: 103 VA732315 NC Relay Instl. Pilots Overhead Panel E.O.: 100, 002, 101 h. Chapter 76 ENGINE CONTROL tA760000 A Engine Controls Instl. - Strut E.O.: 002A VA760014 A Drum Instl. - Eng. Controls E.O.: 100, 101 VA760015 A Bracket Assy - Pulley ESTA 100 E.O.: 105 g Additional ',.neets Ard Attached .U.SCIP(11989.0.600 71 y'` - • EFTA00277875 -` • AAYft'GtA` t, k • CANER!. 7 D. I.N DATts 2 g • Itt DESCRIPTIQN OF WORK ACCOMPLISHED (tontinued) :;"11 . i.- Chapter 77 ENGINE INDICATING - VA771005 NC Indicator Engine Pressure Ratio EPR, E.O.: co! EXHAUST Engine Strut controls:'Instl..E.O.: 002. . )Flt Deck 'Indicator Instl T/RSys. E.0.L.003, 004 Thrust Reverser System Wiring. Diagram 002'(Rev. G) :Support Bracket AsSy:=:T/R'COntrOl Valve R/S 100 (ReV. E) •Placards*E.O.:pp,0308 'Relay Instl.. -. ThruStReverter Control E.O.: 003' : .:Mixer, Exhaust -‘ Instl..727E.10.: 100 • No. 2 Engine TM Wiring Peactiviation E.O.: 002 - Chapter 78 ENGINE VA780000 B • VA783010. E VA783011 F VA783013 D VA783017 J' VA783024. VA783028 A • VA783101 C. k. Chapter 91 CHARTS VA910002. A * VA910008 NC *New driwings added to modification. Instl. ElectriCal Wire Harness E.O.:. 003, 004, 005, 006, 007 Wire List V727RE E.O.: 001, 002, 003 B. Boeing 727 Service Bulletin 72753A0171, *dated December'14, 1989. Subject: Fuselige - Station 1182 Pressure Bulkhead Web, • Crack Repair'and Preventive Modification . • C. The. aircraft empty weight and center of.gravity was revised in accordance with Boeing Weight and Balance Manual D6-21200. . Weight and Balance Manual Supplement, VA-CR279' •is attached. EFTA00277876 r I I l I k 榦 攥 私 ＞ , } 討 一 ： ： 一 ． 一 · 一 l I I . I F - ' “ 义 〉 : ， 一 一 一 r f - . I ' l !! EFTA00277877 ttk arc -tee_ 29 1991 0.t" q. No.212J-0018 0 . , - -- APPLICATION FOR us orpslinorr AIRWORTHINESS a lionwiu.ion • Fecteral Mahon 5" 010't S CERTIFICATE earrenraranon INSTRUCTIONS-Print or type. Do not write in 'laced antes: these are kr vs.,' use only. Submit Oulnal only to aniauthorized FAA Repreientalow. II additional space is required.-usean attachment. For special fl ght porn. Is complete Sections It and VI or VII as applicable. I. AIRCRAFT ❑ESCRIPT1ON 1 .REG.STRA C. 2.AIRCRAFT BUILDERS NAME (Mew C 50 Eti U 6 . 1 AIRCRACT MODEL DESIRNATIOI4 - .ift 1 72 7 — Avaritspi,4-> MA .• /..i.3 O. I. AIRCRAFT SERrAL NO 0 / /S. 6. ENGINE BUILDER'S NAMEThaikci IL) . I. ENGiNi .MODEL DESIGNATI Br> .1-. .7 A - 21 et - . 7. NUMBER OF ENGINES si ti fte O. PROPEL!, ER Still pr.11- AME AL .-; 9. *ROPE ..1.5 R MODEL 0ESiGNATION 10. AIRCRAFT iS (Crack ii SODiatit, _,..3 • all ik._>I/ I 'IMPORT APPUCATION IS HEREBY MADE FOR: (Cheek atftlicible iremsi. ' . le. A V ' STANDARD AIRWORTHINESS CERTIFICATE Umlaute carvuo., . iit i•••••••O I jUliLITY ACROBATIC] 1 TRANSPORT 1 _1 GLIDER BALLOON B L SPECIAL AIRWORTHINESS CERTIFICATE (Check app. onique din!. \ 2 LIMITED .- 1 - - G. ASS I S PROVISIONAL (indicatekraal 1 2 . • -CLASS II • g 0 se AGRICULTURE AND PEST CONTROL 2 AERIAL SURVEYING $ AERIAL ADVERTISING CC . 1 . RESTRICTED/Indicate Os co/Murat:ft • operehon(0 ID • FOREST (Wareile conservahwq 3 PATROLLING : ' II WEATHER CONTROL O • - • •• • . 7 CARRIAGE OF CARGO 0 OTHER iSpecdp/ ' 1 .. • . 1 RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT .3 EXHIBITION i A EXPERIMENTAL (InditeM to De ccoducted) Operettor(s) . - . .- )itk RACING S CREW TRAINING N MKT. SURVEY d •' bi TO SHOW COMPLIANCE WITH FAR ' • - • • • 1 FERRY FLIGHT FOR REPAIRS, ALTERATIONS. MAINTENANCE OR STORAGE SPECIAL FLIGHT PERMIT (Indicate 2 EVACUATE FROM AREA OF IMPENDING DANGER • • . operation to be conducted. Section VI then i c. Vil • — ' - i - ' OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKEOFF WEIGHT . • complete applicable on mites or es. saes: • a DELIVERING OR EXPORT 1.51 I PRODUCTION FLIGHT TESTING $ . CUSTOMER DEMONSTRATION FLIGHTS C 1 MULTIPLE AIRWORTHINESS CERTIFICATE (Check ABOVE -Restricted Opera)ion- and 'Standard' Or linuted.- as applwablej A. REGISTERED OWNER (Ar shown on cashier-aloof aircraft registration) IF DEALER. CHECK HERE I NAM!, , N10 41-44650-61" ge, LA I Ws. . • • .. ,( e,s90 Cenp Ay on. • ADDRESS ... rat PCS-Vole PA4 VA 15 cale era, Ai? rater koAn 61.6. lei 1I3t tor Lws W6-Tew beAsioa ilIo3 A. AIRCRAFT CERTIFICATION BASIS (Check applicable blocks and complete arms as indica ad) g P 3 - AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE and Revision No.) DATA SHEET (Owe No. AIRWORTHINESS DIRECTIVES (Chock it all inviable AD's complied with end wee latest AD NO.1 F I AIRCRAFT USTING (Give page number(s)) • SUPPLEMENTAL TYPE CERTIFICATE (List number °I each STC incorporated) 0 . C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS . . I bi CHECK IF RECORDSIN • COMPLIANCE WITH FAR 91.173 TOTAL AIRFRAME HOURS Pf gg'ie 2 • . . --., iF Tli ikkE EXPERIMENTAL ONLY (Enter hours flown since lest certiliiiale issued or renewed/ /9, g 0. CERTIFICATION — I hereby Willy thal I Administration In accordance with Section 50 aftworthy and eligible (or the aliworthine se certificate m the registered owner (or his earl) Of me airalft desCribed abort that IN aircraft of thefts:Mt Availed Act cal 1958. and applicable Federal AviatiorilleguLshons and . - . .. raquesiat - -" • . is registered with the Federal Aviation thal I he Sucre II hes beer nine salld .1. ATION . DATE OF ORLI,. ATION " Si/ 19 10 NAME AND TITLE (Print or type) rue • I ....t • ... (02441.17- • ?KA. 7 - / SI • A. 710 AIRCRAFT ESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Carnivore retie 'capon onty if FAR 21 183W) epphesl Z 0z 0 5 r; r t 61 . 'Tr:7, itli\ FAR PART 121 OR 127 CERTIFICATE HOLDER (Try Certificate Nal . . . ai Art (O CERTIFICATED MECHANiC (Owe . Culibcito No.) - CERTIFICATED REPAIR S(Al-ION:6,n Ceihhcaiii No.) 0 ° C ! • € I tili • XIPITRAFT MANUFACTURER/0Ni ahem* Of thin) i! i • DATE • TITLE. i .,: . SIGNATURE (Check ALL applicable blocks in items A end% .' 1 THE CERTIFICATE REO 'ESTEE, A. I find Om the aircraft described in Section I or VII male reiediremente lot, ot AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE • 1 g B. Inspection tor • special Mght pernalundir SectiOn VII -, • • • i FAA INSPECTOR FAA DESIGNEE ?.1 3 was conducted bir . ., CERTIFFCATF HGIOER UNDER: FAR 55 I 1FAR 121. 127 0 1351 1 FAR 145 . s g a DATE 45:61 49° DISTRICT.OFFICE - .' S EFIV" Altb0 ' ANAT .1649S .- . , " 40 DESIGNEES ., SIGNATURE AND NO . . • . ' . 1 AA INSPECTOR'S SIGNATURE • • FAA Conn 81304 (1243) SUPERSEDES PREVIOUS EDITION ' . 74,..ite. • • EFTA00277878 VI. PRODUCTION FLIGHT TESTING &MANUFACTURER. NAME - • , . . ADORPCS - ` B. PRODUCTION BASIS (Chock epootabie hemp PRODUCTION CERTIFICATE (Gee prOducUon creficate number) TYPE CERTIFICATE ONLY , APPROVED PRODUCTION INSPECTION SYSTEM C. GIVE QUANTITY OF CERTIFICATES REQUIRED FOR NEEDS OPERATING DATE OF APPLICATION NAME AND TITLE (Print Or type) T SIGNATURE VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER THAN PRODUCTION FLIGHT TEST A. DESCRIPTION OF AIRCRAFT REGISTERED OWNER ADORES.) BLIILOER (Make) .. MODEL . • SERIAL NUMBER • • - N .. • REGISTRATION MARK ,:' • • . .. • • • • ' .... . . . ,, . . . I B. DESCRIPTION OF rucirkr.... • . ' “. ..._.. 4 &STORER DEMONSTRATION WORTS 0 tailor It sPOliceloW FROM ---• ...- VIA DEPARTURE DATE - • DURATION , • .. -_,.. ' . C. CREW I REQUIRED TO OPERATE THE AIRCRAFT AND ITS EQUIPMENT,. • 'PILOT , I I COPILOT : I I NAVIGATOR • I I OTHER (Specify) D. THE AIRCRAFT DOES NOT MEET THE APPLICABLE AIRWORTHINESS REQUIREMENTS AS FOLLOWS: • • . - • • • . • • ..' .... . ... i . — ..." . .. . . . . • ' - • " . .. " " • - • ' • - .. • 1'1 - " • " ' - r _ . . .. • .i .• : . • • • • • • • • .. ..... .. .. . . . . it . .... .. - • .. - ,. _ - .... . . .. , - . .- . . . . _ •• , - - - E. THE FOLLOWING RESTRICTIONS ARE CONSIDERED NECESSARY f OR SAFE OPERATION (use attachment il necessary) ... .. . . • .... . . .. — . . - '•. - - .. . • . . • ' - • • • . . „. • - • r . . . . . . .,. . _ • .- . S ... : • . . • • • F. CERTIFICATION —1 hereb yceiThlty ItIM larrf the Ng 'marathoner (Or Ms agent) of UmaIrcraft deseri bidabovir.trail the aircraft la registered wish Ih•Federal Aviation Administration In accordance with Section 601 of the Federal Aviation Act of 1956. and applicable Federal AviationFlegulations• and the Sircratt has ban inspected and Ii airworthy for the flight described. ‘ • , • ' • ' . • : • •• • . DATE • • , . . NAME AND TITLE (Pant or rypej: N. • . . • .. .... SIGNATURE i I i 4 I i 3 a Ci g a 4 F V Operating Limitatiora.and Markings in "replant, with FAR • 91. 1 as pUcable CL,Stisteinent of Confcetnity, FAA Foi m 11130-9 (Attach when required) . H. Foreign Airworthiness Codification for Import Airc.A f Attach when required) . . . . . . . "'--: t. ve 2.„ B. Carron' Operating Wildfire Attached% i •• N. ' .. . . . --" C. Data. Drawing's, photographs. fit (Almon when foqukocl) I Pnnious Airworthiness Certificate Issued In Accordance with . FAR 2/. 191(b) CAR (Original Attached) / . D. Current Weight end Balance Inlonnation Available In Aircraft ' ' • • 4 ' E. Major Repair find Aberration. FAA Form 337 (hhech'When *end) • • dance with •L Current Airsortinnere Certificate Issued i Accor (Copy elisch Fan 21 .1910)) g n4 Q?) ed) keir F. This Inspection Recorded in Aircraft Records . 4 • -prewar ' 3`.11.,.. • • • . • EFTA00277879 .• A ^ . This tirWrihlillieseterli kat° is isSbettlinderikaltitilti.6* ofthe FikieratAyifttiCal AO Of 1958 , antl the Federal Aviation Regulations (FAR). B • This alrwo rth iness cert Ificate autho reesthe fated* narittid On thereireMeSidet0 donduct production flight tests, and only production Ng 11631.1:61 aircraft registered in his name. No ' person may conduct production flight tests linderithIS certificate: (1) Carrying persons br property for compensation or hire; and/or (2) Carrying persons not essential to the purpose of the flight. - ' . . . . C ...... n o This airworthiness certificate authorizes the flight speCifted on the reverse side for the purpose shown in Block A. .ii—i This airworthiness certificate certif les that. es of the date of Issuance, the aircraft towhich issued has been inspected and found to meet the requirements of the applicable FAR. The aircraft does not meet the requirements of the applicable comprehensive and detailed airworthiness code Es provided by Annex 8 to the Convention On International Civil Aviation. No person may operate the aircraft described on the reverse side: (1) except in accordance with the applicable FAR and in accordance with conditions and limitations which may be prescribed by the Administrator es part of this. certificate (2) over any foreign country without the special permission of that country. E . % • . Unless sooner surrendered, suspended, or revoked, this airworthiness certificate is effective for the duration and under the conditions prescribed in FAR Part 21. Section 21.181 or 21217. 4•11 1. EFTA00277881 . Form Approved 0 M R. No. 2120-0016 g tri ti set • • a - 0 . - APPLICATION FOR US Deponmere AIRWORTHINESS .- at Ihrepcnohon -i Fedora kakilion CERTIFICATE • Admisercassin - .. J INSTRUCTIONS — Pnnt or type. Do not write in shaded areas: these are for FAA • on cmly. Submit original onty to an authorized FAA Representative If additional - SPaCetarteuired, use an attachment. For special flight permits complete Sect. 0ns • 13 end VI or VII O applicable. I. AIRCRAFT DESCRIPTION I.REGISTRATION MARX iL) SV S e < ZAIRORAFT GuiLoeyrs NAME WON . . CSO Et.)06 }AIRCRAFT mom DESIWiATiON b..W4!' s.:. " — • 727— )00 I. AIRCRAFT SERIAL NO. . i. 0 / 15 Et. ENGINE BUILDERS NAME Wakes Pee be.) - &ENGINE NODEL DESIGNATI , Ji ll 8M ) In' "sk 219 •-.:;":.. .:. ---- . 1. NUMBER OF ENGINES CPROPEU.ER ISUIL7A Ale MOW A PROPELLER MODEL ons GNATION. 10. AIRCRAFT IS rCoock it •orhcicv, ok IMPORT II. CERTIFICATION REQUESTED • ..... APPUCATION IS HEREBY MADE FOR: (Crum solikeeDrit items/ - A :I: STANDARD AIRWORTHINESS CERTIFICATE 'Masco re category(' 'NORMAL' I UT1UTY I 'ACROBATIC' 'TRANSPORT GLIDER i8At.i.00t4 8 `..P Y. SPECIAL AIRWORTHINESS CERTIFICATE (Check stonsonett MIM) LIMITED • L i • it; cuss i • • . PROVISIONAL /inmate clan) . at. III . • z••• AGRICULTURE AND PEST CONTROL '::: AERIAL SURVEYING -;,3. AERIAL ADVERTISING : 3 - RESTRICTED (Immure operations to De committed) ., . „ p66 FOREST (WSW ecoservamml 4: . .. PATROLLING .e WEATHER CONTROL y. tit i 'CARRIAGE OF CARGO . . ilf- OTHER (Speedy; j • 9 RESEARCH AND DEVELOPMENT ...' B. AMATEUR BUILT .•- 3 EXHIBITION • EXPERIMENTAL ihNOVIIO operation/ s i .:• 4o PO cOnductodi • ‘44I RACING 40 . CREW TRAINING X MKT SURVEY ' 1 t .7. " 4 tit IA TO SHOW COMPLIANCE WITH FAR e FERRY PLIGHTFOR REPAIRS. ALTERATIONS. MAINTENANCE OR STORAGE SPECIAL FLIGHT PERMIT ilndcalo '2 EVACUATE FROM AREA OF IMPENDING DANGER °pew/on to be conducted illy.: Sedan VI VII as ''.:3 OPERATION IN CXCESS OF MAXIMUM CERTIFICATED TAKE-OFF WEIGHT cc-nplele or applicable on reverie idea B DELIVERING OR EXPORT .61 I PRODUCTION FLIGHT TESTING • .74.. CUSTOMER DEMONSTRATION FLIGHTS C PS. I MULTIPLE AIRWORTHINESS CERTIFICATE (Check ABOVE liestnaml Oraranner end -Steislare or -Lveded. 'as applicable.) ' g .t 9 14* 5 0 A. REGISTERED OWNER (As shown on certificate of welsh npistrstion) J..; IF DEALER. CHECK HERE ----w- I "'t NAME 1,g 1. NOttilAuti261 1401-0tOtr t 0-400 0 rp iTi On . ADDRESS Foil tecs-Ries 41 .64Pti MT &.k Pi-4?-4 1$ WM kh1,11419 ;tent letAti IAA 1 M6-7,P1 Wfrigintha irfff03 B. AIRCRAFT CERTIFICATION BASIS (Cheek applicable blacks ana comps. awns as indicated) t AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE Diri A sliEET (Give Na end Revision Na) . : . AIRWORTHINESS DIRECTIVES latest AO No.) (Chest 4 all amicable AOS merged WWI and give AIRCRAFT LISTING (Give aga number(sc SUPPLEMENTAL TYPE CERTIFICATE lbw rhimber OleeCh STC income/area. • C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS . / CHECK IF RECORDS IN COMPLIANCE WITH FAR 01.173 . TOTAL AIRFRAME HOURS • . " PI' .,gs-1, 2.: 3, A ..8j Et d PERIor MEN tenn TALadOINLY (E/ 76::::„8„ ,sil.o.,..ince,„„cesid.coe D. Administration &moiety CERTIFICATION — I hereby cattily that I in accordance with Section 50 and eligible for the einvorthinna madam am Me registered owner far his agent) Of the @naafi daunted above: MN the sworn of the Federal Mutton ANY IEEE. rdappliCableFriferst Aviation Regurabons, and reauested. % . . ' • . . - - • •• . • . tiered with the Federal Aviation mat eve we has been inane and es DATE•OF APPLVATI0N / 5/ / 9c• .:.- NAME AND TITLE/Penaor tysiN . er-1 . tati4•41-7 ._, - eat..O 7— , IV. INSPECTION AGENCY VERIFICATION A THE ESCRII3ED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Complete Ma when only it FAR AIRCRAFT 21. WWI Aghast .{.1, trot FAR PART 121 OR 121 CERTIFICATE HOLDER (Om Certificate No.) • % CERTIFICATED MECHANIC (One. Certificate Nat • . CERTIFICATED REPAIR 5 ANON (Give Certificate Nal rit AIRCRAFT MANUFACTURER (Give nem or Wm) DATE TITLE SIGNATURE s .-"IeN Nie - • aw.. cs (Check ALL epplecebte Mocks In items A endial ' THE CERTIFICATE REOUESTE9 ms A. I lend that me aim reh described In Section I or VII meets (immanent* for. .7.>1 AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CEMIFICATE a. Inspection tor a special MgM permit under Section VII FM INSPECTOR, FAA DESIGNEE i.8. was conducted by: CERTIFICATE HOLDER UNDER: FAR 6S , ' FAR 121. 127 a1351 1 FAR tits 47 2. i g i ri DATE Q5-6/-90 DISTRICT OFFICE SEA-Mtbc, • . 4$ DESIGNEE'S SIGNATURE AND NO. I- 1- Jr -4V. AA INSPECTORS SIGNATURE . • • . • mmeicias .. FAA Form 8130.6 (1243) SUPERSEDES PREVIOUS EDITION • •e z • I% e t-c='..- • 5'11•• /A' • ` - y,Y A•St • r-. - • • •r• ti . i. -a A EFTA00277882 一一：7 老汹一d 一： 一一L3．一一・．一一c EFTA00277883 VALSitikkaktliEtts_:. . 3014 .Westcheiter :Averiue Purchase's, N.Y. :10577 ..• (914)":694-3600 I. May 1, 1990 FAA, `ANM"1085 . 7300 Perimeter Rd. Seattle, WA 98108 • :Dear Sir, '• Attadhed is FAA form 8130-6, Application for Airworitaneths ...Certificate, for adding "Market Survey° to the authorized operations of our Experimental Airworthiness Certificate. The aircraft is a Boeing 727-100 which has been retrofitted with P & W JT8D-219 engines on 'the POD positions and -7B in the center position. We have flown the aircraft approximately 17 hours under the presently issued Experimental Certificate.S We are requesting "Market Survey" so that we may take a TV reporter and cameraman from Paine Field, Everett, Washington to Grant County Airport, Moses Lake, Washington on 1 May 1990 for demonstration of the- Stage IIV Noise Characteristics:.. ' .The duratiOn of the "Market •Survey" portidn of this .Experimental Certificate :will be only. :for `the. one, flight' from Paine Field to Grant County Airport. The: certificate will then revert to "Show Compliance with FAR's" 'until expiration of the certificate on. ,1 August. 1990. • -ze EFTA00277884 V rr-re,ar,PKv-, a•ALL.... • • - EFTA00277885 -FAA. AIRCRAFT REGISTRY CAMERA NO. N DATES 02- gi USDepartment ; • , of Transportation ' Federal Aviation Administration 4,At,r14.,Ac:t Manufacturing Inspection District Office 7300 Perimeter Road South Seattle, WA 98108 May 1, 1990 EXPERIMENTAL- SHOW COMPLIANCE WITH FAR's/MARKET SURVEY MAKE: Boeing MODEL: 727-31 SERIAL NO. 20115 REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft must be operated in accordance with the following limitations: 1. No person may operate this aircraft for other than the purpose of Show Compliance with the FAR's and Market Survey to accomplish the tests outlined in the applicant's program letter dated May 1, 1990 describing compliance with FAR 21.193(d). • Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). 2. All flights shall be conducted within the geographical areas described as follows: 1. Western United States of America bounded on the East by the Mississippi RiVer, on the North by the U.S.A./Canadian border, on the South by the• U.S.A./Mexico border, and bounded on the West by no more than 200 miles from the Wedt Coast of the United States of America. 2. Base of operations is Palmdale/ Lancaster Airport, Palmdale, California and secondary base of operation to be Moses Lake Airport, Moses Lake, Washington. 3. The 'pilot-in-command of aircraft must, as applicable, hold an appropriate category/class rating, have an aircraft type rating, have a flight instructor's log book endorsement or possess a "Lgtter of Authorization"\issued by an FAA-General Aviation or Air CaYrier'Operations Inspectbr. , 4. This aircraft shall not be flown unless it is maintained and operated in accordance with .Boeing-Low Ut'Jlization Program, I/A/W FAR 91.169(f)(4). 5. Upon changing between operating purposes of a Multiple Purpose Certificate, the operator shall determine that the aircraft is in a condition appropriate for the purpose intended and has documented that finding in the aircraft log. 6. This., aircraft shall contain the placards, markings, etc. required by FAR 91.31. • '7 - -st EFTA00277886 , Federal Aviation` Administration Manufacturing Inspection District Office - - • , • Experimental - Show Compliande with FAR's/Market Survey, Cont'd Page 2 of 2 7. The'Lcognizant FAA office Must'be.notified and their response '.received'in writing prior to flying'this aircraft after' • incorporating a major change as defined 'by:FAR 21.93. 8. This aircraft approved f(* .itair/night VFR/IFR only. • 9. No operations shall be'conduCtid. over densely populated areas :or in congested. airways excejytfOr.takeoffs and landings, and when - under ATC control. ' 10. No person may be carried in this‘aircrait during flight unless that person is .essential for the purpoie of the. flight while in the ' Show Compliance category. '11. Thib aircraft is prohibited from aerobatic flight;sthat is, an intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved.by the cognizant O' A Office. 12. If aircraft, engine or propeller operating limitations are exceeded, an appropriate entry will be made in the historical records. ' 13. After the aircraft 'has been re -engined, the pilot-in-command must make a log book entry stating.the aircraft complies with FAR 91.42(a) and FAR 91.42(b).. Mic ael J. Aviation Sa -ty Inspector (Mfg) SEA-MIDO, ANM-10SS These limitations will expire on August 1, 1990. EFTA00277887 VALSAN PARTNERS . 3014 WeatcheAtet.Avenue Purchase,'Na.- -10577.. ' • . f914) 6943600' May 1, FAA,\ANM-74.08S.: , 7300 Perimeter:Rs:I.e.: .Seettlei:WAH 98108- AttaCiled is; FAA form 813076,. Application for -Airwerthibeea. Certificate for adding "Market .SurVey" .to the authorized operations of our Expeiimental Airuorthihess: Certifibate. -• - • - • . . . . The aircraft'is a Boeing 727-100...Whibhhas been retrofitted with P & W.JTBD-219 engines on the POD pOsitiOnS•And -78 in the center position. We have flown the aiicraft'AppiOximately 17 hoUrsunder the presently issued Experimental Certificate. We are requesting "Market Surveil." so that we may take a TV reporter and cameraman from Paine Fie10,-EverettOiashingioeto'Grant County Airport, Moses Lake, Washington .Oa 1 May 1990 forsaemenstration of the Stage Noise Characteristics..; s . . c _ The duration .of 'the "Market Survey" of Experimental Certificate will be only for the one, flight'fiom. Paine Field to Grant County Airport. The. certificate will'thenrevert to. "Show Compliance with FAR's" until expiration of the certificate. on: 1 August, 1990. . • Sincerely yours, EFTA00277888 FAA. AIRCRAFT REGISTRY CAEERA ICO„ iN DATE: 2 — — et,..aar 51 - a .4 tia*. (FL st, t‘ 4:5'n YAtEstmmakibik 'DERARTmENToFTRANSPORTATION-FEDERALAVIAYIDNADMINISTRATiolt1 SPECIAL AIRWORTHINESS CERTIFICATE Any eh on, reProduction or misuse of this certificate ma /table by a fmc not exceeding S L000 or imprisonment o exceeding 3 years, or tinik THIS CER11FICATE MUST BE DI LA YED IN THE AIRCRAFTIN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS FAA FORM 0130-7 (7-70) USE PREVIOUS EDITION • `Y:epterr'r let ter . •• . - ' EFTA00277890 407 US.Departant of Transportation Federal Aviation Administration February 2, 1990 Manufacturing bispection District Office. 16501 SherinanWayi—Suite 200 Van Nuys, CA .91406 . . EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's 3-4 MAKE:'Boeing MODEL: 727-31 SERIAL NO. 20115 REG. NO. N505C THESE OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT This aircraft mustbe operated in accordance with the following Iimitations: No. person may operate•this .aircraft for--other than-the purpose of Show Compliance With the FAR's to accomplish the tests outlined in the applicant's program letter dated February 2, 1990 detcribing compliance with FAR 21.193(d),_Additionally, this aircraft shall be operated in accordance with applicable air traffic and general operating rules of FAR 91, and all additional limitations herein prescribed under the provisions of FAR 91.42(e). ' • 2. All flights shall be conducted within the geographical areas described as. follows: ' 1: Western United States of America bounded on the East by the Mississippi River, on the North by the U.S.A./Canadian.border, on the South by the U.S.A./Mexico border, and bounded on the West by no more than 200 miles from the West Coast of the United States of America. 2. Base of operations is. Palmdale/Lancaster Airport, Palmdale, California and secondary base of operation to.be Moses Lake Airport, Moses Lake, Washington. 3. The pilot-in-command of aircraft must, as applicable, hold an appropriate --""166 -bboirentibitVme ss ss1"1:etter of Authorfiationft-issued'by an FAA category/class r tin , aircraft tYPe rating,.. have a flight instructor's General Aviation or Air Carrier Operations Inspector. ' 4. This aircraft shall not be flown unless it is maintained and operated in . accordance with Boeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. This aircraft shall contain the platards, markings, etc: required by FAR 91.31. 6. The cognizant FAA office must be notified and their response received in writingprior to flying..this aircraft after incorporating a major change as defined by FAR 21.93. . 7 This aircraft.approved.for day/fiight:VFR/IFR only. EFTA00277892 FAA, AIRCRAFT REGISTRT CAT:ERA NO. I DATE: 02. g ;,..;••• s , "Fedelll AViAtiott AdidiAittiatia Manufacturing Iiiipectitid Oistrii*Offitt-- Experimefital - Show CompliaNdi'With cdntsd Page 2 of 2 % 8. No operations shall be conducted over densely populated areas or in :congested-airways except for"takeofft and landings, and when under ATC control. 9. No person 'may be carried ,ip:thisaircraft dUring flight unless that person is essential for the purpose of the flight. 10. This aircraft is prohibited from aerobatic flight; that is, in_ intentional maneuver involving an abrupt change in the aircraft's attitude, an abnormal attitude or abnormal acceleration not necessary for normal flight unless approved by'the cognizant FAA office. 11. If aircraft, engine or propeller operating limitations are exceeded, an apprdpriate entry will be-made in the historical records. 12. After the aircraft has been,re-engined, the pilot-in-command must make a log boOk entry stating the aircraft complies with FAR 91.42(a) and FAR.91.42(b). bert Stagg R-48-AC-NM 'These limitations will expire on August 1, 1990. ect.,:gm te**"" r ...‘4!‘ '‘';'N"te.00.6frte4i0,44:'""--"- `: • EFTA00277893 FAA AiRCRAFT.REG1STEE CA? ELA WO. i. ,tr DATE: 2-21- 9 fd mow...—...a.,--... dir:ah. 0.••••••••••••.. •-• rt, • •- • • . 0 MAJOR REPAIR ALTERATION L I S I D e v o r t i n e m as scruDortaucc . (Airframe, Powerplant, Propeller, or Appliance) Pearce Aviation Acteriatishotion • • . . .... . . ' . • Form Approved OMB No. 2120-0020 For FAA Use On:y Office Identification ,S0- Fs a 0 --/sr INSTRUCTIONS: Print or type all entries. See FAO 43.9, FAR 43 Appendix 'land AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. This report is required by law (49 U.S.C. 1421). Failure to report can result in a civil penalty not to exceed $1,000 for'each such violation (Section 901 Federal Aviation Act of 1958). I. Alrcraft Make • Boeing Model . B727-31 Serial No. • • • 20115 Nationality and Registration Mark N5 0 OLS - 2. Owner • 1. Name (As shown on registration certificate) .. •• • • VorthweS€ Holding •.Corporation - . Address (As shown on registration certificate) . . • P.O. Box 7138 Wilmington, DE 19803 3. For FAA Use Only - • • ‘ • .• - -- ;.• , . . - . , . - : . . .. .-- . , . . _ „ „.. .• . ,.. • • 4. Unit Identification 5. Type Unit • • Make Model Serial N9. Repair Alteration AIRFRAME .... Os described in Item 1 above) • • •• X POWERPLANT • - ., . PROPELLER \ • • ----7N s • • • APPLIANCE Type • • .: . . .. . - ( -,._ Manufacturer • 6. Conformity Statement A. Agency's Name and Address B. Kind of Agency C. Certificate No. Page Avjet Corporation . 9809 Tradeport .13r4ye '. Orlando/a_ Florida 32827 . U.S. Certificated Mechanic OS4R425M • Foreign Certificated Mechanic A Certificated Repair Station _ Manufacturer D: I cert ifAhat the repair and/or alteration made to the un t(s) identified have been made in accordance with the requirements of Part furnished herein Is true and correct to the bested my know in item 43 of the U.S. 4 above and Federal Aviation deicribed on the Regulations reverse or attachments hereto and that the information . • • . e. Dal.) • . gnature of Aut Individual . .. .. 7. Approval for R urn To Service t, • Pursuant Administrator By • to the authority given persons specified below, the` nit identified in item 4 was inspected in the manner prescribed by the of the Federal Aviation Administration and Is APPROVED 0 REJECTED • • FAA Flt. Standards Inspector Manufacturer Inspection Authorization • Other (Specify) • • • FAA Designee x Repair Station Person Approved by•Tranapart Canada Ainvonhiness Group Date of Approval lit 6E,Pr. or Rejection 90 Certificate or Designation No. • : 0S4R425If. ' Signar—obailhorized iteAr8 Individual / .. d:41,,?! -.7n/L i.i . FAA corm 337 • etiaftZVotcesere.Lesz• scraslY -co;341-- . EFTA00277894 z 4Q • z -1.5t)c'er:k-t fr,4- t"\.- Jr ' ;G• . . - NOTICE Weight and balance& operating limitation changes stiell.be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the aPplicable airworthiness requirements. • 8. Description of Work Accomplished • fit more space is required, attach additional Sheets. Identify with aircraft nationality and registration mark and date work completed.) B727-31 S/N 20115 1. -MODIFIED J:POWERPLANT-:-INSTALLATION :4).1-FACILITATE RE-ENGINE PRODUCTION. FOR AIRCRAFT HAVING REMOTE ENGINE OIL REFILL SYSTEM IN ACCORDANCE WITH' VA 71000, REV. .48:,...DRAWINGS PER DER'TH0MAS F. . tCUBRAN NM-a83, APPROVED BY-8110 DATED SEPTEMBER 4, 1990. PERFORMED AIRSTAIR INSTALLATION :IN ACCORDANCE WITH REPORT. 442 (STRUCTURAL SUBSTANTIATION. OF.EXTERNALDOUBLER AND .MISCELLANEOUS COMPONENTS FOR INSTALLATION OF: FORWARD AIRSTAIR) AND REPORT 444 (INSTALLATION INSTRUCTIONS, BOEING'727f00 FORWARD‘AIRSTAIRI AND 6 IN'ACCORDANCE WITH• 750-1-P002. DATED 94101990 BY D.E.R. BOYD SMITH S0-351. • PROVIDED WEIGHT AND.BALANCE UPDATE. 'EQUIPMENT -LIST UPDATED ACCORDINGLY.. ALL SYSTEMS OPS CHECKED AND DO INTERFERE WITH OTHER SYSTEMS. •ALLPERTINENTDETAILS OF. WORK. ACCOMPLISHED ARE ON FILE PAGE, AVITETCORPORAT;Pki UNDER WORK ORDERS'4706.AND 6778, DATEP://ri/sJT:Ani(07,. END ,, ,,„,,agic„„iggetroiralt.‘aantatrra` • EFTA00277895 Twvemqs7PapIlilvt%"=c- iTlA alECKAFT REGISTRY CA'r,ERA p0.7 N DATE: 12-21-90 • r r • • .;it••• • rat -1;1:jilt/Ilea 31;sammi,spdpeammisMINIa _-zdaRatagec.-- EFTA00277897 gicgorglict—Soscref&r.t.kirrs FAA AlRCF.AFT REGISTRY C.UtIF.A N DATE: 12-41-90 • •• ••=. - t:•4; ..40;rs.g. .AL • •:'44 '• ••• UNITED STATES Of AMERICA DEPARTMENT OF TRANSPORTATION—FEDERAL AVIATION ADMINISTRATION ' STANDARD AIRWORTHINESS CERTIFICATE NATIONALITY AND REGISTRATION MARKS N505C 2 MANUFACTURER AND MODEL BOEING 727-31 3 AiriCRAL7 SERIAL NUm0E0 20115 4 CATEGORY TRANSPORT 5 AUTHORITY AND BASIS FOR ISSUANCE • Trtsalmorthinefulcertilicela is issuedpursuanl toilleFederal Aviation Aci of 1958andcerfilles ai oftheMte of iisuance aircraft to which issued has been inspected and found to conlorm 10 the Ilse cenificale therefor lo be m cvochhon for salt operation, and has bean shown lo hysel the requer errant& of the applicable comnrenensive an detailed aimontimuss coot as provided by Annex a to the Convention ohIntematoonal Cml Aviation.excem as noted herein EaraptiOnt • NONE ' • ' B. TERMS ANO CONDITIONS LIMN* 5004r surrendered. suspended. revoked. or a termination date us otherwise etlabhiliel tw.the AdmatflatOr ibis alnvorthincee certificale is ellimint N long as Me maintenance preventative maintenance and nitenitiort air perlotn*d In IccordencewithPerts21.43.andfll ol Huffed**, Aviation Regulations. estop, ate find the aircraft •i registered itIll•ets• d Stets& DATE OF ISSUANCE 7/23/90 Any attenition.feprohuclion.tx CellibefratemaybeliontinITM nol exert 000.o implisd'imtolmilexerealmj 3 years. or boib. THIS CERTIFICATE MUST BE DISPLAYED IN THE_AIRCRAFT IN ACCORDANCE WITH APPLICABLE I-El:WAAL AVIATION REGULATIONS. FAA Form 8100-2' ore2) CPO ena•nt•4 usa of \hosso FAA REPRESENTATIVE % WING C. CHIA. ea% DESIGNATION NUMBER DAR-41-FS-NM • i.cm..4 O.:my boa - 8. ;frial: • -Nisi, lab • ••••• •••• Cfr• EFTA00277898 a•74.1 ..J1V-r•-_ -"Wiii'illr.7. , .cam, , :,r; FAA AIRCRAFT REGISTRY .CA4TRA R0. 7 N DATU ...c; s4op • • doittacaYom. P•46 .--•)4 • ear-t;s6--"aAl.:- WASEA.I.TAMILle••=iliaWEi.rfcq ',..!gt• • R. . tr•U•••_. vs' EFTA00277899 AA AIRCRAFT REGISTRY C RA NO. 7 N DATE: 8- 15- 90 r N a . ireg., • - 1.0” . . . 1 .it-- ....., • , * 1)10 ty • $,• t • • • .a.t."' vow Form Approved • . 0.M .8. No. 2120-0018 I , APPLICATION FOR I Ultieoccirned . AIRWORTHINESS • Federal ‘4311on CERTIFICATE mhastranon INSTAUC710NS -- PrInter typo. Do not wrlte in shaded areas; those are for FAA use only. Submti original only to an authorized FAA Representative. If additional Space's required, usean attachment. Forspeoial flight permits compleloSections II and VI 01.VII LIS 440floa,b11).; , I I. AIRCRAFT l DESCRIPTION ltREGUSTRADON MARK I1S05C 2.A1RCRAFT BUILDER'S NroCE (AEON Boeing AIRCRAFT MODEL SI NATtON \ ,J - D ‘ t\ - • •• to-;ti 727 -31 • - YR. WA 4, COOING 69 FAA / 3 ,gc70/0 • . 5. AIRCRAFT SERIAL NO. i 20115 5 & ENGINE f3UI L DER'S NAME mak; Pratt S Whitney - 7. ENGINE MODEL DESIGNATION - JT8D-,76 ,k5 3 ts'm 8. BER OF ENGINES 3 • . 9. PROPELLER BUILDER'S NAME (Make) 10. PROPELLER MODEL DESIGNATION 11. AIRCRAFT IS (Check it appttc•bio) 1 IMPORT 0 a F iB = -e, APPUCAT1ON IS HEREBY MADE FOR: (Choc applicatninimu A I STANDARD AIRWORTHINESS CERTIFICATE (/rtcocatit cerog,try) I 'NORMAL I 'UTILITY 1 'ACROBATIC' 'TRANSPORT 1 'GLIDER I I BALLOON El SPECIAL AIRWORTHINESS CERTIFICATE (Check appropriate ilinu) e `3 .. LIMITED 1 CLASS I .. cl PROVISIONAL (Indicate attl) 2 CLASS II 1 ' AGRICULTURE AND PEST CONTROL 2 AERIAL SURVEYING 3 AERIAL ADVERTISING 1 RESTRICTED ffnetteste opershonEt)I0 be conducted) 8 FOREST (WrAlloto consarvenan) I ,, pATROLLING a WEATHER CONTROL --, I CARRIAGE OF CARGO 0 OTHER (Specify) 4/ . RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT '8 EXHIBITION 4 nd EXPERIMENTAL (Indicate operetiOn(a) to a conducted) 4 RACING I CREW TRAINING MKT. SURVEY l X ei X TO SHOW COMPLIANCE WITH FAR • 7 FERRY FLIGHT FOR REPAIRS, ALTERATIONS, MAINTENANCE OR STORAGE SPECIAL FLIGHT PERMIT Warta 2 EVACUATE FROM AREA OF IMPENDING DANGER 3 operation to be Conducted. then complete Section VI or VII as I OPERATION IN EXCESS OF MAXIMUM CERTIFICATED TAKE-OFF WEIGHT a applicable on remise style) . 4 DELIVERING OR EXPORT I I1 I PRODUCTION FLIGHT TESTING - • • a CUSTOMER DEMONSTRATION FLIGHTS c I a♦ MULTIPLE AIRWORTHINESS CERTIFICATE (Check ABOVE 'Restricted °potation" and "Standard' or -Limtled.- as applicable) z 0 p 5 a €€ ii : • i, Iii S it A. REGISTERED OWNER (As shown on ceittficale of aircraft registration) IF DEALER, CHECK HERE 1 NAME • Northwest Holding Corporation ADDRESS Foulkstone Plaza, Suite 102 1409 Foulk Road, P.O. Box 7138, Wilmington,DE B. AIRCRAFT CERTIFICATION BASIS (Check applicable blocks and complete darns as indicated) 1.9B03 r AIRCRAFT SPECIFICATION OR TYPE CERTIFICATE DATA SHEET (One Na end Revision No.) A3WE X AIRWORTHINESS DIRECTIVES (Check it all Appic ego AD's con) plied watt and pare West AD No.) 90-02-19 AIRCRAFT LISTING (Ciro page numbs:fit) Rev, 18 - Dated February 20, 1987 SUPPLEMENTAL TYPE CERTIFICATE (Cut number of each SIC Incorporated) C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS X CHECK IF RECORDS IN COMPLIANCE WITH . FAR 97175 TOTAL AIRFRAME HOURS . 