EFTA00603223.pdf

Gul£stream A OMMRAI. DYNAMIC* COMPANY PRELIMINARY INVOICE ParVModel #: CIV AC Serial No)Tail No.: 550 Connole Street - Brunswick. Georgia 31525 Mail Remittance To: Overnight Remittance To: Wire Remittance To: Gulfstream Aerospace Corporation Gulfstream Aerospace Corporation (Box # 730349) Ciulfstrcam Aerospace Corporation P.O. Box 730349 do JP Morgan Chase Bank, NA JP Morgan Chase Bank, NA Dallas, Texas 75373-0349 ATTN: Dallas National Wholesale Lockbox TXI-0029 Chicago, IL 60670 14800 Frye Road Ft. WOrdl, TX 76155 Fedwire Routing No. (ABA) 021 000 021 S.W.I.F.T. CHASUS33 ACH Credit Routing No. (ABA)071 000 013 Invoice Number. Bill To: JEGE LLC Invoice Date: 1/19/2017 C/O GALAXY AVIATION INC Customer IDI ATTN: LARRY VISOSKI P.O. Number. 3800 SOUTHERN BLVD, SUITE 204 Repair Station: FAA CRS GR4D216111 WEST PALM BEACH, Florida 33406 In Date: 01/13/2017 United States Out Date: 01/21/2017 Payment Type: Net 30-Open terms Payment Terms: Title: JEGE LLC 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 Part/Model tr: CIV Customer Coordinator: James White AC Serial No./Tail No.: TSNJTSO: CSN/CSO: Aircraft Time: Discrepancy: 1.1 kciurn tm acre ice Resolution: Step: 1.1.1 Open Inspection Labor Only 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 Accomplish Preflight Inspection Resolution: Step: 1.3.1 Open Insure key has been returned to acft or customer if removed Step: 1.3.2 Open SC Maintenance/Hangar/ Primary Codes / Touch Labor Onb Discrepancy: 1.4 Tool Clearance Resolution: 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 IInure 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 Part/Model 14: GIV Customer Coordinator: James White 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 Completed Inspection Labor Only Step: 6.1.2 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 Completed Hangar( Primary Codes /Touch Labor Only Step: 6.3.2 Completed Inspection Labor Only Step: 6.33 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 Pan/Model #: GIV Customer Coordinator: James NN bite 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 Billing Method Hours Rate Total Services USD: 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 Part/Model N: cay Customer Coordinator: James While 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-II 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 1159W40226-1land 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  Bill To: Invoice Number: Step: 8.1.20 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 Step: 8.1.21 Completed 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: