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Gu]£stream' PRELIMINARY INVOICE A OSSISRAL DYNAMICS COMPANY 7 Char Drive - Westfield, Massachusetts 01085-1493 ParUModel GIV AC Serial No./Tail No.: 1085 / NI20JE 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. Worth, TX 76155 Wire Remittance To: Gulfstream Aerospace Corporation JP Morgan Chase Bank, NA Chicago, IL 60670 Account No. Fedwire Routing No. (ABA) S.W.I.F.T. CHASUS33 ACH Credit Routing No. (ABA) Bill To: JEGE LLC C/O GALAXY AVIATION INC MTN: LARRY VISOSKI 3800 SOUTHERN BLVD, SUITE 204 WEST PALM BEACH, Florida 33406 United States Title: JEGE LLC Invoice Number: Invoice Date: Customer ID: P.O. Number: Repair Station: In Date: Out Date: Payment Type: Payment Terms: 6918002027 6/28/2018 BJ419 CRS LEGR039G 05/16/2018 06/29/2018 Net 30-Open terms INVOICE SUMMARY FOR WORK ORDER NUMBER: Time & Materials SC18654 Flat Rate Total Labor USD: $78,671.72 $90,820.00 $169,491.72 Parts USD: $92,740.57 $9,672.00 $102,412.57 Services USD: $11,461.17 $0.00 $11,461.17 Misc Charges USD: $5.231.00 $5.231.00 Detail Subtotal USD: 5188,104.46 5100.492.00 5288,596.46 Freight USD: $1,536.19 Subtotal USD: $290,132.65 Funds on Deposit USD: $56,139.50 Total USD: SCHEDULED MAINTENANCE FAR PART 91 LARRY VISOSKI 917-868.6145 Peter Rawson 973.879-2060 N120.1E RE: PROPOSAL# 7042687 R00 (GAC0218-2687.GIV.1085.R00) MSP (APU) HAPP RR CORP CARE $233,993.15 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 1 of 117 Printed: 6/28/2018 9:39:11M Reel EFTA00808939 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Item: 1 AIRFRAME Gulfstream GIV Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes Part/Model #: GIV AC Serial No./Tail No.: 1085 / NI2OJE TSN/TS0: CSN/CS0: Aircraft Time: Discrepancy: 1.1 RETURN TO SERVICE FOR GENERAL MAINTENANCE OR INSPECTION. Resolution: ACTT: 9746.1 ACTL: 4430 DATE: WORK ORDER NUMBER: SC18654 ITEM(S): THE MAINTENANCE LISTED ABOVE WAS PERFORMED IN ACCORDANCE WITH CURRENT FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RETURN TO SERVICE WITH REGARDS TO THE MAINTENANCE ACCOMPLISHED. FURTHER DETAILS ARE ON FILE AT THIS REPAIR STATION UNDER THE ABOVE WORK ORDER. A COPY OF THIS WORK ORDER HAS BEEN PROVIDED TO THE OPERATOR SIGNATURE: DATE: Discrepancy: 1.2 COMPLY WITH DEBRIEF USING INDUCTION / ARRIVAL DEBRIEF CHECKLIST - CMP 010010. CMP GIV 010010 SERVICE CENTER MAINTENANCE INDUCTION CHECKLIST Resolution: Complied with CMP GIV 010010 Service Center Maintenance Induction Checklist Step: 1.2.1 Completed ACCOMPLISHED 90 DAY DUELIST REVIEW. Step: 1.2.2 Completed ACCOMPLISHED REMOVALAND SECURING OF CUSTOMER VALUABLES AS REQUIRED. Step: 1.2.3 Completed LISTED OPERATOR'S AIRWORTHINESS REQUIREMENTS. Discrepancy: 1.3 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 DOCUMENT IN THE WORK ORDER. Resolution: ADVISED 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 IN THE WORK ORDER. 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 2 of 117 Printed: 6/28/2018 939:11A? Reel EFTA00808940 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 1.4 CONSUMABLES AND SHOP SUPPLIES. Resolution: Billing Method I louts Rate Total Misc Charges USD: Time and Material $5,000.00 Total USD: $5,000.00 Miscellaneous Charge: Ref. No. Miscellaneous Charge 1.4 #1 CONSUMABLES & SHOP SUPPLIES Step: 1.4.1 Open CONSUMABLES Amount USD $5,000.00 Discrepancy: 1.5 ACCOMPLISH INBOUND INSPECTION AND VIDEO. Resolution: ACCOMPLISHED INBOUND INSPECTION AND VIDEO. Step: 1.5.1 Completed ACCOMPLISH INBOUND PRELIMINARY INSPECTION USING FORM M-4. Step: 1.5.2 Waiting ACCONIPLISII ED INCOMING VIDEO OFAIRCRAFT AS APPLICABLE. Insp Discrepancy: 1.6 ASSIST CUSTOMER WITH ARRIVALAND DEPARTURE AS REQUIRED. Resolution: ASSISTED CUSTOMER WITH ARRIVAL AND DEPARTURE. Discrepancy: 1.7 SERVICE TOILET/WASTE TANK. Resolution: Discrepancy: 1.8 ACCOMPLISH COVER AND PROTECT OF THE AIRCRAFT INTERIOR AND EXTERIOR, AS REQUIRED. Resolution: ACCOMPLISHED COVER AND PROTECT OF THE AIRCRAFT INTERIOR AND EXTERIOR, 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_WorkOrderPrelitninaryInvoice.rpt 2011 Page 3 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00808941 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 1.9 ACCOMPLISH HYDRAULIC FLUID CONTAMINATION CHECK. Resolution: ACCOMPLISHED HYDRAULIC FLUID CONTAMINATION CHECK. Discrepancy: 1.10 ACCOMPLISH AIRCRAFT CLEANING Resolution: Discrepancy: 1.11 REVIEW LOGBOOK EN I RN. PRIOR FO D EPA RIIRE Resolution: Discrepancy: 1.12 ACCOMPLISH OUTBOUND INSPECTION AND VIDEO. Resolution: Step: 1.12.1 Open ACCOMPLISH OUTBOUND INSPECTION MAINTENANCE CHECKLIST 5.1 7. Step: 1.12.2 Open ACCOMPLISH OUTBOUND VIDEO OF AIRCRAFT AS APPLICABLE. Discrepancy: 1.13 TOOL CLEARANCE Resolution: Discrepancy: 1.14 ACCOMPLISH PREFLIGHT INSPECTION AS REQUIRED. Resolution: N/ PREFLIGHT INSPECTION NOT 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 4 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00808942 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 1.15 ACCOMPLISH BILLING OF CUSTOMER APPROVED OVERTIME AS REQUIRED. Resolution: ACCOMPLISHED BILLING OF CUSTOMER APPROVED OVERTIME AS REQUIRED. Discrepancy: 1.16 STM PROJECT MANAGEMENT Resolution: Step: 1.16.1 in Progress SVC Step: 1.16.2 Open AVI Step: 1.16.3 Open AVS Step: 1.16.4 Open RFB Item: 6 AVIONICS Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes Part/Model #: AC Serial NolTail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 6.1 THE BATTERY VOLTAGE INDICATIONS ON THE EPMP ARE ERRATIC AND CHANGE WITH DIMMER ROTATION. Resolution: Billing Method flours Rate Total Labor USD: Time and Material ST 13.55 @ $142.00 $1,924.10 Parts USD: Time and Material $29,700.00 Services USD: Time and Material SI0,718.00 Total USE): $42,342.10 Paris: Ref. No. Part number: Description Quantity Sell price USD Extended USD 6.1 #1 1159SCAV373-1007 PANEL,ELEC POWER 1 $29,700.00 $29,700.00 NIGNIT-1B118-2/1,3118-2-D Services: Ref. No. Description Quantity Sell Price USD Extended USD 6.1 #2 GAC REPAIRS 1.00 $10,718.00 $10,718.00 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). GAC_WorkOrderPreliminaryInvoicelpt 2011 Page 5 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00808943 Bill To: JEGE LLC Step: 6.1.1 WO It SC18654 Invoice Number: 6918002027 Completed REMOVED EPMP P/N 1159SCAV337-1007,S/N N1069. INSTALLED A REPAIRED EPNIP WITH P/N 1159SCAV337-1007, S/N 063C-2295. REFERENCE FORM 8130 WITH TRACKING # GAL-L18-ELE-014 DATED 15-FEB-2018 FROM GULFSTREAM AUTHORIZATION# CRS2GDR2I6B . ALL WORK DONE IN ACCORDANCE WITH CMP CODE 245060. Discrepancy: 6.2 WHILE C/W ANTENNA COAX CENTER CONDUCTOR INSPECTION FOUND ATG4000 -.16 (RED) COAX CENTER CONDUCTOR SHORTED TO SHIELD. Resolution: DISCONNECTED ALL CONNECTORS FROM ATG4000 AND CHECKED CENTER CONDUCTOR TO SHIELD, FOUND OPEN, CHECKED GOOD AT THIS TIME. WORK WAS DONE WITH REFERENCE TO GOGO BUSINESS AVIATION ATG 4000, GOGO BIZ, INSTALLATION MANUAL, INSTALLATION MANUAL PART NUMBER D13485. RECONNECTED ALL CONNECTORS TO ATG4000. Labor USD: Total USD: Billing Method Hours Rate Total Time and Material ST 1.00 ® $142.00 $142.00 $142.00 Discrepancy: 63 THE TCAS SYSTEM HAS FAILED. COMPUTER WILL NOT RESPOND TO SELF TEST INPUTS. Resolution: GAINED ACCESS TO THE TOP TCAS ANTENNA. PERFORMED RESISTANCE CHECK OF THE ANTENNA COAXIAL CONNECTIONS, (ANTENNA SIDE). FOUND THAT J4 (RED) RESISTANCE READING WAS CONSIDERABLY LOWER THAN MINIMUM ALLOWABLE RESISTANCE, (READING WAS 58 OHMS, PROPER READING SHOULD BE 2000 (+/- 200 OHMS), AS PER HONEYWELL SYSTEM DESCRIPTION INSTALLATION MANUAL. WORK WAS DONE WITH REFERENCE TO HONEYWELL SYSTEM DESCRIPTION INSTALLATION MANUAL, 34-43-00. REMOVED UPPER TCAS ANTENNA P/N 7514060-902 SN 91091059. WHILE REMOVING UPPER TCAS ANTENNA, FOUND COAX CONNECTOR 501AN1P3, PN 225349-6 TO SPIN FREELY INDICATING FAULTY SHIELD CRIMP. INSTALLED NEW COAXIAL CONNECTOR WITH PIN 225554-6, NSN FROM GAC BAF MAIN STOCK ROOM. PERFORMED CENTER CONDUCTOR TO SHIELD CHECK AND CONTINUITY CHECK OF COAX. BOTH CHECKS TESTED GOOD. ALL WORK PERFORMED IAW WESTERN COMMANDER DWG# 08069372, TR CONNECTIVITY DRAWING NO. C-225349. RECEIVED AN OK TO INSTALL AND INSTALLED AN INSPECTED TCAS TOP ANTENNA P/N:7514060-902, S/N:ANE53059, RECEIVED FROM ACSS REPAIR AND OVERHAUL, WITH CERT. NO:L3ZR029X, REF. FORM 8130-3 TRACKING NO:CQ-68732, DATED 28 FEB, 2018, IAW GIV CMP CODE 344315. REFER TO SQUAWK 17.25 FOR THE REQUIRED TCAS FUNCTIONAL TEST. SEE STEPS 63.1 UP TO 63.6 FOR DETAILS OF WORK ACCOMPLISHED. Billing Method Hours Rate Total Labor USD: Time anti Material ST 23.17 ® $142.00 $3,290.14 Parts USD: Time and Material $10,044.25 Total USD: $13,334.39 Pans: Ref'. No. Part number: Description Quantity Sell price USD Extended USD 63 #1 7514060-902 ANTENNA, DIRECTIONAL, TCAS, AT-910 1 $9,995.00 $9,995.00 63#3 225554-6 CONNECTOR, TNC 90 DEGREE 1 $41.49 $41.49 COAX 63#4 ATUM500-0 HEAT SHRINK W/SEAL 1/2 1 $5.00 $5.00 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). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 6 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00808944 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Parts: Ref'. No. Part number: Description Quantity Sell price USD Extended USD 63 #6 NA.S1149C0332R WASHER 12 $0.23 Step: 6.3.1 Completed GAINED ACCESS TO THE TOP TCAS ANTENNA. PERFORMED RESISTANCE CHECK OF THE ANTENNA COAXIAL CONNECTIONS, (ANTENNA SIDE). FOUND THAT J4 (RED) RESISTANCE READING WAS CONSIDERABLY LOWER THAN MINIMUM ALLOWABLE RESISTANCE, (READING WAS 58 OHMS, PROPER READING SHOULD BE 2000 (+1- 200 OHMS), AS PER HONEYWELL SYSTEM DESCRIPTION INSTALLATION MANUAL. WORK WAS DONE WITH REFERENCE TO HONEYWELL SYSTEM DESCRIPTION INSTALLATION MANUAL, 34-43-00. Step: 6.3.2 Completed GAINED ACCESS TO AND REMOVED UPPER TCAS ANTENNA P/N 7514060-902 SN 91091059. ALL WORK ACCOMPLISHED IAW GIV MM 34-47-05 Step: 6.3.3 Completed WHILE REMOVING UPPER TCAS ANTENNA, FOUND COAX CONNECTOR 50IANIP3, PN 225349-6 TO SPIN FREELY INDICATING FAULTY SHIELD CRIMP. CONNECTOR THEN REMOVED FROM CABLE, WILL REQUIRE REPLACEMENT. ALL WORK ACCOMPLISHED GIV MM IAW 34-47-05, WESTERN COMMANDER DRAWING 08069372 Step: 6.3.4 Completed CHECKED CONTINUITY OF COAX CABLES BETWEEN TCAS UPPER ANTENNA AND TCAS COMPUTER. THE FOLLOWING RUNS WERE VERIFIED: 501ANIPI TO 502AIPIA PIN I, 50IANIP2 TO 502AIP IA PIN 2, 50IANIP3 TO 502AI PIA PIN 3, AND SOIAN I P4 TO 502AI PIA PIN 4. ALL RUNS CHECKED GOOD. NO DEFECTS NOTED. ALL WORK ACCOMPLISHED IAW WESTERN COMMANDER DWG 08069372. Step: 6.3.5 Completed INSTALLED NEW COAXIAL CONNECTOR WITH PIN 225554-6, NSN FROM GAC BAF MAIN STOCK ROOM. PERFORMED CENTER CONDUCTOR TO SHIELD CHECK AND CONTINUITY CHECK OF COAX. BOTH CHECKS TESTED GOOD. ALL WORK PERFORMED IAW WESTERN COMMANDER DWG# 08069372, TR CONNECTIVITY DRAWING NO. C-225349. Step: 6.3.6 Completed RECEIVED AN OK TO INSTALL AND INSTALLED AN INSPECTED TCAS TOP ANTENNA P/N:7514060-902, S/N:ANE53059, RECEIVED FROM ACSS REPAIR AND OVERHAUL, WITH CERT. NO:L3ZR029X, REF. FORM 8130-3 TRACKING NO:CQ-68732, DATED 28 FEB, 2018, IAW GIV CMP CODE 344315. REFER TO SQUAWK 17.25 FOR THE REQUIRED TCAS FUNCTIONAL TEST. $2.76 Item: 7 INTERIOR Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes PartfModel #: AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 7.1 Resolution: TO PROVIDE DOCUMENTATION OF REMOVED/REINSTALLED INTERIOR COMPONENTS ONLY. Discrepancy: 7.2 CUSTOMER REQUESTS TO REMOVE ENTRYWAY WOODWORK AND PROVIDE TO HIM. Resolution: Billing Method Hours Rate Total 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_WorkOrderPreliminaryInvoicelpt 2011 Page 7 of 117 Printed: 6/28/2018 9:39:11M Reel EFTA00808945 Bill To: JEGE LLC WO #: SC18654 Labor USD: Time and Material ST 5.51 @ $142.00 Total USD: Invoice Number: 6918002027 $782.42 $782.42 Step: 7.2.1 Completed PROVIDED THE FOLLOWING INTERIOR PIECES TO THE CUSTOMER: L/H NlED CURTAIN CABINET DOOR (RI 170) AFT ENTRYWAY PANEL (RI 200) FWD ENTRYWAY PANEL (RI 199) COPILOT ENTRY PANEL (RI 174) PILOT SIDE ENTRY PANEL (RI 173) FWD ENTRYWAY BULKHEAD JAMB (RI 177) Item: 9 PAINT Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes Part/Model #: AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 9.1 PAINT REPLACEMENT R/H IB FLIGHT SPOILER BOARD TO MATCH AIRCRAFT. Resolution: PREPPED TOP SIDE AND BOTTOM SIDE OF R/H IB SPOILER BOARD. MASKED OFF AREAS NOT TO BE PAINTED. WASHED TO REMOVE CONTAMINANTS.APPLIED JET-GLOW BLACK AS TOPCOAT. ALL WORK liA/W GIV SRM 51-07-10 Billing Method Hours Rate Total Labor USD: Time and Material ST 10.14 @ $142.00 $1,439.88 Total USD: $1,439.88 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 9.1 #1 U01955-QT PAINT, JET GLO GLOSS BLACK, 1 $0.00 QUART Step: 9.1.1 Completed PREPPED BOTTOM SIDE OF R/H IB SPOILER BOARD AND MASKED OFF AREAS NOT TO BE PAINTED. THEN SOLVANT CLEANED AND APPLIED EPDXY PRIMER FOLLOWED BY JET GLOW 01955 BLACK TOP COAL ALL WORK I/A/W GIV SRM 51-07-10 Step: 9.1.2 Completed PREPPED TOP SIDE OF Rai