EFTA00603223.pdf

Gul£stream PRELIMINARY INVOICE A OMMRAI. DYNAMIC* COMPANY 550 Connole Street - Brunswick. Georgia 31525 ParVModel #: CIV AC Serial No)Tail No.: Mail Remittance To: Gulfstream Aerospace Corporation P.O. Box 730349 Dallas, Texas 75373-0349 Overnight Remittance To: Gulfstream Aerospace Corporation (Box # 730349) do JP Morgan Chase Bank, NA ATTN: Dallas National Wholesale Lockbox TXI-0029 14800 Frye Road Ft. WOrdl, TX 76155 Wire Remittance To: Ciulfstrcam Aerospace Corporation JP Morgan Chase Bank, NA Chicago, IL 60670 Fedwire Routing No. (ABA) 021 000 021 S.W.I.F.T. CHASUS33 ACH Credit Routing No. (ABA)071 000 013 Bill To: JEGE LLC C/O GALAXY AVIATION INC ATTN: LARRY VISOSKI 3800 SOUTHERN BLVD, SUITE 204 WEST PALM BEACH, Florida 33406 United States Title: JEGE LLC Invoice Number. Invoice Date: Customer IDI P.O. Number. Repair Station: In Date: Out Date: Payment Type: Payment Terms: 1/19/2017 FAA CRS GR4D216111 01/13/2017 01/21/2017 Net 30-Open terms INVOICE SUMMARY FOR WORK ORDER NUMBER: Time & Materials Flat Rate Total Labor USD: $39,016.28 50.00 $39,016.28 Parts USD: $34,180.66 $1,560.65 $35,741.31 Services USD: $0.00 51,500.00 $1,500.00 Detail Subtotal USD: $73,196.94 $3,060.65 $76,257.59 Subtotal USD: $76,257.59 Funds on Deposit USD: $0.00 Total USD: $76,257.59 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 1 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603223 Bill To: Invoice Number Item: I AIRFRAME Culfstream CIV Team Manager. Jeff Stahl Customer Coordinator: James White Discrepancy: 1.1 Resolution: Step: 1.1.1 kciurn tm acre ice Open Inspection Labor Only Part/Model tr: CIV AC Serial No./Tail No.: TSNJTSO: CSN/CSO: Aircraft Time: Discrepancy: 1.2 Comply with Inbound and Outbound Inspections in accordance with Traveler RSQCT-57 Rev. 21 Resolution: Complied with Inbound/Outbound Inspection per RSQCT - 56 Rev. 17 Labor USD: No Charge N/ C Step: 1.2.1 Completed Inbound Preliminary Inspection Step: 1.2.2 Open Outbound Inspection Step: 1.23 Open SC Maintenance/Hangar/ Primary Codes / Touch Labor Only Step: 1.2.4 In Progress Inspection Labor Only Discrepancy: 13 Resolution: Accomplish Preflight Inspection Step: 1.3.1 Open Step: 1.3.2 Open Insure key has been returned to acft or customer if removed SC Maintenance/Hangar/ Primary Codes / Touch Labor Onb Discrepancy: 1.4 Resolution: Tool Clearance Discrepancy: IS CMP CIV NISC3 010010-Service Center Maintenance Induction Checklist Resolution: Complied with Service Center Maintenance Induction Checklist. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 2 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603224 Bill To: Invoice Number: Discrepancy: 1.6 Advise customer of preservation requirements per chapter 10 of the relevant maintenance manuals for airframe. engines, and APU; review requirements in relation to scheduled outdate and possible extensions of outdate: and perform maintenance or preservation actions as directed by the customer and documented on the work order item list. Resolution: Advised customer of preservation requirements. None requested. Discrepancy: 1,7 Billable Consumables & Shop Supplies (% per published Rate Letter), calculated based on the total labor revenue man-hours invoiced on work order. Resolution: Completed as Required Billing Method I Inure Rate Total Parts USD: Flat Rate 41,560.65 Total USD: 41,560.65 Discrepancy: IS Cover and Protect Aircraft Interior and Exterior as Required Resolution: Completed as Required Labor USD: No Charge N/ C Discrepancy: 1.9 Service Chemical Toilet Clean Galley Resolution: Completed as Required Labor USD: NO Charge NI C Discrepancy: 1.10 Arrival! Departure Assist & Video Aircraft Resolution: Completed as Required For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 3 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603225 Bill To: Invoice Number. Discrepancy: 1.11 Comply with hydraulic fluid contamination checks on the hydraulic cart. Resolution: Completed as Required Discrepancy: 1.12 Aircraft Cleaning Resolution: Completed as Required Discrepancy: 1.13 FUEL Resolution: Step: 1.13.1 Open FUEL/ DEFUELAS REQUIRED Step: 1.13.2 Open TICKET = GALLONS FUELED= DATE = Item: 6 AVIONICS Team Klanager. Jeff Stahl Customer Coordinator: James White Part/Model 14: GIV AC Serial No./Tail No.: TSN/TSO: CSNICSO: Aircraft Time: Discrepancy: 6.1 Copilot DLIDI erratic. (Shakes) "Customer on Bopp*** Resolution: Removed and replaced Copilot Standby DDRMI / DBDI P/N 520-3030-003 SIN 11534 with REPAIRED P/N 520-3030-003 S/N 210. Performed operational checks and compass swing with no defects noted. Reference items 11.8, 11.10, and 11.13 for work performed. Billing Method Hours Rate Total Labor USD: Time and Material ST 9.95 ® 5136.00 51,353.20 Labor USD: Time and Material OT 0.47 ® 5204.00 595.88 Parts USD: Time and Material 46,382.