EFTA00615063.pdf

Gulfstream' A 0 •NfAAL DYNAMICS COMPANY 15 February 2013 Mr. Larry Visoski Hyperion Air, Inc. 3800 Southern Blvd., Suite #204 West Palm Beach FL 33406 Office: Dear Mr. Visoski, In response to your request, Gulfstream is pleased to provide the following Service Center proposal for maintenance to be accomplished on this Gulfstream GIV aircraft. After review of this proposal and its attachments (if applicable), should you have any questions, concerns, or scheduling requests, please feel free to contact me, so we can coordinate a mutually agreeable input date for your aircraft. Furthermore, if this proposal with its attachments and Terms and Conditions is acceptable to you, please sign and return the Summary page to or Thank you for considering Gulfstream for the proposed workscope on your aircraft. Please do not hesitate to call me with any questions or for additional information. Sincerely, Tom Baliya National Sales Mana er Office: Mobile: Fax: WPUdlh EFTA00615063 ctifirkS t fr l erf ea DYNAMICS COMPANY WORKSCOPE 1. Aircraft Records and Condition Survey (Exhibit I) Labor and Materials $24,000.00 GAC0213-408-GIV.OCS-R00 15 February 2013 Hyperion Air. Inc. Description: The Aircraft Records and Condition Survey includes Records / Logbook Research and Pre-buy Inspection Schedule of Events • Review workscope and identify points of contact with both buyer and seller present and have both parties sign the Hold Harmless Agreement. • The party requesting and financially obligated for the Aircraft/Records and Condition Survey (usually the Buyer) must have an authorized representative sign the work order and the Hold Harmless. • There will be a representative from all parties involved that will make decisions on all minor corrective actions to be accomplished during Aircraft/Records and Condition Survey. • If there is no representative present, no corrective action can be accomplished until authorized. • Upon completion of the Aircraft/Records and Condition Survey, the discrepancy list will be provided to the party(s) responsible for disposition. • If a second or third party is involved with rectification of any discrepancies found, the parties will identify who will be responsible for the corrective actions. • At this time, separate work orders will be opened and responsibilities assigned to each party for the work requested. • All parties involved, based on the Service Center workload, at that time will mutually agree to the downtime schedule for the authorized work. The Aircraft/Records Survey includes the following: Review of Maintenance History and Records: A review of all available maintenance records will be accomplished. The review will include a search for recorded damage history, special inspections accomplished, missing records, compliance with required inspections, maintenance, and mandatory directives. Any problems with incomplete or improper maintenance entries, missing certificate numbers or signatures, or disorganized maintenance logs will be documented in the report. If a complete reconstruction of maintenance records or logbooks is desired, it will be considered an effort over and above the basic Survey price and schedule and will be performed at time and material upon approval. Documentation of Non-Applicable Maintenance Bulletins: Gulfstream will update the aircraft records for non-applicable or previously accomplished directives (ACB, CB & AD) that are not documented in the maintenance records. A budgetary, estimate to research and document non-applicable or previously accomplished bulletins is S75 per occurrence. Incomplete records may substantially increase this cost. Review of Required Aircraft Documentation: A review of weight and balance, equipment list, and electrical load analysis will be performed to determine that the known current aircraft configuration is reflected. All data will be cross-referenced against Major Repair and Alteration FAA Form 377 found and the avionics inventory. Subject matter and date of Form 337 and any related Supplemental Type Certificates (STC's) numbers will be listed. The certificate of airworthiness and current registration will be checked to ensure a match to the aircraft. Review of Required Flight Manuals & Supplements Gulfstream approved flight manuals will be reviewed to determine revision status and presence of all required approved flight manual supplements. Flight manual supplements will be cross-checked against STC's. Update of Required Flight Manuals and Supplements: If required, Gulfstream will update any missing or outdated items in the flight manual supplements section of the flight manual or supplement binder with current data. A budgetary estimate to research and retrieve missing flight manual supplements is S75 per occurrence. Incomplete records may substantially increase this cost. Page 2 of 9 This proposal is confidential between Gulfstream and the customer. EFTA00615064 Gulfstreant A OISNERAL