IB SPOILER BOARD. MASKED OFF AREAS NOT TO BE PAINTED. WASHED TO REMOVE CONTAMINANTS.APPLIED JET-GLOW BLACK AS TOPCOAT. ALL WORK UA/W GIV SRM 51-07-10 $0.00 Item: 10 ADMINISTRATIVE USE ONLY, NO RETURN TO SERVICE REQUIRED - NON-REGULATORY ITEMS Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes Part/Model #: AC Serial NolTail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 10.1 ADMINISTRATIVE USE TO PROCESS PARTS FOR RETURN FOR CREDIT ONLY. Resolution: 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 8 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00808946 Bill To: JEGE LLC Parts: WO #: SCI8654 Invoice Number: 6918002027 Ref. No. Part number: Description Quantity 10.1 #12 SE05000901-912S73-37 BUSHING, STD REPAIR-CONT SURF 1 10.1 #I5 1159C520443-51 WEIGHT ELEVATOR BALLAST 1 IO.I #I6 1159C520443-53 DOUBLER ELEVATOR BALLAST I Discrepancy: 10.2 ADMINISTRATIVE USE TO HOLD PARTS AND SERVICES THAT REQUIRE BILLING ON SQUAWKS. Resolution: Billing Method Hours Rate Total Parts USD: Time and Material $54.82 Services USD: Time and Material S2.90 Total USD: $57.72 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 10.2 #1 MS20004-18 BOLT 2 $14.21 528.42 10.2 #2 MS20004-20 BOLT 2 $7.42 $14.84 10.2 #3 MS20004-22 BOLT 2 $5.78 511.56 Services: Ref. No. Description Quantity Sell Price USD Extended USD 10.2 #1 ENGINEERING 1.00 $1.45 51.45 10.2 #2 ENGINEERING 1.00 $1.45 51.45 Discrepancy: 10.3 ADMINISTRATIVE USE TO FUEL AND DEFUEL AIRCRAFT AS REQUIRED. Resolution: Item: 11 DISCREPANCY RESOLUTION FOLLOW ON CMP CODES FOR MAINTENANCE MOBILITY DOCUMENTATION Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes PartfModel #: AC Serial Nolan No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 11.1 CMP GIV 282017 FUEL BOOST PUMP (LEFT ALTERNATE) - REMOVAL/ INSTALLATION RELATED TO ITEM 15.27 Resolution: COMPLIED WITH CMP GIV 282017 FUEL BOOST PUMP (LEFT ALTERNATE) - REMOVAL / INSTALLATION TORQUE WRENCH ID 141698M00 CAL. DUE DATE: 03/21/2019. 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 9 of 117 Printed: 6/28/2018 939:11M Reel EFTA00808947 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 11.2 CMP GIV 282018 FUEL BOOST PUMP (RIGHT ALTERNATE) - REMOVAL / INSTALLATION RELATED TO ITEM 15.32 Resolution: COMPLIED WITH CMP GIV 282018 FUEL BOOST PUMP (RIGHT ALTERNATE) - REMOVAL / INSTALLATION TORQUE WRENCH ID #1698M00 CAL. DUE DATE: 03/21/2019. Discrepancy: 113 CMP GIV 245060 Electrical Power Management Panel - Removal Installation Resolution: Discrepancy: 11.4 CMP GIV 535004 TAIL CONE - REMOVAL / INSTALLATION RELATED TO ITEM 13.24 Resolution: COMPLIED WITH CMP GIV 535004 Tail Cone - Removal / Installation Discrepancy: 11.5 CMP GIV 974560 ASC456 WING SPOILER REPLACE (RIGHT INBORAD FLIGHT) RELATED TO ITEM 14.18 Resolution: COMPLIED WITH ASC NUMBER 456 FLIGHT CONTROL SYSTEMS ATA27 WING SPOILER BOARD REPLACEMENT RIGHT INBOARD FLIGHT DATED MAY 21, 2004 UPDATED CMP GIV 974560 ASC456 WING SPOILER REPLACE RIGHT INBOARD FLIGHT 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 10 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00808948 Bill To: JEGE LLC WO It SC18654 Discrepancy: 11.6 CMP GIV 316701 XM WEATHER ANTENNA Invoice Number: 6918002027 RELATED TO ITEM 14.68 Resolution: COMPLIED WITH CMP GIV 316701 XM WEATHER ANTENNA. Discrepancy: 11.7 CMP GIV 245061 PANEL, EPMP—OPS TEST RELATED TO ITEM 6.1 Resolution: Discrepancy: 11.8 CMPO IV 974541 ASC 454A SPOILER BOARD REPLACEMENT (RIGHT GROUND) RELAfED TO ITEM 14.67 Resolution: COMPLIED NS1TH CMP GIV 974541 ASC 454A SPOILER BOARD REPLACEMENT (RIGHT GROUND) DATED 3-11-08. THE 24 MONTH HONEYCOMB BOND TEST (CMP 510070) AND THE 72 MONTH COMPOSITE NDT INSPECTION (CMP 570075) DO NOT APPLY TO THIS SPOILER BOARD. UPDATED WEIGHT AND BALANCE AS REQUIRED. Discrepancy: 11.9 CMP GIV 304025 WINDSHIELD HEAT CONTROLLER (LEFT FRONT / RIGHT SIDE) - REMOVAL / INSTALLATION RELATED TO 18.5 Resolution: COMPLIED WITH CMP GIV 304025 WINDSHIELD HEAT CONTROLLER (LEFT FRONT / RIGHT SIDE) - REMOVAL / INSTALLATION REMOVED AND REINSTALLED WINDSHIELD HEAT CONTROLLER (LEFT FRONT / RIGHT SIDE) P/N 574-3, S/N 0949. ALL WORK PERFORMED LAW GIV MM 30-04-01. SEE ITEM 11.11 FOR OPERATIONAL CHECK 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_WorkOrderPreliininaryInvoice.rpt 2011 Page 11 of 117 Printed: 6/28/2018 9:39:11M Reel EFTA00808949 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 11.10 CMP GIV 304026 WINDSHIELD HEAT CONTROLLER (RIGHT FRONT / LEFT SIDE) - REMOVAL / INSTALLATION RELATED TO 18.5 Resolution: COMPLIED WITH CMP GIV 304026 WINDSHIELD HEAT CONTROLLER (RIGHT FRONT / LEFT SIDE) - REMOVAL / INSTALLATION REMOVED AND REINSTALLED WINDSHIELD HEAT CONTROLLER (LEFT FRONT/ RIGHT SIDE) P/N 574-3, S/N 0568. ALL WORK PERFORMED lAW GIV MM 30-04-01. SEE ITEM 11.11 FOR OPERATIONAL CHECK Discrepancy: 11.11 CMP GIV 304001 WINDSHIELD HEAT—OPS TEST RELATED TO 18.5 Resolution: COMPLIED WITH CMP GIV 304001 WINDSHIELD HEAT—OPS TEST Discrepancy: 11.12 CMP GIV 240108 STANDBY POWER SYSTEM - OPERATIONAL TEST RELATED TO 18.5 Resolution: COMPLIED WITH CMP GIV 240108 Standby Power System - Operational Test Discrepancy: 11.13 CMP GIV 276052 SW, R GRD SPOIL WARN(0752)-ADJ Resolution: COMPLIED WITH CMP GIV 276052 SW, R GRD SPOIL WARN(0752)-ADJ 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_WorkOrderPrelintinaryInvoice.rpt 2011 Page 12 of 117 Printed: 6/28/2018 939:11M Reel EFTA00808950 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Discrepancy: 11.14 CMP GIV 344315 TRAFFIC COLLISION AVOIDANCE SYSTEM TOP ANTENNA - REMOVAL/ INSTALLATION RELATED TO SQUAWK 6.3 Resolution: COMPLIED WITH CMP GIV 344315 TRAFFIC COLLISION AVOIDANCE SYSTEM TOP ANTENNA - REMOVAL / INSTALLATION. REMOVED UPPER TCAS ANTENNA P/N 7514060-902 SN 91091059. RECEIVED AN OK TO INSTALL AND INSTALLED AN INSPECTED TCAS TOP ANTENNA P/N:7514060-902, S/N:ANE53059, RECEIVED FROM ACSS REPAIR AND OVERHAUL, WITH CERT. NO:L3ZR029X, REF. FORM 8130-3 TRACKING NO:CQ-68732, DATED 28 FEB, 2018, IAW GIV CMP CODE 344315. Discrepancy: 11.15 CMP GIV 344315 TRAFFIC COLLISION AVOIDANCE SYSTEM TOP ANTENNA - REMOVAL/ INSTALLATION RELATED TO 6.3 Resolution: N/A DUPLICATE ITEM Discrepancy: Resolution: Resolution: Aborted Item: 12 WCR'S Team Manager: Charles Heiwig Customer Coordinator: Shannon Sykes Part/Model #: AC Serial NolTail No.: TSN/TS0: CSN/CS0: Aircraft Time: Discrepancy: Resolution: Resolution: Aborted 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 13 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00808951 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Item: 13 72 MONTH FLIGHT CONTROL INSP (GIV SN 1085) Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes ParVModel #: AC Serial Nofrail No.: TSN/TS0: CSN/CS0: Aircraft Time: Discrepancy: 13.1 72 MONTH FLIGHT CONTROL INSPECTIONS Resolution: Labor USD: Parts USD: Total USD: ACCOMPLISH THE GIV 72 MONTH FLIGHT CONTROL INSPECTIONS. (SEE EXHIBIT 1) NOTE: CUSTOMER HAS THE OPTION TO PURCHASE THE 72 MONTH FLIGHT CONTROL KIT OR ORDER PARTS SEPARATELY. THIS ITEM AS QUOTED INCLUDES THE FLIGHT CONTROL KIT. SOME COMPONENTS INCLUDED IN THIS KIT MAY NOT BE REQUIRED DUE TO VARYING HARDWARE CONFIGURATIONS. IF THE 72 MONTH FLIGHT CONTROL KIT IS REQUESTED AND OPENED, A RESTOCKING FEE WILL BE REQUIRED FOR RETURNED KITS. ANY COMPONENTS NOT INCLUDED WITH THIS KIT WILL BE BILLED SEPARATELY. THE SEVENTY-TWO (72) MONTH KIT PROVIDES PARTS NECESSARY TO COMPLY WITH SEVENTY-TWO (72) MONTH FLIGHT CONTROL INSPECTION ITEMS ONLY. ANY REQUIRED PARTS THAT BECOME NECESSARY DUE TO DAMAGE FOUND (I.E., CORROSION AND/OR NORMAL WEAR AND TEAR TO ANY PARTS REMOVED AND/OR INSPECTED) ARE NOT PRICED IN THIS PROPOSAL AS THEY ARE PROVIDED "AS NEEDED". THIS KIT DOES NOT INCLUDE THE FLIGHT CONTROL BELL-CRANKS. RE: PROPOSALS/ 7042687 ROO (GACO218-2687-GIV-1085-R00)-1.1 Billing Method Hours Flat Rate Flat Rate Rate Total $38,088.00 $9,672.00 $47,760.00 Discrepancy: 13.2 Resolution: Parts: Ref. No. COMPLY WITH THE 72 MONTH FLIGHT CONTROL INSPECTION SERVICE CMP CODES BELOW: Part number: Description Quantity 13.2 #23 G4 72N1ONTH KIT 1 72 MONTH INSPECTION 11000-3999 13.2 #1 NAS6604DI9 BOLT, HEX HD-CL TOL, DRILLED SIIK 13.2 #2 NASII49D041611 WASHER, FLAT ALUMINUM 2 13.2 #3 NAS1149D046311 WASHER 2 13.2 #4 MSI7825-4 NUT SELF 4 LKG-CASTELLATED,STEEL 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 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808952 Bill To: JEGE LLC Parts: Ref. No. Part number: WO14: SC18654 Description Invoice Number: 6918002027 Quantity 13.2 #5 MS24665-I53 PIN, COTTER 8 13.2 #6 NAS6604D2I BOLT HEX IID-CL TOL,DRILLED SIIK 13.2 1$7 44GNOII-30Z TOUCHUP KIT, DEFT EPDXY SPRAY 3 PRIMER & CATALYST - ADD WATER [INTERNAL USE ONLY) 13.2 08 7416-6101-132 SHIM,.030 THK,5 IN X 20 IN,ARTUS 1 13.2 #9 NAS6604DI4 BOLT, HEX HD-CL TOL, DRILLED 2 SHIC, JIT 13.2 #10 NAS6606D3I BOLT liEX IID-CL TOL,DRILLED StIK 13.2 011 NAS6606D3I BOLT liEX 11D-CL TOL,DRILLED 1 StIK 13.2 #12 MS24665-302 COTTER PIN 2 13.2 #13 MS27039-1-1' SCREW-MACHINE,PAN HEAD 13.2 #14 MS35338-43 WASHER 13.2 015 NASI149F0363P WASHER, FLAT STEEL 13.2 016 MS2I042-3 NUT, SLF-LKG, 450 DEG, RDC HEX, RDC IIGT, RING BASE, NON-CRES 13.2 017 NASI149D0332J WASHER 2 13.2 018 MS2I042L3 NUT 2 13.2 019 NASI581F3T2 BOLT 2 13.2 #20 MS27039-08Il SCREW-MACHINE, PAN HD, CROSS REC 13.2 #21 MS2I042-08 NUT-SELF LOCKING,RING BASE 13.2 022 PR1422A2 SEALANT 13.2 024 NAS6204-IID BOLT 13.2 025 NAS6204-I6D BOLT 6 13.2 026 NAS1149D0416II WASHER, FLAT ALUMINUM 10 13.2 027 I159SCF457-15 VINYL DOTS, SCREW HEAD RECESS 50 COVER (GREEN) 13.2 #28 AMS-SUO2TYPE2B2 SEALANT (6 OZ.) 2 13.2 029 NASI149C0563R WASHER-FLAT CRES 2 13.2 030 AN3I0-5 NUT 13.2 031 NAS6204-I5D BOLT 13.2 #32 AN3I0-5 NUT 13.2 #33 NASI149DN832H WASHER, FLAT 8 13.2 034 MS5I957-46B SCREW 8 13.2 #35 NASI149CN832B FLAT WASHER 8 13.2 036 MSI7825-6 NUT, SELF LOCKING-CASTELLATED,STEEL 13.2 037 NASII49C0663R WASHER 2 13.2 038 NAS6605D66Y BOLT 13.2 039 MS21059L08 NUTPLATE, SELF-LOCKING 3 13.2 040 MSI7826-4 NUT 2 13.2 041 MS24665-153 PIN, COTTER 14 13.2 #42 NAS6204-46D BOLT 2 13.2 #43 MS20002C4 WASHER 2 13.2 #44 NASII49F0432P WASHER, FLAT STEEL (SAME AS 4 AN960-416L) 13.2 #45 MSI7826-4 NUT 2 13.2 #46 MS24665-151 COTTER PIN 3 13.2 #47 NASI149D046311 WASHER 13.2 #48 MS24665-I53 PIN, COTTER 5 13.2 #49 MSI7826-8 NUT 13.2 #50 MS20002-6 WASHER 13.2 051 MS27039-I-07 SCREW 13.2 052 NAS1149D0316II WASHER 2 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_WorkOrderPreliminarylnvoice.rpt 2011 Page IS of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808953 Bill To: JEGE LLC Parts: Ref. No. Part number: Description BOLT NUT WASHER, FLAT STEEL WIRE, SAFETY CABLE .032 x Hi" KEY LOCK SCREW BOLT BOLT SCREW SCREW,MACHINE,FLAT CTSK HD,100DEG,STFtL SCREW, MACHINE BUTTON HEAD SCREW SCREW,MACHINE,FLAT CTSK liD,100DEG,STRL SCREW WASHER WASHER COTTER PIN BOLT HEX HD-CL TOL,DRILLED SEIK WASHER JUMPER-ELEC BONDING,7.0 IN JUMPER, ELECTRICAL BONDING 5 IN JUMPER-ELEC BONDING,I0 IN KIT, 2 OZ MATTERHORN WHITE/TOPCOAT SCREW,MACHINE,FLAT CTSK IlD,100DEG,STRL BOLT, 100 DEG FRII, OFS CRUCIFORM, 95 KSI SCREW BOLT WASHER-FLAT ALUM NUT, STEEL SELF-LOCKING CASTELLATED SEALANT,6OZ #654 SEMKIT SCREW SCREW NUT-SELF LOCKING,RING BASE WASHER, FLAT STEEL WO #: SC18654 Invoice Number: 6918002027 Quantity 13.2 #53 13.2 #54 13.2 #55 13.2 #56 13.2 #57 13.2 #58 13.2 #59 13.2 #60 13.2 #61 13.2 #62 13.2 #63 13.2 #64 13.2 #65 13.2 #66 13.2 #67 13.2 #68 13.2 #69 13.2 #70 13.2 #71 13.2 #73 13.2 #74 13.2 #75 13.2 #76 13.2 #77 13.2 #78 13.2 #79 13.2 #80 13.2 #81 13.2 #82 13.2 #83 13.2 #84 13.2 #85 13.2 #86 13.2 #87 Services: Ref. No. NASI303-5 AN3I0-5 NASI149F0332P CIO-218 NAS559-3 MS24694S4 GAB5IIGA3-4 GAB5IIGA3-3 M52469454 MS24694-S3 NAS600-I6P NAS601-I6P MS24694-S50 MS24693550 MS20002C4 MS20002-4 MS24665-I55 NAS6604DI7 MS20002C8 MS25083-2BB7 MS25083-2BB5 MS25083-2BBI0 MATTERHORN-KIT-2O MS24694-552 NASI581C3T2 NASI581C3T3 NAS6605-24 NAS1149D0563II MSI7825-5 PRI440B1-2-654 MS24694C4 MS35206-244 MS2I042-08 NASI149FN816P Description GAC REPAIRS 1159SB30144-15 GAC REPAIRS 1159SB30144-16 13.2 #1 Part Ref: 13.2 #2 Part Ref: 13.2 #3 Part Ref: 13.2 #4 Part Ref: 13.2 #5 Part Ref: GAC REPAIRS 1159SB30144-1I GAC REPAIRS 1159SB30144-12 GAC REPAIRS 1159SB30144-19 13.2 #6 GAC REPAIRS CRANK ASSY CRANK ASSY CRANK ASSY CRANK ASSY CRANK ASSY 2 2 I0 4 12 50 75 12 4 4 3 2 3 3 10 1 30 10 1 II 6 4 9 4 2 4 Quantity 1.00 1.00 1.00 1.00 1.00 1.00 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). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 16 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808954 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Services: Ref. No. Description Quantity Part Ref: 1159SB30144-20 CRANK ASSEMBLY Discrepancy: 13.3 ACCOMPLISH INCOMING AND OUTGOING FLIGHT CONTROL THROWS USING THE GIV 72 MONTH FLIGHT CONTROL THROWS TRAVELER QCT 071 Resolution: Discrepancy: 13.4 CMP GIV 271002 LATERAL PWR SYS—OPS TEST Resolution: COMPLIED WITH CMP GIV 271002 LATERAL PWR SYS-OPS TEST Discrepancy: 13.5 CMP GIV 271003 LATERAL CONT SYS-FRICTION CK Resolution: COMPLIED WITH CMP GIV 271003 LATERAL CONT SYS-FRICTION CK Discrepancy: 13.6 CMP GIN' 272001 RUDDER CONT SYS-OPS TEST Resolution: COMPLIED WITH CMP GIV 272001 RUDDER CONT SYS--OPS TEST Discrepancy: 13.7 CMP GIV 273001 ELEVATOR CONTROL SYS, OPS CK Resolution: COMPLIED WITH CMP GIV 273001 ELEVATOR CONTROL SYS, OPS CK Discrepancy: 13.8 CMP GIV 276008 GROUND SPOILER SYS-RIG CHECK 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 17 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808955 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Resolution: COMPLIED WITH CMP GIV 276008 GROUND SPOILER SYS-RIG CHECK Discrepancy: 13.9 CMP GIV 276005 Speed Brake - Operational Test Resolution: COMPLIED WITH CMP GIV 276005 Speed Brake - Operational Test Discrepancy: 13.10 CMP GIV 276030 Speed Brake System - Rigging Check Resolution: RQCI COMPLIED WITH CMP GIV 276030 SPEED BRAKE SYSTEM - RIGGING CHECK DURING RIGGING CHECK, NOTED L/H & R/H GROUND SPOILERS THROWS TO BE OUT OF LIMITS. ADJUSTED G/S INPUT ROD TO BRING THROWS WITHIN LIMITS [ANY GIV MM 27-02-00. OPS CHECK GOOD AT THIS TIME. Discrepancy: 13.11 CMP GIV 273003 ELEVATOR FREE PLAY - INSPECTION *ACCOMPLISH BEFORE AND AFTER ELEVATOR MAINTENANCE.* Resolution: COMPLIED WITH CMP GIV 273003 Elevator Free Play - Inspection Discrepancy: 13.12 CMP GIV 271011 Aileron Trim Tab Actuator - Inspection Resolution: COMPLIED WITH CMP GIV 271011 Aileron Trim Tab Actuator - Inspection Discrepancy: 13.13 CMP GIV 271009 ACTUATOR, AILERON TRIM TAB Resolution: RQCI COMPLIED WITH CMP GIV 271009 ACTUATOR, AILERON TRIM TAB REMOVALAND INSTALLATION. 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_WorkOrderPrelintinaryInvoice.rpt 2011 Page 18 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808956 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 13.14 CMP GIV 271019 Aileron Actuator (Left) - Inspection Resolution: COMPLIED WITH CMP GIV 271019 Aileron Actuator ( Left) - Inspection Discrepancy: 13.15 CMI' GIN 271017 ACTCAIOR, LEFT AILERON Resolution: RQCI COMPLIED WITH CMP GIV 271017 ACTUATOR, LEFT AILERON Discrepancy: 13.16 CMP GIV 271020 Aileron Actuator (Right) - Inspection Resolution: COMPLIED WITH CMP GIV 271020 Aileron Actuator (Right) - Inspection Discrepancy: 13.17 CMP GIV 271018 ACTUATOR, RIGHT AILERON Resolution: RQCI COMPLIED WITH GIV CMP 271018 AILERON ACTUATOR (RIGHT) REMOVAL/INSTALLATION REMOVED AND INSTALLED SERVICABLE R/H AILERON ACTUATOR P/N 1159CSH252-2G S/N 2073GT Discrepancy: 13.18 CMP GIV 271023 Aileron Boost Bellcrank (Left) - Inspection Resolution: COMPLIED WITH CMP GIV 271023 Aileron Boost Bellcrank (Left) - Inspection 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_WorkOrderPreliininaryInvoice.rpt 2011 Page 19 of 117 Printed: 6/28/2018 939:11A? Reel EFTA00808957 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 13.19 CMP GIV 271024 Aileron Boost Bellcrank (Right) - Inspection Resolution: COMPLIED WITH CMP GIV 271024 Aileron Boost Bellcrank (Right) - Inspection Discrepancy: 13.20 CMP GIV 272011 Rudder Actuator & Fwd Attach Fitting - Inspection Resolution: COMPLIED WITH CMP GIV 272011 Rudder Actuator and Fwd Attach Fitting - Inspection Discrepancy: 13.21 CMP GIV 272017 Rudder Trim Actuator - Inspection Resolution: COMPLIED WITH CMP GIV 272017 Rudder Trim Actuator - Inspection Discrepancy: 13.22 CMP GIV 272014 ACTUATOR, RUDDER TRIM Resolution: RQCI COMPLIED WITH CMP GIV 272014 ACTUATOR, RUDDER TRIM Discrepancy: 13.23 CMP GIV 272034 Rudder Torque Tube - Inspection Resolution: COMPLIED WITH CMP GIV 272034 RUDDER TORQUE TUBE - INSPECTION RUDDER TORQUE TUBE ASSEMBLED USING NEW HARDWARE PAK: P/N 1159CGSK272034, NSN, PART OF G4 72MONTH KIT 1 PICKED FROM GAC-WESTFIELD STOCK.. INSTALLED RUDDER TORQUE TUBE USING NEW BEARING P/N 1159SCB203-1, NSN, REF GAC-SAV PACKING SLIP SASH#17-175934, DATED 12/15/2017. TORQUE WRENCH I.D. 1750T00, DUE 4/1/2019 TORQUE WRENCH I.D. 1750X00, DUE 2/15/2019 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_WorkOrderPrelintinaryInvoice.rpt 2011 Page 20 of I l 7 Printed: 6/28/2018 939:11M Reel EFTA00808958 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 13.24 CMP GIV 272009 Rudder Assembly Resolution: RQCI COMPLIED WITH CMP GIV 272009 RUDDER - REMOVAL / INSTALLATION PART NUMBER OFF/ON: 1159CS30004-3 SERIAL NUMBER OFF/ON: 1276 Discrepancy: 13.25 CMP GIV 272035 Rudder Torque Tube - Removal / Installation Resolution: COMPLIED WITH CMP GIV 272035 RUDDER TORQUE TUBE - REMOVAL / INSTALLATION TORQUE WRENCH I.D. 1750T00, DUE 4/1/2019 TORQUE WRENCH I.D. 1750X00, DUE 2/15/2019 Discrepancy: 13.26 CMP GIV 273009 Elevator Actuator - Inspection Resolution: COMPLIED WITH CMP GIV 273009 Elevator Actuator - Inspection Discrepancy: 13.27 CMP GIV 273077 Elevator Hinge Fitting (Left) - Inspection Resolution: RQCI COMPLIED WITH CMP GIV 273077 ELEVATOR HINGE FITTING (LEFT) - INSPECTION TORQUE WRENCH I.D. 1750T00, DUE 4/1/2019 TORQUE WRENCH I.D. 1750X00, DUE 2/15/2019 Discrepancy: 13.28 CMP GIV 273007 Elevator (Left) - Removal / Installation Resolution: 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 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00808959 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 13.29 CMP GIV 273015 ACTUATOR, L ELEV TRIM TAB Resolution: RQCI COMPLIED WITH CMP GIV 273015 ACTUATOR, L ELEV TRIM TAB REMOVAL AND INSTALLATION. Discrepancy: 13.30 CMP GIV 273078 Elevator Hinge Fitting (Right) - Inspection Resolution: RQCI: COMPLIED WITH CMP GIV 273078 ELEVATOR HINGE FITTING (RIGHT) - INSPECTION Discrepancy: 13.31 CMP GIV 273008 Elevator (Right) Resolution: Discrepancy: 13.32 CMP GIV 273016 ACTUATOR, R ELEV TRIM TAB Resolution: RQCI COMPLIED WITH CMP GIV 273016 ACTUATOR, R ELEV TRIM TAB Discrepancy: 13.33 CMP GIV 276011 Ground Spoiler Actuator (Left) - Inspection Resolution: COMPLIED WITH CMP GIV 276011 Ground Spoiler Actuator (Left) - Inspection 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_WorkOrderPreliininaryInvoice.rpt 2011 Page 22 of 117 Printed: 6/28/2018 939:11M Reel EFTA00808960 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 1334 CMP GIV 276009 ACTUATOR, L GRD SPOILER Resolution: RQCI COMPLIED WITH CMP GIV 276009 ACTUATOR, L GRD SPOILER Discrepancy: 13.35 CMP GIV 276081 Ground Spoiler Bellcrank Assembly (Left) - Removal / Installation Resolution: RQCI COMPLIED WITH CMP GIV 276081 GROUND SPOILER BELLCRANK ASSEMBLY (LEFT) - REMOVAL/ INSTALLATION. REMOVED L/H GROUND SPOILER BELLCRANK ASSY, P/N: 11595B30144-19 INSTALLED REPAIRED BELLCRANK ASSY, P/N: 115951B0144-19. REF GAC SAV, CERT# GR4R216M, 8130-3, DATED 01 JUNE 2018 WITH TRACKING# 20180601003859 AND ATTACHED WO# RC556415.5. REMOVED WORN GROUND SPOILER BELLCRANK PIN WITH P/N 1159CM30252-15 AND INSTALLED A NEW GROUND SPOILER BELLCRANK PIN WITH PIN 1159CM30252-15 RECEIVED FROM GAC WITH 8130 TRACKING #20180325035202 DATED 25 MAR 2018, CERT #ODA-511131-CE. Step: 1335.1 Step: 1335.2 Completed Completed REMOVED WORN GROUND SPOILER BELLCRANK PIN WITH P/N 1159CM30252-15 AND INSTALLED A NEW GROUND SPOILER BELLCRANK PIN WITII P/N 1159CM30252-15 RECEIVED FROM GAC WITH 8130 TRACKING #20180325035202 DATED 25 MAR 2018, CERT #ODA-511131-CE. REMOVED LAI GROUND SPOILER BELLCRANK ASSY, P/N: 1159SB30144-19 AND SENT TO GAC SAV FOR REPAIIR. RECIEVED REPAIRED BELLCRANK ASSY, P/N: I159SB30144-19. REF GAC SAV, CERT', GR4R216M, 8130-3, DATED 01 JUNE 2018 WITH TRACKING# 20180601003859 AND ATTACHED WO# RC556415.5. Discrepancy: 13.36 CMP GIV 276012 Ground Spoiler Actuator (Right) - Inspection Resolution: COMPLIED WITH CMP GIV 276012 Ground Spoiler Actuator (Right) - Inspection Discrepancy: 1337 CMP GIV 276010 ACTUATOR, R GRD SPOILER Resolution: RQCI COMPLIED WITH CMP GIV 276010 ACTUATOR, R GRD SPOILER 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_WorkOrderPrelintinaryInvoice.rpt 2011 Page 23 of 117 Printed: 6/28/2018 939:11M Reel EFTA00808961 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 13.38 CMP GIV 276082 Ground Spoiler Bellcrank Assembly (Right) - Removal / Installation Resolution: RQCI PERFORMED MAGNETIC PARTICLE INSPECTION ON GROUND SPOILER BELLCRANK ASSEMBLY BOLT. INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON DESTRUCTIVE PROCEDURES MANUAL 4.0 MAGNETIC PARTICLE REVISION 25 DECEMBER 15, 2017. NO DEFECTS NOTED. REMOVED OLD BELLCRANK ASSY WITH P/N 1159SB30144-20, SIN NSN. INSTALLED A REPAIRED BELLCRANK ASSY WITH P/N 115951B0144-20, S/N NSN. REFERENCE 8130-3 WITH TRACKING #20180607121725 DATED 07 JUN 2018 FROM GAC SAVANNAH AUTHORIZATION# CRS GR4Ft216M . ALL WORK DONE IN ACCORDANCE WITH CMP CODE 276082. TQ WRENCH ID# 1750U00 CAL NEXT DUE DATE 10/16/2018 TQ WRENCH ID# 1750Y00 CAL NEXT DUE DATE 2/15/2019 Step: 13.38.1 Completed PERFORMED MAGNETIC PARTICLE INSPECTION ON GROUND SPOILER BELLCRANK ASSEMBLY BOLT. INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON DESTRUCTIVE PROCEDURES MANUAL 4.0 MAGNETIC PARTICLE REVISION 25 DECEMBER 15, 2017. NO DEFECTS NOTED. Discrepancy: 13.39 CMP GIV 276033 Flight Spoiler Actuator (Left) - Inspection Resolution: COMPLIED WITH CMP GIV 276033 Flight Spoiler Actuator (Left) - Inspection Discrepancy: 13.40 CMP GIV 276031 Flight Spoiler Actuator (Left) - Removal / Installation Resolution: RQCI COMPLIED WITH CMP GIV 276031 Flight Spoiler Actuator (Left) - Removal / Installation Discrepancy: 13.41 CMP GIV 276077 Outboard Flight Spoiler Bellcrank Assembly (Left) - Removal / Installation Resolution: RQCI COMPLIED WITH CMP GIV 276077 OUTBOARD FLIGHT SPOILER BELLCRANK ASSEMBLY (LEFT) - REMOVAL / INSTALLATION. REMOVED L/H OUTBOARD FLIGHT SPOILER BELLCRANK ASSY, P/N: 1159SB30144-15. INSTALLED REPAIRED BELLCRANK ASSY, P/N: 1159SB30144-15. REF GAC SAV, CERT# GR4R2I6M, 8130-3, DATED 01 JUNE 2018 WITH TRACKING# 20180601000335 AND ATTACHED WO# RC556415.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 24 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00808962 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Step: 13.41.1 Completed ENTERED IN ERROR MOVED STEP TO PROPER ITEM 13.42 Step: 13.41.2 Completed REMOVED VII OUTBOARD FLIGHT SPOILER BELLCRANK ASSY, PIN: 1159SB30144-15 AND SENT TO GAC SAV FOR REPAIIR. RECIEVED REPAIRED BELLCRANK ASSY, P/N: 1159SB30144-15. REF GAC SAV, CEEMIGR411216M, 8130-3, DATED 01 JUNE 2018 WITH TRACKING# 20180601000335 AND ATTACHED WON RC556415.1. Discrepancy: 13.42 CMP GIV 276079 Inboard Flight Spoiler Bellcrank Assembly (Left) - Removal / Installation Resolution: RQCI COMPLIED WITH CMP GIV 276079 INBOARD FLIGHT SPOILER BELLCRANK ASSEMBLY (LEFT) - REMOVAL /INSTALLATION. REMOVED L/H INBOARD FLIGHT SPOILER BELLCRANK ASSY, P/N: 1159SB30144-11 AND SENT TO GAC SAV FOR REPAIIR. RECIEVED AND INSTALLED REPAIRED BELLCRANK ASSY, P/N: 1159SB30144-11. REF GAC SAV, CERT# GR4R216M, 8130-3, DATED 01 JUNE 2018 WITH TRACKING# 20180607114035 AND ATTACHED WO# RC556415.3. PERFORMED MAGNETIC PARTICLE INSPECTION ON OUTBOARD FLIGHT SPOILER BELLCRANK ASSEMBLY BOLT. INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON DESTRUCTIVE PROCEDURES MANUAL 4.0 MAGNETIC PARTICLE REVISION 25 DECEMBER 15, 2017. NO DEFECTS NOTED. Step: 13.42.1 Completed PERFORMED MAGNETIC PARTICLE INSPECTION ON OUTBOARD FLIGHT SPOILER BELLCRANK ASSEMBLY BOLT. INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON DESTRUCTIVE PROCEDURES MANUAL 4.0 MAGNETIC PARTICLE REVISION 25 DECEMBER 15, 2017. NO DEFECTS NOTED Step: 13.42.2 Completed REMOVED Ulf INBOARD FLIGHT SPOILER BELLCRANK ASSY, PIN: 1159SB30144-11 AND SENT TO GAC SAV FOR REPAIIR. RECIEVED REPAIRED BELLCRANK ASSY, P/N: 1159M330144-II. REF GAC SAY, CERT# CR41221661, 8130-3, DATED 01 JUNE 2018 WITH TRACKING# 20180607114035 AND ATTACHED WON RC556415.3. Discrepancy: 13.43 CMP GIV 276034 Flight Spoiler Actuator (Right) - Inspection Resolution: COMPLIED WITH CMP GIV 276034 Flight Spoiler Actuator (Right) - Inspection Discrepancy: 13.44 CMP GIV 276032 Flight Spoiler Actuator (Right) - Removal / Installation Resolution: RQCI COMPLIED WITH CMP GIV 276032 Flight Spoiler Actuator (Right) - Removal / Installation 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 25 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00808963 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 13.45 CMP GIV 276078 Outboard Flight Spoiler Bellcrank Assembly (Right) - Removal / Installation Resolution: RQCI REMOVED WORN OUTBOARD FLIGHT SPOILER BELLCRANK BOLT WITH P/N NAS1310-56D AND INSTALLED A NEW OUTBOARD FLIGHT SPOILER BELLCRANK BOLT WITH P/N NAS1310-56D. RECEIVED C OF C FROM KLX, W/O# WEP018-02645 PACKING SLIP DATED 5-30-18 REMOVED OLD BELLCRANK ASSY WITH P/N 11595630144-16, SIN NSN. INSTALLED A REPAIRED BELLCRANK ASSY WITH P/N 115951230144-16, SIN NSN. REFERENCE 8130-3 WITH TRACKING # 20180601005613 DATED 01 JUN 2018 FROM GAC SAVANNAH AUTHORIZATION# CRS GR4R216M . ALL WORK DONE IAW GIV CMP 276078 TQ WRENCH ID# 