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). OAC_WorkOrderPreliminaryInvoicerpt 2011 Page 4 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603226 Bill To: Invoice Number: Total USD: 57,831.08 Pans: Re. No. Pan number: Description Quantity Sell price USD Extended USD 6.1 NI 520-3030-003 INDICATOR, BEARING DISTANCE I 56,382.00 $6,382.00 Step: 6.1.1 Step: 6.1.2 Completed Inspection Labor Only Completed AV1 Electrical Labor Only Discrepancy: 6,2 /42 IRU intermittent fail message. Note: Customer has already swapped IRU's and FWC's and problem didn't follow. Customer suspects a faulty bus controller. Resolution: Removed and Replaced Bus Coupler 5M16 P/N 1159SCAV400-I SRI 5105 with "NEW" P/N 1159SCAV400-1 S/N 031767, and Coupler 55A24 P/N 1159SCAV400-1 S/N 4357 with "NEW" P/N 1159SCAV400-1 S/N 031766. Performed operational checks with no defects noted. Reference 11.14, 11.15, 11.18, and 11.19 for work performed. See steps for details of work performed. Billing Method I tours Rate Total Labor USD: Time and Material ST 2033 fa $136.00 $2,792.08 Labor USD: Time and Material OT 0.89 'a $204.00 $181.56 Parts USD: Time and Material $1,318.24 Total USD: 54,291.88 Parts: Ret. No. Part number. lkseription Quantity Sell price USD Extended USD 6.203 1159SCAV400-1 COUPLER 2 5659.12 $1,318.24 Step: 6.2.1 Completed Inspection Labor Only Step: 6.2.2 Completed AV1 Electrical Labor Only Step: 6.2.3 Completed Trouble shoot IRU system 02 with power on aircraft and radio master on IRU 01 and 02 fails (that's normal) Selected IRU on only the 01 fail message cleared indicating the flight guidance is not seeing IRU data during the power up test. Swapped 1RU 02 with IRU 01 still failed swapped IRU back to original locations. Swapped FCC 01 and 02 still failed, swapped FGC back to original locations. More trouble shooting required. Step: 6.2.4 Completed Swapped NAV computers 01 and 02 still failed swapped NAV computers back to original locations. Removed IRU 02 checking pins. all looks good, reinstalled IRU 02. Started to check FCC and IRU computers by placing the aircraft in maintenance mode checking ASCB data. the aircraft failed to go in to maintenance mode, also noticed aircraft airspeed at 50 knots indicating the aircraft is in the air mode. After speaking with costumer maintenance tech was advised this airspeed at 50 knots in normal for this aircraft. Re-racked both FGC reboot aircraft system now abele to go into maintenance test. Access maintenance test checking the FGC on ASCII data buss they checked good.. Checked the IRU. The 01 IRUis on the ASCB data buss. The 02 IRU is not received on ASCB data buss. After 2 hours IRU 02 faults cleared IRU checked good in maintenance test howed on ASCB date buss. I suspect buss coupler 55A16 and 55A24 for IRU 02 bad, place 2 on order. Discrepancy: 63 Rill AFT up-wash light loop. Resolution: Removed and replaced the aft right hand up-wash light and performed the operational check with no defects noted per the CIV Supplemental Manual 25-20-30. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 5 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603227 Bill To: Invoice Number: Billing Method I lours Rate Total Labor LSD: Time and Material ST 3.75 Ir 5136.00 S510.00 P.,ri. LSD: Time and Material S80.65 Total USD: 5590.65 Parts: Ref: No. Pan number: Description Quantity Sell price USD Extended USD 63#1 AL-1235-T-1320 LAMP I $80.65 $80.65 Step: 6.3.1 Step: 6.3.2 Step: 6.33 Completed Hangar( Primary Codes /Touch Labor Only Completed Inspection Labor Only Completed AVE / Electrical Labor Only Discrepancy: 6.4 During trouble shooting of the IRS SQWK.. Found the aircraft will not go into maintenance test and airspeed at 50 knots constantly Resolution: Suspected there was trash in the pilot static lines, Complied with CIV MM 34-01-00 pitot static system drain and purging. We did get some mud bobber out of the lines but airspeed still at 50 knots, contacted the current customer maintenance group and was told the 50 knots in normal for this aircraft. pulled the FCC CB and re-rack FCC #1 and #2 reset CB aircraft then accessed the maintenance test page. No further action required. Labor USD: No Charge Step: 6.4.1 Completed Hangar / Primary Codes / Touch Labor Only Step: 64.2 Completed Inspection Labor Only Step: 6.43 Completed Mil / Electrical Labor Only Step: 6.4.4 Completed PITOT/STATIC RECONCECF CHECK REQUIRED Step: 6.4.5 Open Operational test required for MCI and 2 removed for troubleshooting. Item: 7 INTERIOR Team Manager. Jett Stahl Customer Coordinator: James NN bite Pan/Model #: GIV AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 7.1 Per customer request comply with the following cleaning polish items 4 club scat leather cleaning. (Fwd four) 4 ea "E" window surround polish. Polish Left and Right inlet cowlings. Polish Left and Right TR's Resolution: Completed as Requested Services USD: Billing Method Hours Rate Total Flat Rate $1,500.00 Total USU: 51,500.