DYNAMIC• COMPANY GAC0213-408-GIV.OCS-R00 15 February 2013 Hyperion Air. Inc. The Condition Survey includes the following: Functional Test of Avionics Equipment: An avionics ramp check is performed and involves powering up all major avionics equipment and functionally testing navigation, communication and flight management systems for proper operation. Results will be fully documented on the work order and findings will be highlighted in the Survey. As the Survey progresses, discrepancies may be identified. At this point, discrepancies will be listed on summary sheets and provided to customer. They will be identified as information items or items required for return to service and will be performed at Time and Material. Any Engineering dispositions will be an additional expense and will be billed, As Required. Inventory of Avionics and Emergency Equipment: A physical inventory of major avionics equipment will be accomplished and the results recorded in the report. The avionics inventory is limited to accessible areas only, additional access will be billed at time and material. This inventory will be cross- referenced against the equipment list during the documentation review. All cabin and cockpit installed emergency equipment will be inventoried and recorded in the report. Physical Survey: Is in accordance with attached Gulfstream CMP (Computerized Maintenance Program) tasks, which provide a detailed view of specified areas of aircraft. The suggested survey workscope is intended to provide you with a thorough physical evaluation of selected areas of the aircraft. Cockpit and Cabin Compartment above Floor Inspection: A general visual Inspection will be performed of cockpit. cabin, and baggage compartments for mechanical and cosmetic discrepant conditions which are deemed as unsatisfactory. This above floor inspection does not include operational testing of components or equipment. Corrections and repairs to discrepant conditions found will be accomplished as time and materials. Interior access will not be required or included for this general visual inspection. Aircraft Records and Condition Survey Report: The report is a bound document and is divided into fourteen (14) indexed sections. The format facilitates rapid access to desired information and highlights the major elements of the Survey. All findings and information yielded by this Survey will be provided in the report and on the related work order upon completion of the Survey. Two (2) copies of the report will be provided to the purchaser of the Survey and one (I) copy of the discrepancies noted to the owner (additional report copies are available at $150.00/each). Copies will not be provided to any other party including the owner of the aircraft unless expressly authorized in writing by the purchaser of the Survey. Ootional Services Gulfstream also offers a complete in-house detailing service for your Gulfstream aircraft. Our experienced team of professionals can perform any detailing service; from a dry wash of the aircraft exterior to shampooing and stain-treating carpets and furnishings. Exterior services include washing of the aircraft (to include landing gear), waxing the aircraft with Aeroglaze, buff and polish of leading edge "brite work", and sanding to remove surface corrosion. An application of Teflon coating is also available to enhance the life of your paint as well as to reduce aircraft exterior cleaning time and costs. Interior services include sanitizing galley and lavatories, re-corking of drawers, shampooing of carpets, re-oiling of leather, and an application of soil and stain repellent for the carpet and upholstery. 2. Option: Auxiliary Power Unit Borescope (Exhibit 2) Labor and Materials $900.00 Task: Perform APU Borescopes. 3. Option: Engine Runs and Borescopes (Exhibit 3) Labor and Materials S14,500.00 Task: Perform Engine Runs and Borescopes. Page 3 of 9 This proposal is confidential between Gulfstream and the customer. EFTA00615065 Gulfstreanef A osesanAL DYNAMIC• COMPANY GAC0213-408-GIV.OCS-R00 15 February 2013 Hyperion Air. Inc. 4. Option: Landing Gear Corrosion Inspection (Exhibit 4 Dunlop I Exhibit 5 ABS) Labor and Materials $23,000.00 Note: For budretary planning purposes, estimated material and outside services for the above quoted CMP package is approximately $500.00 and it does not include material required for clearing of any discrepancies. 5. Option: Two (2) Pilot's for Condition Survey Flight (Must be Performed with Engine Runs and Borescopes) Labor and Materials $5,500.00 Task Two (2) Pilots for Condition Survey Flight (Based on an eight (8) hour day). Condition Survey Flight • Engine runs and borescopes will be required prior to performing a Gulfstream Condition Survey Flight and is not included with this option. • The Engine Runs and Borescope Option must be selected / performed prior to the Condition Survey Flight: • The flight test card will be identical to the one used by our own Gulfstream Flight Department to evaluate pre-owned aircraft that are being considered for purchase by Gulfstream. • This is an extensive flight test regimen flown by Gulfstream test pilots (at an additional expense). • Test flight results are fully documented and reported in work order and Survey Report. The optional Flight Test may affect downtime. • All pilot's fees and travel expenses will be the responsibility of the customer per the Gulfstream labor rate letter and is not included in this proposal. Note: Fuel will be billed on actuals. 