1750U00 CAL NEXT DUE DATE 10/16/2018 TQ WRENCH ID# 1750Y00 CAL NEXT DUE DATE 2/15/2019 Step: 13.45.1 Completed REMOVED WORN OUTBOARD FLIGHT SPOILER BELLCRANK BOLT WITH P/N NASI310-56D AND INSTALLED A NEW OUTBOARD FLIGHT SPOILER BELLCRANK BOLT WITH PIN NASI310-56D. RECEIVED C OF C FROM KLX, W/O# WEPOI8-02645 PACKING SLIP DATED 5-30-18 Discrepancy: 13.46 CMP GIV 276080 Inboard Flight Spoiler Bellcrank Assembly (Right) - Removal / Installation Resolution: RQCI REMOVED WORN INBOARD FLIGHT SPOILER PIN WITH P/N 1159CM20264-13 AND INSTALLED A NEW INBOARD FLIGHT SPOILER PIN WITH P/N 1159CM20264-13. RECEIVED FROM GAC SAV PACKING LIST #SASH#13-62020 DATED 05-29-2013. REMOVED OLD BELLCRANK ASSY WITH PIN 1159S630144-12. NSNB. REPLACED WITH REPAIRED BELLCRANK ASSY WITH P/N 11595B30144-12. NSN. REFERENCE 8130-3 WITH FORM TRACKING NUMBER 20180601002058 DATED 01 JUN 2018 FROM GAC SAVANNAH CRS# GR4R216M. ALL WORK DONE JAW GIV CMP 276080. TQ WRENCH ID# 1750U00 CAL NEXT DUE DATE 10/16/2018 TQ WRENCH ID# 1750Y00 CAL NEXT DUE DATE 2/15/2019 Step: 13.46.1 Completed REMOVED WORN INBOARD FLIGHT SPOILER PIN WITH P/N 1159C8120264-13 AND INSTALLED A NEW INBOARD FLIGHT SPOILER PIN WITH PIN II59CM20264-13. RECEIVED FROM GAC SAV PACKING LIST !MASH/013-62020 DATED 05-29-2013. Discrepancy: 13.47 CMP GIV 552011 Elevator Trim Tab Hinge Fitting (Left) - Inspection Resolution: COMPLIED WITH CMP GIV 552011 Elevator Trim Tab Hinge Fitting (Left) - Inspection 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_WorkOrderPrelitninaryInvoice.rpt 2011 Page 26 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808964 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 13.48 CMP GIV 273013 Trim Tab, Elevator (Left) Resolution: COMPLIED WITH CMP GIV 273013 Elevator Trim Tab (Left) - Removal / Installation Discrepancy: 13.49 CMP GIV 552012 Elevator Trim Tab Hinge Fitting (Right) - Inspection Resolution: COMPLIED WITH CMP GIV 552012 Elevator Trim Tab Hinge Fitting (Right) - Inspection Discrepancy: 13.50 CMP GW 273014 Trim Tab. Elevator (Right) Resolution: RQCI: COMPLIED WITH CMP GIV 273014 ELEVATOR TRIM TAB RIGHT REMOVAL/ INSTALLATION TORQUE WRENCH ID NUMBER 1750T00 CAL DATE: 4/1/2018 NEXT CAL DUE 4/1/2019 Discrepancy: 13.51 CMP GIN' 554015 Rudder / Hinge - Inspection Resolution: RQCI COMPLIED WITH CMP GIV 554015 RUDDER / HINGE - INSPECTION TORQUE WRENCH ID 1752A00 CAL DATE: 4/19/2018 TORQUE WRENCH ID 1750500 CAL DATE: 4/19/2018 Discrepancy: 13.52 CMP GIV 576011 Aileron Hinge Fitting (Left) - Inspection Resolution: RQCI COMPLIED WITH CMP GIV 576011 AILERON HINGE FITTING (LEFT) - INSPECTION 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 27 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00808965 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 13.53 CMP GIV 271013 Aileron (Left) Resolution: RQCI COMPLIED WITH CMP GIV 271013 Left Aileron - Removal / Installation Discrepancy: 13.54 CMP GIV 576012 Aileron Hinge Fitting (Right) - Inspection Resolution: RQCI COMPLIED WITH CMP GIV 576012 AILERON HINGE FITTING (RIGHT) - INSPECTION Discrepancy: 13.55 CMP GIV 271014 Aileron (Right) Resolution: RQCI COMPLIED WITH CMP GIV 271014 RIGHT AILERON - REMOVAL / INSTALLATION PART NUMBER OFF/ON: 1159CS20006-8 SERIAL NUMBER OFF/ON: 1086 Discrepancy: 13.56 CMP GIV 576015 Aileron Trim Tab Hinge Fitting - Inspection Resolution: COMPLIED WITH CMP GIV 576015 Aileron Trim Tab Hinge Fitting - Inspection Discrepancy: 13.57 CMP GIV 271008 Trim Tab, Aileron Resolution: COMPLIED WITH CMP GIV 271008 Aileron Trim Tab - Removal / Installation 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 28 of 117 Printed: 6/28/2018 939:11At Reel EFTA00808966 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 13.58 CMP GIV 577005 Flight Spoiler / Hinge (Left Inboard) - Inspection Resolution: COMPLIED WITH CMP GIV 577005 FLIGHT SPOILER / HINGE (LEFT INBOARD) - INSPECTION Discrepancy: 13.59 CMP GIV 276071 Inboard Flight Spoiler (Left) - Removal / Installation Resolution: RQCI - COMPLIED WITH CMP GIV 276071 INBOARD FLIGHT SPOILER (LEFT) - REMOVAL/ INSTALLATION Discrepancy: 13.60 CMP GIV 577006 Flight Spoiler / Hinge (Right Inboard) - Inspection Resolution: COMPLIED WITH CMP GIV 577006 Flight Spoiler / Hinge (Right Inboard) - Inspection Discrepancy: 13.61 CMP GIV 276072 Inboard Flight Spoiler (Right) - Removal / Installation Resolution: RQCI COMPLIED WITH CMP GIV 276072 INBOARD FLIGHT SPOILER (RIGHT) - REMOVAL / INSTALLATION. REMOVED THE R/H INBOARD FLIGHT SPOILER P/N 1159CSH400050-2 S/N 1090 98897. INSTALLED A REPAIRD R/H INBOARD FLIGHT SPOILER P/N 1159CS40701-10 S/N 1202557 RECEIVED FROM GULFSTREAM SAVANNAH WITH APPROVAL NUMBER GR4R216M. REFERENCE 8130-3 WITH FORM TRACKING NUMBER 20180410125532 DATED APRIL 10, 2018..WORK DONE IAW GULFSTREAM GIV 974560 ASC456 WING SPOILER REPLACE RIGHT INBORAD FLIGHT. TORQUE WRENCH I.D. NUMBER 1750T00 CAL DATE 04/01/2019 AND TORQUE WRENCH I.D. NUMBER 17961(00 CAL DATE 02/01/2019 RE-CALCULATED WEIGHT AND BALANCE PER ASC 456. PROVIDED CUSTOMER WITH ICA DOCUMENT# GIV-SGER-292 REV "A" MODIFICATION INSPECTION PROCEDURES SUPPLEMENT REPORT. 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_WorkOrderPreliininaryInvoice.rpt 2011 Page 29 of 117 Printed: 6/28/2018 939:11M Reel EFTA00808967 Bill To: JEGE LLC WO It: SC18654 Invoice Number: 6918002027 Step: 13.61.1 Completed RQCI COMPLIED WITII CMP GIV 276072 INBOARD FLIGHT SPOILER (RIGHT) - REMOVAL/ INSTALLATION. REMOVED THE Rill INBOARD FLIGHT SPOILER P/N 1159C511400050-2 Sri 1090 98897. INSTALLED A REPAIRD RAI INBOARD FLIGHT SPOILER PIN 1159CS40701-10 SIN 1202557 RECEIVED FROM GULFSTREAM SAVANNAH WITH APPROVAL NUMBER GR4R216M. REFERENCE 8130-3 WITII FORM TRACKING NUMBER 20180410125532 DATED APRIL 10, 2018..WORK DONE IAW GULFSTREAM GIV 974560 ASC456 WING SPOILER REPLACE RIGHT INBORAD FLIGHT. TORQUE WRENCH I.D. NUMBER 1750T00 CAL DATE 04/01/2019 AND TORQUE WRENCH I.D. NUMBER 17%K00 CAL DATE 02/01/2019 Step: 13.61.2 Completed RE-CALCULATED WEIGHT AND BALANCE PER ASC 456. PROVIDED CUSTOMER WITH ICA DOCUMENT# GIV-SGER-292 REV "A" MODIFICATION INSPECTION PROCEDURES SUPPLEMENT REPORT. Discrepancy: 13.62 CMP GIV 577007 Flight Spoiler / Hinge (Left Outboard) - Inspection Resolution: COMPLIED WITH CMP GIV 577007 Flight Spoiler / Hinge (Left Outboard) - Inspection Discrepancy: 13.63 CMP GIV 276073 Outboard Flight Spoiler (Left) - Removal / Installation Resolution: RQCI: COMPLIED WITH CMP GIV 276073 Outboard Flight Spoiler (Left) - Removal / Installation Discrepancy: 13.64 CMP GIV 577008 Flight Spoiler / Hinge (Right Outboard) - Inspection Resolution: COMPLIED WITH CMP GIV 577008 Flight Spoiler / Hinge (Right Outboard) - Inspection Discrepancy: 13.65 CMP GIV 276074 Outboard Flight Spoiler (Right) - Removal / Installation Resolution: RQCI: COMPLIED WITH CMP GIV 276074 Outboard Flight Spoiler (Right) - Removal / Installation Discrepancy: 13.66 CMP GIV 577009 Ground Spoiler/ Hinge (Left) - Inspection 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_WorkOrderPrelitninaryInvoice.rpt 2011 Page 30 of 117 Printed: 6/28/2018 9:39:11M Reel EFTA00808968 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Resolution: COMPLIED WITH CMP GIV 577009 Ground Spoiler/ Hinge (Left) - Inspection Discrepancy: 13.67 CMP GIV 276075 Ground Spoiler (Left) Resolution: RQCI: COMPLIED WITH CMP GIV 276075 GROUND SPOILER (LEFT) - REMOVAL / INSTALLATION Discrepancy: 13.68 CMP GIV 577010 Ground Spoiler / Hinge (Right) - Inspection Resolution: COMPLIED WITH CMP GIV 577010 Ground Spoiler / Hinge (Right) - Inspection Discrepancy: 13.69 CMP GIV 276076 Ground Spoiler (Right) Resolution: RQCI COMPLIED WITH CMP GIV 276076 GROUND SPOILER (RIGHT) - REMOVAL / INSTALLATION REPLACED THE DAMAGED SPOILER BOARD P/N 1159CSH40070-2 S/N 1091 98897 WITH A NEW BOARD PIN 1159CS40700-10 S/N 1193058. REFERENCE EASA FORM 1 FROM SAFRAN NACELLES LIMITED, APPROVAL # UK.21G.2117, FORM TRACKING # 80298609-1 DATED 27 OCT 2017. WORK DONE IAW ASC454A (REF ITEM 11.8) AND CMP 276076 (REF ITEM 13.69) Item: 14 72 MONTH FLIGHT CONTROL INSP DISCREPANCIES Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes ParVModel #: AC Serial NoJTail No.: TSN/TSO: CSN/CS0: Aircraft Time: Discrepancy: 14.1 ITEM FOR ADDITIONAL TIME DUE TO EXCESS PAINT BUILD UP NOTED WHILE ACCESSING BODY FAIRINGS AND FLIGHT CONTROLS. Resolution: BILLED ADDITIONAL TIME 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 31 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00808969 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Billing Method Hours Rate Total Labor USD: Time and Material ST 14.67 @ $142.00 $2,083.14 Parts USD: Time and Material S1.00 Total USD: ¶2.084.14 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.1 #1 TY2SM TY RAP W/NIETAL LOCKING 2 50.50 $1.00 TAB(BARB) Discrepancy: 14.2 WHILE C/W 276011 L/H GROUND SPOILER ACTUATOR INSPECTION FOUND GROUND SPOILER PIVOT PIN TO BE GALLED. Resolution: REMOVED DEFECTIVE LH GROUND SPOILER BELLCRANK PIVOT PIN P/N: 1159CM30252-15 NSN AND REPLACED WITH NEW PIN PIN: 1159CM30252-15 NSN RECEIVED FROM GAC-SAV ODA-511131-CE FAA FORM 8130-3 TRACKING# 20180325035202 DATED 25 MAR 2018 IAW GIV CMP 276009 REF ITEM 13.34 FOR FINAL INSTALLATION OF LH GROUND SPOILER ACTUATOR & BELLCRANK. Billing Method Hours Rate Total Labor USD: Time and Material ST 0.58 @ $142.00 582.36 Parts USD: Time and Material $272.73 Total USD: $355.09 Parts: Ref'. No. Part number: Description Quantity Sell price USD Extended USD 14.2 #1 II59CM30252-15 PIN BELLCRANK-GROUND 1 $272.73 $272.73 SPOILER Discrepancy: 14.3 WHILE C/A 276033 IJH FLIGHT SPOILER ACTUATOR INSPECTION FOUND BOTH PIVOT BEARINGS TO BE FROZEN. Resolution: CLEANED AND VISUALLY INSPECTED INBOARD & OUTBOARD LH FLIGHT SPOILER BEARINGS WITH NO DEFECTS NOTED. AFTER CLEANING BEARINGS ARE NO LONGER FROZEN AND ARE IN SERVICABLE CONDITION FOR CONTINUED USE. NO FURTHTER ACTION REQUIRED AT THIS TIME. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.05 @ $142.00 $149.10 Total USD: $149.10 Discrepancy: 14.4 WHILE C/W 276033 LJH FLIGHT SPOILER ACTUATOR FOUND OB SPOILER BELLCRANK PIVOT BOLT TO BE SCORED. 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 32 of 117 Printed: 6/28/2018 9:39:11AI Ref:/ EFTA00808970 Bill To: JEGE LLC WO It: SC18654 Invoice Number: 6918002027 Resolution: REMOVED SCORED LH FLIGHT SPOILER BELLCRANK PIVOT BOLT P/N: NAS1310-56D NSN AND REPLACED WITH NEW BOLT P/N: NAS1310-56D NSN RECEIVED FROM SKY MANUFACTURING INC PO# 23654 DATED 23 MAR 2000 IAIV GIV CMP 276077 OUTBOARD FLIGHT SPOILER BELLCRANK ASSEMBLY (LEFT) - REMOVALANSTALLATION. REF ITEM 13.41 FOR FINAL INSTALLATION OF OUTBOARD FLIGHT SPOILER BELLCRANK ASSEMBLY INSTALLATION. Billing Method Flours Rate Total Labor USD: Time and Material ST 0.62 @ $142.00 $88.04 Parts USD: Time and Material $157.25 Total USD: $245.29 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.4#1 NAS1310-56D BOLT I $157.25 $157.25 Discrepancy: 14.5 WHILE C/W CMP GIV 271019 AILERON ACTUATOR (LEFT) - INSPECTION FOUND THE AILERON TO BOOST BELLCRANK FITTING TO BE CORRODED AND HAVE IMPACT DAMAGE. Resolution: FOUND IMPACT DAMAGE TO BE A MINOR CHAFE. REMOVED SURFACE CORROSION WITH SCOTCHBRITE AND BLENDED MINOR CHAFE ON LH AILERON BOOST BELL CRANK FITTING IAW GIV SRM 53-13-20. APPLIED BRUSH CAD TO LH AILERON BOOST BELL CRANK FITTING AS NECESSARY IAW GAMPS 6103 REV F. PRIMED SURFACE AFTER CAD PLATING. ALL WORK DONE IAW 51-07-10 Billing Method Hours Rate Total Labor USD: Time and Material ST 1.85 @ $142.00 $262.70 Total USD: $262.70 Step: 14.5.1 Completed REMOVED SURFACE CORROSION WITH SCOTCHBRITE AND BLENDED IMPACT DAMAGE ON LH AILERON BOOST BELL CRANK FITTING IAN; GIV SRM 53-13-20. Step: 14.5.2 Completed APPLIED BRUSH CAD TO LH AILERON BOOST BELL CRANK FITTING AS NECESSARY IAW CAMPS 6103 REV F. Discrepancy: 14.6 WHILE C/W CMP 276011 L/H GROUND SPOILER ACTUATOR INSP FOUND L/H WING GROUND SPOILER ACTUATOR TO HAVE A FROZEN PISTON BEARING. Resolution: VISUALLY INSPECTED AND EXERCISED LH GROUND SPOILER ACTUATOR PISTON BEARING WITH NO DEFECTS NOTED. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.17 @ $142.00 $166.14 Total USD: $166.14 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 33 of 117 Printed: 6/28/2018 9:39:11A? Rent EFTA00808971 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 14.7 WHILE C/W 276011 Li I GROUND SPOILER ACTUATOR INSPECTION FOUND BELLCRANK PIVOT FITTING ON REAR SPAR TO HAVE LIGHT SURFACE CORROSION IN THE BORES. Resolution: REMOVED LIGHT SURFACE CORROSION FROM UPPER AND LOWER LH GROUND SPOILER ACTUATOR BELLCRANK PIVOT FITTING BORES WITH SCOTCHBRITE. MINIMAL MATERIAL LOSS WAS NOTED WORK DONE IAW GIV SRM 51-13-20. Billing Method Flours Rate Total Labor USD: Time and Material ST 2.25 @ 5142.00 $319.50 'total USD: $319.50 Discrepancy: 14.8 WHILE C/W 577007 LJH FLIGHT SPOILER HINGE INSPECTION FOUND OUTBOARD FLIGHT SPOILER OB HINGE BEARING MIGRATING OUT OF BOSS. Resolution: RQCI - REMOVED MIGRATING BEARING FROM LH FLIGHT SPOILER OUTBOARD HINGE P/N: MS28913-4C NSN, INSTALLED A NEW BEARING P/N MS28913.4C NSN REF PACKING SLIP SASH#18-78950 FROM GULFSTREAM AEROSPACE CORP DATED 5/26/18. ALL WORK DONE IAW GAC DWG 1159CSM40034 Billing Method Flours Rate Total Labor USD: Time and Material ST 2.95 @ $142.00 $418.90 Parts USD: Time and Material $106.29 Total USD: $525.19 Parts: Ret No. Part number: Description Quantity Sell price USD Extended USD 14.8#1 MS28913-4C BEARING 1 $106.29 $106.29 Step: 14.8.1 Completed REMOVED MIGRATING BEARING FROM LH FLIGHT SPOILER OUTBOARD HINGE P/N: MS28913-4C NSN IAW GAC BP II S9CSM40034 REV (B) - FITTING ASSY HINGE. Discrepancy: 14.9 WHILE C/W 577009 L/H GROUND SPOILER HINGE INSPECTION FOUND IB HINGE OB HEAR OF HINGE, BUSHING CAME OUT OF EAR WHEN REMOVING SLIP BUSHING. Resolution: THOROUGHLY CLEANED FITTING AND BORE AND DETAIL INSPECTED. BORE DIAMETER, CONCENTRICITY AND SURFACE FINISH ALL IAW GAC BP 1159CSM40051. INSTALLED NEW BUSHING PIN LS3859FR8-10 RECEIVED FROM GAC SAV UNDER ENTERPRISE TRANSFER NUMBER 000888740 DATED 05/26/2018. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.26 @ $142.00 $320.92 Parts USD: Time and Material $35.17 Total USD: $356.09 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 34 of 117 Printed: 6/28/2018 939:11M Reel EFTA00808972 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.9 #1 LS3859FR8-10 BUSHING 1 $7.92 $7.92 14.9 #2 PR1440B1-2DAB-KIT SEALANT, 50 GRAM KIT (CUP & 1 $27.25 $27.25 SYRINGE) Discrepancy: 14.10 WHILE C/W CMP CODE 537010 LEFT AFT WING / FUSELAGE FAIRING INSPECTION FOUND SEVERAL AREAS OF CORROSION ON SKIN AND SUPPORT STRUCTURE UNDERNEATH AFT WING TO FUSELAGE FAIRING. Resolution: REMOVED LIGHT SURFACE CORROSION ON LH SKIN AND SUPPORT STRUCTURE UNDERNEATH AFT WING TO FUSELAGE FAIRING AND APPLIED ALODINE. PERFORMED THICKNESS CHECKS TO FUSELAGE SKIN WHERE SURFACE CORROSION WAS REMOVED AND FOUND TO BE WITHIN LIMITS (.035 MIN NOTED, .030 ALLOWABLE). PRIMED AND PAINTED AS REQUIRED. ALL WORK DONE IAW GIV MM 53-50-00 AND SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 6.52 @ $142.00 $925.84 Parts USD: Time and Material $95.07 Total USD: $1,020.91 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.10 #1 MATTERHORN-KIT-2O KIT, 2 OZ MATTERHORN 1 $65.81 $65.81 WHITE/TOPCOAT (578-520/570-535) CAP W/O BRUSH )INTERNAL USE ONLY) 14.10 #2 515X333-2OZ KIT, TOUCH UP, EPDXY PRIMER, 2 1 $29.26 $29.26 OZ, GREEN Step: 14.10.1 Completed REMOVED LIGHT SURFACE CORROSION ON LH SKIN AND SUPPORT STRUCTURE UNDERNEATH AFT WING TO FUSELAGE FAIRING AND APPLIED ALODINE IAW GIV SRM 51-13-10. Step: 14.10.2 Completed PERFORMED THICKNESS CHECKS TO FUSELAGE SKIN WHERE SURFACE CORROSION WAS REMOVED AND FOUND TO BE WITHIN LIMITS (.035 MIN NOTED, .030 ALLOWABLE). WORK DONE IAW GIV MM 53-50-00. Discrepancy: 14.11 WHILE C/W CMP CODE 537010 LEFT AFT WING / FUSELAGE FAIRING INSPECTION FOUND AFT END OF TRAILING EDGE BOX BREATHER ANGLE IS CRACKED. Resolution: CUT OUT CRACK ON BREATHER ANGLE P/N 1159B40296-119, NSN, AND REPLACED WITH NEW BREATHER ANGLE P/N 1159B40296-119. NSN, ON L/11 WING, AFT END OF TRAILING EDGE BOX. RECEIVED FROM GULFSTREAM SAVANNAH WITH AUTHORIZATION # ODA-511131-CE. REFERENCE FORM 8130-3 WITH FORM TRACKING # 20171011023851 DATED 11 OCT 2017. REPAIRED IN ACCORDANCE WITH GIV MM 53-30-00 PG 618. Billing Method Hours Rate Total Labor USD: Time and Material ST 11.17 @ $142.00 $1,586.14 Parts USD: Time and Material $509.55 Total USD: $2,095.69 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 35 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808973 Bill To: JEGE LLC Pans: WO #: SC18654 Invoice Number: 6918002027 Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.11 #1 1159B40296-H9 ANGLE I S356.76 $356.76 14.11 #2 GAFSI IAB0S-200 FASTENER BLIND 3 58.18 $24.54 SELF-LOCKING,130DEG SHEAR 14.11 #3 MS20605S3W3 RIVET 3 S0.45 $1.35 14.11 #4 MS20605S3W4 RIVET 3 S0.51 $1.53 14.11 #5 NAS192111105-04 RIVET 7 S3.53 $24.71 14.11 #6 NAS192111105-03 RIVET 7 S6.02 $42.14 14.11 #7 515X333-2OZ KIT, TOUCH UP, EPDXY PRIMER, 2 2 $29.26 $58.52 OZ, GREEN Discrepancy: 14.12 WHILE C/W CMP CODE 537011 RIGHT AFT WING / FUSELAGE FAIRING INSPECTION FOUND SEVERAL AREAS OF CORROSION ON SKIN AND SUPPORT STRUCTURE UNDERNEATH RIGHT AFT WING TO FUSELAGE FAIRING. Resolution: REMOVED LIGHT SURFACE CORROSION ON LH SKIN AND SUPPORT STRUCTURE UNDERNEATH AFT WING TO FUSELAGE FAIRING AND APPLIED ALODINE. PERFORMED THICKNESS CHECKS TO FUSELAGE SKIN WHERE SURFACE CORROSION WAS REMOVED AND FOUND TO BE WITHIN LIMITS (.034 MIN NOTED, .030 ALLOWABLE). PRIMED AND PAINTED AS REQUIRED. ALL WORK DONE IAW GIV MM 53-50-00 AND SRM 51-13-10. Labor USD: Total USD: Step: 14.12.1 Step: 14.12.2 Billing Method Hours Rate Total Time and Material ST 6.74 ® $142.00 $957.08 Completed Completed $957.08 REMOVED LIGHT SURFACE CORROSION ON RH SKIN AND SUPPORT STRUCTURE UNDERNEATH AFT WING TO FUSELAGE FAIRING AND APPLIED ALODINE IAW GIV SRM 51-13-10. PERFORMED THICKNESS CHECKS TO FUSELAGE SKIN WHERE SURFACE CORROSION WAS REMOVED AND FOUND TO BE WITHIN LIMITS (.034 MIN NOTED, .030 ALLOWABLE). WORK DONE IAW GIV MM 53-50-00. Discrepancy: 14.13 WHILE C/W CMP CODE 537011 RIGHT AFT WING / FUSELAGE FAIRING INSPECTION FOUND AFT END OF TRAILING EDGE BOX BREATHER ANGLE IS CRACKED. Resolution: CUT OUT CRACK ON BREATHER ANGLE P/N 1159B40296-120, NSN, AND REPLACED WITH NEW BREATHER ANGLE P/N 1159B40296-120, NSN, ON R/H WING, AFT END OF TRAILING EDGE BOX. RECEIVED FROM GULFSTREAM SAVANNAH WITH AUTHORIZATION # ODA-511131-CE. REFERENCE FORM 8130-3 WITH FORM TRACKING # 20170216130503 DATED 16 FEB 2017. REPAIRED IN ACCORDANCE WITH GIV MM 53-30-00 PG 618. Labor USD: Parts USD: Total USD: Billing Method Flours Rate Total Time and Material ST 9.96 ® $142.00 $1,414.32 Time and Material $282.67 $1,696.99 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 36 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00808974 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Pans: Ref'. No. Part number: Description Quantity Sell price USD Extended USD 14.13 #1 1159640296-120 ANGLE 1 $282.67 $282.67 Discrepancy: 14.14 WHILE C/W CMP CODE 276034 R/H FLIGHT SPOILER ACTUATOR INSPECTION FOUND R/H FLIGHT SPOILER ACTUATOR WING ATTACH POINT BUSHINGS CORRODED. Resolution: RQCI - REMOVED CORRODED R/H FLIGHT SPOILER ACTUATOR WING ATTACH POINT BUSHINGS X2 WITH P/N UNK, NSN. INSTALLED NEW R/H FLIGHT SPOILER ACTUATOR WING ATTACH POINT BUSHINGS X2 WITH P/N 11595B30210-67 NSN. REFERENCE 8130-3 WITH FORM TRACKING # 20150119071140 DATED 19 JAN 2015 FROM GULFSTREAM AEROSPACE CORP APPROVAL# ODA-511131-CE . ALL WORK DONE IAW 1159WM30808 REV C Billing Method flours Rate Total Labor USD: Time and Material ST 4.15 @ $142.00 $589.30 Parts USD: Time and Material $131.98 Total USD: $721.28 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.14 #1 1159SB30210-67 BUSHING 2 $51.36 $102.72 14.14 #2 515X333-2OZ KIT, TOUCH UP, EPOX1 PRIMER. 2 1 $29.26 $29.26 OZ, GREEN Discrepancy: 14.15 WHILE C/W CMP CODE 577010 R/H GROUND SPOILER / HINGE INSPECTION FOUND R/H GROUND SPOILER BOARD INBOARD ATTACH POINT BEARING DOES NOT ROTATE. Resolution: LUBED BEARING AND FOUND TO BE SERVICEABLE WORK DONE IAW GIV MM 27-02-00. Billing Method Hours Rate Total Labor USD: Time and Nlaterial ST 1.22 @ $142.00 $173.24 Total USD: $173.24 Discrepancy: 14.16 WHILE C/W CMP CODE 577010 R/H GROUND SPOILER / HINGE INSPECTION FOUND R/H GROUND SPOILER BOARD OUTBOARD ATTACH FITTING ON REAR BEAM IS CORRODED ON TOP. Resolution: REMOVED SURFACE CORROSION FROM TOP OF R/H GROUND SPOILER BOARD OUTBOARD ATTACH FITTING ON REAR BEAM BY MECHANICAL MEANS WITH SOFT ABRASIVE PAD. VISUALLY INSPECTED WITH MINIMAL MATERIAL LOSS AND NO FURTHER DEFECTS NOTED. WORK DONE IAW GIV SRM 51-13-23.APPLIED BRUSH CAD TO TOP OF R/H GROUND SPOILER BOARD OUTBOARD ATTACH FITTING ON REAR BEAM IAW GAMPS 6103 REV F. PRIMED ALL AFFECTED SURFACES JAW GIV SRM 51-07-10. 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 37 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00808975 Bill To: JEGE LLC Billing Method WO It: SC18654 Hours Rate Invoice Number: 6918002027 Total Labor USD: Time and Material ST 4.67 @ $142.00 $663.14 Parts USD: Time and Material $304.18 Total USD: $967.32 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.16 #1 11904010 ID-10P POLY JACKET IS/PKI I 50.011 $0.00 14.16 #2 2023 SOLUTION,PLATING,DALIC 1 $304.18 $304.18 CADMIUM,1 LTR Step: 14.16.1 Completed REMOVED SURFACE CORROSION FROM TOP OF Rill GROUND SPOILER BOARD OUTBOARD ATTACH FITTING ON REAR BEAM BY MECHANICAL MEANS WITH SOFT ABRASIVE PAD. VISUALLY INSPECTED WITH MINIMAL MATERIAL LOSS AND NO FURTHER DEFECTS NOTED. WORK DONE IAW GIV SRM 51-13-23. Step: 14.16.2 Completed APPLIED BRUSH CAD TO TOP OF FUN GROUND SPOILER BOARD OUTBOARD ATTACH FITTING ON REAR BEAM IAW CAMPS 6103 REV F. Discrepancy: 14.17 WHILE C/W CMP CODE 577010 R/H GROUND SPOILER / HINGE INSPECTION FOUND R/H GROUND SPOILER BOARD HAT BUSHING IN HOLE ID 1-3 IS TOO SHORT. Resolution: REMOVED R/H GROUND SPOILER BOARD HAT BUSHING IN HOLE ID 1-3. RECEIVED O.K. TO INSTALL AND INSTALLED A NEW BUSHING P/N GABI0C10-15 NSN. REFERENCE FAA FORM 8130-3 WITH FORM TRACKING NUMBER 20180509155322 FROM GULFSTREAM AEROSPACE CORPORATION DATED 09 MAY 2018 APPROVAL/AUTHORIZATION NO.: ODA-511131-CE. ALL WORK DONE JAW GAC DWG 1159CSM40048 REV A. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.63 @ $142.00 $231.46 Parts USD: Time and Material $48.13 Total USD: $279.59 Parts: Ref'. No. Part number: Description Quantity Sell price USD Extended USD 14.17 #2 GABI0CI0-15 BUSHING 1 $48.13 $48.13 Discrepancy: 14.18 WHILE C/W CMP CODE 577006 R/H INBOARD FLIGHT SPOILER / HINGE INSPECTION FOUND CORROSION ON UPPER AND LOWER SURFACES OF R/H INBOARDS SPOILER BOARD. Resolution: FOUND SPOILER TO REQUIRE REPLACEMENT DUE TO REPAIR REQUIEMENTS/DOWNTIME. SEE ITEM 11.5 (ASC 456) FOR UPGRADE REF ITEM 13.61 FOR REMOVALAND REPLACEMENT OF I/11 Ft/Fl FLIGHT SPOILER. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.97 @ $142.00 $563.74 Parts USD: Time and Material 525,747.13 Total USD: 526.310.87 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 38 of 117 Printed: 6/28/2018 9:39:11AI Ref: EFTA00808976 Bill To: JEGE LLC Pans: Rd: No. Part number: WO #: SC18654 Description Invoice Number: 6918002027 Quantity Sell price USD Extended USD 14.18 “1 II59CS40701-10 SPOILER ASSY. FLIGHT INBD RH 1 $25,130.66 $25,130.66 14.18 #2 MS24665-302 COTTER PIN 2 50.23 $0.46 14.18 #3 MS27039-0811 SCREW-MACHINE, PAN HD, CROSS 2 50.25 $0.50 REC 14.18 :;4 ASC456-I G4 KIT, WING SPOILER BOARD 1 $610.00 $610.00 14.18 #5 MS24665-153 PIN, COTTER 6 $0.22 $132 14.18 #6 MS14183P-C8 WASHER 1 $4.19 4.19 S Discrepancy: 14.19 WHILE C/W GIV CMP 576011 AILERON HINGE FITTING (LEFT) INSPECTION NOTED MIDDLE HINGE FITTING HAS A BAD BEARING. Resolution: RQCI REMOVED DEFECTIVE LH AILERON MIDDLE HINGE FITTING BEARING P/N: MS28913-4C NSN. CLEANED AND VISUALLY INSPECTED FITTING WITH NO DEFECTS NOTED. MEASURED INSIDE DIAMETER AND OBTAINED READING OF (.9012"). WORK PERFORMED IAW GAC BP 1159WM20202 - FTG (RBS 375 & 406) AILERON HINGE OUTBD - REV (F). APPLIED BRUSH CAD TO I.D. OF LH AILERON MIDDLE HINGE FITTING IAW GAMPS 6103 REV F. INSTALLED NEW BEARING P/N MS28913-4C NSN REF PACKING SLIP NUMBER SASH#18-78949 FROM GULFSTREAM AEROSPACE CORP DATED 5/26/2018 ALL WORK DONE IAW GAC DWG 1159WM20202 - FTG (RBS 375 & 406) AILERON HINGE OUTBD - REV (F). Labor USD: Parts USD: Total USD: Pans: Billing Method Flours Rate Total Time and Material ST 3.93 (§ $142.00 $558.06 Time and Material $108.93 $666.99 Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.19 #1 M528913-4C BEARING $106.29 $106.29 14.19 #2 M520615-5MPI3 RIVET 4 $0.22 50.88 14.19 #3 M520615-5MPI3 RIVET 8 $0.22 S1.76 Step: 14.19.1 Step: 14.19.2 Step: 14.19.3 Completed Completed Completed REMOVED DEFECTIVE LH AILERON MIDDLE HINGE FITTING BEARING P/N: M528913-4C NSN. CLEANED AND VISUALLY INSPECTED FITTING WITH NO DEFECTS NOTED. MEASURED INSIDE DIAMETER AND OBTAINED READING OF (.9012"). WORK PERFORMED IAW GAC BP 1159WM20202 - FTG (RBS 375 & 406) AILERON HINGE OUTBD - REV (F). APPLIED BRUSH CAD TO I.D. OF LH AILERON MIDDLE HINGE FITTING IAW GAMPS 6103 REV F. INSTALLED NEW BEARING PIN MS28913-4C NSN REF PACKING SLIP NUMBER SASH#18-78949 FROM GULFSTREAM AEROSPACE CORP DATED 5/26/2018 ALL WORK DONE IAW GAC DWG 1159WM20202 Discrepancy: 14.20 WHILE C/W GIV CMP 576011 AILERON HINGE FITTING (LEFT) - INSPECTION NOTED #3 OUTBOARDMOST HINGE FITTING TO HAVE CORROSION IN MOUNTING HOLE. 