29820 Hours • - a EXPERIMENTAL ONLY (Enter hours flown salts leaf cart tficels issued Oe renewed) -0- D. = CERTIFICATION — I hereby certIty tttat I Administration In eccord•nce with Section 50 orrery:011y and eIrgitale for the mrworthineas certificate em the /agitated owner (or his agent) of the aircraft of tr. Federal Aviation AcI of 1958. end applicable reatenfed• deacnbed above; that the aircraft Firtkra/ Avila:an RegutsIon : and is registered with the Federal Artaticm that the aircraft has been inspected and rs DATE OF APPlICAT ION - February 2. 1990 n oTIT I or I f Valsan .Program R.A. Braulik naineerina & Manager SIGNATURE Z g t t AP 1 g et c V A. THE AIRCRAFT DESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Compite• tan seefron only-if FAR 21. BT(d) applies) e I FAR PART 121 OR 127 CERTIFICATE Carolicat• No.) HOLDER (One ' S I CERTIFICATED Certificate Na) MECHANIC (Cl.. . _ - CERTIFICATED REPAIR STATION (Give COf I, lc a la No.) -.2 ..06 .4 _ AIRCRAFT MANUFACTURER (Dire nem* of firm) J DATE e TITLE SIGNATURE t . F p 0Z CR 3 3 >.1:4 SC N . (Check ALL applicable blocks in items A and Ell THE CERTIFICATE REQUESTED J A. I hnd that the anctalt des/tithed in Section I or VII Ibsen requirements for. 4 AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE B. Inspection tor a apecsal WI privet under SWIM WI ' • FAA INSPECTOR FAA DESIGNEE was conducted by: .. . • -..1. -- CERTIFICATE HOLDER UNDER. _ FAR 65 i _ FAR 121. 127 or 1-...y r frAR 145 DATE 9A-- %pa DISTRICT OFFICE • ‘,(01-0‘ , Nays not goo. . • • 7> 2.• - , ATUR N NO. D --Ape -sr --.9 . ..:::- .....- A., ni , 1 AA INSPECTORS SIGNATURE FAA Form 8130-6 (6.06) SUPERSEDES PREVIOUS EDITION • :V• ...... • "f - " • . • EFTA00277900 E. THE FOLLOWING RESTRICTIONS ARE CONSIDERED NECESSARY FOR saFE OPEFIATIONJUI.datteChInent UneawFwri • . • P. agamealsOpa- eats demay mu i am In reCettered Ores iahsa9.nU Oi Me *wall described ton. Mai the airalin is registered with the Federal Aviation Adminsbetion in itCardenitlitvilh Elect100 al 00 the Feeterel Aviation Act of lelle, end oppaceete Federal Aviation Regulations. end Mat the Wenn has been inspected and is airworthy for the Mod tesic W.= EFTA00277901 ,. UNITED STATES OF AMERICA •• .. DEPARTMENT OF TRANSPORTATION - FEDERAL AVIATION ADMINISTR . ATiOt,.}- i, SPECIAL AIRWORTHINESS CERTIFICATE A BATEGORY/DESIGNATIONri ,A-Zrel - If6t denr PURPOSE ijalAret, . B. • MANU- FACTUFIER NAME ADDRESS ifh• 'C I" FLIGHT . ... FPON1 Atg _7 $: • To 4,4 arta D NmAcc isof SERIAL NO. Z e.tr . MODEL "77:-.0„,/,' BUILDER E . DATE OF ISSUANCESOffrar t /4'99 EXPIRY zehery/f/InetV• A PART OF THIS CERTIFICATE OPERATI LIMITATIONS DATEDS04,09/475WRE WO OF r e ard ed i FAA ATM — DESIGNATION OR OFFICE NO. A r 7 -4 Cbg0 • - — ' . _ .. Any alteration. repmduction or me 1 this carlificaer may be punishable by a line not exceeding 51.000 or Imprisonment not exceeding 3 yearn, or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA FORIIM30.7 me . CPC arl/FligF Ainr EFTA00277902 AA AIRCRAFT REGISTRY RA NO. 1 N DATE: 8- 15- 90 A ^ This airworthiness cenificale is issued under (he authority Wipe Federal Aviation Act of 195‘. and the Federal Aviation Regulations (FAR). • • .. B . . This airworthiness certifiCate authorizes the manufacttiret named on the reverse side to conduct production flight tests. and only production flight tests, of aircraft registered in his narne.,Wo person may conduct production flight tests under this, cestfficpte: (1) Carrying' persOns or prqperty for compensation or hire: and/or (2) Carrying persons not essential to the pitrpose of theilight. . .•• , .• C c' This'aInvorthiness certificate authorizes the flight Specified on the reverssside for the purpose shown in Block A. .. • o . . . . , . . . . ,.. .. , . This airworthiness certificate certifies that, as of the date of issuanCe, the aircraft to which issued has been inspected and found to meet the requirements of the applicable FAR. The aircraft does not meet the requirements of the applicable comprehensive and detailed airworthiness code op provided by Annex 8 to the Convention On International Civil Aviation. NO Person may operate .thaaircraft described on the reverse side: (1) except in accordance with the applicable FAR and in accordance with conditions and limitations which may be preacribed by the Administrator as part of this certificate:.(2) over any foreign country without the special permission of that country. . - r . . . . . . . . .. • - . c F • . . . • • . Unless sooner surrendered. suspended. or revoked. this ainvorthiness certificate is effective for the duration and tinder the conditions prescribed in FAR Part 21. Section 21:181 or 21217. ... . • • - EFTA00277903 1/ UNITED STATES OF AMERICA DEPARTMENT. OF TRANSPORTATION -FEDERAL AVIATION ADMINISTRATION • • STANDARD AIRWORT I ESS CERTIFICATE • • NATKMALITT AND REGISTRATION MARKS 2. MANUFACTURER AN . NSOSC , Boeing . • ; S. AUTNORITX AND BASIS FOR ISSUA I This airworthiness certificate i s urwont • dote of issuance, the aircraft h issued 1 'therefor, to be in condition 1dfe, opera 4 • cornprawnsive and detailed. f iwo /miss i Aviation, except os noted n Exceptions: F. TERMS AND CIADITIONS Unless soon*, sumndirredersu this airworthiness artifice performed in accordance w aircraft is registered In I nil ri 1 DATE OF ISSUANCE FAA REPR IV Exchange 06 oltied,\61‘ long os and 91 of AIRCRAFT SERIAL MOOT 5 Transport 1 and certifies that, as of the t • nform to the type certificate he s ;cements of the applicable • ntion on Internalionol Civil • is net toblished by the Administrator, t. f pints:mance, and alterations or. I *lions, as appropriate, and the DESIGNATION NUMBER Any alatatio reproduction, or misuse of certif.( o ;skiable by a fine no exceeding $1,000, or :tn. prisonme of exceeding 3 years. or both. IS CE TE MUST SE DISPLAYED IN THE AIRCRAFT IN ACCORD. ANCE N APPLICABLE FEDERAL AVIATIO REGULA S. FAA Form 8100-2 (7-6n . • v FORMERLY FAA FORM 5352 „ , • . . —tr. et EFTA00277904 " > > > ＂ 脚 ＾ 州 ＞ 哟 阃 蝉 蝉 。 审 川 帅 阀 6 ' ' ” 是 。 ’ 鸿 ＞ ～ ° ＞ 闩 忡 ＂ 啪 l 料 动 t 漶 EFTA00277905 UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION - FEDERAL AVIATIOArADMINISTR.,TION SPECIAL AIRWORTHINESS CERTIFICATE A CATEGORY/DESIGNATION V rguiTAL PURPOSE TO SHOW CON CE watt, . Roes B MANU- FACTUR ER NAME N •'4:4' 65", ADDRESS _, /-' C FLIGHT 13Y n FROM "-...y \ TO 1 ..6- ttli N- 5456 I Y. l'S ER* 0. 20115 IRJ I L O E R Boeing c t i MODE 727- 1 DATE OF ISSUANCE Fe -t, 1 E 8/01/90" E OP IN M •TION cy 2 PART OF THIS CERT! F ICATE St ae r0 AA %- ORATION OR OFFICE NO. - it • • ' .- • . B RT OAR-48-AC-M . Any ohm on, rtproclliCtIOD or misuse of this artificats way bo punishable by a fine not tzenedina S1,000 or imprisnntnent not ezecerfing 3 yens, or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE writ APPLICABLE FEDERAL AVIATION REGULATIONS. • .. . FAA PORM 6130-7 l7-7P) USE PREVIOUS EDITION SEE REVERSE UDE . 'zierta." EFTA00277906 A - — This airworthiness certificate is issued under the authority of the Federal Aviation'Am of 1958 and the Federal Aviation Regulations (FAR). B , - . This airworthiness certificate authorizes the manufacturer named on the reverse side to con- ' duct production flight tests, and only production flight tests, of aircraft registered in his name. No person may conduct production flight tests under this certificate: (I) Carrying per- sons or property for compensation or hire; and/or (2) Carrying persons not essential to the purpose of the flight. C "' This airworthiness certificate authorizes the flight specified on the reverse aide for the pm- pose shown in Block A. , air- ' • ,. ' This airworthiness certificate certif161 that, as of the date of issuance, the aircraft to which' issued has been inspected and found to meet the requirements of the applicable FAR. The aircraft does not meet the requirements of the applicable comprehensive and detailed worthiness code as provided by Annex B to the Convention On International Civil Aviation. No person may operate the aircraft described on the reverse side: (1) except in accordance with the applicable FAR and in accordance with conditions and limitations which may be prescribed -by the Administrator as part of this certificate; (2) over any foreign country with- out the special permission of that country. c E . . - Unless sooner surrendered, suspended, or revoked, this airworthiness certificate is effective for the duration and under the conditions prescribed in FAR Part 21, Section 21.181 or . 21.217. +t fo EFTA00277907 1.• A -s - ••••••• • • T• • p. USDepairreor of Transportation Federal Aviation Aderdnismation February,2, 1990 EXPERIMENTAL - SHOW COMPLIANCE WITH FAR's MAKE: Boeing MODEL: 727-31 SERIAL NO. 20115 REG. NO. N505C - THESE-`OPERATING LIMITATIONS SHALL BE ACCESSIBLE TO THE PILOT rw Manufacturing Inspection District Office. 16501 Sherman Way, Suite 200 Van Nuys, CA. 91406 This aircraft must be operated in accordance with the following limitations: • 1. too person may operate this-aircraft for other.than-the purpose of Show Compliance with the FAR's to accomplish the tests outlined in the ' applicant's program—letter dated%February.2, 1990 describing compliance with FAR 21.193(d). Aldditionally, thit aircraft-shall be operated in accordance with applidable air-traffic and general operating rules of fAR 91, and all .additional liMitations herein prescribed under the provisions of FAR 91.42(4). . 2. -All flights. shall.be conducted within the geographical areas \ • described as follows:. 1. Western Mnited States of America bounded on the East by the Mississippi Riier, on the North by the U.S.A./Canadianborder, on the South. by the U.S.A./Mexi,co border, and bounded on the West . by no more than 200 mileS. froM the West Coast of the United States of America. • 2. . Base Of operations is Palmdalettancaster Airport, Palmdale, 'California and secondary base of operation to be.Moses Lake Airport, Moses Lake,.Washington. f ' 3. The pilOt-in7command of"afrdraft must, as applicable, hold an appropriate category/class rating: have an aircraft type rating, have a flight instructor's. — log book-endorse:lent. of"possesi a "Letter of Authorizatton"-lssued by an -FAA • . General Aviation'or Air Carrier Operations Itspector. 'A. This aircraft shall not be flown Unless it is maintained and operated in accordance with"BOeing Low Utilization Program, I/A/W FAR 91.169(f)(4). 5. -This aircraft shall contain the platards., markings, etc: required by .FAR 91.31. • 6. The cognizant FAA office must be notified and their responge received in writing prior.to flying this aircraft after incorporating a major change as defined by FAR 21.93:. 7. , This aircraft approved for day/light .VFR/IFR -":1" rv$1777= "T-IlenialrgitykraMr-rce-- • ?-4 rf EFTA00277908 Federal Aviation Aftinistration Manufacturing Inspection District OffiCa , • ! - .:. • - Experimental -Shell Compliance.With FAN'S, Page 2 of 2 8. • No operations shall be conducted over densely:OnOulated-ardo or in, 'congested airways except for takeoffs and1andings, and When,Under.ATC.O0tre!. . ••• . ',No persOri.may be carried in this aircraft during flight unlets that -person is essential for-the purpose of the flight. 