6. Option: ASC 416A - MSG3 Maintenance Program Task Accomplish ASC 416A - Time Limits/Maintenance Checks (ATA 5) MSG-3 Maintenance Program Conversion. Description The MSG-3 Maintenance Program Conversion is based upon an analytical process designed to identify scheduled tasks and maintenance intervals based on the aircraft operating capabilities. This inspection program reduces maintenance costs without affecting aircraft safety or reliability. Gulfstream, operators, suppliers and the FAA participated in the development of the MSG-3 program. The man-hours required for converting to the MSG 3 Program will vary with each aircraft configuration and the standardization between aircraft in an operator's fleet. ASC-416A is a managed program. Please contact Gulfstream Customer Support at I.800.810.4853. MSG-3 Program savings include but are not limited to the following: • Extending the current I50-flight hour check to 450 flight hours, known as an "A" check. • The number of annual or calendar inspections are reduced based on a 12 month "C" check interval. • Engine options is available per Rolls-Royce Service Bulletin 70-1493 Page 4 of 9 This proposal is confidential between Gulfstream and the customer. EFTA00615066 Gulfstream® A osesanAL DYNAMICS COMPANY Budgetary Pricing Only Phase I • GIV-GER-1197 (Aircraft Transition Plan) $10,000 • Initial Engineering Review $20,000 • Rolls Royce Service Bulletin 70.1493/1517 - $5,000 Phase II • ASC 416A (Parts 1 & 2) - $15,000 • Structural Audit (Fatigue and Damage Tolerance Evaluation) - $30,000 GAC0213-408-GIV.OCS-R00 15 February 2013 Hyperion Air. Inc. Notes: • Military and Special Missions Aircraft require additional research to evaluate the Mission Plan and flight operations. Pricing is subject to change on these aircraft and aircraft not outfitted at a Gulfstream facility. • Pricing varies depending on aircraft configuration, repairs and modifications that have to be evaluated. Down Time: Down-time typically not required, unless supplemental inspections required prior to ASC416A Part 2 sign off. Process: Operator commits to the Program with a signed agreement and purchase order. The Aircraft is scheduled and transition is initiated 7. Option: ASC 488 - Fuselage Station (FS) 793 Bulkhead Cap Angle - Replacement Labor and Materials $137,209.00 Task Accomplish Aircraft Service Change (ASC) 488 - Fuselage Station (FS) 793 Bulkhead Cap Angle - Replacement. This price is predicated on performing ASC 488 and the 5000 Landing Structural Rat Rated Inspection concurrently. Aircraft Service Change Description The FS 793 Cap Angle may require replacement as a result of performing the FS 793 Aft Bulkhead Cap Angle - NDT Inspection (CMP 535201). This service change replaces the existing two (2) aluminum cap angles on the aft side of the FS 793.75 bulkhead with a one-piece stainless steel cap angle to reduce the possibility of cap angle fatigue cracks. Effectivity: This service change is applicable to all GIV Aircraft. AIRFRANIE CONTINGENCIES This proposal does not include correction/clearing of any discrepancies and/or corrosion that may be found. outside services. additional due items (i.e. customer requirements. completion/outfitter requirements. Part 135 "for hire" requirements. etc.). and/or consumables. These issues will be addressed separately from this proposal with the customer and may impact scheduled downtime. Any revision(s) to Chapter 5/Maintenance Schedule issued prior to aircraft arrival may affect the inspection price. Should additional work be required. it will be accomplished on a time and material basis, unless otherwise noted. For aircraft with standard paint schemes (one (I) base color and two (2) stripes), the sealing and touch-up (by brush) of panels will be considered part of the inspection hours for that task. Aircraft with non-standard paint schemes will be charged for the additional time required to complete the paint touch-up. Time required to seal and touch-up sealant for discrepancies on items not open for inspection being performed during this visit will be billed at time and material. Page 5 of 9 This proposal is confidential between Gulfstream and the customer. EFTA00615067 Gulfstream® A OSIMMAL DYNAMICS COMPANY REMITTANCE INSTRUCTIONS GAC0213-408-GIV.OCS-R00 15 February 2013 Hyperion Air. Inc. Checks: Gulfstream Aerospace Corporation (Overnight) Gulfstream Aerospace Corporation (Box #730349) P.O. Box 730349 do JP Morgan Chase Bank. NA Dallas, TX 75373-0349 Ann: Dallas National Wholesale Lockbox TX1-0029 14800 Frye Road Ft. Worth, TX 76155 Wire Transfer Gulfstream Aerospace Corporation Instructions: JP Morgan Chase Bank. NA I Bank One Plaza Chicago. IL 60670 Account No. 10-15825 Reference your Five (S) Digit Customer Number (XX-XXX) Bank Fedwire Routing No. (ABA) 021 000 021 Identifiers: S.W.I.F.T CHASUS33 ACH Credit Routing No. (ABA) 071 000 013 Note: Please reference one of the following (as applicable): • Invoice No. • Sales Order No. • Job or Work Order No. • Aircraft Serial or Tail No. • Contact Name • Customer Account No. (XX-XXXX) TERMS AND CONDITIONS Gulfstream Aerospace Corporation requires the estimated amount be paid in full for Aircraft/Records and Condition Survey prior to aircraft induction to Service Center. All Aircraft/Records and Condition Survey related discrepancies must be paid in full prior to aircraft departure. Except as set forth below, payment terms are net 30 days from date of invoice. For Work estimated to exceed 5100.000. Customer agrees to make progress payments on the following schedule: 113 of the estimated amount prior to commencement of Work on the Aircraft. 1/3 within 10 days after Gulfstream's written notice that the Work is approximately 50% complete. and final payment 30 days from date of final invoice. Additional deposits may be required for long-lead or special purchased pans. which are not refundable should the visit be cancelled or work scope changed to eliminate those items. If any portion of an invoice is disputed. then Customer shall nevertheless pay all undisputed amounts per this schedule. Gulfstream shall not be required to release Customer's Aircraft to depart if Customer's total outstanding balance owed to Gulfstream exceeds the lesser of $100.000.00 or Customer's available credit limit. All sums past due bear interest at the lesser of 1.5% per month. or the maximum rate allowable by law, plus reimbursement for attorney fees and other costs of collection. All prices stated herein are exclusive of freight. fuel, flight costs, and / or environmental fees. Additionally. customer is responsible for all federal, state, local and foreign taxes, levies, penalties and tariffs applicable to the work performed hereunder. the materials used or transportation (other than taxes on income of Gulfstream) and customer shall indemnify and hold Gulfstream harmless with respect thereto. This proposal is not valid at Gulfstream's Luton United Kingdom facility. Work items not quoted in this proposal will be billed on a time and material basis per our published labor rates at the time of aircraft induction for Maintenance. Electrical. Avionics. Refurbishment, and Engine/APU Maintenance. For time and materials work: (a) labor (including engineering services) is billed according to the rates set forth in the Gulfstream Labor Rate Letter in effect as of the date the work is performed.. and (b) materials are billed according to Gulfstreant's standard prices in effect on the date the material is used. Any incremental charge under Gulfstream's Component Exchanged Program will be billed by supplementary invoice. This proposal is contingent on all work being accomplished during the same timeframe. unless otherwise noted. Page 6 of 9 This proposal is confidential between Gulfstream and the customer. EFTA00615068 cg fStreanf DYNAMICS COMPANY TERMS AND CONDITIONS (continued) GACO213-408-GIV.00S-R00 15 February 2013 Hyperion Air. Inc. The quoted prices are valid for a period of thirty (30) days of receipt of proposal. unless otherwise noted. Gulfstream recommends a firm schedule be established and work be completed within the next three (3) to six (6) months from the date of this proposal. Any change in workscope and/or schedule may require review by Gulfstream and requires revision of this proposal. Gulfstream reserves the right to pass on price increases to the customer. The Customer is responsible for making certain that all specific preservation tasks related to the Aircraft. its engines or systems. that are required or may become required while the Aircraft is at Gulfstream's facility for the Workscope be indentified on the Work Authorization squawk list. Gulfstream warrants that the work conforms to the pertinent specifications prescribed by the applicable aircraft I component manufacturer. and that any components or other items supplied hereunder (but excluding customer-furnished items) are free from defects in material and workmanship. This warranty extends to defects discovered within twelve (12) months. or one thousand (1.000) flight hours. whichever comes first, after completion of the work: except that the warranty period for any work performed as warranty work is equal to the pre-existing unexpired warranty period. Parts qualifying for the "Exclusive Gulfstream Parts Warranty Extension" Program. or other extended published