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 39 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808977 Bill To: JEGE LLC Resolution: RQCI: PERFORMED REPAIR SE05000102-913D6-20 TO LH #3 AILERON HINGE FITTING P/N 1159WM20202-5. BORE MEASURES .4065, INSTALLED SE05000901-913D6-20 BUSHING. WO #: SC18654 Invoice Number: 6918002027 WORK DONE IAW GAC DWG SE05000901 REV E. REF STEPS BELOW FOR FURTHER DETAILS. THIS IS A MAJOR REPAIR, REF ITEM 14.70 FOR 8100-9 APPROVAL AND 337 INFO. Labor USD: Parts USD: Total USD: Pans: Ref. No. Billing Method Hours Rate Total Time and Material ST 4.16 @ $142.00 $590.72 Time and Material $752.02 Part number: Description 14.20 #2 SE05000901-913D6-20 DOG-SLEEVE BUSHING 14.20 #4 44GN01I-3OZ TOUCHUP KIT,DEFT EPDXY SPRAY PRIMER Step: 14.20.1 Step: 14.20.2 Step: 14.20.3 Completed Completed Completed $1,342.74 Quantity Sell price USD Extended USD 1 5697.49 $697.49 1 $54.53 $54.53 REAMED LH AILERON #3 HINGE FITTING PIN: 1159WM20202-5 FROM NOMINAL (0.3125") TO 0.4065" TO INSTALL SE05000901-913D6-20 REPAIR BUSHING. WORK PERFORMED IAW GAC BP SE05000102 REV E - STD. REPAIR - CONTROL SURFACE HINGE FITTINGS. BRUSH CAD PLATING REQUIRED OF #3 HINGE FITTING BORE IAW CAMPS 6103 REV F RECEIVED REPAIR DOG SLEEVE BUSHING P/N: SE05000901-913D6-20 NSN FROM GAC-SAV PURCHASE ORDER SAP014-49961 DATED 26 MAR 2015. WITH INSPECTORS APPROVAL INSTALLED DOG SLEEVE BUSHING INTO II59WM20202-5 AILERON HINGE FITTING. WORK PERFORMED IAW GAC BP SE05000102 REV E - STD. REPAIR - CONTROL SURFACE HINGE FITTINGS. Discrepancy: 14.21 WHILE C/W GIV CMP 576012 AILERON HINGE FITTING (RIGHT) - INSPECTION NOTED THE #1 INBOARD MOST HINGE FITTING MOUNTING HOLES TO BE OUT OF TOLERANCE. INDEX NUMBERS 1-1 THRU 1-3. Resolution: RQCI PERFORMED FIRST INCREMENT OS REPAIR TO LH AILERON #1 HINGE HOLES (3 PLACES). BORES MEASURE .3280, INSTALLED NA56605D40X, NAS6605D54X, AND NAS6605D66X O/S HARDWARE. WORK DONE IAW GAC DWG SE05000901 REV E. REF STEPS BELOW FOR FURTHER DETAILS. THIS IS A MAJOR REPAIR, REF ITEM 14.70 FOR 8100-9 APPROVAL AND 337 INFO. Labor USD: Parts USD: Time and Material Total USD: Pans: Ref. No. Part number: Description 14.21 #1 NAS6605D40X 14.21 #2 NAS6605D54X 14.21 #3 NAS6605D66X BOLT BOLT, OVERSIZED BOLT Billing Method Hours Rate Total Time and Material ST 3.40 @ $142.00 $482.80 $507.84 $990.64 Quantity Sell price USD For detail description of the work complied with see the Work Order Detail report. S93.82 $174.02 $240.00 Extended USD $93.82 $174.02 $240.00 Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 40 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00808978 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Step: 14.21.1 Completed OVERSIZED AILERON HINGE HOLES AND AILERON ATTACH FITTING HOLES TO THE FIRST BOLT OVERSIZE 03280 .IAW GAC DRAWING SE05000102.TIIIS IS CONSIDERED A MAJOR REPAIR. Discrepancy: 14.22 WHILE C/W 271024 RH AILERON BOOST BELLCRANK INSP FOUND BOTH BEARINGS FROZEN ON THE INNER BELLCRANK OF THE BOOST BELLCRANK ASSEMBLY Resolution: RQCI INSTALLED TWO NEW BEARINGS P/N MS27646-38 NSN AND ONE NEW SPACER ASSEMBLY P/N 1159C20213-5 NSN. REFERENCE GULFSTREAM PACKING SLIP WITH ENTERPRISE TRANSFER NUMBER 0008900208 DATED 06/01/2018 FROM GULFSTREAM SAVANNAH FOR BEARINGS. REFERENCE GULFSTREAM PACKING SLIP WITH ENTERPRISE TRANSFER NUMBER 000890283 DATED 06/01/2018 FROM GULFSTREAM SAVANNAH FOR SPACER ASSEMBLY. ALL WORK DONE IAW GAC DRAWING 1159CM20216 REV D. Labor USD: Parts USD: Total USE): Parts: Billing Method Hours Rate Total Time and Material ST 0.98 @ $142.00 $139.16 Time and Material $482.60 $621.76 Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.22 #1 MS27646-38 BEARING 2 $48.64 $97.28 14.22 #2 1159C20213-5 SPACER ASSEMBLY 1 $385.32 $38532 Step: 14.22.1 Completed UPON INVESTIGATION FOUND BOTH BEARINGS AND INNER SPACER TUBE UNSERVICABLE. REMOVED 2 EA BEARINGS P/N MS27646-38 NSN AND 1 EA SPACER P/N 1159C20213-5. CLEANED AND INSPECTED BELLCRANK AND FOUND TO BE SERVICABLE. WORK DONE IAW GAC DWG 1159CM20217 Discrepancy: 14.23 WHILE C/W 271024 RH AILERON BOOST BELLCRANK INSP FOUND THE SMALL BEARING FROZEN ON THE OUTER BELLCRANK OF THE BOOST BELLCRANK ASSEMBLY Resolution: RECEIVED A NEW RH AILERON BOOST BELLCRANK BEARING P/N MS27646-38 NSN. REFERENCE PACKING SLIP WITH ENTERPRISE TRANSFER NUMBER 000890592 FROM GULFSTREAM SAVANNAH DATED 06/04/2018. SENT BELLCRANK, P/N 1159CM20217-10 TO GAC SAV FOR REPAIR (BEARING INSTALLATION). RECEIVED REPAIRED BELLCRANK, P/N 1159CM20217-10. REF GAC SAV, CERT# GR4R216M, 8130-3, DATED 17 JUNE 2018 WITH TRACKING# 20180617114330. Labor USD: Parts USD: Services USD: Total USD: Pans: Ref. No. Billing Method Hours Rate Total Time and Material ST 1.27 @ $142.00 Time and Material Time and Material Part number: $180.34 $48.64 $740.27 $969.25 Description Quantity Sell price USD 14.23 #2 MS27646-38 BEARING Services: Extended USD 1 $48.64 Ref. No. Description Quantity Sell Price USD 1.00 5740.27 14.23 #2 GAC REPAIRS Pon Ref: 1159CM20217-10 BELLCRANK ASSEMBLY, AIL For detail description of the work complied with see the Work Order Detail report. $48.64 Extended USD $740.27 Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminarylnvoice.rpt 2011 Page 41 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808979 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Step: 14.23.1 Completed REMOVED UNSERVICABLE BEARING P/N MS27646-38 NSN IAW GAC DWG 1159CM20217, REV F. INSPECTED CRANK BORE AND FOUND TO BE SERVICABLE. Discrepancy: 14.24 WHILE C/W 271024 RH AILERON BOOST BELLCRANK INSP FOUND THE OUTER BELLCRANK CHAFED AROUND THE SMALL BEARING EAR OF THE BOOST BELLCRANK ASSEMBLY. Resolution: REMOVED CHAFE FROM Ft/H AILERON BOOST BELLCRANK. CLEANED AND PRIMED AFFECTED AREA. ALL WORK DONE JAW GIV SRM 51-07-10. Labor USD: Total USD: Billing Method Hours Rate Total Time and Material ST 0.92 @ $142.00 $130.64 $130.64 Discrepancy: 14.25 WHILE C/W CMP 273008 FOUND HEAVY CORROSION ON LANDING UNDER PANEL 38-TE-UPR-1 Resolution: CAREFULY REMOVED CORROSION FROM STRAP. DURING REMOVAL OF CORROSION NOTED THAT CORROSION APPEARED TO EXTEND UNDER UPPER SKIN. REMOVED FASTENERS TO ALLOW INSPECTION UNDER SKIN. VERY MINOR SURFACE CORROSION NOTED AND REMOVED. ALL WORK IAW GIV SRM 51-13-00. THE POST BLEND THICKNESS MEASUREMENTS ON THE 1159CSM20163 DOUBLER/STRAP ARE STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. ALL EVIDENCE OF CORROSION HAS BEEN REMOVED, LOCALLY HAND PASSIVATED USING CLEAN SCOTCH BRITE PADS AND TOUCHED UP WITH ZINC DUST PRIMER (MIL-P-26915) FOLLOWED BY (2) COATS OF 3012 EPDXY PRIMER. INSTALLED NEW FASTENERS PREVIOUSLY REMOVED. APPLIED NEW BED SEALANT TO PANEL LANDING. ALL WORK IAW GIV SRM 55-10-00 AND ENGINEERING DISPOSITION SC18654 14.25.4. SEE STEPS FOR DETAILS. Billing Method Hours Rate Total Labor USD: Time and Material ST 20.50 @ $142.00 $2,911.00 Labor USD: Time and Material ST 1.50 @ $231.00 $346.50 Parts USD: Time and Material $126.41 Misc Charges USD: Time and Material $231.00 Total USD: $3,614.91 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.25 #2 NAS1097AD4-3 RIVET 7 $0.23 $1.61 14.25 #3 GAS530D10-3 SLEEVE-BLIND NUT,100 DEC CSK 4 $16.02 $64.08 14.25 #4 GAE530A10 BOLT, BLIND, EXPANDER 4 $531 $21.24 14.25 #5 NAS1200h14-5 RIVET, 100 DEG COUNTERSUNK 7 $0.23 $1.61 REDUCED 14.25 #6 NAS1097E5-6 RIVET 4 $2.80 $11.20 14.25 #7 PR1440B1-2-654 SEALANT,6OZ #654 SEMK1T 1 $26.67 $26.67 Miscellaneous Charge: Ref. No. Miscellaneous Charge Amount USD 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 42 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808980 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Miscellaneous Charge: Ref. No. Miscellaneous Charge 14.25 #1 NDT LABOR Step: 14.25.1 Completed Step: 14.25.2 Step: 14.25.3 Step: 14.25.4 Amount USD CAREFULY REMOVED CORROSION FROM STRAP. DURING REMOVAL OF CORROSION NOTED THAT CORROSION APPEARED TO EXTEND UNDER UPPER SKIN. REMOVED FASTENERS TO ALLOW INSPECTION UNDER SKIN. VERY MINOR SURFACE CORROSION NOTED AND REMOVED. ALL WORK IAW G IV SRM 51-13-00. Completed PERFORMED ULTRASONIC THICKNESS TESTING OF STRAP AFTER REMOVAL OF HEAVY CORROSION. INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL 2.0. ULTRASONIC REVISION 7 - DECEMBER 15TH, 2017. MEASUREMENTS WRITTEN ON MASKING TAPE ON AIRCRAFT. Completed REQUEST ENGINEERING EVALUATION OF REMAINING STRAPTHICKNESS FOR SERVICABILITY. Completed ENGINEERING DISPOSITION: THE POST BLEND THICKNESS MEASUREMENTS ON THE 1159CSM20163 DOUBLER/STRAP ARE STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. IFALL EVIDENCE OF CORROSION HAS BEEN REMOVED, LOCALLY HAND PASSIVATE USING CLEAN SCOTCH BRITE PADS AND TOUCH UP WITH BRUSH CAD PLATE OR ZINC DUST PRIMER (MIL-P-26915) FOLLOWED BY (2) COATS OF 3012 EPDXY PRIMER. Step: 14.25.5 Completed HAND PASSIVATED USING CLEAN SCOTCH BRITE PADS AND TOUCHED UP ZINC DUST PRIMER (MIL-P-26915) FOLLOWED BY (2) COATS OF 3012 EPDXY PRIMER. ALL WORK lAW ENGINEERING DISPOSITION SCO118654 14.25.4. $231.00 Discrepancy: 14.26 WHILE C/W CMP 273008 FOUND CORROSION IN D-RING ON R/H SIDE OF THE HORIZONTAL Resolution: REMOVED LIGHT SURFACE CORROSION FROM R/H HORIZONTAL D-RING BY LIGHT HAND SANDING WITH NO MATERIAL LOSS. ALL WORK DONE IAW GIV SRM 51-13-23. Labor USD: Total USD: Billing Method Hours Rate Total Time and Material ST 4.04 ® $142.00 $573.68 $573.68 Discrepancy: 14.27 WHILE C/W 271020 AND 271019 L/H AILERON ACTUATOR INSPECTION FOUND ANTI TORSION BUMPERS TO BE WORN OR MISSING. Resolution: INSTALLED FOUR NEW ANTI TORSION BUMPERS P/N 87048 REFERENCE CERTIFICATE OF CONFORMANCE WITH PACKING LIST # SASH#18-79226 DATED 29-MAY-2018 FROM GULFSTREAM AS REQUIRED. NO DEFECTS NOTED. WORK DONE lAW GIV MM 27-02-00 Labor USD: Parts USD: Billing Method Flours Rate Total Time and Material ST 1.02 ® $142.00 $144.84 Time and Material $116.36 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_WorkOrderPrelintinarylnvoice.rpt 2011 Page 43 of 117 Printed: 6/28/2018 939:11A? Reel EFTA00808981 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Total USD: $261.20 Parts: Ret No. Part number: Description Quantity Sell price USD Extended USD 14.27 #1 87048 PLUG 4 $29.09 $116.36 Discrepancy: 14.28 WHILE C/W 271020 RH AILERON ACTUATOR INSPECTION FOUND ACTUATOR MOUNT FITTING TO BE MISSING PRIMER. Resolution: APPLIED PRIMER ACTUATOR MOUNT FITTING AND OTHER AREAS IN CLOSE PROXIMITY. ALL WORK DONE IAW GIV SRM 51-07-10 Billing Method Hours Rate Total Labor USD: Time and Material ST 0.53 @ $142.00 $75.26 Total USD: $75.26 Discrepancy: 14.29 WHILE C/W 577007 L/H SPOILER HINGE INSPECTION FOUND L/H GROUND SPOILER BOND WIRE BROKEN. Resolution: REMOVED BROKEN BOND WIRE FROM GROUND SPOILER HINGE NPN NSN AND INSTALLED NEW BOND WIRE P/N M83413-8A004BB RECEIVED FROM GAC BAF STOCK. ALL WORK DONE IAW GIV AMM 20-24-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.00 @ $142.00 $142.00 Parts USD: Time and Material $4.98 Total USD: $146.98 Pans: Ret No. Part number: Description Quantity Sell price USD Extended USD 14.29#I M8341341A004BB JUMPER CABLE ASSY 2 $2.49 $4.98 Discrepancy: 14.30 WHILE C/W CMP 273007 FOUND HEAVY CORROSION ON LANDING UNDER PANEL 37-TE-UPR-1 Resolution: CAREFULLY REMOVED ALL CORROSION ON PANEL LANDING. THE POST BLEND THICKNESS MEASUREMENTS ON THE 1159CSM20163 DOUBLER/STRAP ARE STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. ALL EVIDENCE OF CORROSION HAS BEEN REMOVED, LOCALLY HAND PASSIVATED USING CLEAN SCOTCH BRITE PADS AND TOUCHED UP WITH ZINC DUST PRIMER (MIL-P-26915) FOLLOWED BY (2) COATS OF 3012 EPDXY PRIMER. APPLIED NEW BED SEALANT TO PANEL LANDING. ALL WPORK lAW G IV SRM 55-10-00 AND ENGINEERING DISPOSITION SC18654 14.25.4. SEE STEPS FOR DETAILS.. 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 44 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00808982 Bill To: JEGE LLC WO #: SC 18654 Invoice Number: 6918002027 Labor USD: Parts USD: Total USD: Parts: Billing Method Hours Rate Total Time and Material ST 15.06 @ $142.00 $2,138.52 Time and Material S7.72 $2.146.24 Ref. No. Part number: Description Quantity Sell price USD Extended USD 1430 #1 MS20426E5-4 RIVET 4 $1.93 $7.72 Step: 1430.1 Completed CAREFULY REMOVED CORROSION FROM STRAP. NDT THICKNESS CHECKS PERFORMED WITH SATESFACTORY RESULTS. PROTECTED ALL BARE METAL WITH 3012 PRIMER. ALL WORK IAW G IV SRM 51-13-00. Step: 1430.2 Completed PERFORMED ULTRASONIC THICKNESS TESTING OF STRAP AFTER REMOVAL OF HEAVY CORROSION. INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL 2.0. ULTRASONIC REVISION 7 - DECEMBER 15TH, 2017. MEASUREMENTS WRITTEN ON MASKING TAPE ON AIRCRAFT. Step: 1430.3 Completed HAND PASSIVATED USING CLEAN SCOTCH BRITE PADS AND TOUCHED UP WITH ZINC DUST PRIMER (MIL-P-26915) FOLLOWED BY (2) COATS OF 3012 EPDXY PRIMER. ALL WORK IAA` ENGINEERING DISPOSITION SC18654 14.25.4. Discrepancy: 1431 WHILE C/W CNIP GIV 576015 AILERON TRIM TAB HINGE FITTING - INSPECTION NOTED WORN #2 HINGE UPPER OUTBOARD AILERON TRIM TAB BUSHING. (NOTE - THIS IS A REPAIR BUSHING FROM PREVIOUS OS REPAIR) Resolution: RQCI. REMOVED #2 FITTING OUTBOARD HINGE REPAIR BUSHING. RECEIVED OK TO INSTALL AND INSTALLED A NEW AILERON TRIM TAB #2 FITTING OUTBOARD HINGE REPAIR BUSHING P/N SE05813103-41. REF COC WITH PACKING LIST # SAP018-03701 DATED 1-25-18 FROM GULFSTREAM AEROSPACE CORP. ALL WORK DONE IAW GAMPS 2226 Labor USD: Parts USD: Total USD: Billing Method Hours Rate Total Time and Material ST 1.00 @ $142.00 $142.00 Time and Material $26635 $40835 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 1431 #1 SE05813103-41 REPAIR BUSHING Step: 1431.1 1 $26635 $26635 Completed REMOVED AILERON TRIM TAB. REMOVED #2 FITTING OUTBOARD HINGE REPAIR BUSHING. WORK PERFORMED IAW GAC DWG SE05813103 - BUSHING RPR - AILERON TRIM TAB HINGE FITTINGS REV (A). Discrepancy: 14.32 WHILE C/W CMP GIV 272011 RUDDER ACTUATOR & FWD ATTACH FITTING - INSPECTION NOTED I.JH FWD ATTACH FITTING TO BE ELONGATED BEYOND MM LIMITS. Resolution: RQCI: COMPLIED WITH REWORK OF RUDDER ACTUATOR FORWARD ATTACH FITTING -901 INST. I/A/W GAC DRAWING# 1159RDB729, NO REV. THIS IS A MAJOR REPAIR AND IS SUBSTANTIATED BY FAA 8100-9, DATED 06/15/2018, PROJECT NO. TR-07-2018-0014 FROM GAC SAV AUTHORIZATION# ODA-511131-CE, CERT 0336099. EXECUTED FAA FORM 337 DATED JUN 26, 2018. SEE STEPS FOR DETAILS. 