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoicerpt 2011 Page 6 of 22 Printed: U19/2017 4:33:16PM Ref:312 EFTA00603228 Bill To: Invoice Number. Item: 8 MECHANICAL Team Manager. Jeff Stahl Customer Coordinator: James While Part/Model N: cay AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: DisercpancN: 8.1 Repair Left and Right Wheel Wells Corrosion. itcsolumm: installed final rivet on lower inboard of Left Hand trailing edge per B/P 1159N`40226 and 1159W40504 Rev C. All work performed ref Engineering Disposition: Acceptable alternate fastener with 130 degree head is GAF511AB3-xx. Use in areas inaccessible to install b/p Composilok type fasteners due to installation tool. u304769 MRB 028 Engineering Disposition: Acceptable to trim material from "L" clip for seal reatiner installation to maintain clearance with Sponson plate lug. Maintain minimum 2 X dia edge distance on rivets. Condition due to production variation. Touch up 213, 2012 per GAFI4A. u304769 MRB 028 Engineering Disposition: Use IIL18-08 IliLok pin with IIL70 collar per GANIPS2206 as alternate fastener in horizontal holes and NAS1919M05 rivets per GAMPS2232 in vertical holes at subject outbd locations for MLG seal retainer structure due to fastener and installation tool availability. Touch up 213, 2012 process code, holes and surfaces, per GAF14A. u304769 MRB 028 Billing Method Hours Rate Total Labor USD: Time and Material ST 131.17 6f., $136.00 $17,839.12 Labor USD: Time and Material OT 4.25 (e!.., $204.00 $867.00 Labor USD: Time and Material ST 4.00 (e!.., $222.00 $888.00 Parts USD: Time and Material $4,396.10 Total USD: $23,990.22 Parts: Rel. No. Part number: Description Quantity Sell price USD Extended USD 8.1 HI 1159W40226-1IB ANGLE I $614.44 $614.44 8.1 #2 I159W40226-12B ANGLE I S284.92 $284.92 8.1 #3 HLGPL9SP-V05B03 PIN 21 $8.00 $168.00 8.1 #4 SLFC-MV05 COLLAR 80 $5.48 $438.40 8.1 #5 GASI3AN-1-41 SEAL, BUTTONED STRIP, WHEEL 2 $113.42 $226.84 WELL DOOR (5' SECTION) 8.1 #8 GAFMIAB08-200 BLIND RIVET 60 $9.27 $556.20 8.1 #9 HLGPL9SCV05B03 PIN 70 $6.42 $449.40 8.1 #10 HLGPL9SP-V06804 LOCK BOLT 10 $10430 $1,043.00 8.1 #11 NASI399C5-3 RIVET 16 $433 $69.28 8.1 #14 GMS5005-II EPDXY PRIMER COATING, 3012 1 $7.64 $7.64 TYPE II- 1 OZ KIT 8.1 HIS GAF511AB08-300 RIVET-BLIND,SELF LOCKING 8 $22.90 $183.20 8.1#16 GAF511AB3-300 BLIND BOLT 10 $16.64 $166.40 8.1 H2O PR1440B1-2-654 SEALANT, 6 OUNCE #654 SEMK IT I $52.56 $52.56 1/2 HOUR WORK LIFE 8.1#21 GAISHAB08-200 BLIND RIVET 10 $9.27 $92.70 8.1 #22 GMS5005-II EPDXY PRIMER COATING, 3012 1 $7.64 $7.64 TYPE II- 1 OZ KIT 8.1 #23 GMS5005-II EPDXY PRIMER COATING, 3012 I $7.64 S7.64 TYPE II- 1 OZ KIT For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 7 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603229 Bill To: Invoice Number. Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.1824 NASI921M05-06 RIVET 4 56.96 $27.84 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 8 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603230 Bill To: Invoice Number: Step: 8.1.1 Completed Hangar/ Primary Codes /Touch Labor Only Step: 8.1.2 Completed Inspection Labor Only Step: 8.1.3 Completed Painted LIH and RfH breather angles per Ramps 4000 per customers request Step: 8.1.4 Completed Removed corroded 1.11 and RH gear door aft seal support angles 1159W40226-11 and 059W40226-12. Step: 8.1.5 Completed Disassembled LH and RH gear door support angles. Step: 8.1.6 Completed Match drilled new LI1 gear door aft seal support angle pin 1159W40226-I I per CAMPS 8316. Step: 8.1.7 Completed Match drilled new RH gear door aft seal support angle p/n 1159W40226-12 per CAMPS 8316. Step: 8.1.8 Completed Assembled LH gear door aft seal support angles p/n 1159W40226-1 land 1159W40226-15 per GAC Drawing 1159W40504 rev C. Step: 8.1.9 Completed Assembled RH gear door aft seal support angles pin 1159W40226-12 and 059W40226-I6 per CAC Drawing 1159W40504 rev C. Step: 8.1.10 Completed Request engineering disposition to fill extra hole on angle bracket pin 1159WII40201-29. Step: 8.1.11 Completed Request engineering disposition to use alternate fastner for clearance issues as required. Blueprint fastner pin GAB512GC. Request to use either Jo-bolt pin GAF311AB or Hi-tigue pin GABMOGT. Step: 8.1.11.1 onipleted Engineering Disposition: Acceptable alternate fastener with 130 degree head is GAFMIAB3-xx. Use in areas inaccessible to install b/p Composilok type fasteners due to installation tool. u304769 MRB 028 Step: 8.1.12 Completed Engineering Disposition for step 8.1.10: Double flush plug extraneous 430 hole in 059WM40201-29 clip only with "AD" rivet material. Backdrill from adjacent hole and install hip fastener. Touch up process code 213. 2012 per GAF14A. u304769 MRB 028 Step: 8.1.13 onipleted Recieved ok to install and installed all but four fastners throught RJH brakets P/N 1159W40226-12 and 1159W40226-16 per drawing 1159WH40201 Rev. B. (Four fastners not installed Marked with streamer and tape). Step: 8.1.14 Completed REQUEST ENGINEERING REVIEW USE OFALTERNATE FASTENERS ON LIB AND RAI FWD LOWER TfE BOX BRACKETS GOING THROUGH THE 1159W40226-11 AND -12 AND THE -13 CLIP (0/8 2 HORZ HOLES). ALTERNATE FASTENERS ARE ALSO NEEDED FOR THE FASTENERS GOING THROUGH THE -II AND -12 AND THE -17AND -III CLIPS (0/8 2 VERT HOLES). REQUESTING USE OF HILOCS FOR THE HORZ HOLES AND BLIND RIVETS FOR THE VERTICAL HOLES DUE TO INTERFERENCE ISSUES. Step: 8.1.14.1 Completed Engineering Disposition: Use 11118-08 HiLok pin with HI..70 collar per GANIPS2206 as alternate fastener in horizontal holes and NASI919M05 rivets per GAMPS2232 In vertical holes at subject undid locations for MLG seal retainer structure due to fastener and installation tool availability. Touch up 213,2012 process code, holes and surfaces. per GAF14A. u304769 MRB 028 Step: 8.1.15 Completed REQUEST ENGINEERING REVIEW TRIMMING THE LM 1159W40226-13 "I." CLIP FOR CLEARANCE FROM SPONSON RIB AFT LU(. Step: 8.1.15.1 Completed Engineering Disposition: Acceptable to trim material from "I." clip for seal reatiner installation to maintain clearance with Sponson plate lug. Maintain minimum 2 X dia edge distance on rivets. Condition due to production variation. Touch up 213. 2012 per GAFI4A. u304769 MRB 028 Step: 8.1.16 Completed R/H Wing Lower Trailing Edge Box. Installed QTY 2 H118-08 HiLoks with HL 70 Collars in the bin (yrm) most horizontal holes. Installed QTY 2 NAS1919h105 Blind Rivets in the () r vertical holes (FWD of the Composite Panel). All work Completed per Eng. Disposition in step 8.1.14. Step: 8.1.17 Completed Install Rill and till Aft Gear well Seal. Step: 8.1.18 Completed Complied with Engineering Disposition for step 8.1.10: Double flush plug extraneous 830 hole in I159WM40201-29 clip only with "AD" rivet material. Backdrill from adjacent hole and install b/p fastener. Touch up process code 213.2012 per GAFI4A. u304769 MRB 028 Step: 8.1.19 Completed Complied with Engineering Disposition for step 8.1.10: Double flush plug extraneous #30 hole in I159WM40201-29 clip only with "AD" rivet material. Backdrill from adjacent hole and install b/p fastener. Touch up process code 213.2012 per GAF14A. u304769 MRB 028 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminarylnvoice.rpt 2011 Page 9 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603231 Invoice Number: Bill To: Step: 8.1.20 Completed Step: 8.1.21 Completed Installed 1.11 gear door aft seal support angles p/n 1159W40226-11and 1159W40226-15 per GAC Drawing 1159W40504 rev C. Except one rivet inboard lower TE Box. All work performed ref Engineering Disposition: Acceptable alternate fastener with 130 degree head is GAF511AB3-xx. Use in areas inaccessible to install b/p Composite:4c type fasteners due to installation tool. u304769 MRS 028 Engineering Disposition: Acceptable to trim material from "I." clip for seal reatiner installation to maintain clearance with Sponson plate lug. Maintain minimum 2 X dia edge distance on rivets. Condition due to production variation. Touch up 213. 2012 per GAF14A. u304769 MRB 028 Engineering Disposition: Use 111.18-08 HiLok pin with 111.70 collar per GAMPS2206 as alternate fastener in horizontal holes and NASI919N105 rivets per GANIPS2232 in vertical holes at subject outbd locations for MLG seal retainer structure due to fastener and installation tool availability. Touch up 213,2012 process code, holes and surfaces. per GAF14A. u304769 MRB 028 Installed final rivet on lower inboard of Left Hand trailing edge per B/P I159W40226 and 1159W40504 Rev C. All work performed ref Engineering Disposition: Acceptable alternate fastener with 130 degree head is CAE5IIAB3-xx. Use in areas inaccessible to install b/p Composilok type fasteners due to installation tooL u304769 MRB 028 Discrepancy: 8.2 Comply with full bleed air system integrity check per acft AMM. Resolution: Complied with full bleed air system integrity check per G1V AMM 21-00-00. 36-00-00 and 36-13-00. No defects noted. Billing Method Hours Rate Total Labor USD: Time and Material ST 70.20 (t, $136.00 $9,547.20 Labor USD: Time and Material OT 4.21 €1; $204.00 $858.84 Parts USD: Time and Material $81.07 Total USD: $10,487.11 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.242 S2L226 0 -RING SEAL FLUOROCARBON 4 $4.17 $16.68 (VITON) LOW COMPRESSION. 2.00 IN. 8.243 S2L226 0-RING SEAL. FLUOROCARBON 4 51.17 $16.68 (VITON) LOW COMPRESSION. 2.00 IN. 8.287 GAC835MG2OP CONTACT 10 $0.78 $7.80 8.288 GAC115P1 LUBRICANT/SEALANT-SILICONE 1 539.91 $39.91 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). 0AC_WorkOrderPreliminaryInvoice.rpt 2011 Page 10 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603232 Bill To: Invoice Number. Step: 8.2.1 Completed Hangar/ Primary Codes /Touch Labor Only Step: 8.2.2 Completed Inspection Labor Only Step: 8.23 Completed Performed Air Conditioning operational test per GIV MM 21-00-00. Step: 8.2.4 Completed Performed Bleed Air Configuration Annunciation operational test per GIV MM 21-00-00. Step: 8.2.5 Completed Performed Bleed Air System- Operational test Per GIV MM 36-00-00. Step: 8.2.6 Completed Removed the APU Air Check valve and performed an APU Air Chick Valve - Inspection. Ref. 11.6 for inspections Step: 8.2.7 Completed Installed the APU Air check valve per GIV MM 36-13-00. Ref. item 11.7 for Installation. Step: 8.2.8 Completed Complied with Tempurature Control Valve ( Cockpit ) - Removal/Installation per CMP GIV 216082. Swapped Cockpit and cabin temperature control valves for troubleshooting purposes. Reference item 11.3 for ChIP task card Removed PN: 397122-2-1 Removed SN P-502 Installed PN: 397122-2-I Installed SN: 1335 Step: 8.2.9 Completed Complied with Tempurature Control Valve ( Cabin ) - Removal/Installation per CMP GIV 216080. Swapped Cockpit and cabin tempurature control valves for troubleshooting purposes. Reference item 11.4 for CMP task card Removed PN: 397122-2-I Removed SN: 1335 Installed PN: 397122-2-I Installed SN: P-502 Step: 8.2.10 Completed Complied with Servo Air Pressure Regulator Valve ( Cockpit ) - Removal/Installation per CMP GIV 212055. Swapped Cockpit and Cabin Servo Air Pressure Regulators for troubleshooting purposes. Reference item 11.1 for CN1P task card Removed PN: 3214068-2-1 Removed SN: 1076 Installed PN: 3214068-2-1 Installed SN: 1074 Step: 8.2.11 Completed Complied with Sono Air Pressure regulator Valve ( Cabin ) - Removal/Installation per CMP GIV 212056. Swapped Cockpit and Cabin Servo Air Pressure Regulators for troubleshooting purposes. Reference item 11.2 for CN1P task card Removed PN: 3214068-2-I Removed SN: 1074 Installed PN: 3214068-2-1 Installed SN: 1076 Step: 8.2.12 Completed Leak checked the precooler inlets and fan air valves on the pylons. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page II of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603233 Bill To: Invoice Number: Step: 8.2.13 Completed Complied with ACM Bypass Shutoff Valve ( Left ) - Removal/Installation per ChIP GIV 212085. Swapped valves for troublshooting purposes. Reference item 11.11 for CMP task card Removed PN: 3289922-2-1 Removed SN: 326 Installed PN: 3289922-2-1 Installed SN: 335 Step: 8.2.14 Completed Complied with ACM Bypass Shutoff Valve ( Righ )- RemovaUlnstallation per ChIP GIV 212086. Swapped valves for troublshooting purposes. Reference item 11.12 for CMP task card Removed PN: 3289922-2-1 Removed SN: 335 Installed PN: 3289922-2-I Installed SN: 326 Step: 8.2.15 Completed Complied with resistance cks to cabin anticipator and both temp sensors per GIV.ANINI 21-01-05 and 21-01-06. all readings ek good. Complied with comparison readings of cockpit and cabin overhead rheostats during with the cabin was found to be INOp in all auto settings. Replacement overhead control panel on order. meter # 567201. Due 05/17 Step: 8.2.16 Completed During troubleshooting. cabin and cockpit anticipator were swapped per GIV ANINI 21-01-06. need to be re-installed in origional locations. Step: 8.2.17 Completed While running A/C system found this A/C has a switch dividing cabin and cockpit