10. This aircraft is prohibited from aerobetic flight; that is, an. intentional maneuver` involving an.abrupt -change in the'ait.craft's attitude, an' abnormal attitude or abnormal acceleration not necessary for:normal flight unless approved.by the cognizant FAA office. - . . . 11. .If-aircraft, engine or propeller operating limititions are-exceeded, • an appropriate entry. will be made, in the historical records: 12. After the'aircraft hasImen re-engined, the pilot-in-command must make a log book entry stating the'aircraft complies with FAR 91.42(a) and FAR 91.42(b). T6eieilimitati0nS:*11.1 expire on August 1, 1990. EFTA00277909 AnclAPT NEOISTAV CAMBIA NO. 1 N DATE: 8- 15- 90 VALSAN• PARTNERS 3010 Westchester Avenue. Purchase. New %TX 10577 .* • (914) 694.3600 Telex: 825379 VALSAN OF Fax: (914) 694.6062 ADelawareLtavtedRinnemhip Febfbify 1990 Marketing Office: 99 Washington Street. Norwalk, CT 06854 (M3)866-6051 • • Telex: 6714726 DALAV UW Fax: (203) 855-0362 Product Support Office: 3605 Long Beach Blvd, #205 Long Beach, CA 90807 Tel: (213) 424-2145 Fax: (213) 595-0920 Mrt Bud Martell, Manager • . . Federal Aviation Administration Manufacturing Inspection District Office.• In reply . .16501 Sherman Way, Suite 200 • refer to Van NuyS, CA 91406 * . 001020290 .Subject: Application fortxperiMental Airworthiness Certificate • (To'Show Compliance. withFA,Ri) .- • • Gentlemin: This letter is toinfotii\You.thai- Valsan intends to operate Boeing • . . 727-31 ,. Registration N505C, Serial #20115 owned by Northwest_ Holding COrporation,Foulkstohe Plaza, Suite 102, 1409 Foulk Road, P.O. Box 7138, Wiliiiington,Delaware 19803 in an experimental. flight test prograM. The flight test program is in support of the Valsan JT8D-219 Re-Engining:PrOgram TIA NM-100S-1320. / Terms and conditions of the. Experimental Airworthiness Certificate are as follows: •• • • Valid for six (6) months fromLeffeCtive date of the . certificate. 2. Geographic area :is the, Western United States of AMerica. 3. Operation of. aircraft'will be in. accordance with alt. , applicable F:AjWs and:F.A:A. 8130-6 (attached).. Aircraft to'be maintained in accordance with Federal Aviation RegUlatiOns Part 91.169(f)(4), a current inspectiOn program recommended by the. manufacturer (Boeing Low Utilization Maintenance Program). R.A. Broulik Valsan Program/Engineering Manager C/O - Rockwell International 2825'East Avenue P Palmdale, CA 93550 Attachment RAB:lg t•-•••**0.,.. . • . EFTA00277910 烤 暮 · 儿 黧 h 亡 m EFTA00277911 US .DEPAPTAIDIT a TIVIONVOITIAT1ON - .. ..---,• ..sai ' FEDERALAVIATION ROINOSTRATION Sadsaltriiii No. 04-11060.1 . J . 4 ' atiumt WHIR AND ALTERATION tPOD FAA WE ONLY i ., OFFICE ,IDENTIFICAT1ON (Airframe, Pewerplent, Propeller, or Apptione0) '101F-PHX-FSDO s INSTRUCTIONS: Print or type Ill entries. . See FAR 43.9. F4/1 43 Appendix 8, sod AC 43.9-1 (or subsequent revision thels..1) for instructions and disposition of this form. - ... ..•- • AWE I MOOR - • • BOEING • I Z.21.7.31 I. AnKilAn Sing NO. - • 'NATIONALITY AND REGISTRATION MARK . • . .4 i 0115 i N505C • \ NAN& (As shown on nigistnation mi i rtificars) I ADDRESS (As shown.on mpildration ionOcoto( • 7. OWNEI • . FB TRANSPORT INC. 1 100 PINE ST 2.1 FLOOR I P RUNT . c i2 SAN FRANCISCO. CA 94121. 1 MR FAA USE Min • • , . , . ... • • . - . ... - - . . .. . , • . ... I. UNIT IDENTIFICATION S. net , • 1 -. . . onto L ...----- . -. Ulna NO. " SPAS *me- Anon • AIIIPRAME . IIMNIOMONOANISOMMIN (As thootni a slim I oboe)me teen . . POirrEltPtAte - . . MOMS • • • : t • - . APPLIANCE roe . o •. mAsanakras ; • A. CINFOIMITY STATEMENT A. AGENCY'S NAME AND ADDRESS . R. KIND Of AGENCY ' , C. CERTIFICATE NO. • • vs. Ceetiticatur Pi1Cooksic • . . DYNAIR TECH OF ARIZONA. INC: .3737 E. BONANZA WAY ' -. p is rer.t.rO4cominweci micmanic oCeenrICATID RIM! Inaptis • CRS A07-36 -AIRFRAME.IV ' PHOENIX. ARIZONA -. 85034't .. • satiuMCWItt D. I certify that the repair and/or alteration made to ' • inachtnents•heritobave been made in accardanie. with and that the information furniihed Stein is true and the uriiiIst identified in item .4 above and described on the reverie or the requirements of Pan 43 of the U.S. Federal Aviation Regulation! correct to the best of my knowledge. DATE " - • , ' AUGUST 10 1989 SIGNATURE OF AUTHORIZED INDIVIDUAL' . ' : . • • I . KENNETH ROWBOTHAM—Wernenta.a 4AP44 ,."-- 7. APPROVAL FOR INTIM TO SERVICE - -A' Pursuant to‘rba authority peen persons specified below, the unit identified in item 4 ',rasa:edin the manner prescribed, by she Administrator of the Pt Aviation Administration and is ®APPROVED O RE) • It • 'AA Pit. suitopuits aaaWACNINI . . OTHER aativ) IMPICTI0NSONOIWATION . IAA Otteill XXX illia. SUMO.. CAHN:KAN OrMITOUNT - Or NAMPO., worecrot v.Xr DOI OP AMOVAt a RIIICTION . AUGUST 10. 1989 OR =ON NO . CRS 407-36 SIGNATURE Of WM D I DANIEL WEAR , . . . (1320) EFTA00277912 'F i.At8cRATT ItniS/RY CAMtKA NO. / 41 DATE: 8 • NOTICE iliWeight and balance_or operating limitation changes shall be entered-in the appropriate aircraft record. An reiteration. mitst: be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF' WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify witIleircraft nationality and registration mark and date work completed.) 1. FABRICATED S INSTALLED REPAIR ANGLE ON LOWER EDGE OF FUSELAGE SKIN FOR NO. 2 ENGINE SIDE COWL AT FIREWALL BULKHEAD 'APPROXIMATELY FS 1455 PER SRM 5.1-40-4.. 2. REWIRED 'CRACK AT RH HORIZONTAL STABILIZER LEADING EDGE APPROXIMATELY STA 78.3- 88.3q PER SRM*55-10-3. 3. . REMOVED CORROSION. CUT OUT BULGED AREA IN EXTERIOR FUSELAGE SKIN, INSTALLED DOUBLER APPROXIMATELY FS 1157 AT STRINGER 27R PER SRO 53=30-3. : 4. REPAIRED FUSELAGE' SKIN CORROSION. DAMAGE BS -1166 - 1174 AT STRINGER 27L IN. ACCORDANCE WITH BOEING REPAIR MESSAGE NO. BPI423200D. it U.S. GOVSINSINIVIT PRINTING OCCICE: ISS6-689-121/43146 osspAltia-wft" EFTA00277913 ,____ ,,,,_ ill U.S DEPARDAINT Of TRANSPORTATION • . ,. •. FEDERAL AVIATION ADMINISTRATION RA Fine App. ed ,Bage t Pinta. N.. 04-Ito60.: MAJOR REPAIR AND ALTERATION -- -• 4 - . . (Airframe, Peworplant, Propellor, or Appliance+ VNYF. SD; OFFIcrF07R Et; fictictalltEop4ONLY 00/7 INSTRUCTIONS: Print or typsell entries. S.. FAR 43.,. F4R 43 Appendia D. end AC 43.9-I lot subsequent revision thereon for instructions sad disposition of this form. 1. AllCitArf•••• MAKE • . .REOEIVED.FAA !mote , - EING ' • "1 ' • •• 727-100 SERIAL Fib! rAy 0. • 1. 1990 'NATIONALITY AND REGISTRATIDN MARK I , . N505C , . 20115. 2.CIVINEI, . NAME Os shown on registrstion tortifi.cetiamv Fq..)0 ADDRESS (As shown qn reoistrotion cerriScorto) LIMITED INCORPORATED - • • -- ""- '7 -- - 4387 International G'ateway - 'Col umbus > Ohio : 43219 • • . . • 1. fOR fAA USE ONLY . , • • • '•• . • • • . -.• , . ...... ...._ .... .. . .. ... ..-. .. ._ .- • .,. . • . . . . ; ... , : • ., . . • - , .... . 4. IT IDENTIFICATION S. TYPE- Watt Mont • f • • ' . Melia NO. ' • IIIIPMII Anti- *Now AIRFRAME . .. . _ . • • _ . esetweteneeniennotoe (As thoscreed m Ihom ) obovoineeenbaseenreevraseem X • tantrum • . . , . - . . .. . . . . . . . . ' • . . X PROPELLER . . .. . . . , ' • . APPLIANCE ern i • • • •• • • r • . sensusecuu a . . . . • • . • • • . • • 4. CSINFORIIITY STATEMENT • ekr, A. AGENCY'S NAME AND ADDRESS S. KIND Of AGENCY • C. CERTIFICATE NO. North American Aircrat' - . -- - -- . •••--- Y.N. tannest** setetiaisse flOt8WepSlAniant Rockwell International Corporation . foam*. cestmcarto macmAwic Class 3 2825 E. Avenue P . . X "CIPIPICAIT0 NMI' STATION. . • Y " • . NXAR688K Palmdale, Ca.. . 93550 . auireRIACTRATO . . .: . O. I certify that threepall sad/or -alteratitia-made to the unit(*) identified in item attachments hereto Inve'been made in accordance with the requirements of Part and that the information furnished berein is true and cornet to the best of my 4 above on described on the reverse or 43 of the U eral Aviation Regulation,', knowledge. DATE . • • SIGNATURE. OF AUTHORIZE nigli ti ot7 tj . /0 9e) I .D.A. Perazzo INDIVID • . d ; 1. APPROVAL FOR RETURN TO.SERVIC - S r. . Peasant to the authority jinn venom speciied below. the tink4enti6ed In Ste 4 was Impened In the manner prescribed by • KW Administrator N St h& ide Aviation Administration and is • APPROVED REJEC , i • . I IIIA Ot b/IMG t. SY suanatites . ~toss saniatiwno•• Orrin ISesehi • • IAA WOWS i X Ilia PATCH • .cataagui Ro n . 'Of TRANSPORTmunatto . : AISM. • .• • • DATE OF APPROVAL OR RAJ! i f t 97 4.4 .199a CERTIPECATI 'OR SIONATUkt ? MTH ED INDIVIDUAL • ' DESIGNATION NO. • L. . a" • NXAR688K ' 4 .....4.-frics) EFTA00277914 .,„ NOTICE " Weight and ba lance or operating limitation changes shall be entered In the appropriate aircraft record. An . " altmition must be compatible with all previous alterations to assure continued conformity with the : • applicable al/worthiness requirements, 8... DESCRIPTION OF WORK ACCOMPLISHED Ott amore. space is required, attach additional sheets. Identity with aircraft nation4lity and registration mark and date wort con pletad,) A. Modiinalloqing Model 727-100 , Seiial Number 20115, in accordance with supple- ' mental' type certificate SA4363NM, amended•September 1, 1989 "as follows: 1. Valsan-Boeing127-200.Re-engining Document VA000001, Revision F, dated January 2i. The following dftwings and engineering orders (al's) are in addition to the above document: - • NOTE: - °VA" denotes Valsan Deaiting. a: `'Chapter 24 ELECTRICAL POWER • A240000 A Electrical .System Instl. - Strut E.O.: 003A,'101 VA240007 E -, Panel-Load Control Center Modification. E.O.: 003A, 004, 005, 006 b.. Chaster 28 FUEL SYSTEM INSTALLATION. T- , STRU • . . VA280001 B Tube, Assy - Fuel Strut Feed Thru E.O.: '100 Chapter 48, MISC A481100 .A VA481200 C.. VA481300 C VA481324 NC VA481325. NC Pressure Buldhead Reinforcement Sect. 48-727 E.O.: 101, 102 Frame Assy'Sta 1263 E.O.: 101, 103 Fuselage Skin E.O.: 106, 114A, 114, 116 Intercostal Assy, - BSTA 1223 to BSTA 1243 W/L244.39 E.O: 106 Intercostal Assy, - BSTA 1223 to BSTA 1243 W/L234.06 E.0: 105 Chapter.53 FUSELAGESTRUCTURE A530001 B Ballast Weight Instillaticin E.0: 100, 102 VA530003 C Ballast geight, Support Structure Assy. E.O.: 002,100 — VA530004 NC Ballast Weight Instl. STA 312 - 360,E.O.: 002, 100 Chapter 54 NACELLES & PYLONS - ,VA543000 C Main Strut Assy 2, & 5) E.O.:-003 VA543100 D Firewall Rib,.Side Engine LO:.36A,003A Chapter 71 POWER PLANT _ A710000 NC Power Plant Instl. - Engine Pod V727RE 002, 1058, • 109, 108, 001k 104A, 005A,.004, 110, 003, 111,1106A Chapter 73 ENGINE FUEL AND CONTROL- . . A732301. K .Approach Idle Solenoid Wiring Diagram E.0: 002(Rev . 002 (Rei. M), 003(Rev::M) VA732303 D Relay Inttl. Approach Idle Solenoid E.O.: 103, 003, 1008. • , VA732304 . D • Switch/IND Light Instl --Approach Idle E.O.: 002, . VA732310_ 'A Switch' Instl. --Nose Gear Position Approach Idles-E.O.: 103 VA732315 NC Relay-Inttlf Pilots Overhead Panel E.O.: 002; 101, Chapter 76 ENGINEIOTROl. ' • A760000 A .Eng)ne COntrols,Instl. - Strut-E.O.: 002A VA760014 A . Drum Instl. Eng. Controls E.O.:- 100, 101 VA760015 A . Bradkit Assy.:.- Pulley ESTA 100 E.O.: 105 EFTA00277916 DESCRIPTION OF WORK ACCOMPLISHED (Cf:iiitiPliel) • . Serial No. 201lt . Cha ter 77 ENGINE INDICATING * ! A771005 Indicator• Engine Pressure Ratio EPR, E.O.: 001 Chapter 78 ENGINE A780000 VA783010 E. 