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 45 of 117 Printed: 6/28/2018 939:11A1 Ref: EFTA00808983 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Labor USD: Parts USD: Total USD: Pans: Billing Method Time and Material Time and Material I lours Rate Total ST 1138 @ $142.00 $1,615.96 $46.74 $1,662.70 Ref. No. Part number: Description Quantity Sell price USD Extended USD 1432 #2 AISI4340 BAR,ROUND,2 IN DIA,SS 4 58.96 $35.84 1432 #3 NAS1307-12D BOLT 1 S0.00 $0.00 1432 #4 NA56607D14 BOLT S10.90 $10.90 Step: 1432.1 Completed FABRICATED 2 EA PIN 1159RDB729-9Il OUT OF 4340 STEEL LOT # LT06-124493 I.A.W. DWG#1159FtDB729 Step: 1432.2 Completed REQUEST ENGINEERING: REQUEST USE OF GAC BP 1159RDB729 ON AIRCRAFT G IV SIN 1085. FINAL DIMENSIONS OF ATTACH BORES .6320. Step: 1432.3 Completed ENGINEERING DISPOSITION: REWORK IAW 1159RDB729-901 (REV -) REWORK - RUDDER. THIS IS A MAJOR REPAIR AND WILL REQUIRE AN 8100-9 FAA APPROVAL Step: 1432.4 Completed RQCI: REMOVED FWD BOLT FROM RUDDER ACTUATOR AND FWD BOLT FROM SERVO INPUT LINK TO FACILITATE REMOVAL OFACTUATOR FROM FWD FITTING. REAMED HOLES IN FITTING. WET INSTALLED 2 EA REPAIR BUSHINGS, P/N II 59RDB729-911. WORK DONE I/A/W GAC BP 1159RDB729, NO REV. INSTALLED ACTUATOR INTO FWD FITTING AND INSTALLED ORIGINAL SERVO INPUT LINK BOLT AND TEMPORARILY INSTALLED ORIGINAL FWD MOUNT BOLT. Step: 1432.5 Completed INSTALLED NEW ACTUATOR FWD ATTACH BOLT WITII PART NUMBER NAS6607D14. NSN. REFERENCE GULFSTREAM PACKING SLIP WITH SASH #18-90183 DATED 06118/2018. ALL WORK DONE IAW AMM 27-03-00. TQ WRENCH ID 1698000 NEXT CAL DUE 6/142019 Step: 14.32.6 Completed MAJOR REPAIR 1159RDB729 REV NC DATED 1-07-82 APPROVED BY FORM 8100-9 FAA PROJECT # TR-07-2018-0014 CERT 0336099 DATED 6-15-2018. Discrepancy: 14.33 WHILE C/W CMP GIV 272011 RUDDER ACTUATOR & FWD ATTACH FITTING - INSPECTION NOTED RUDDER ACTUATOR TO HAVE SIGNS OF SKYDROL LEAKING THAT WILL REQUIRE FURTHER EVALUATION. Resolution: OPERATED RUDDER ACTUATOR UNDER L&R HYDRAULIC SYSTEM POWER FOR 30 COMPLETE CYCLES AND NOTED NO EVIDENCE OF LEAKAGE IAW GIV MM 29-00-00. Labor USD: Total USD: Billing Method Hours Rate Total Time and Material ST 3.42 ® $142.00 $485.64 $485.64 Discrepancy: 14.34 WHILE C/W CMP CODE 273003 ELEVATOR FREEPLAY INSPECTION FOUND LJH ELEVATOR PLAY OUT OF LIMITS AT 5/16" (LIMIT IS 1/4") , AND R/H ELEVATOR PLAY AT LIMITS AT 1/4" 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 46 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00808984 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Resolution: RQCI: DISSASSEMBLED L/H ELEVATOR HORN FITTING. MEASURED AND REMOVED ALL BUSHINGS FROM HORN AND UNIVERSAL ELEVATOR FITTINGS. RECIEVED 4 NEW LH ELEVEVATOR "A4" BUSHINGS P/N 1159CSM20095-15 FROM GAC STOCK AND MACHINED FACES TO .0625. RECEIVED 2 NEW BUSHINGS P/N 159CSM20095-11 FROM GAC STOCK AND MACHINED FACES TO .0720. RECEIVED 2 NEW LH ELEVATOR "A2" BUSHINGS P/N 1159CSM20095-21 FROM GAC STOCKAND MACHINED FACES TO .0720. INSTALLED ALL 8 NEW BUSHINGS MENTIONED ABOVE IN LEFT ELEVATOR HORN AND UNIVERSAL FITTING. ALL WORK IAW GAC BP 1159CSM20066REV F AND CAMPS 2226 REV B. REMOVED WORN LH ELEVATOR "Al" BUSHING P/N 1159CSM20095-1 FROM HORN AND REPLACED WITH NEW BUSHING P/N 1159CSM20095-1, RECEIVED FROM GAC SAV REF PACKING SLIP ENTERPRISE TRANSFER NUMBER 000891952, DATED 6/7/2018. REF ITEMS SC18654.14.45 AND SC18654.14.46 FOR NEW BUSHING INSTALLATION ON RIGHT ELEVATOR. VERIFIED LEFT AND RIGHT ELEVATOR FREEPLAY TO BE WITHIN LIMITS PER GIV MM, CH. 27-01.00. Billing Method Hours Rate Total Labor USD: Time anti Material ST 7.64 ® $142.00 $1.084.88 Parts USD: Time anti Material $1.371.42 Total USD: $2,456.30 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.34 #1 II59CSM20095-11 BUSHING 4 $79.55 $318.20 14.34 #2 II59CSM20095-15 BUSHING 8 $90.91 $727.28 14.34 #3 II59CSM20095-21 BUSHING 4 $17.73 $70.92 14.34 #4 II59CSM20095-1 BUSHING I $47.51 $47.51 14.34 #5 44GN011-3O1 TOUCHUP KIT,DEFT EPDXY SPRAY 1 $54.53 $54.53 PRIMER 14.34 #6 NASI306-52DH BOLT I $49.28 $49.28 14.34 #7 MS20002C6 WASHER 4 $0.70 $2.80 14.34 #8 II59CSM20094-25 SLEEVE 1 $61.98 $61.98 14.34 #9 II59CS20000-21 NUT 1 $34.73 $ ..9736 14.34 #I0 MS24665-I53 PIN, COTTER 18 $0.22 1334 14.34 #I1 MS24665-304 COTTER PIN I $0.23 0.23 $ 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 47 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00808985 Bill To: JEGE LLC Step: 1434.1 Step: 1434.2 Step: 14.34.3 Step: 14.34.4 Step: 1434.5 WO it: SC18654 Invoice Number: 6918002027 Completed RECEIVED 2 EA P/N 1159CSM20095-21 AND TURNED DOWN THE FACE FROM .10125 TO FINAL liAT THICKNESS OF .071-.072, RECEIVED 2 EA OF PIN 1159CSM20095-11 AND TURNED DOWN THE FACE FROM .10125 TO FINAL HAT THICKNESS OF .071-A72, RECIEIVED 4 EA OF PIN 1159CSM20095-15 AND TURNED THEM DOWN FROM .101 TO FINAL HAT THICKNESS OF .0625-.0635. ALL WORK DONE IAW GAC DWG 1159CSM20066 REV F. Completed RQCI: DISSASSEMBLED VII ELEVATOR HORN FITTING. MEASURED AN REMOVED ALL BUSHINGS FROM HORN AND UNIVERSAL ELEVATOR FITTINGS. RECIEVED 4 NEW BUSHINGS PIN 1159CSM20095-15 FROM GAC STOCK AND MACHINED FACES TO .0625. RECEIVED 2 NEW BUSHINGS P/N 159CSM20095-21 FRM GAC STOCK AND MACHINED FACES TO .0720. RECEIVED 2 BUSHINGS PIN 1159CSM20095-2I FROM GAC STOCKAND MACHINED FACES TO .0720. INSTALLED NEW BUSHINGS IN ELEVATOR HORN AND UNIVERSAL FITTING. ALL WORK IAW GAC BP I159CSM20066REV F AND GAMPS 2226 REV B. Waiting VERIFIED ELEVATOR FREEPLAY TO BE WITHIN LIMITS PER GIV MM, CII. Insp 27-01-00. Completed RQCI: REMOVED WORN BUSHING PIN 1159CSM20095-1 FROM HORN AND REPLACED WITH NEW BUSHING PIN 1159CSIV120095-1: RECEIVED FROM GAC SAV UNDER ENTERPRISE TRANSFER NUMBER 000891952 DATED 61712018. ALL WORK IAW GAC BP 1159CSM20066, REV F AND CAMPS 2226 REV B. Completed STEP ADDED TO DOCUMENT CERTS USED ON PARTS INSTALLED IN STEPS: 4EA NEW BUSHING P/N 1159CSM1120095-15, NSN, REF FAA 8130-3 FORM TRACKING NO. 20160525083830, ISSUED BY GAC-SAV, APPROVAL NO. ODA-511131-CE, DATED 25 MAY 2016. 2EA NEW BUSHING P/N 1159CSM20095-11, NSN, REF FAA 8130-3 FORM TRACKING NO. 20170214095605, ISSUED BY GAC-SAV, APPROVAL NO. ODA-511131-CE, DATED 14 FEB 2017. 2EA NEW BUSHING PIN 1159CSM20095-21, NSN, REF FAA 8130-3 FORM TRACKING NO. 20160808083152, ISSUED BY GAC-SAV, APPROVAL NO. ODA-511131-CE, DATED 08 AUG 2016. Discrepancy: 14.35 WHILE C/W CMP 273007 LIH ELEVATOR R&I FOUND STATIC WICK ON 109-BUL-2 BROKEN. Resolution: WHILE REMOVING BROKEN STATIC WICK FOUND DISCHARGER BASE SET SCREW TO BE FROZEN IN PLACE. REMOVED STATIC WICK BASE CLEANED PREPPED AND ALODINED AREA.INSTALLED STATIC WICK DISCHARGER BASE AND FILET SEALED TO 109-BUL-2 FAIRING IAW GAC BP 1159C520109 REV D - : BULLET TOP-SKIN INSTL.STA.871- 892. BONDING CHECK AND RESISTENCE CHECK COMPLETED. ALL WORK DONE IAW GIV 23-05-00. PREPPED, PRIMED AND PAINTED STATIC WICK BASE AND AFFECTED AREAS. ALL WORK DONE IAW GIV SRM 51-07-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.26 @ $142.00 $320.92 Parts USD: Time and Material $422.48 Total USD: $743.40 Parts: Ret No. Part number: Description Quantity Sell price USD Extended USD 1435 #5 2-145C-I STATIC WICK 2 $80.55 $161.10 1435 #7 2-46 DISCHARGER BASE 1 $225.81 $225.81 143508 MS20426AD4-I0 RIVET 10 $0.23 $230 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 48 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00808986 Bill To: JEGE LLC Pans: WO It SC18654 Invoice Number: 6918002027 Ref. No. Pan number: Description Quantity Sell price USD Extended USD 1435 #9 PR 1440111-2-654 SEALANT, 6 OUNCE #654 SEMKIT 1 $26.67 $26.67 1/2 HOUR WORK LIFE 1435#10 NAS1097B4-8 RIVET 10 $0.41 $4.10 1435 #11 NIS20426B4-5 RIVET, 100 DEGREE COUNTERSUNK 5 $0.50 $2.50 Step: 1435.1 Completed Step: 1435.2 Completed Step: 14.35.3 Step: 1435.4 Completed Completed WHILE REMOVING BROKEN STATIC WICK FOUND DISCHARGER BASE SET SCREW TO BE FROZEN IN PLACE. REMOVED STATIC WICK BASE CLEANED PREPPED AND ALODINED AREA. TEMP INSTALLED NEW BASE WITH CLEKOS. RIVETS ON ORDER. ALL WORK DONE IAW GULFSTREAM DWG # 1159CS20109 REV.D. INSTALLED STATIC WICK DISCHARGER BASE AND FILET SEALED TO I09-BUL-2 FAIRING IAW GAC BP 1159CS20109 REV D - : BULLET TOP-SKIN INSTL.STA.871- 892. BONDING CHECK AND RESISTENCE CHECK COMPLETED. ALL WORK DONE IAW GIV 23-05-00. PREPPED, PRIMED AND PAINTED STATIC WICK BASE AND AFFECTED AREAS. ALL WORK DONE IAW GIV SRM 51-07-10. Discrepancy: 14.36 WHILE REMOVING L/H ELEVATOR TRIM TAB, FOUND OB BOND WIRE BROKEN. Resolution: REPLACED BROKEN BONDING WIRE ON THE LEFT HAND ELEVATOR TRIM TAB WITH NEW P/N MS25083-2BB5 IAW GIV 27-04-00. Labor USD: Parts USD: Total USD: Parts: Ref. No. 1436 #I Billing Method Hours Rate Total Time and Material ST 1.63 @ $142.00 $231.46 Time and Material $6.14 Part number: MS25083-2BB5 Description JUMPER, ELECTRICAL BONDING 5 2 53.07 IN $237.60 Quantity Sell price USD Extended USD $6.14 Discrepancy: 14.37 WHILE REMOVING FUH ELEVATOR TRIM TAB, FOUND OB BOND WIRE: BROKEN Resolution: REPLACED BROKEN BONDING WIRE ON THE RIGHT HAND ELEVATOR TRIM IAB WITH NEW P/N MS25083-2BB5 IAW GIV AMM 27-04-00. Labor USD: Total USD: Billing Method flours Rate Total Time and Material ST 1.62 @ $142.00 $230.04 $230.04 Discrepancy: 14.38 WHILE REMOVING LIGHTED FLAP HANDLE CLOSEOUT PANEL, NOTED BROKEN ATTACHING HARDWARE. 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 49 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00808987 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Resolution: REMOVED BROKEN LOWER MOST FLAP OVERLAY SCREW AND REPLACED WITH A NEW CAPTIVE SCREW P/N MS3498-8 NSN RECIEVED FROM GAC BAF STOCK IAW GAC DWG 1159FP40084 Billing Method flours Rate Total Labor USD: Time and Material ST 0.43 @ $142.00 $61.06 Parts USD: Time and Material 511.98 Total USD: $73.04 Pans: Ref. No. Part number: Description Quantity Sell price LSD Extended USD 1438 #1 M24308-25-9F LOCK, MALE SCREW I $1.07 $1.07 1438 #2 M53498-8 SCREW ASSEMBLY 1 $10.91 $10.91 Discrepancy: 14.39 WHILE COMPLYING WITH GIV CMP 273077 - ELEVATOR HINGE FITTING (LEFT) INSPECTION NOTED STATIC / BONDING STRAP FOR NO. 2 HINGE BROKEN. Resolution: REMOVED BROKEN L/H ELEVATOR BONDING STRAP NPN NSN FROM #2 HINGE AND INSTALLED A NEW BONDING STRAP P/N MS25083-2BB5 NSN RECEIVED FROM GAC BAF STOCK. ALL WORK DONE JAW GIV AMM 20-24-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 130 @ $142.00 $184.60 Parts USD: Time and Material $3.07 Total USD: $187.67 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 1439 #1 31525083-2BB5 JUMPER, ELECTRICAL BONDING 5 I $3.07 $3.07 IN Discrepancy: 14.40 WHILE COMPLYING WITH GIV CMP 273077 - ELEVATOR HINGE FITTING (LEFT) INSPECTION NOTED LOWER BOSS ON HORZ STAB NO.1 HINGE TO BE OUT OF TOLERANCE. INDEX HINGE LINE NO.1. Resolution: RQCI: UPON FURTHER INVESTIGATION FOUND HORIZONTAL STABILIZER FITTING TO BE WITHIN LIMITS. HOLE SIZE 3212-.3145. IAW GIV CMP 273077 - ELEVATOR HINGE FITTING (LEFT) INSPECTION. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.10 @ $142.00 $440.20 Total USD: $440.20 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 50 of 117 Printed: 6/28/2018 939:1IAI Reel EFTA00808988 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 14.41 WHILE COMPLYING WITH GIV CMP 273077 - ELEVATOR HINGE FITTING (LEFT) INSPECTION NOTED LEFT ELEVATOR HORN PIVOT BEARING UNSERVICEABLE DUE TO RESISTANCE FELT DURING ROTATION (RATCHETING). Resolution: REMOVED BEARING RETAINER PLATE BY REMOVING FOUR(4) BOLTS, WASHERS, NUTS. REMOVED WORN BEARING. CLEANED AND INSPECTED BORE WITH NO DEFECTS NOTED. RECEIVED NEW BEARING PIN MS28913-10C: RECEIVED FROM GAC SAV UNDER ENTERPRSE TRANSFER NUMBER 000889433 DATED 5/30/2018. INSTALLED BEARING WET WITH 2012 PRIMER AND INSTALLED BEARING RETAINER PLATE WITH ORIGINAL HARDWARE. ALL WORK IAW GAC BP 1159CSM20067. Billing Method flours Rate Total Labor USD: Time and Material ST 2.20 @ $142.00 $312.40 Parts USD: Time and Material $325.07 Total USD: $637.47 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.41 #1 MS28913-10C BEARING 1 $325.07 $325.07 Discrepancy: 14.42 WHILE COMPLYING WITH GIV CMP 273077 - ELEVATOR HINGE FITTING (LEFT) INSPECTION NOTED ELEVATOR HORN UNIVERSAL BUSHING A4 TO HAVE CORROSION DAMAGE TO HAT SURFACE. Resolution: SEE ITEM 14.34 FOR LH ELEVATOR HORN REBUSHING Discrepancy: 14.43 WHILE COMPLYING WITH GIV CMP 273077 - ELEVATOR HINGE FITTING (LEFT) INSPECTION NOTED ELEVATOR HORN BUSHINGS A2 AND Al TO HAVE SCORING AND FRETTING CORROSION ON I.D. Resolution: SEE ITEM 14.34 FOR LJH ELEVATOR HORN REBUSHING Discrepancy: 14.44 WHILE COMPLYING WITH GIV CMP 273077 - ELEVATOR HINGE FITTING (LEFT) INSPECTION NOTED LEFT ELEVATOR HINGE NO.4 BOSSES, LINE INDEX 4-4 AND 4-5 WORN BEYOND TOLERANCE. 