Gulfstream warranty programs. if any. are entitled to an extended warranty period pursuant to the terms of such Programs as they exists on the date this agreement is executed. Proposal pricing and schedules are contingent upon the customer supplying the existing avionics, electrical, and aircraft system prints, drawings and diagrams. which accurately represent the current condition of the aircraft. Any changes from the existing drawings will be performed on a time and material basis with customer approval. Any relocations of existing equipment required due to space limitations will be performed at time and materials until a firm proposal can be prepared. Detailed parameters of this proposal may require modifications following an in-depth physical inspection. Materials used during the clearing/correction of discrepancies and/or items based on time and material will be quoted and/or invoiced on an "As Required" basis. There will be a 3.5% charge for consumables. to a maximum of 54.000.00. on all work orders containing labor revenue charges. This charge will be calculated based on the total labor revenue man-hours invoiced on the work order. Only invoices defined as a "Road Trip Invoice" will be exempt from this charge. Customer furnished parts and drop shipments will be subject to a handling fee of 15% based on current manufacturer list price. The handling fee will not apply to parts originally purchased from Gulfstream. Proof of purchase from Gulfstream must be shown to waive the handling fee. If enrolled in Gulfstream's PlanePartsni program. certain components supplied in regard to this proposal will be at no charge to the Customer. To enroll or learn more about the program. please visit http://www.gulfstream.com/product suopon/planepans/. Any estimates given for outside services are not intended to be exact figures. Repair. calibration, overhaul. and/or exchange pricing will be billed as accrued, be it either less than or more than quoted. Changes to the Completion Center Maintenance Handbook (CCMH) or Cabin Operating Manual (COM) are not included as part of this proposal. Should a modified CCMH or COM be requested. it will be quoted separately or performed on a time and materials basis. Any changes to the Minimum Equipment List (MEL) are the Customer's responsibility and are not included herein. All exchange parts prices are subject to our vendor acceptance of exchange core. Should exchange core be rejected or subjected to an extra charge by Vendor at any time for reasons of abnormal wear and tear, damage. unauthorized modifications. or other discrepancies. the customer agrees to reimburse Gulfstream for resultant extra costs. Any existing unused wiring will be capped and stowed. Wiring removal (if requested/required) will be handled on a time and material basis and billed additional to the proposed amount. All removed equipment will be retained by Gulfstream. unless otherwise noted. Interior access will be performed on a time and material basis. unless otherwise noted within this proposal. Page 7 of 9 This proposal is confidential between Gulfstream and the customer. EFTA00615069 Gulfstream' A GUN DYNAMICS COMPANY TERMS AND CONDITIONS (continued) GAC0213-408-GIV.OCS-R00 15 February 2013 Hyperion Air. Inc. When aircraft is firmly scheduled into a Gulfstream facility, preliminary engineering and planning commences, and materials / components are ordered for the workscope. If the workscope is canceled. the customer will be charged for any labor expended and/or any restock charges incurred on materials I components ordered. If materials / components cannot be returned to vendor(s), customer will be billed in full for these items. In such case, the materials I components would become the property of the customer. If the workscope is rescheduled for a later arrival, these charges will be applied to the rescheduled visit. Working days are defined as Monday through Friday. Should additional work be required. other than that quoted herein, the estimated downtime may require extension. This proposal does not include overtime. Any overtime required will be approved by the customer prior to work commencing. All non-scheduled NDT will be on an overtime basis due to NDT planned scheduling. Customer's oral changes increasing the scope of the Work or approving overtime are binding (unless otherwise provided by law). International Contingencies (If Applicable; Foreign Registered Aircraft Only with Domestic Input): Foreign Operators Civil Air Authority (FOCAA). FAA. or concurrence of both agencies must first approve this STC Project prior to start of aircraft modification. Any cost involved in this approval process will be charged as time and materials. Upon customer's acceptance of this proposal. Gulfstream will submit an "Undue Burden" Project Request or FOCA certification fees to the FAA ACO or FOCAA as applicable. Once the FAA and/or FOCA approves the "Undue Burden" Project Request