temp control panels. Complied with A/C system ops ck per GIV MM 21-00-00. All systems check good with no abnormal sounds or vibrations at fwd seats. Discrepancy: 8.3 Left hand wing lower TE box has three oversized holes where angle was removed in item 8-1. Each hole marked with tape. Resolution: FILLED DICREPANT HOLES WITH 50/50 MIXTURE OF RESIN AND CHOPPED CARBON FIBER PER ENGINEEERING DISPOSITION IN STEP BELOW.Redrilled and recountersunk holes after resin cure. Installed B/P fastners. All work done per engineering disposition in step 8.4.1.1 and drawing 1159W1I40201. Billing Method Hours Rate Total Labor USD: Time and Material ST 8.00 (iThir, $136.00 $1,088.00 Total USD: 41,088.00 Step: 8.3.1 Completed Request Engineering disposition for repair countersink hole lower left hand TE box Step: 8.3.1.1 Completed Engineering Disposition: Fill c'sk hole with 50/50 mixture of EA956 B/A and chopped carbon fiber cloth. Allow full cure and re-drill for b/p fastener. u304769 MRB 028 Step: 8.3.2 Completed Service Engr Labor Only Step: 8.3.3 Completed SC Maintenance/Hangar/ Primary Codes / Touch Labor Only Step: 8.3.4 Completed Inspection Labor Only Discrepancy: 8.4 Right hand wing lower TE box has three oversized holes where angle was removed in item 8-1. Each hole marked with tape Resolution: FILLED DICREPANT HOLES WITH 50/50 MIXTURE OF RESIN AND CHOPPED CARBON FIBER PER ENGINEEERING DISPOSITION IN STEP BELOW.Redrilled and recountenunk holes after resin cure. Installed B/P fastners. All work done per engineering disposition in step 8.4.1.1 and drawing 1159W1I40201. For detail description of the work complied with sec the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPrcliminaryInvoice.rpt 2011 Page 12 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603234 Bill To: Invoice Number: Billing Method Hours Rate Total Labor USD: Time and Material ST 4.95 @, S136.00 $673.20 Labor USD: Time and Material OT 1.27 @, S204.00 $259.08 Total USD: $932.28 Step: 8.4.1 Step: 8.4.1.1 Step: 8.4.2 Step: 8.4.3 Step: 8.4.4 Step: 8.4.5 Completed Request Engineering disposition for repair countersink hole lower right hand TE box Completed Engineering Disposition: Fill c'sk hole with 50/50 mixture of EA956 B/A and chopped carbon fiber cloth. Allow full cure and re-drill for b/p fastener. u304769 MRB 028 Completed Service Engr Labor Only Completed SC 3Iaintenance/Hangar / Primary Codes / Touch Labor Only Completed Inspection labor Only Completed Redrillcd and recountersunk holes after resin cure. Installed B/P fastners. All work done per engineering disposition in step 8.4.1.1 and drawing I159W1140201. Discrepancy: 8.5 Left hand and right hand turbine bypass shut off valve requires safety wire on cannom plug. NO LABOR Resolution: Safetled left and right hand turbine bypass shut off s als e carillon plugs as per GIV AMM 20-70-41. Discrepancy: 8.6 CUSTOMER REQUESTS TO REMOVE IAI AND RAI WATER SEPERATORS AND INSPECT FOR POSSIBLE PRESSURIZATION ISSUES WITH BLEEDS ON. Resolution: Removed tilI and Rill water separator as per CIV CMP 217070 and 217071, Ref. 11.24 and 11.25. Performed water separator bag inspection as per GIVAMM 21-01-12 PG. 301. SEE 8.7 AND 8.8 FOR SQUAWKS SEE 11.24 AND 11.25 FOR REMOVALAND REPLACEMENT OF MI AND RAI WATER SEPERATORS. Billing Method Hours Rate Total Labor USD: Time and Material ST 4.00 @ $136.00 $544.00 Parts USD: Time and Material $691.78 Total USD: S1,235.78 Pans: Rd. No. Pan number: Description Quantity Sell price USD Extended USD 8.6 #1 83237-20 SOCK, WATER SEPARATOR, 2 532729 $655.78 CONDENSER BAG 8.6 #3 S2L-232 O-RING SEAL, FLUOROCARBON 4 59.00 $36.00 (VITON) LOW COMPRESSION, 2.75 IN. Step: 8.6.1 Completed Removed LIR and 12. 11 ss aster sepa as per GIV CMP 217070 and 217071, Ref. 11.24 and 11.25. Performed %sorer separator bag Inspection as per GIV AM NI 21-01-12 PC. 301. For detail description of the work complied with sec the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 13 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603235 Bill To: Discrepancy: ti Left hand water separator condensor assembly has pitting corrosion of vanes. Invoice Number. REF 11.24 FOR R&R Resolution: Repair recertify and return to stock Part 91 Billing Method Hours Rate Total Parts USD: Time and Material $10,630.82 Total USD: $10,630.82 Pans: Ref. No. Pan number Description Quantity Sell price USD Extended USD 8.7 #1 2340186-2-3 SEPARATOR, WATER I $10,600.00 $10,600.00 8.7 #2 521.345 0 -RING SEAL, FLUOROCARBON 2 $15.41 $30.82 (VITON) LOW COMPRESSION. 