'VA783011 F VA783013 D • VA783017 J VA783(et VA784028:. • ' • A, VA781101:- EXHAUST Engine Strut controls Instr. E.O.: 002_ Flt Deck Indicator Instl. T/R-Sys. E.O.: 003,:004 Thrust Reverser System Wiring Diagram'E.0:: -002 (Rev. G) Support-Bracket Assy - .T/R Control Valve -R/S E.O.: 100 (Rev Placards E.O.: 007,, 008 - • Relay Instl. - Thrust. Reverser Control E.O.: 003 Mixer, Exhaust - Instl. 727E E.0::.100 No: 2 Engine T/R Wiring Deaetiiiation E:0 002 , - Chapter 91 CHARTS:. VA910002 A • Instl. 7.EleCtriCal Wite Harness 603,*4,-605, VA910008 : NC : Wire List V727RE E.O.:-00.1,.002, 003 • • ••: *New drawings added to: modification 127:SerVice:Bulletin 727-'53A0171, dated December 14, 1989... FUselage's., Station. 1182 Presture'Bulkhead,Weh: • Crackllepair.inCPreventiVe • Modification'. . • , . The aircraff.eiptY ueigtit.and center of gravity was .revised in accordance with Bbeing Weightand Balance Manual D6-21200.- . Weight and BalanCe Manual Supplement,'VA7CR279 ' is attitched • EFTA00277918 SCALE READING Left Outboard-Main 24402 Left Inboard Main 21865 Right Outboard Main 1 X23687 Right Inboard Main t -•4777%..14,4).% Left Nose Right Nose „4 :04T414,V.C .i4t ,4**-Kns. Subtotal (Nose) Items 4WW0AnAPDTVREA5K- part of Basic Weight but not Weighed AIRCRAFT. BASIC WEIGHT gsctvxivw?;antfpk Au' ti,j1m4 44. 111.221 = (MI) Distance tram the jig point to the main axis Centerline 520.1 1 • (M2) Distance -betweinthe• lettilose axle centerline and the jig point. eie.nl e (N3) Distance bitween•the right nose axle centerline and the jig point. 330.101 • (RI) Distance fres the referent. dates to the jig point of the aircraft. 950.121 a (A) Nein LOS Reaction' 311.371 = (I) Nose 'Axle liaction. :Ti litttaeVeRgirtiitid6;:%irtrisi • REMARKS 883253 176804 The aircraft was weighed in a level attitude and in an enclosed hanger. . .• 4k - 2. The wing panel jack' point was used for the aircraft jig point. 3. This is the summation of'the 3 weighings. - _- 4. Baseline Weight Results for Post Mod Flight Test, dated 4/10/RO. J EFTA00277920 •1 Y. rr_f', EFTA00277921 727 — 100:/ 200 Weighing Form Left Outboard Main Left Inboard Main Right Outboard Main Right Inboard'Main riffix• Left Nose Rightlifose Subtotal 89563757 part of Basic Weight Basic Weight but not Weighed 1 AIRCRAFT BASIC WEIGHT 4.4?.. • :ijki?-77-r= .,504 •`x i 1 . 96173 931.278139.33% tsrilfzt , CORRECTIONS „"tittiga, Items NOT weighed but night Basic Weight mEAsuREmEtrie 118.22) ..(.1) Distant, from thelig point to Vie gain axle eantenlin, 320.11 s (112) Distant* between the left-toss axle centerlinaand tha jig point. c (M3) Distinta.batenn the right noel axle centerline and tha jig point. s (R1) Distant, froa Lb, referants data to the jig point of the aircraft. 950. 121 s (A) Main 'Rile Reaction A s .R1041 311.371 (s) 'sits•'ail Reaction II a R1-(1124443)/2 The aircraft was weighed in a level attitude and in an enclosed hanger. • • 2. The wing panel jack point was used for the aircraft jig point. 3. This is weighing 1 of 3 .4=447Awan,1147' EFTA00277922 潜嗨置鲢薄鬈鑫坚： EFTA00277923 JAL AIRCRAFT REGISTRY CAMERA NO. 1 N DATE: 8 75- 90 .. .. • ....::•7; i 727 - 100 1_ 200 • : C. • .• .. ..r. . • -'"t;..II ' WeigIving.FOrm • -,: ' L *Alt.il ...fl. “;:ic._ .: . • •• Date 'Model .18eriail c Number Place Weighed' Technician Phone 4/18/90 727-100 10115 - N505C . •ALMDALE FOLEY (805)265-2151 REACTIONS ' ' . • SCALE READING . •'41.1 • " ‘.TARE . NET • - ARM it $ WEIGHT ... .. , ... ''• MOMENT . - • • *. :tot& 4 • xi 1.qt • • ••••• \ 1.••". • % ;;;;;.;.A.4.,*:::*;14., Left Outboard. Main- 24402 • t• !.. I.7;!et. . ..2..::gi.19Firei. Vt.; *.:' r 6 24408 >. - . .41 " . Left Inboard. Main. 21865 t. 2 21867 •:.:;;;2;.:444.4.!."211.11#•dia.,4;;I:f .t'it l4 1(tl':cliii: L. •:.'ner&E,4:40.4,Fer, .....ip.bv..1-....e,:•:•.•.:../Y41:11,A .47:3;4 ". is . .3•1 %'•.I 1"i . • ' • 4 ••••• -,..•: 8( 7 ...4.- ! !. 1Wi " rt:" .... :Sri .: • ' -‘ ' " I !!! 31 174. -- gyel;..‘ 17... Ca •:. , ..„;..f.t ,:......g:Ca Right Outboard Main 23689 4 23680 ::::-..44:k..t412: ...Q..: .:.....,•• .. Tr .•! 0. • ..bP .1) ... .h:il 'Cer ... %'.. .81 ••• .!'t 4.• u •/, 9 far 4.10, if f, .. 3 23384 ..4. • "ran.... ktype ,... .....;:;:oA.;:•.i:-. •...t..i,.5 Right Inboard:Main' 23381 r i 5-ef-,4s .4. 8 Tiv....,. - ...:....04! ;.:..:1.:44.%;.:. . n..f .......:.=:. ... 4 s.01.5 4 ..2 ' . . 4. so ...:0 12 C I.:nil" • ' .... ' 'C .175 ‘g`:r•••••••.:•:• '" 7 93344 A - 950.12 ' Subtotal (Mains) 93337 . . •• • r I 88688001 ee i o. • 2-: 7. ti 5 ik 'Men 4tPitir .:11 OA , . • Left Nose •'. . 1338 i;V:Z - na 1338 - -, t• . • . Right Nose - .- 1501 0 1501 --- ,, fairgiN9! .".1.1,z44/P .‘ I. - 4,1' •:. it •,,,, zi k2,F2 • v,..•-mts t... ..44.,KAcre. 1.-- . 4.:. . r: l'• Subtotal (Nose) 2839 1 e 0 .2839 us 311.37 A htili.5.04.ekl ie0 161 17 1 r rs.sranons•• .......•: .• r ti. ,t:if- 883979 “.... ' AL • ri Ze•;•• ... .iia"VV %at fier;":::! el :, TOTAL 96176 id,41. 7 96183 931.27 e.- - 89571981 4;i . . ite rae liti at.t' ",..., e YL i•str ,.... , • -$7 AwAt "k" lt t 4,1.,41, sIr..t.;!" •;514 • • aka ! , 7 t 1: -AAc“..2 f.h. .." ..!5".f,33C.4 a " . E., t t a:1 7;;;:t.:•Ir Items NOT part of'Basic Weight o :)...e • r, • o PLUS t"4"717 R41411V-gitilVP.Vialt;01,3 Airefti:- 4 „.. • . • A ' .. sto ", ..m il'llilkin,?/•:gial-iR.; Items part of Basic Weight,but not Weighed ofay AN. • -.J . 0 pp •• •:.: • . ....tVrait % 4.; ••;•.: V % ••!..•:"•••• :: V& .• 34,41,1 Ltlit.142:::4:' ..:94..A., 0. A.M.S.< Arty r .1 gi' •ri: it .4.!”71. .11LX:Z4 itSC•A••• : diefk :.. .., u. ii . V2 — .4. :: f: •••• AIRCRAFT BASIC WEIGHT • 96183[ 931.27 39.33X 89571981 tlirlektspiflt r 1.9wA *"' 11 - 11'1. 22 14 •161"*".•a!"4(1•24#‘ •• • 'clus‘'" 4t•Pc.C*11#7ite 0 K. s , - ir. h -. „ • C lr,, laii ,, rd . frtrat trit: '4-.02."{ 4n;.2:- l. ••• 4 CORRECTIONS a :,..:tit ts2..... y:. :,. m: . s. Sq.. 4 •cit. •.1 .• ;A:t. • NOT Part of Basic Weight r Items NOT weighed but Part of - Basic Weight Description Weight Arm Moment Description Weight Arm Moment 1 • . TOTAL ; 0 0 1TOTAL 0 ,..i.fi,-orritez.f , k-r.• .. .,:,16.4. .,..-Z2.4-,A.:.. -7. _W. l*:.,..*.e..:t . . . err 4,- , . ....., t4.4itatift! .i..J.•r „ t 1)ilgzliii . mustummurrs ‘ ,,,SS ;A— • , : ,... i .. ' '119.22 a Oil) Dieter*, fro, the. 310 point to the sain.axle .centerline I 920.11 a (142) Distrito between the loft nose axle centerline and the jig point. 910.991 a (11.1) Distance between the right ;Se axle centerline-end the jig point. ilS0.901. a (R1) Distance fecal the .referenle data to the 319 Point -of •The aircraft. 950 . 121 a (A) Rain Axle Reaction' Ori‘111011 . . 4 . 311 371 a Cal Sim Axle ...action a s R1-(112019)/2 . • .. • Elifiliiiit,:i*:2;.!t1;- ..ci,n ..lin.. 100,1i.:\Vitil REMARKS" 11:0F0Fitt l.‘' '•-•.:.T.I.ty.i'vill: '•.141.9)! 4-'1474.4fi.L.i n • . . . 1. - The aircraft was' Weighed in alevel ..attitude and in an- . enclosed hanger.' • . . • . . . • - 2_. The wing' panel jack point was used for the- aircraft jig ,point. • . 3. This is 'weighing' 2 of 3.: • • . .- • EFTA00277924 tIAA AaRCRART REGISTRY Mini WO. .1 N DATE: 8- 75- 90 • • •";-•'"7 • • • a 4. u"ktin'ti EFTA00277925 6 24407 2 21864 Items NOT part of Basic Weight PLUS 1 771',iS :14:;!:r AigligteieiT:tra$5ZitiMil0.,4.6 Items part of .Basic Weight .but not Weighed ......7...;,„•:,Fc, i..,,,,,:i.:::a..491:4:;514.t. AIRCRAFT? BASIC -WEIGNZ 96180. 931.30139.35X 8957232 •i TrA43114114-2i;, ..1;!.P..1.51,c, ea'. fill• s,,,w-Pirsi34•tksz.srsta‘wt:ttiormike*A" alliq2:2:filf,f•O:z•• -':i.3rit;.-• Vci.14•::, 044Kiat• aictilfii • 4.:•• ••tilref•air ••••- • %'d :- • fisttel•• N.*, • 4 I'i3„.. .ese4:71,*...:-6w:etonttit4,4ti -C"RECTIONS 6.,:04410T.”44:1:%'?...1 59.5:Tt2 fritii11444( .. . tifizeFitsic. NOT Part of • Items NOT weighed but Part of • Basic Weight Basic Weight Description a (MI) biltince tree the jig•point to the ;Pain axle centerline .•. el.( 12). 01ittence-betweeri .the.loft -nose•axle•centerline and the jig point: c••(Iii).Diatance•between the right mese axle' centerline and the fig point. (Ii1) Distance from the reference-ditue to. the 'fig paint of the etrcraft. (A) Hain Axle Reaction imam . " (II) joie Axle React/en aR1-(1424443)/2 • 4 , REMARKS 1.. The aircraft waa vieighid in a 1pvel attitude apd iri an enclosed hanger. The wing' pane1. jaaki point:weis used for the aircraft jig point. 3. 1 This. fr ...weighing Of 3 • • . . • . • 1 • EFTA00277926 r'lvAr3414" 4241:44- -.4s-Aats <ler L 2 64'n, -4prer,liar# - - • — EFTA00277927 '• - e • war. Etir WnANDroaTATI0N pie tired dger wean No. 04-R060.1 FEDERAL AVIATION ADMINISTRATION MAJOR REPAIR AND ALTERATION' - FOR FAA USE ONLY • (Airframe, Powerplant, Propeller, or Appliance) IDE TOO - Cy • INSTRUCTIONS: Print or type ail entries. - See FAR 43.9, FAR 43 Appendix-B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. 1. AIRCRAFT MAKE Boeing • MODEL. '-727-31 SERIAL NO. 20115 NATIONALITY AND REGISTRATION MARK N5051 • 2. OWNER NAME (As shown on registrallavontificate) Tenneco Inc. ADDRESS (As shown on registration certificate) 16951 J.F. K. Blvd. Houston, TX 77032 • • 3. FOR FAA USE ONLY • • - • • . Ninti: ; ,..: -.4..1:.-•. • ...:•• -.J., :• •- -; , • • 4. UNIT IDENTIFICATION S. TYPE UNIT ;MAKE MODEL SERIAL NO. REPAIR . ALTER- ATION AIRFRAME ateweeentweenneetee (As described in ;tern T. above) XX POWERPLANT PROPELLER • APPLIANCE TYPE MANUFACTURER 6CONFORMITY SlATFJAENT A. AGENCY'S NAME AND ADDRESS B. KIND OF AGENCY C. CERTIFICATE NO. U.S. CERTIFICATED MECHANIC . • Tenneco Inc. FOREIGN CERTIFICATED MECHANIC 16951 J.F.K. Blvd. X CERTIFICATED REPAIR STATION 205-10 Houston, TX 77032 • MANUFACTURER D. I certify that the repair and/or alteration made to attachments hereto have been made in accordance with and that the information furnished herein is true and the unit(s) identified in item 4 above and described on the reverse or the requirements of Pan 43 of the U.S. Federal Aviation Regulations correct to the best of my knowledge. DATE . . . 04-04-85 • SIGNATURE OF AUTHORIZED INDIVIDUAL • 7. APPROVAL FOR RETURN TO SERVICE Pnrsuan to the authority given persons specified below the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is Ir4 APPROVED O REJEL. CU) EY FAA R.T. STANDARDS INSPECTOR MANUFACTURER ' INSPECTION AUTHORIZATION OTHER (Specify) , FAA DESIGNEE X REPAIR STATION ' CANADIAN DEPAREMENT OF TRANSPORT INSPECTOR of AIRCRAFT DATE OF APPROVAL OR RU1°1°01-04-85- CERTIFICATE OR DESIGNATION NO. 205-10 - - •• SIGNATURE OF AUTHORIZED INDIVIDUAL ....4/O • iAT....- t- a tre :•.;?:Ps_ • • ••`:—.. •' " "I ••:• '14.‘11•.'.44 • • • d • . • ? ‘ "e' . j..: •••e I••••• ms•S • EFTA00277928 FAA AIRCRAF REGISTRY„ CAMERA DO. DATE: '71- "." -....r.T•T • NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An atterotion' must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements.; 8. DESCRIPTION OF WORK ACCOMPLIShED (If more space is required, attach additional sheets. Identify with air- Craft nationality and registration mark and date work completed.) CREW AREA CHAIR INSTALLATION I. Re4ovecifolding,couch:from L/H crew compartment station 400. II. Installed (1 each) Tosington T1150M24 F/A AFT facing single chair on sliding rails from station 420-tOTstaticih :380. • III. This alteration. was completed in accordance with Threshold Engineering Company of.San Antonio, TX, drawing #270 and instructions identified in report #259. IV. All engineering drawing and reports were drafted and approved on FAA Form 8110-3 by J. A. Dugelby D.E.R. .