or FOCA certification fees. the ACO will notify the Foreign Civil Air Authority (FCAA). Once the FAA ACO receives concurrence from the FCAA. the ACO will notify Gulfstream. Gulfstream will submit Application (8110-12). Cert. Plan and an LOI to the FAA ACO and/or FOCA. Please note (if applicable), the time estimated to accomplish these steps is approximately three (3) to six (6) months depending on resource availability of the FAA and/or FOCA. If there is any conflict between these Terms and Conditions hereof and any document incorporated herein by reference. then these terms and conditions shall control unless such document expressly states the contrary. Quoting Contact: Dan Hyde. Mechanical Quotin Mana er Tele: or email: Page 8 of 9 This proposal is confidential between Gulfstream and the customer. EFTA00615070 Gulfstream' A GUN DYNAMICS COMPANY PROPOSAL SUMMARY GAC0213-408-GIV.OCS-R00 15 Febniary 2013 Hyperion Air. Inc. • Please initial items in Accept/Decline columns. (Please note that quoted dollars and downtime may vary based on concurrent %lurk with accepted/declined items.) Item Workscope Amount Accept Decline I. Aircraft Records and Condition Survey $24,000.00 2. Option: Auxiliary Power Unit Borescope $900.00 3. Option: Engine Runs and Borescopes $14,500.00 4. Option: Landing Gear Corrosion Inspection $23,000.00 5. Option: Two (2) Pilot's for Condition Survey Flight (Must be Performed with Engine Runs and Borescopes) $5,500.00 6. Option: ASC 416A MSG3 Maintenance Program See Item 7. Option: ASC 488 — Fuselage Station $137,209.00 ♦ Downtime required for this workscope will be eleven (11) working days. This downtime estimate is subject to any discrepancies that may be found. ♦ Leadtime required for this workscope will be five (5) calendar days after proposal acceptance and is subject to equipment availability. ♦ The Aircraft Records and Condition Survey is limited in scope, and Gulfstream cannot guarantee that this Survey will uncover all problems that exist with the inspected aircraft. Ultimately, the buyer must rely on their own judgment as to the aircraft value and the seller's warranty, if any, as to the aircraft's condition. ♦ This proposal (or estimate) expressly incorporates and is subject to Gulfstream Aerospace Corporation's standard work authorization Terms and Conditions. Your acceptance of all or any portion of this proposal (or estimate confirms your agreement to accept those standard Terms and Conditions. (Please sign and return this page to Proposal Acceptance Signature Date This proposal summary does not include items based on time and material, discrepancies or corrosion found or other materials required. handling fees. or other additional expenses outside the specified workscopc of the enclosed proposal. Page 9 of 9 This proposal is confidential between Gulfstream and the customer. EFTA00615071 GIV Aircraft / Records and Condition Survey (Exhibit 1) NON-MSG3 Aircraft RFQ # GAC0213-408-GIV.OCS-R00 CMP Primary Code Description 100310 CK AIRWORTHINESS DIRECTIVES 100320 CK SERVICE BULLETINS 134401 C/W AVIONICS INVENTORY 191108 REVIEW A/C STATUS AND RECORDS 231001 AVIONICS--FUNC RAMP TEST 291030 Combined Hyd Sys DPI (Eng-driven Pump Bypass) - Inspection 291031 Flight Hyd Sys DPI (Eng-driven Pump Bypass) - Inspection 291032 Combined Hyd Sys DPI (Main Pressure) - Inspection 291033 Flight Hyd Sys DPI (Main Pressure) - Inspection 291034 Combined Hyd Sys DPI (Main Return) - Inspection 291035 Flight Hyd Sys DPI (Main Return) - Inspection 292020 Auxiliary System DPI (Pressure) - Inspection 292021 Auxiliary System DPI (Return) - Inspection 292024 Utility System DPI (Pressure) - Inspection 292025 Utility System DPI (Pump Bypass) - Inspection 330007 Emergency Exit Lights - Operational Test 330010 Exterior Lights - Operational Test 324108 Wheel Brake Lining - Wear Check (Brake-By-Wire) 324268 Brake Linings - Wear Check (HMAB / Dunlop) 351005 Crew Oxygen System (Pilot) - Operational Test 311006 Crew Oxygen System (Copilot) - Operational Test 521009 Baggage Door Inflatable Seal Sys - Ops Test 532005 Cabin Compartment Above Floor - Inspection 532017 Cockpit Compartment Above Floor - Inspection 532027 Entrance Compartment Behind Panel - Inspection 532041 Baggage Compartment Above Floor - Inspection 532067 Tail Compartment Above Floor - Inspection 533005 Exterior Fuselage - Inspection 534015 Main Landing Gear Installation (Left) - Inspection 534016 Main Landing Gear Installation (Right) - Inspection 534018 Main Landing Gear Wheel Well Compartment - Inspection 534020 Nose Wheel Well and Gear - Inspection 535008 Nose Compartment / Radome Interior - Inspection 541017 Pylon External / Internal (Left) - Inspection 541018 Pylon External / Internal (Right) - Inspection 551019 Horizontal Stabilizer/ Elevator (Exterior) (Left} - Inspection 273003 ELEVATOR FREE PLAY--INSP (Related Code) 551020 Horiz Stabilizer / Elevator (Exterior) (Right) - Inspection 553005 Vertical Stabilizer / Rudder (Exterior) - Inspection 554007 Rudder External - Inspection 571005 Wing Exterior (Left) - Inspection 571006 Wing Exterior (Right) - Inspection 490002 AUX POWER UNIT--OPS TEST 490005 APU Enclosure - Inspection 490052 APU - Operational Test 490053 APU Enclosure GTCP36-150(G) - Inspection GTCP36-100 APU ONLY GTCP36-100 APU ONLY GTCP36-150(G) ONLY GTCP36-150(G) ONLY Page 1 of 5 EFTA00615072 Auxiliary Power Unit Horoscope (Exhibit 21 RFC)/ GACO2B-40g-GIV.00S-R00 (NIP PrUnarm, Code newt-lotion 49000' APU GTCP 36-100 - Borewope 490000' APU GTCP 36-150 - Borewope EFTA00615073 Op Engine Runs and Borescopes (Exhibit 3) RFQ# GAC0213-408-GIV.OCS-R00 COP Primary Code Description 710019 Powerplant internal- Inspection 711009 Cowl Latch. Engine (Left) - Rigging (Related Code) 710025 Engine Borescope inspection 710031 Engine-Ops Test 732001 Engine Acceleration - Test! Adjustment (Related Code) 732005 Engine Deceleration - Test! Adjustment (Related Code) 732049 Engine Handling (ACU) Solenoid - Ops Check (Related Code) 732057 Engine Approach Idle Solenoid - Ops Check (Related Code) 732011 Ground Idle. Engine - Test! Adjustment (Related Code) 732013 Approach Idle - Adjustment / Test (Related Code) 783013 T/Rev Interlock Feedback Sys (LH) - Ops Test (Related Code) 783014 T/Rev Interlock Feedback Sys (RH) - Ops Test (Related Code) 783017 Maximum Rev Thrust (LH) - Ops Test f Adjust (Related Code) 783018 Maximum Rev Thrust (RH) - Ops Test! Adjustment 730001 Fuel Contamination Check. Engine - Inspection 742001 Engine Ignition System • Ops Check 742006 No.2 Igniter Plug - Removal / Installation 742016 No.2 Igniter Plug - Inspection 774955 Engine Chip Detector- Visual Check 792007 Filter. Engine Pressure Oil • Cleaning / Inspection 791033 Eng Oil Level - Check / Service. Using Onbd Sys (Related Code) 792013 Engine Scavenge Strainers - Inspection 710020 Powerplant internal- Inspection 711010 Cowl Latch. Engine (Right) - Rigging (Related Code) 710026 Engine Borescope Inspection 710032 Engine • Ops Test 732002 Engine Acceleration - Test! Adjustment (Related Code) 732006 Engine Deceleration - Test / Adjustment (Related Code) 732050 Engine Handling (ACU) Solenoid - Ops Check (Related Code) 732058 Engine Approach Idle Solenoid - Ops Check (Related Code) 750006 Airflow Control System - Test (Related Code) 732012 Ground Idle. Engine - Test I Adjustment 732014 Approach Idle - Adjustment /Test 730002 Fuel Contamination Check. Engine - Inspection 742002 Engine Ignition System • Ops Check 742008 No.2 Igniter Plug - Removal / installation 742018 No.2 Igniter Plug - Inspection 774956 Engine Chip Detector- Visual Check 792009 Filter. Engine Pressure OU - Cleaning / Inspection 791034 F.ng Oil Level - Check / Service. Using Onbd Sys (Related Code) 792014 Engine Scavenge Strainers - Inspection Page 3 of 5 EFTA00615074 Landing Gear Corrosion Inspection (Exhibit 4) Dunlop Wheels and Brakes RFQ N GAC02B-108.61V.OCS-R00 CMP Primars Code Description 320011 Nose Landing Gear and Components • Detailed Inspection 1N1006 Nose Landing Gear and Systems - Lubncation 1N1027 Nose Landing Gear Axle Assy - Corr Inhib Comp App 320028 Nose Landing Gear Shock Sum Assy - Con Inhib Comp App 320030 Nose Landing Gear Truss Brace Amy - Corr Inhib Comp App 320031 Nose Landing Gear Upper Upper Trunn Attach Points Corr Inhib Camp App 320032 Nose Landing Gear Upper Drag Brace Attach Pm - COI( Inhib Comp App 320033 Nose Landing Gear Striker Arms - Corr Inhib Comp App 322028 Nose Gear Shock Strut - Service 322036 Nose Gear Axle Fitting - Removal / Installation 123001 Landing Gear Normal - Rinctional Test 123004 Landing Gear Emergency Extension - Rinctional Test 124009 Nose Gear Wheel Any (Left) - Removal / Installation 124010 Nose Gear Wheel Any (Right) - Removal /Installation 125001 Nose Wheel Steering - Functional Test 325010 Nose Wheel Steering Unit Removal/Installation 320013 Main Landing Gear and Components (Left) - Detailed Inspection 320004 MW and Systems (Left) Lubrication 320015 MW Axle Fitting Attach Pin (Left) Corr Inhib Comp App 320017 MW (Left) Axle Fitting - Corr Inhib Comp App 320019 MLG (Left) Shock Absorber - Corr Inhib Camp App 120021 MW (Li) Side Brace Act Attach Pins & Trunn Area Corr Inhib Comp App 320023 MW (Leh) Uplock Roller - Corr Inhib Comp App 320023 MW (Leh) )Striker Ann Corr )dub Comp App 321013 MW Spindle Pin (Leh) Removal / Installation 321031 MW Shock Absorber (Leib- Removal /Installation 321073 Main Landing Gear Trunnion Pin (Leh Alt) - Removal/Installation 323002 Landing Gear Cycling - Operational Check 323015 Actuator. Main Landing Gear Side Brace (Lett) 324250 MW Wheel Assy (la Outboard No. I) -Rem/ Ina (Dunlop) 324231 MW Wheel Assy (L. Inboard No. 2)- Rem 1 Inst (Dunlop) 324220 MW Wheel Bearing IL Outboard No. 1) - Inspection 1 Pack 324221 MW Wheel Bearing IL Inboard No. 2)- Inspection / Pack 324260 Main Gear Brake (Left. Outboard No.1) - Removal / Install 324261 Main Gear Brake (Left. Inboard