4.00 IN. Discrepancy: 8.8 Right hand water separator condensor assembly has pitting corrosion of vanes. REF 11.25 FOR R&R Resolution: Repair, recertify, and return to stock Part 91 Billing Method Hours Rate 'fetal Parts USD: Time and Material $10,600.00 Total USD: $10,600.00 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.8 NI 2340186-2-3 SEPARATOR, WATER 1 S10.600.00 $10,600.00 Discrepancy: 8.9 Resolution: Durin- preflight LH art p) loo light failed to operate. Item: 9 PAINT Team Manager. Jeff Stahl Customer Coordinator. James White Pan/Model #: GIV AC Serial No./Tail No.: TSNUTSO: CSN/CSO: Aircraft Time: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 14 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603236 Bill To: Invoice Number. Discrepancy: 9.1 Blow in Lill and R/II AI•T wheel wells where repairs was made Resolution: Complied with perpping and repainting area behind the I./II and R/II AFT wheel wells where repairs was made. PER CAMPS 4000 Billing Method I lours Rate Total Labor USD: Time and Material ST 11.17 (a; $136.00 $1,519.12 Total USD: 41,519.12 Step: 9.1.1 Step: 9.1/ Completed SC Paint Labor Only Completed Complied with prepped.applied and sanded overcoat to contour then masked off 1./H and RIB AFT lower wings just AFT of wheel wells per stamps 4000 Item: 10 OUTSTANDING PARTS, MATERIALS AND I OR SERVICES AT DEPARTURE Team Manager Jeff Stahl Customer Coordinator: James White PartiModel 0: GIV AC Serial No./Tail No.: TSNUTSO: CSN/CSO: Aircraft Time: Discrepancy: 10.1 Resolution: Engineering Labor Discrepancy: 10.2 Resolution: Backorder Parts Services USD: Services: No Charge N/C Ref. No. Description Quantity Sell Price USD Extended USD 10.2 PI 10.2 #2 CLEANING A/C EXTERIOR CLEANING A/C INTERIOR 1.00 1.00 $0.00 $0.00 $0.00 $0.00 Discrepancy: 103 Parts to be Returned Resolution: Parts USD: No Charge N/C Services USD: No Charge N/C Parts: Ref. No. Part number. Description Quantity 10.3 04 S2L345 O-RING SEAL, FLUOROCARBON 4 (VITON) LOW COMPRESSION. 4.00 IN. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 15 of 22 Printed: 1/192017 4:33:16PM Ref:312 EFTA00603237 Bill To: Invoice Number. Services: Ref: No. Description Quantity 10.3 MI VENDOR SERVICES 1.00 Item: 11 FOLLOW ON CMP/ MAINTENANCE TASKS Team Manager. Jeff Stahl Customer Coordinator. James White Pan/Model 4: ay AC Serial No./Tail No.: TSNUTSO: CSN/CSO: Aircraft Time: Discrepancy: 11.1 CMP GIV 212055 VA, Cockpit Servo Air Press Reg Ref 8.2 Resolution: COMPLIED WITH CMP GIV 212055 VA, Cockpit Servo Alr Press Reg Discrepancy: 11.2 CMP GIV 212056 VA, Cabin Servo Air Press Reg Ref 8.2 Resolution: COMPLIED WITH CMP GIV 212056 VA, Cabin Servo Air Press Reg Discrepancy: 11.3 CMP GIV 216082 Valve, Cockpit Tempature Control Ref 8.2 Resolution: COMPLIED WITH CMP GIV 216082 Valve, Cockpit Tempature Control Discrepancy: 11.4 CMP G1V 216080 Valve. Cabin Tempature Control Ref 8.2 Resolution: COMPLIED WITH CMP GIV 216080 Vale. Cabin Tempature Control For detail description of the work complied with sec the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 16 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603238 Bill To: Invoice Number. Discrepancy: 11.5 CMP CIV 215005 Air Conditioning System—OPS Test Ref 8.2, 11.1, 11.2, 11.3, & 11.4 Resolution: COMPLIED WITH CMP GIV 215005 Air Conditioning System—OPS Test Discrepancy: 11.6 CMP CIV 361053 APU Air Check Valve - Removal I Installation Ref 8.2 Resolution: COMPLIED WITH CMP GIV 361053 APU Alr Check Valve - Removal / Installation Discrepancy: 11.7 CMP CIV 361056 APU Air Check Valve - Inspection Ref 8.2 Resolution: COMPLIED WITH CMP GIV 361056 APU Air Check Valve - Inspection Discrepancy: 11.8 CMP GIV 342032 Copilot Standby DDRMI DBDI - Removal / Installation REF Item 6.1 Resolution: COMPLIED WITH CMP CIV 342032 Copilot Standby DDRMI DBDI - Removal / Installation part number off:520-3030-003 serial number off:11534 part number on:520-3030-003 serial number on:1210 Discrepancy: 11.9 CMP GIV 342038 Compass Swing No. 2 REF item 6.1 Resolution: Entered in error. Canned squawk was for 342037 #1 Compass Swing. #2 Compass swing was required by 6.1. For detail description of the work complied with sec the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 17 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603239 Bill To: Invoice Number. Discrepancy: 11.10 CMP CIV 342034 Standby DDRMI / DBDI Indicator - Operational Check REF item 6.1 Resolution: COMPLIED WITH CMP GIV 342034 Standby DDRMI I DBDI Indicator - Operational Check Tic Box - CN: 567976 Cal Due: 11117 Discrepancy: 11.11 CMP GIV 212085 Air Cycle Machine Bypass