(designation number.SW.7256) and are available. to the administrator on request. . • V. .All work performed utilizing acceptable methods, techniques, and practices per AC. 41i13-1A. .VI. )Aircraft weight and balance amended. ---END--- • ADDITIONAL SHEETS ARE ATTACHED , •• ••. • . _ , . _ _ . *US. GOVERNMENT PRINTING OFFICE: 1977-771.021/344 EFTA00277929 . . • ." ::,e4; ). • • • I - contmea Of Tatuvonnou:: • FEDERAL AVIATION SINISTRATI0N . • . - NIAJQR REPAIR AND ALTERATION - -(Aidrame,Weirerilent,'Propeller,.or Appliance) • in &tinned fistoWer Biroce No .04-R060.I • FOR FAA USE ONLY OFFICE IDENWICATION Sai-feloo , . . . . . INSTRUCT ONS: Print or type all entries. See FAR. 43.9,•FAR 43 Appendix S. and AC 43.9—I Lot.inbsequent revision di • for instructions and disposition of thie,forta. . - • MAKE•• MODEL Boeing. ' : . 72-7-31 • - 1. AIRCRAFT SERIAL NO.20115 r ' NATIONALRY' AND REGISTRATION MARK -71. N505T - 2. OWNER • . NAME (Asshcam on registration certificate) ---. CADDRESS Tenneco: Inc • : ... : • • _ (As short on registration ceitificcrte) • 16951 JFK Blvd. . • , . .Hotis t on , Texas 77032 - • - 3. FOR FAKIISE. MI • • • • to dalatMeSian Identified herein complied with applicable airworthiness requirements and Is approved for the above described aircraft subject to conformity' inspection by a person authorized in FAR 43, Section 43.7. • • • .... . / 2:raCC • babe Signatur of F seeder ' - 4. UNIT IDENTIFICATION .5. TYPE I • UNIT . . MAKE • - . • MODEL . SERIAL NO. . REPAIR ALTER- • ATI0N • • . AIRFRAME • - ' • . . • • . " . - . . ' • • ' .7PIII•••••••••••••••In4 (As descited in item 1 above) .- XX . POVIERPbOlT . - • • • • , PROPELLER ..- : . - . • . TYPE . APPLIANCE MANUFACTURER . .. , t • 6. CONFORMITY STATEMENT . A. AGENCY'S NAME .AND ADDRESS B. KIND OF AGENCY C. CERTIFICATE NO. Tenneco Inc U.S. CERTIFICATED MECHANIC • 16951. JFK Blvd. FOREIGN CERTIFICATED MECHANIC .• Houston, Tx. 77032 x aunkuoui REPAIR STATION 205-1.6 • • • MANUFACTURER - . ca. • D. i Certify that the repair and/or alteration made to attachments hereto have been made in accordance with and that the information furnished herein is true and the unit(s)• identified in item 4 above and described on the reverse or the requirements of Part 43 of the U.S. Federal Aviation Regulations correct to the best of my knowledge. DATE • • - . . - SIGNATURE OFI C7 IN IVIDUAl. 7. APPROVAL FOR RETURN TO SERVICE Put uant to the •authority given persons specified below the unit fintified injtern 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is' APPROVED O REJECTED - FAA RT. STANDARDS INSPECTOR • fg MANUFACTURER INSPECTION AUTHORIZATION OTHER (Specify) BY FAA DESIGNEE , /lc WAN STATION CANADIAN DEPARTMENT Of TRANSPORT INSPECTOR Of ARCIAFT • DATE Of APPROVAL OR VA CTION I,2.- 30-14 CERTIFICATE OR . DESIGNATION NO. ,do s^ rb • SIGNATURE OF AUDI IZED I DWI UAL .. . • _ .. .-.._ EFTA00277930 . NOTICE . . • . Weight•and balance o- operating limitation changes shall be entered in the appropriate aircraft record. An altiratiOn must be compatible. with alt previgus attetations to assure continued conformity•with the - .. applicable airworthiness requirements. • • • • • • 8; DESCRIPTION OF WORK. ACCOMPLISHED (if more space is required, oltach additional sheets. craft nationality and registration mark and date work completed.) • Mounted T.T.G. (Time to go) .Preset•Unit forward of center console, below existing Radar Indicator: (.5# @ Sta 210) • IV. Meunted .D.I.U. (Digital Interface Unit) with suppliers rack on shelf adjacent to ATC-1 Transponder in A & E Bay, R/H Side. (8# @ Sta 463) Installed 2 amp klixon CB on:fetwara-end pf.#2'Essential Radio Bus CB.Paneli. • '.Left side. of cockpit. (Ste 261) • • • • Installed wiiing and associated hardware VII. Complete system installed, tested, and operationally checked, in accordance with the manufacturers manual #910600, Tenneco Inc. Interface Wiring Diagram . 011586, and acceptable methods, techniques; and ptactices per AC 43.13-1A Chapter 5, Chapter 11 Sections 2 thru 7, Chapter 15, AC 43.13-2A Chapters 1 and 2, • EFTA00277931 FAA MCRAE REGISTRY CAMERA NO. DATE: v i - g9 adell••• . • 1 :s>.•••:: • 2 B 0' e. 1 PI WOO awri--;-•?-5 1 3 ••• v pc Mus—ia;--Wr DC Revues — r/Pt WAIT+ • your- ' -ist RIN+ I A is , _ /7 1- 6 7 (9 22 • t3 ‘ 24 I 17 • • 33 45 Ts 44 35 3 : se 443 49 30 • 34 Ls RIN- am Ott ans. C CO • 3 • ø X Guntur POSAM PTIONAL CABIN OWN« CONMOI. UNIT (DCI4 3 . } • AIII.fR0W 1OO (0101 Jfr 39,t eaWark, Okilla .1.1.64k6 J~/46‘7i2 Cs. jeCITE BEN/a18 noso frotwrort. -7"••• - • • • a AM Mt acts ets.sAse A S aW 4440%90 Aso Ott/ VIC44'0 14440 Attn. ELIMINATE ALTER ran OCU ,GOWN. MANSE. PEZ OCh LOG It 2S1 /043-83 diseer »snit a - CASE PER OW LOt S 29. ~isn't* OM LOS s 36e CAMEL la OtS. 'Earl 4-44 moms bre 4921/14 L4A 30Erts It MY c tea As loff..1205iro4; 1:buisr-te esepstky., RILay. WALL ortJ.E.k P05 Iran: ea! To 1(42 Se vipka - fl A nurse: conraot nkr Ottio4W. 6170140 EZhAftV IS ON tilem. P142 49 GNO AND PM 30 Onal MELDS MAT DISPLAY.. Pnal OPEN AND AfA130 GAN) . YIELDS 11413 OISILAY. P44.29 OPEN AND PIN 30 OPEN ALTS(NAYES OLSAI..11e. ~21 GINO AND fl y 30 0A/0 TIELOC. t.060 DISPLAY. a. 371 CAns Atft£StmtE ~VECTOR Meats/ UNINSELT10A/ 115 /UM 4:*e. ami. tAM£ was 3P1 ØØ as TAW OF Dui . tria le %stir) . ;pc irTERFATC Or Wu To es Z3 t• PORF OF --.Sicsonst_ C.44tutEt tan 1.1 MX ~WED AV AstAte: au in rJA te_setwout [ant Pea n(4 NEnalFFs/ 7t ooTA (Kr . NrA TS oisiN tµYA our. 54 Can 7 - 6-(1404b ~NS .04/0111r) RN Awe ors wag on s r-sr ant atones* twat AM MUSIC sr? insur VHS Z 241 BUS. gasp DI AND 84 IDARIDD 4/4/11- OVA/ AND le2 2.4V SVC WOIE: AU-17110E ENCINO IIPLIT nor use stnei ARA•tC 414 miIPUT1 ARE REG4ft£Q annee P/J-PLAY annsneryz oersinEa P7104 ACOSTA W AR//AC 419 1411/1: fox REPEOXE roc osr" ohm AV Conifer SPERRY AZ-243. CCIPINECYOR 7S /4- 47 10 PIN 5, 47I4- 47 ro sin 4 IND 9J/4-44 ro rain. 4,2 AR/NC 2 fVK£ 010~ BE USED FOR DIGITAL ADS IF rsys ot one CONNECTED. art AC/NC CAM ea- ast-is BV #2 INS Ode ONE a - DIGITAL ADS nor asap- nS. TOC IALT a Ow, 83331 2 WIRE AND t YOKE 4.11/K OUT/WY "OUP ar wswecreo IF AVADABLE.. 4. AVOID swore& cost WITH orace IttaRAPT WO/N& MOWING. morn ~TM* DIRJLEAITZ • 3. ALL .11/1aDED Inter 117 NAVE AVSZDATED "setter. sinew: ro at atenfoco TO can-warn rani At MADAVID 100 D/D RACA' END. At AND At OZUI COVACC71X team/re-4:os° ossnerse «nu. goat MAW» SE ta/C433 IN rot tan' sun r>/OFTN. 24MI, OPTS:WILL CSCEPT Ate aura /moor. NOTEst: ream. ormatwin sPECUYED, CONNECTOR. TABLE RET soarcedmom 1 acre-aszsre MAC P.,W LPL earn enzscuucu-oon rum 6/sole ' 2P/ Pr PrOGI -43-15 PTOcc-S-÷s 625'00 8 _3 PI In 3 /24 F -I41-12.9 442.5- O/P in' i4S31.22E-444-/PS HS3Il2E - /F-.7S 4250/7 3.12 1/3/1i .94 ati EISC tlut..c NO 625O/9 I ()MI COO( NC(I0 Offif 10F.PariNG IVA .i MIA? • 140110CLATUINC ON OESCSNITON ' . PARTS UST I 'fl. ~En OMONFSL SeNaNCO ' man NO ~MU OISCatias . ~9~a Me. Int ~era otessios skails = = ASPIC, MICORIOCA TED HitfC MY FORD W. 7211714 CA 421 SO • APINON•45 OlfC ''t"..1 amoretten aiLDED larl13 1NTElittNAIECT WIRING AIRSHOW 100 WITH DCu Nal Ufa ON APPIXATiON 00 NOT SOU Oliastosa 910600 gvp SEEET 31 SM D tom socsa so; OLNYINC. FO. Ina 4.-- T . 9 20410 F IT.ccT / Of _~.wi.-s. 3 ..b. •-).:;•;if:. •• . • 4 •1' • •r •t .•1: C.:;;; .. • • 7 :•_7 — nee, plit;es •' • • ••• ' -• 49•;:“" •154„; • ea. 2 o. . Svc, EFTA00277932 -115%021.771 •*.seiffirs . , • • et I PYDED our 75 al• } oars •••• az Argitoc 4141,14Z 9 O.47-A — 2•M/l% It REF AMEN TA 170,0C eft SIG .1. • r/HE't kr av Dosnm Com-Ro S16 - • . ISMINItrrai sfaitW.-e-A-6ta . - . ' • _.• - ;.- EFTA00277933 - FAA A IRCRAF CAMERA EO. rtami REGISTRY • DATE: MYOPIA: OMNI O/LTLAT OM ma UNIT WO* NAP VCR • -erf INFO Mira. Iko A enalar-S PROW Vat PE Ae«.0)14 e.g. APPUCATION jct. ATE &W/NO VIDEO A a Dc Atin tsetil VOCag0 An0 arr.& GUIMINATE ALTERsaTE DLL COMV.,_ is 0git -AGE DIAPMG PER 2•I • trzonm toe /04J-03 Akre r0-20431tate 12 ft-fil a," ora22004 gott0 D Gaol PER OW tot • 2.96 c LALIMEW7704 LOG a 164 30CTES 00,4 CaMat SZE tieM i4/ doFf- Powhtg 15 er.weEr.: in pa, "'UK /i/ALL 0774£7,. .231, 15 Suoy1/Eli ra Rd it le If. »tor A agrater LL' ogrou TAE ouPtiV. &ROUND RETURN it ON WIELD. ,c9k Gam AND ems° OPEN naps MAP DISPLAY. Arm Et OPEN AND Ft.W.30 6.40 YIELDS INTO DIM«. Ram?, OPEN AND ~30 OPEN ALTEcivareS Dtsietny. RaVn 6040 ANO Paa 30 4,110 YIELDS L060 DISPLAY_ 3S1 (ACM AttatiME Waeablt eCCOW CaUMEtTIMU 76 "(MO bal. SW CAME won 3F1 Ottitidels *3 tier OF /KU cma FOC pericoic. OtTIERFAtt Or tol -nb 23 t • roar etc fetsons L ZáMfUlElt. mate« 43 marstrauct 7Y Assn.: MU AI OW JEte-itérimmi ItS,t3z font nm bescoutTOM r.t 90617. OUT 3 ‘. 11,0.TA rT DATA. • Z ton air STS 610MMS 7 Tra.m.NA , 4031440 pi swag FOt asmaCers wing ate I t.v/ taut titaliaOO.4 town ~Aisle arli ermor ova z 241, BUJ. ammo Or ~Oa MillatCarf INAPT aver itmo az 2W 60.0 gore: ~Iron ~DNS avato-Nor IWO WHEN ~at 429 INPOT.f ARE irealarea arrrurr£ or.rpur pairrrerray . OBTAINED FROM AIZILITA OW AR/AC 424 AWIL17: Pot REFERENCE: POE oar . DMPLAY CONNECT SPERRY AZ-Zett CONINECMC 77 IA- 47 TO PM/ 5, 7.TIA- 47 TO P/N G ISO 1-T14-44 TO rum. &In AR/NC 2 Witt tHOLICO BE VIED FOR DIGITAL ADS IF INS OR ONt CONNECTED. Art AtiNC CAN BE ant BV si2 INS 04 OAV er DIGITAL. ADS flOT USED- . LI\ roe • hut OR ow, to». 2 WIRE AnD G WIRE AXING •OUTPLIT .11ARILD BC convocreo AVAILABLE- a. AVM', /(01/7"Ne COAX win< orate ~CRAFT ewers.* AIOATE PROOLICYN6, CYLALiNTt. 3. AL( .nwricoco mar TO wave ~Area JACKET . SMIELAT TV BE IMWACCO TO CONVECTOR SHELL AT ARTNOW i00 DILI RACK EARS. a at Ant Ar mix apmeerac .caumee case 04400ETER COAX. 1654 name) IPLICED Av TOR WNW RUN 0/0,7'1. 1124 AIVO OPTIONAL EXCEPT fait POWER ~POT. "NW runtrr omen's:Er EPECIIII£0) CON.VEC773A TABLE REF OUTZIPTION ALTERNATE *PAC P/N In OIS7.1111PC7t3ZELY-000ITZto) 61s-o/e 20/ RPTOL£--8-lS Procr-8-+S 625008 5.91 1153,26F-10-ap 625Die . 3.01 nS3I22E-/f-IPS 33:12E-M-425 6250/7 -3JZ uslv 4g 20 aNC etxx HD 6250/8 l iatioTcoor rain OR Mine I•1 co NOT OAMMNS flll COCRIPTOI AIMS (Zr '910600 gEVP : ,SHEETr 31 2 410eC. ~tattoo rev «WC 147F0A0 CD. 77.137/N CA ILI 20 INTERCONNECT WIRING AIRSHOW 100 WITH DCU r- et. C LL 0 C • 920410 'parts • of: • EFTA00277934 • ORAIRMIDif Of VIANIPORTAVON ' • . .. • . 'SPA AVIMIOt4 ADMINISTRATION t• . .- -. • Fern t r...vgat Bw4ei wren No. 04-R06-0.1 ... MAJOR' REPAIR FOR FAA USE ONLY . ANO .ALTERATION, orna IDENTOF • (Airframe, Powerplant, Propellers, ei Agi011arim) .‘ ak , # - INSTRUCTIONS: Print or type all entries :Sri PAR 45.9* PAR 43 'Appridlx Di red AC 43.9-1 (or subsequeist revision tbeteci .: for lasaructions sad disposition of this form; -. ',‘ 1 . ; •••••.' • - ' -- - . _ -46-MODS; 1. MAGNI MAKE • - • _ ' HOF I NG - . ' • • '. ' 727-31., , SERIAL NO. . • ...... , ann5 NATIONALITY AND PROSTRATION MARK • - USA N51.15T . . .__ HAW (Ais them, TENNECO on. registration eartIllare) INC. ADDRESS (As.showr on registration certitioste) • . .16951H3.F.K. Blvd. • _ .1lottiton: TX 77032 fr A. (Olt FAA OFF ONLY >. , • . .. imposorwasse ss. is scIt.to.itiiiip....rf:47:3364:r... irma ilsoraionvogru bs rife.; id . t • 4,11: IDOMFIGTIOIL , 5. ME UNIT MAO .1 ,,..„. - • MOM • • • . 7 SUMS PIO. .: - tiPAIR ALTelt- ATION AIRFRAME e • . werwanneoes•444.• iit dirtErill; Orr' V aboar) J. mirOimistraus . ,. • . . • . X POWERFLANT - • - . . • • .. _ . , . - • . .. PROPELLER C ;-- • • ' • ' APFLIANCE VIM '` _ ' IMNIPACIIMIN ..- ' i. (OISMNITT _STAMM A. AGENCY'S NAME AND ADDRESS S. KiND OF AGENCY C. CERTIFICATE NO. G. C. Kolb el.t. CIETIPICAT19 MIOLANIC Tenneco Inc. POUCH OITOICATITS MICNANC • 16951 J.F.K. Blvd. X •FINTIOCATID SPAR STATION 205-10 Si. TX . 