No.1)- Removal?Inaall 324206 11)droMecharucal Analog Brake Wear• Detailed Inspection 324207 Parking /Emergency Brake Operational Test 320014 Alain Landing Gear and Components IRIghtl • Detailed Inspection 3N/005 MW and Systems (Right ) Lubrication 3N)016 MW Axle Fatting Attach Pin (Right) - Corr Inhib Comp App 320018 MW (Right) Axle Fining- Corr Inhib Comp App 320020 MW (Right) Shock Absorber - Con !Myth Comp App 313022 MW (II) Side Brace Act Attach Pins & Trunn Area - Con Inhib Comp App 320024 MLO (Right) Uptick Roller- Con Inhib Comp App 120026 MW (Right) Striker Arm - Con Inhib Comp App 321016 MW Spindle Pin (Right) - Removal / Installation 321032 MW Shock Absorber (Right) - Removal I Installation 321076 Main Landing Gent Manton Pm (Right Aft) - Rem / Inst 323016 Actuator. Main Landing Gear Side Brace (Right) 324252 MW Wheel Assy(R. Inboard No. 3)- Rem 1 Inst (Dunlop) 324253 MW Wheel Any(R. Outboard No. 4)- Rem/ Inn (Dunlop) 324222 MW Wheel Bearing (R. Inboard No. 3)- Inspection/Pack 324221 MW Wheel Bearing IR. Outboard No. 4) - Inspection / Pack 324263 Main Gear Brake (R. Inboard No. 3) - Rem / Inst (Dunlop) 324264 Main Gear Brake (R. Outboard No.4)- Rem / Inst (Dunlop) EFTA00615075 (Al' liandiad Gear Coreallo MaritalIan 03000 Si ABS Wheat sad BoArt ;hamar. Coe Diarisiew 321003 Mails laminae Gen Componseue 03-Detailed Canada laiipeoded 3210= ?Inn Larding Our aril, • Iriteicanan 321221 }heat hiding One CIC Rearclo•.4hoe <Leh • 2212111 311(1 Axle Nude Mush Pm Leh iC1C App1aassi 321235 MUG Axle fitted .Ina A0e Luang Nut (Lehi Cif APPlaulan 321239 >ILO =act Abeoita Upper Lama Much Pint 11.1 CIC Aptilieasu 221243 Seletirano Actuate. Allah Ras Timmins AnalLcOI CIC Antlitaxa 321247 Main Landing Gear Oriole Wks IWO Of Arrkeaion 321251 >las Idedeng One Su0a Nml1n0ICICApplkdua 321029 Ilan. Gal MIN/. Pin deft A0). Renaud / Ineullarse 321217 MIDI Lading Gear Shock Absolve lLt(il• Reward 1' Irsallalion nix,' Nina Lading Coat Shwt Atewbcs NUN) SenucwIg 324101 Bukc Aunahly itert Ositholedi • RmuvalfInWlnwa 3241% Doke Auntie>(Len Idwasdi • Raaavalf InsdNm0 224144 MI10 Willitelt Gra Brak Assent!). (Lail °inboard) D Inspection 3241.15 Slems lauding One Beale Aisenty(140 bibrun) • D. Inepailoa 3242lC Asiustid • R111:1101141 Ted 224221 Wheel Spud Traneducer iLehOisibtunb• Remove / Ireaalleuon 3242= Wheel SgeolTiartediees dell Remota I lissallaion 32)011 Mak Leading Gra 50threot (40 • Removal I 11.•111411•Xl 323903 Unclad Gear • Pentland Toi 321901 LAMM( Gra Enniecua Oasis.. • Opearsaul Tea 52400) Slain Mad Averrily tido Ointamth • Renaud 22400) Shin Larding Ord Mad Krunng Oak °abated. hemmer if Clad 324004 Shia WIed Auciebly iLOl hawed, • Reseed Insiallaias 324010 >Ina 1-ding (-me Med Bang 'Len luboads • llopcupos (Check 224010 ?bin Lading Ord Whorl Buffing (Lou Inboard. Int/coca /Cheek 321004 Ws Landis* Gear Componcels 'RI • Detailed Corrosion Iteptellon 321036 Ilaas lauding Case ittelio • labiluaitia 3212 Main Lading Gra CICRa0glia0n(Rigtll 3212,2 5ILLI Axle Aiwa Aiierh (ROO C1C Appbeitace 3212!6 SILO Axk Rung and Ade Fining Net illtierlitiCIC Agthe aeon 321210 }ILO Shock Atsoibire Urpti to Louts Much PinsIR)0C Appkaawn 221244 Seleteate Accuse. Allah Piss nasals* Ana tRisho CIO Archaean) 221241 >las lauding One Uplork Rote 11400 C1C Apple:80m 321232 Main Lading Ord Suites Ann (Right, Cr APPliedall 321030 >Ins Greg Tffillt0111 • Ruowl/liistallation 321214 >Ins lauding Our Shod. Ateadiee iRatho• Removal lestallaion 3212(C >Ins lauding (kW Sail Ah.lbet IIRathi)• Scruas? 521107 bake Aurally iRigls Nevada RCOWVIII fLisialbusa 324101 Bake Mandl> ((`gilt Outhaedi • Raaavel 324011 >Ins leading( Whorl Bmmgllagk Inbasdi• lava-hie ICed 524146 Man Lading Cad brake Aseeentayakitla kdaludi D ImMuun 324223 Vaal Spail Tiandhsees Multi hied)- Renaud/ laullalon 324234 Vaal Spail Tiandhsees iRple Outbounl)• Removal/ laaallaion Nhan Lading Gras Sedtbr•ge • RtmCnaliing4IIMX. 3:51030 Ilais Whorl Aneably lRitO Inbourib• Remove, tbaallaion 324012 She. lasting Caw Whorl Busing Oagk Oittersoli•lespcvuoatebak 324036 Mem Wheel Av•orkly 'Right drily: m.0 • Rertired I kr/aliases 324147 Ilea. Lading Oat Brute Atienadh Multi Outkunti • D litspouon 322003 Nese LaaiNag Gear Capeants• Detailed Camels. Impettlan 321235 Nose Landing Oa Stock Sind kW Axle Autubly CIC ADPIKOKa 321256 Nose Lasing Goa MOWS A./sully ('IC Appligbiros 321259 Nose Lahti/ Gus Tease War AucenNy ('IC Applgs41011 321203 Novo Landing Gee liner Truman Ana h Pea (IC ACTliediss 321263 Nose Laidinr Gra I' pro Dug hove Allah Pis CC Apple:awn 321264 Nose Laidine Ore Sakti Amu (IC Anliorhos !212t) Nat LasWini Cc.: CM RtafPheaKa 322034 Nose LseiJita Ore • baba:anon 3222CC Nose Ladd/ Gees Slack Suet- &Moog 323903 Undies Gan'- Ewan-eat Tot 324101 Nay Mud AssemblyIWO • Rmm'all 1114.1120M 324007 NoseVan:1 Bewails:ado • Inaeoliont Pak 32404 None 0101 Assembly (Recta • Removal / Insialdecu MOW Nose Volicyl Bannpullbgluel Inspecuen/ Pack 325033 Song • Saichaul Toe EFTA00615076