Shutoff Valve (Left) - Removal / Installation Ref. 8.2 Resolution: COMPLIED WITH CMP GIV 212085 Air Cycle Machine Bypass Shutoff Valve (Left) - Removal/ Installation Discrepancy: 11.12 CMP CIV 212086 Mr Cycle Machine Bypass Shutoff Valve (Right) - Removal / Installation Ref. 8.2 Resolution: COMPLIED WITH CMP GIV 212086 Aft Cycle Machine Bypass Shutoff Valve (Right) - Removal Installation Ref. 8.2 Discrepancy: 11.13 Chili GIV 342038 Compass Swing No. 2 Resolution: COMPLIED WITH CMP GIV 342038 Compass Swing No. 2 Discrepancy: 11.14 CMP CIV 314116 ASCB DATA COUPLER (55A16) Ref item 6.2 For detail description of the work complied with sec the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 18 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603240 Bill To: Invoice Number. Resolution: COMPLIED WITH CMP GIV 314116 ASCB DATA COUPLER (55A16) part number off: I159SCAV400-1 serial number off:5105 part number on:1159SCAV400-1 serial number on:031767 Parts USD: No Charge N/ C Discrepancy: 11.15 CMP GIV 314124 ASCB DATA COUPLER (55A24) Ref Item 6.2 Resolution: COMPLIED WITH CMP GIV 314124 ASCB DATA COUPLER (55A24) part number off:1159SCAV400-1 serial number off4357 part number on:1159SCAV400-1 serial number on:031766 Parts USD: No Charge N/ C Discrepancy: 11.16 cm> GIV 342034 Standby DDRMI / DBDI Indicator -Operational Check Resolution: DUPLICATE SQUAWK SEE ITEM 11.10 FOR SQUAWK RESOLUTION Discrepancy: 11.17 CMP GIV 344067 BATTERY PACK, #3 IRU Resolution: Item written in error Discrepancy: 11.18 CMP CIV 344006 Inertial Reference Unit No. 2 - Removal / Installation Resolution: COMPLIED WITH CHIP GIV 344006 Inertial Reference Unit No. 2 - Removal / Installation. Reference item 6.2 part number off:11G1075AEO3 serial number off:208/AE02 part number on::HG1075AEO3 serial number on:2081AE02 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 19 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603241 Bill To: Invoice Number: Discrepancy: 11.19 CMP CIV 344086 Attitude and Heading Reference System / Inertial Reference Unit - Operational Check. Reference item Resolution: COMPLIED WITII CMP CIV 344086 Attitude and Heading Reference System /Inertial Reference Unit - Operational Check Discrepancy: 11.20 CMP CIV 216050 Selector, Cabin Tempature Cont Removal/Installation Cabin Overhead Temp Rehostat INOP Ref. 8.2 Resolution: COMPLIED WITH CMPGIV 216050 Selector, Cabin Tempature Cent Removal! Installation P/N OFF: 622150-1-1 S/N OFF: 068C-0229 PIN ON: 622150-1-1 S/N ON: 026C-0035 Ref. 8.2 Discrepancy: 11.21 CMP CIV 216050 Selector, Cabin Tem pat wee ( tint RC [Ill II/ Original Pan installed Ref. 8.2 Resolution: COMPLIED WITH CMP GIV 216050 Selector, Cabin Tempature Cent P/N OFF: 622150-1-1 S/N OFF: 026C-0335 PIN ON: 622150-1-1 S/N ON: 068C-0229 Discrepancy: 11.22 CMP CIV 341076 Pitot / Static System (Pilot) - Reconnect Check For detail description of the work complied with sec the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 20 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603242 Bill To: Invoice Number. Resolution: COMPLIED WITH CMP GIV 341076 Pitot / Static System (Pilot) - Reconnect Check DPS 5000- 560115 2/17 IFR 6000 566411 12/17 Discrepancy: 11.23 CMP CIV 341093 Picot / Static System (Copilot) - Reconnect Check Resolution: COMPLIED WITH CMP GIV 341093 Pilot / Static System (Copilot) - Reconnect Check DPS 5000- 56015 CAL DATE 2/17 IFR 6000- 566411 CAL DATE 12/17 Discrepancy: 11.24 CMP CIV 217070 Water Separator, I. Ref. 8.6 Resolution: COMPLIED WITH CMP GIV 217070 Water Separator. L P/N off 2340186-2-3 S/N off 87-283 P/N on 2340186-2-3 S/N on 1101 Discrepancy: 11.25 CMP GIV 217071 Water Separator, R Ref. 8.6 Resolution: COMPLIED WITH CMP GIV 217071 Water Separator. R P/N off 2340186-2-3 S/N off 87-289 P/N on 2340186-2-3 S/N on 47-845 Discrepancy: 11.26 Comply with clearance check of newly installed IA and Rt T/E box angles. Ref. item 8.I. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 21 of 22 Printed: 1/19/2017 4:33:16PM Rd:312 EFTA00603243 Bill To: Invoice Number. Resolution: Complied with clearance check of newly Installed Lt and Rt box angles per CIV AMM 32-00-00, no defects noted. Communications concerning disputed debts, including a check or other instrument tendered as MI satisfaction of a debt, must be forwarded to: Gulfstream Aerospace Ann: Credit Manager M/S 13-05 PO BOX 2206, Savannah, GA 31402 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document arc in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 22 of 22 Printed: 1/19/2017 4:33:16PM Ref:312 EFTA00603244