771112 leNUIACTVIllt D. I certify that the repair and/or altrrittion made to attachments hensto have been made in accordance with obit the information fratthiSiti herein is the unit(s) identified in item 4 above and described on the mete.* or the requirements of Pan 43 of the U.S. Federal Aviation Regulation, best knowledge. sad tree sad correct to the of my DATE • December 21, 1984 SIGNATURE OF AUTHORIZED INDIVIDUAL - LS _....e.... " 7. ifilliflU. _ 44 1 FOP II TO SEMICE %neat to tin autheriey awnpasoes below identified in items 4 inspected in by specified the unit was the manner prescribed dr Administrator of the Mad &Woe Adarakaratier and is Etatinovw allijEc hp BY M4 PLY,• MISS IyallOS a OWILIFAltiat 1141PICOON AUTNOSILATION OTIS fliptin, -='-, - MA MOM X WAS STATION CANALMAN CaUITMINT Ot TIA14,041 !WC" fX ASSAM a DATE OP APPROVAL OR REJECTION • Dec. gat /940k - CERTIFICATE OR DESIGNATION NO. Baer-L>a . — SIGNATURE OF AUTHORIZED INDIVIDUAL • ...dies. - d..-- rce.er • • O. EFTA00277935 . . Weight and batons or Operating limitation changes shall Wintered in Otis appropriate aircraft record. .An altoratiOn:Must be'compaHble with all previous alterations. to assure continued conformity with the . applicalskainiartldnsise requiremeati.. O. DESCIPMOM•OFROMI A(f.OIRLIMED (0 more epos* is required, attach - identify with oil craft nationality and rogidrationinadt and data- work. 000tplohod.) • •-•;V:" . • • . . ,•• ' ' . 7 ,77 .7 t.;1'7". I. t.itenioved Thermador Trash Compactor P/N TI4C-28B S/N 3060438, Having 6 AMP,,,;•,:,0 • 4 a • load, approved on 337 dated 9/19/83. • AL:- Installed:Montgomery Ward Trash Compactor P/N SBW-5235-c S/NT481100442,- 1. Having.10 AMP Load. _ • III. Unit ftinctiOn tested. iatisfactorily; unit operation does not adVersely - affect the safe operation of the aircraft. • IY Installation was same as previouslylpprOyeCoo:N505T 4/01/81'for - -- • -1 Aireseardh Aviation Co. , Los Angelei-,-CC-- 1See previous-weight and BilanCe 's Data Report 11C-3688;) V. Installation using acceptable meaies, techhiques, •andfirectices in dente With AC4313-1A Chapter 11, and Chapter 13. • •VI. Weight and Balance and Equipment List Revised I •_. , - . • C t) iv e>•.- r.,•• • . • ;VI • I . Viq',~.• 71 , a • A ,.:144.0 • & •-••-• e • . tc: :Ism • -7,1•7ostip •., •:* • • rti-.• • • L. • - •••••:. : • • . • !- • .• - : . . . 1!.7 . t •• • EFTA00277936 a ll..... .. ....1.1. 4AIENT Of MANSPOIHATION CEDE AVIATION ADWNISTRADON - , • Form Approved • . Bud;et Buren No. 04-R060.1 ' • t MAJOR REPAIR AND ALTERATION FOR FAA USE ONLY . (Alrfromi,.Powtriitant,.Propollir, or Appliance)' . i zjoarrgri INSTRUCTIONS: Print or type all entries. See FAR 43% FAR.43 Appendix B. and AC 43.94 (or subsequent revision thereof)' for instructions and disposition of this Cos; . . . - - -- - • MAKE Boeing • . MODEL - .. • - • - 77-31. 1. A11101411 SERIAL No. .. 20115 . NATIONALITY AND REGISTRATION MARK • .. N505T 2. OWNER' NAME (As shown on registration certificate) - •Tenheco Inc..-:.. ' ..-. ADDRESS (As shown on registration certificate) . 16951 J.F.K. Blvd: i . Houston. TX 77032 3. FORMA USE Nu • . : • . • . . ignitions Ismlilim Ise is unklISIRIMP •: . , - tilleiteNMS and Is On/1W Ss. i - , ' Wiest to orkentay Is II • I • ., 13.7 D*). • : . :. ‘..... •:pra. . • • -• 4l ' _ , - . . ,...........a. _ k - " I. Will IISTIRCATION S. •TYPE *SNIP . • • 4...L • • SERIAL :40.. MAIM • AMA- ATION AIRFRAME' • . • . •••••••••••••••••••#14 ilestrist in item I abowderamma re••• • : . . • j(X POWERPLANT , I .. -• • , -• ' " • • • ' • FILOISLEILv. ' -c.5 ;• , ..,.. • . . •.. . . . . - .. . : ) ! •. • . . . ...• . , ' • .... . . .•' - - . • , - •••••-• ' , APPUANCI ..._ : . . .1. i :.• .; . - •• . ' .. ".. Lionisation • . .. -. .- • t - 1i. •• . . ,. . Jam : a - £ collethITI STATHAM • , A. AGENCY'S NAME MO Amens • t - y - IL. KIND OF AGENCY C. CERTIFICATE NO. • Tenneco Inc. • , tit. COMFOCATID MECHANIC 16951 J.F.K. B 1 rTrinift- MOO* anararto istamtc ... . . . ' . vd . Houston, TX .' 77032 ' • x. pumnommmmessmnom • '205-10 . • -. • D. 1 certify that the repair andinialteritiois• snide to attachments hereto have been oat in Scootalta with and that the infortisatioo famished, berth ii was and the unit(s)•identified in Item 4 above and described on the reverse or the requirements of Pan 43 of the U.S. Federal Aviation Regulations correct to the best of my knowledge. - • i ... ' . DATE 1 . •!•• ' .. : • - '';' . • 8/3/84 ...!: •!.... :,. ;.• .,- •:‘..", •'. SIGNATURE IN • - • , . • . , 7. RIROVAL FOR IfIRM TO a Pursuant to the eutbarity given persons specified below the unit idendfied in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administradon and is'. al AP/MOVED ORFJECM Ls RT. stistacts . . spareast AIDNOINZADON IV ... ..... . PM OWONft y ...- ... CAM STATION COMIX034 DEMITlect Of CRAMPONS IMPECTOR %en • • • DATE OF AITROyAL. OR CERTIFICATE REJECT107 g it OR . .... . DESIGNATION NO. SIGNATURE. OF : INDIVIDUAL • 10 1/4 ' ‘.7tir r ,.. rditiM;TA: - " 1Z-- . • • ••• • • • %I "flet. EFTA00277937 NOTICE Weight and balance or operating limitation charigei."shell be entered in the appropriate' aircraft record, 7 ' An alteration-must be compatible with all previoaalterations to assure tontinUed canformity with the previous. 'alterations applicable airworthinessrequirements. • • I. DESCRIPTION OF WORK1KOMPLISNED (If more. space is required, attach addit I sheets. Identify with air- craft nationality and registration mark and dote work completed.) -- - • . 1 . • VIDEO ICINITOR ND VCR -INSTALLATION ' . ,L1 ?P•41.1, . Revised-interior (which was preiiously installed and a "proved by Airesearth'; Aiiation Co.. Los Angeles, CA.:.4/7/01 on report. No..C-3588).as follows . Modified Coat Closet (Ft/H.Side"..Sta..814*t5) to.remive_moUnts f.01‘ . installation of the following: * • ;•••:k.r.;1; yipeo• Recorder -MitsubishiNS-33OUR:' it;;;Ithed.,PiOnttoi,,,: :,mit.;sithisht CM-1901 3. Infra-Red Transmitter Nady 1RT-200 -A: Altitude Cut4Ut Switch -.Anint 90500 ,5:.' Power Receptacle ;":7777K1 • • ...,.: . .6. : Pewer:SUpplY..:AC4C: AdiOtehl':',:.NadY,I.A72420 .....:._:::: ,.......: . • . i i Modification of coat clOset in accOrdence:With Structural Substantiation RepOrt NO: 243. and. Draividg-No. 266e submitted and approlied:on'FAA.fOrm.8110-3 by ..L A:. DOgel by.i 0.4.- . it::Ttirettutoleelglileering ',Company, Sin Antonio, TX. : Reports and drawings are available to the AdministratOr:on-request..: ' ' . . , . , . • f A;;', Pei,oer Supply as follows: . . • A. 28V DC Bus No. 1,(Drain Valve,: Shower 3. amp CB, existing). . . • B. .115V AC 60Hi (Utility Outlets Aft .Cabin - 15 amp C8, existing). ! ... • . : .• • • • • • • • : • • • .1 • . IV.. 'Utilized existing !Al tee..755E:Speamers:at.Sta....730.0_. _ : V. 'Systems installation is in aceordanee "N505T VAdeo* - System': dated -7/26/84. : " • _ VI. All work performed utiliii0g4CciOtable methods, techniques, and , practices '.0er AC 43.13-1A4.-Chpi.15:6:04C..43.13,2A -Chott.: 1t6._24.. , . • _ . VII: 'intiallation- waefoiktiohally Itettedat ground level. end at'altitude dUring -performance check- flighti;ihd:.operitedsatisfactorily-404tdid:hOt adversly affect the operation. of .anY'.1)thet:licsterifs-._ - Rircraft' weighed ' ileighnana Bel anCe-a0d . at amended. .. . • ... . " ' - • - • • •-- ••: . • - • • *MS. GOVEMIliata PRINT.04.4 OFFICE: 1977-77,421/2/10 ••• EFTA00277938 MEM OF montoitinnow - • • Ff00AVIATION ADMINISTRA110"4 Fitdpmeived Beiges Bureau Noi 94—R060.1 ' • MAJOR REPAIR AND ALTERATION - FOR FAA USE *NIX- . s lAirfr ok am . Pow•rplant, Propelkr, *r Appleana) ON A6DENTMSATION -6,-17>e, INSTRUCTIONS: Print or type all entries.- See FAR '43.9,, FAR 43 Appendix 'and AC 43.3-1 (or subsequent revision thereof) for instructions and-disposition of this form. . MAKE Boeing •- - MODS • • • . 727-31 I. AIRCRAFT SERIAL NO. • • 20115 . NATIONALITY AND . N5051. REGISTRATION A' i 2. OWNER . NAME (As shown on registration certificate) - Tenneco Inc. • . ADDRESS (As shown on registration °edifice* 16951 J.F.K. Blvd. Houston, IX 77032 . '' . 3. FOR IAA USE An I. . . . . • . . . ' ' . . • : . . . . ... • - . - . . .— . .— ___,....... / —. , • - .. 4. UNIT IDENTIFICATION- .:. 5. TYPE Witt . ,SERIAL NO. /SPAM ALM- Anon AIRFRAME memomennennamne (As dasaind in item 1 above) XX POWERPLANT _ MOMS • APPUAtICE roe . ` • . NANVIACOMINI 0....r. - 4. OINTORINTf SIATEMBIT _ • A. AGENCY'S WALE ANDaRESS. • , • fr K*40 Or AGENCY C. CERTIFICATE NO. Tenneco 1695! J.F.K. Houston, bat Inc. Blvd.,/ - ...I j.:-. TX 77032' U.S. Cternicana maawac :205-10. . twins OVITMCATIO AtIOIANIC •X Penman ammo station, - '''' - tififimpArmana D. I certify 'thin the repair andiot ii/Miatliali'Matitio the ank(e) identified in item 4 above and described on the reverse or attachments bent* have been made inateardateee with the requirements of Pan 43 of the U.S. Federal Aviation Regulations and that the information fissnisbaLhereits:le !tend correct to dribs, ofmytemerledge. •. . . . • DATE `;'..,i ' ! i ; ' ;.i.'1.• =Wart Of. . - " 8/3/84 . - . • t • . ., . - - . ‘,,..- . .. - isenvia fa MINI TO SERVICE I.'. ' • • Pursuant to the authority given persons specified below, the unit identified io item 4 waszbasted in the manner prescribed by the Administrator of the Fedetal•Avistion Adsninistradot; and is igi pPROVED. QM Pm Ittelininsl. . aiiiiii veire.." :.". itelebtleata isitte:MIAllUile...:'c: °M .. _. 4 ._ . '..::.c. . . .. . Nub, ottitanet: - - x ISM ;SIMON Of 17.011f 0t1 SIVE= Of EIMOKAPT - • •••• DATE Of APPROVAL. OR, , REJECTION ' ' ' ' ...... 8/3/84 • CERTIFICATE 01 .. .; . DESIGNATION NO: 205-10 SifirbiPmg. OF . UTK . ..040,M.04'...t.-: - • : - • - •• •: ` 4 • • . I ., '• ' ‘ • d i .• ... • • S s • • • . 1 ••• • ••• : • S. • • • • • • • • • . • • • . . • •• • • • • • ", • •••- : p • •• .15 c.f . -'sr.t .‘ ,;:ri gtettn. ;.;-‘.. • . - • ---- ••..• ••••••••••• EFTA00277939 , I. AA AIRCRAFT REG TR NO. ) DATE: "e".!'•• • . E - Weield'and balance ar..ope ot.npp limit Lion chaeges,shisn be enter.e.d inlipe.appropriate aircraft record. An alteration must be COnqicitible with oil :preirioio.alterations to assorseentiOuod conformity with-thit applicable airworthiness requirements. L7, • • ;_ O. •DESCRIP1104 OF WORK ACCOMPLISHED• (if more ipaai is requires attach additional sheets: , identify with oir- croft nationality. and nigidrallon.:inadc. and dcd• work-annialided.) '". " • ... .• . • . - BODY STATION .950 BULKHEAD FORGING REPAIR • . • • .- • .; --• • Repaired left and right BS 950 foiging, lower Section, *in:accordance with • instructions• provided by Threshol d ,Efigineeri nve.ompany Of :San Antonio, TX. Subject inStrUctionS..t.are identified, in,:i*.eports:K.• 242 and No. 244. Reports We're drafted and apprOved'on- J. A. Dii01 fp E .R and'. are.:avai l abl e the"'Aihnf strator -on: request ' = • _II, All :work performed utilizing accePtahlk, methods;, techniques,- and practices . per..AC 43.13.61A. • --7, I I I • Airctlift and' Balance aliendecl..h . -:- • • •- - • - • .. • ADOIT(044 SHEETS ARE TTACH6 • • . . • • - • • • • • . , . ',':•X•V • .: ,.. . ..;•-•••• --•.• „..; . .. 4 .0 411, - _.... , • EFTA00277940 • . (,- VITNERIT OP. TRANSPORTATION . C . • flittsif AVIATION AomimstRATioN Oat Appeared Budget Bureau No. 04-Rollo.s • . MAJOR REPAIR •AND ALTERATION FOR FAA USE ONLY • , (