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 51 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00808989 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Resolution: RQCI PERFORMED REPAIR 5E05000102-911P5-21 TO LH ELEVATOR HINGE #4. BORES MEASURE .3906 - 3911, INSTALLED SE05000102-911P5-21 REPAIR SLEEVE. WORK DONE IAW GAC DWG SE05000901 REV E. REF STEPS BELOW FOR FURTHER DETAILS. THIS IS A MAJOR REPAIR, REF ITEM 14.70 FOR 8100-9 APPROVAL AND 337 INFO. Billing Method Hours Rate Total Labor USD: Time and Material ST 4.12 @ $142.00 $585.04 Parts USD: Time and Material $979.28 Total USD: $1,564.32 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.4481 SE05000102-911P5-2I STANDARD REOLAIR SLEEVE 1 $979.28 $979.28 Step: 14.44.1 Step: 14.44.2 Step: 14.44.3 Step: 14.44.4 Step: 14.44.5 Completed REAMED LII ELEV HINGE FITTING NO.4 (PIN: 1159CSM20032-1) FROM NOMINAL SIZE TO 1ST OVERSIZE TO INSTALL REPAIR SLEEVE P/N: SE05000102-911P5-21 RECEIVED FROM GAC-SAV PACKING SLIP: SASH#17-160356 DATED 14 NOV 2017. WORK PERFORMED IAW GAC BP 5E05000102 REV E - STD. REPAIR - CONTROL SURFACE HINGE FITTINGS. Completed CAD PLATED NO.4 ELEVATOR HINGE FITTING BORES lAW CAMPS 6103 REV F Completed REAMED LII ELEV NO.4 HINGE MOUNT FITTING ON HORIZONTAL STAB REAR BEAM FROM NOMINAL SIZE TO 1ST OVERSIZE. ALL WORK DONE IAW GAC BP 5E05000102 REV E - STD. REPAIR - CONTROL SURFACE HINGE FITTINGS. Completed CAD PLATED LH ELEV NO.4 HINGE MOUNT FITTING ON HORIZONTAL STAB REAR BEAM IAW CAMPS 6103 REV F. Completed ENTERED IN ERROR Discrepancy: 14.45 WHILE COMPLYING WITH GIV CMP 273078 - ELEVATOR HINGE FITTING (RIGHT) INSPECTION NOTED ELEVATOR HORN UNIVERSAL BUSHING, LINE INDEX A4 AND A8 TO HAVE FRETTING CORROSION ON HAT SURFACES AND I.D. Resolution: RQCI REMOVED THE RH ELEVATOR HORN UNIVERSAL FITTING BUSHINGS AND CLEANED THE BORES. VISUALLY INSPECTED AND DIMENSIONALLY CHECKED RH ELEVATOR HORN UNIVERSAL FITTING - NO DEFECTS NOTED AT THIS TIME. RECEIVED OKAY TO INSTALL 4EA NEW BUSHING P/N 1159CSM20095-15, NSN, REF FAA 8130-3 FORM TRACKING NO. 20160525083830, ISSUED BY GAC-SAV, APPROVAL NO. ODA-511131-CE, DATED 25 MAY 2016 lAW GAC BP 1159CSM20068 REV B - FTG ASSY CONTROL SURFACES. INSTALLED 2 EA HAT BUSHINGS P/N 1159CSM20095-11, NSN & 2 EA HAT BUSHINGS P/N 1159CSM20095-15, NSN ON RIH ELEVATOR HORN UNIVERSAL FITTING IAW GAC BP 1159CSM20068 REV B - FTG ASSY CONTROL SURFACES AND GAMPS 2226. Billing Method Hours Rate Total Labor USD: Time and Material ST 5.00 @ $142.00 $710.00 Parts USD: Time and Material $29.26 Total USD: $739.26 Parts: Ref'. No. Part number: Description Quantity Sell price USD Extended USD 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 52 of 117 Printed: 6/28/2018 939:11A? Reel EFTA00808990 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Pans: Ref'. No. Part number: Description Quantity Sell price USD Extended USD 14.45 #1 515X333-2OZ KIT, TOUCH UP, EPDXY PRIMER, 2 1 $29.26 OZ, GREEN Step: 14.45.1 Step: 14.45.2 Step: 14.45.3 Completed REFER TO STEP 14.46.1 FOR COMPLIANCE WITH TURN DOWN OF NEW BUSHINGS P/N 1159CSM20095-I5. Completed REMOVED THE RH ELEVATOR HORN UNIVERSAL FITTING BUSHINGS AND CLEANED THE BORES. VISUALLY INSPECTED AND DIMENSIONALLY CHECKED RH ELEVATOR HORN UNIVERSAL FITTING - NO DEFECTS NOTED AT THIS TIME. RECEIVED OKAY TO INSTALL 4EA NEW BUSHING FIN 1159CSM1120095-15, NSN, REF FAA 8130-3 FORM TRACKING NO. 20160525083830, ISSUED BY GAC-SAV, APPROVAL NO. ODA-511131-CE, DATED 25 MAY 2016 IAW GAC BP 1159CSM20068 REV B - FTC ASSY CONTROL SURFACES. Completed INSTALLED 2 EA HAT BUSHINGS FIN 1159CSM20095-11, NSN & 2 EA HAT BUSHINGS P/N 1159CSM20095-15, NSN ON RAH ELEVATOR HORN UNIVERSAL FITTING IAW GAC BP 1I59CSM20068 REV B - FTG ASSY CONTROL SURFACES AND CAMPS 2226. $29.26 Discrepancy: 14.46 WHILE COMPLYING WITH GIV CMP 273078 - ELEVATOR HINGE FITTING (RIGHT) INSPECTION NOTED ELEVATOR HORN BUSHINGS, LINE INDEX Al AND A2 TO HAVE FRETTING CORROSION ON I.D. SURFACES. Resolution: RQCI REMOVED THE RH ELEVATOR HORN BUSHINGS , CLEANED THE BORES NO DEFECTS NOTE AT THIS TIME. WORK DONE IAW GULFSTREAM DRAWING NUMBERS 1159CSM20068 AND 1159CSM200066. MEASURED LINE INDEX Al BORE AND OBTAINED 0.7528" WHICH MEETS SPEC (0.7523"-0.7533"). RECEIVED OKAY AND INSTALLED NEW HAT BUSHING P/N: 1159CSM20095-1 NSN RECEIVED FROM GAC-SAV ODA-511131-CE FAA FORM 8130-3 TRACKING# 20131019064004 DATED 19 OCT 2013 lAW GAC BP 1159CSM20066 REV F - FTG ASSY CONTROL SURFACES. VISUALLY INSPECTED AND DIMENSIONALLY CHECKED RH ELEVATOR FITTING HORN - NO DEFECTS NOTED. RECEIVED OKAY TO INSTALL 2 EA HAT BUSHINGS P/N: 1159CSM20095-21 NSN RECEIVED FROM GAC-SAV ODA-511131-CE FAA FORM 8130-3 TRACKING#20160808083152 DATED 08 AUG 2016 IAW GAC BP 1159CSM20066 REV F- FTC ASSY CONTROL SURFACES. INSTALLED 2 EA HAT BUSHINGS P/N 1159CSM20095-21, NSN ON RAH ELEVATOR HORN IAW GAC BP 1159CSM20066 REV F- FTG ASSY CONTROL SURFACES AND GAMPS 2226. Billing Method Hours Rate Total Labor USD: Time and Material ST 5.90 @ $142.00 $837.80 Parts USD: Time and Material $82.97 Total USD: $920.77 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.46 #1 1159CSM20095-1 BUSHING I $47.51 $47.51 14.46 #2 1159CSM1120095-21 BUSHING 2 $17.73 $35.46 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 53 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808991 Bill To: JEGE LLC Step: 14.46.1 Completed WO #: SC18654 Invoice Number: 6918002027 RECEIVED 2 EA P/N 1159CSM20095-2I AND TURNED DOWN THE FACE FROM .10125 TO FINAL HAT THICKNESS OF .0715 - .0725, RECEIVED 2 EA OF PIN I159CSN120095-11 AND TURNED DOWN THE FACE FROM .10125 TO FINAL HAT THICKNESS OF .0715-.0725, RECIEIVED 4 EA OF P/N1159CSM20095-15 AND TURNED THEM DOWN FROM .101 TO FINAL HAT THICKNESS OF .068-.069. ALL WORK DONE IAW GAC DWG II 59CSM20066 REV F. Step: 14.46.2 Completed REMOVED THE Ftll ELEVATOR HORN BUSHINGS IAW GULFSTREAM DRAWING NUMBERS 1159CSM20068 AND 1159CSM200066. Step: 14.46.3 Completed MEASURED LINE INDEX Al BORE AND OBTAINED 0.7528" WHICH MEETS SPEC (0.7523"-0.7533"). RECEIVED OKAY AND INSTALLED NEW HAT BUSHING P/N: 1159CSM20095-1 NSN RECEIVED FROM GAC-SAV ODA-511131-CE FAA FORM 8130-3 TRACKING# 20131019064004 DATED 19 OCT 2013 IAW GAC BP I159CSN120066 REV F - FTG ASSY CONTROL SURFACES. Step: 14.46.4 Completed VISUALLY INSPECTED AND DIMENSIONALLY CHECKED [GI ELEVATOR FITTING HORN - NO DEFECTS NOTED. RECEIVED OKAY TO INSTALL 2 EA HAT BUSHINGS PIN: 1159CSM20095-2I NSN RECEIVED FROM GAC-SAV ODA-511131-CE FAA FORM 8130-3 TRACKING#20160808083152 DATED 08 AUG 2016 IAW GAC BP 1159CSM20066 REV F- FTG ASSY CONTROL SURFACES Step: 14.46.5 Completed INSTALLED 2 EA HAT BUSHINGS P/N 1159CSM20095-21, NSN ON Ft/II ELEVATOR HORN IAW GAC BP I I59CSN120066 REV F- FTG ASSY CONTROL SURFACES AND CAMPS 2226. Discrepancy: 14.47 WHILE COMPLYING WITH GIV CMP 273078 - ELEVATOR HINGE FITTING (RIGHT) INSPECTION NOTED RIGHT ELEVATOR HINGE NO.1 INBD BUSHING BOSS WORN ALLOWING HAT-BUSHING 1-1 MOVEMENT. Resolution: RQCI REMOVED WORN RH ELEV HINGE #1 INBOARD BOSS HAT BUSHING P/N: 1159SB30210-45 NSN & REPLACED WITH NEW BUSHING P/N: 1159SB30210-45 NSN RECEIVED FROM GAC-SAV ODA-511131-CE FAA FORM 8130-3 TRACKING# 20161015125720 DATED 15 OCT 2016 IAW GAC BP 1159CS20002 REV (V) - ELEVATOR ASSEMBLY, CONTROL SURFACES. NO MOVEMENT AFTER REPLACEMENT BUSHING INSTALLATION. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.87 @ $142.00 $549.54 Parts USD: Time and Material $73.93 Total USD: $623.47 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.47 #1 1159SB30210-45 BUSHING 1 518.64 $18.64 14.47 #2 NAS6608D23 BOLT 1 S16.93 $16.93 14.47 #3 1159CSM20094-105 SLEEVE 1 $34.00 $34.00 14.47 #4 MSI7825-8 NUT SELF 1 $4.36 $436 LKG-CASTELLATED,STEEL Step: 14.47.1 Completed REMOVED WORN RH ELEV HINGE #1 INBOARD BOSS HAT BUSHING P/N: 1159SB30210-45 NSN. Step: 14.47.2 Completed REPLACED WITH NEW BUSHING PIN: 1159SB30210-45 NSN RECEIVED FROM GAC-SAV ODA-511131-CE FAA FORM 8130-3 TRACKING# 20161015125720 DATED 15 OCT 2016 IAW GAC BP 1159CS20002 REV (V) - ELEVATOR ASSEMBLY, CONTROL SURFACES. NO MOVEMENT AFTER REPLACEMENT BUSHING INSTALLATION. Discrepancy: 14.48 WHILE COMPLYING WITH GIV CMP 273078 - ELEVATOR HINGE FITTING (RIGHT) INSPECTION NOTED RIGHT ELEVATOR HINGE INBD BUSHING, LINE INDEX 2-1, TO HAVE FRETTING CORROSION ON I.D. SURFACES. 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 54 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00808992 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Resolution: REMOVED CORRODED BUSHING PIN: 1159SB30210-45 NSN FROM NO 2 ELEV HINGE INBOARD FITTING AND REPLACED WITH NEW BUSHING P/N: 1159SB30210-45 NSN RECEIVED FROM GAC-SAV ODA-511131-CE FAA FORM 8130-3 TRACKING/ 20161015125720 DATED 15 OCT 2016 IAW GAC BP 1159C520002 REV (V) - ELEVATOR ASSEMBLY, CONTROL SURFACES Billing Method Hours Rate Total Labor USD: Time and Material ST 1.99 @ $142.00 $282.58 Pans USD: Time and Material $18.64 Total USD: $301.22 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.48 #1 1159SB30210-45 BUSHING 1 $18.64 Step: 14.48.1 Completed REMOVED NO 2 ELEVATOR HINGE FITTING INBOARD HAT BUSHING PIN: 11595B30210-45 NSN IAW GAC BP 1159CSM20139 REV F- FITTING CONTROL SURFACES-ELEVATOR HINGE-ELEVATOR STA 60.58 $18.64 Discrepancy: 14.49 WHILE COMPLYNG WITH GIV CMP 55201 AND 552012 LH AND RH ELEVATOR TRIM TAB HINGE FITTING INSPECTION FOUND CORROSION AT ALL 3 BONDING WIRE ATTACH POINTS ON THE LH AND RH ELEVATOR TRIM TABS. Resolution: REMOVED LIGHT SURFACE CORROSION AT ALL 3 BONDING WIRE ATTACH POINTS ON THE LH AND RH ELEVATOR TRIM TABS BY LIGHT HAND SANDING WITH NO MATERIAL LOSS.APPLIED ALODINE OBTAINED FROM GAC-BAF STOCK. ALL WORK DONE IAW GIV SRM 51-13-21, AND 51-21-21. Billing Method Hours Rate Total Labor USD: Time and Material ST 10.05 @ $142.00 $1,427.10 Total USD: $1,427.10 Discrepancy: 14.50 WHILE COMPLYING WITH GIV CMP CODE 552011 LEFT ELEVATOR TRIM TAB HINGE FITTING INSPECTION FOUND SEVERAL AREAS OF CORROSION ON THE LH ELEVATOR TRIM TAB LEADING EDGE UPPER AND LOWER SURFACES. Resolution: RQCI REMOVED MINOR SURFACE CORROSION FROM THE UPPER LEADING EDGE OF THE L/H ELEVATOR TRIM TAB WITH MINIMAL MATERIAL LOST AT THE FOLLOWING ELEVATOR STATIONS 23.116, 33.676, 76.547, AND 120.174. REMOVED MINOR SURFACE CORROSION FROM THE LOWER LEADING EDGE OF THE L/H ELEVATOR TRIM TAB WITH MINIMAL MATERIAL LOST AT THE FOLLOWING ELEVATOR STATIONS 87.529 AND 109.493. ALODINED AND PRIMER THE AFFECTED AREAS WORK DONE IAW GULFSTREAM GIV SRM 51-13-10 AND 51-07-10. PERFORMED SKIN REPAIR ON THE UPPER FORWARD L/H ELEVATOR TRIM TAB AT BL 45.799-56.0245 AND APPROXIMATELY BL 104. WORK DONE IAW GAC SE05516001. PERFORMED SKIN REPAIR ON THE LOWER FORWARD L/H ELEVATOR TRIM TAB AT BL 45.799-56.0245 AND APPROXIMATELY BL 124. WORK DONE IAW GAC SE05516001. THIS IS A MINOR REPAIR, REF ITEM 14.73 FOR ELEVATOR BALANCE CORRECTION AND VERIFICATION. 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 55 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00808993 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Billing Method Hours Rate Total Labor USD: Time and Material ST 26.61 @ $142.00 $3,778.62 Labor USD: Time and Material ST 1.00 @ $231.00 $231.00 Parts USD: Time and Material $95.62 Total USD: $4,105.24 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.50 #1 PS870B1-2DAB-KIT SEALANT,50 GRAM KIT,CUP AND 1 $36.54 $36.54 SYRINGE 14.50 #6 NASI097AD3-3 RIVET 10 S0.22 $2.20 14.50 #7 MS20426AD4-4 RIVET $0.22 $1.76 14.50 0X MS20426AD4-5 RIVET a $0.22 $1.76 14.50 #9 MS20426AD4-5 RIVET 10 $0.22 S2.20 14.50 #10 MS20426AD3-3 RIVET 10 S0.22 $2.20 14.50 #11 NASI097AD3-3 RIVET 10 $0.22 $2.20 14.50 #12 515X333-2OZ KIT, TOUCH UP, EPDXY PRIMER. 2 1 $29.26 $29.26 OZ, GREEN 14.50014 NASI581C3T2 BOLT, 100 DEG FRH, OFS 10 $0.80 $8.00 CRUCIFORM, 95 KSI 14.50015 NAS1581C3T3 SCREW 8 S0.44 $3.52 14.50016 MS24694-552 SCREW,MACHINE,FLAT CTSK 16 $0.23 $3.68 HD,100DEG,STRL 14.50017 MS24694C4 SCREW 10 $0.23 5230 Step: 14.50.1 Completed REMOVED MINOR SURFACE CORROSION FROM THE UPPER LEADING EDGE OF THE LAI ELEVATOR TRIM TAB WITH MINIMAL MATERIAL LOST AT THE FOLLOWING LOCATIONS: BL47.5, BL52.0, BL75, BL123.5. REMOVED MINOR SURFACE CORROSION FROM THE LOWER LEADING EDGE OF THE L/II ELEVATOR TRIM TAB WITH MINIMAL MATERIAL LOST AT THE FOLLOWING LOCATIONS: BL106.0 AND 82.5. ALODINED AND PRIMED THE AFFECTED AREAS. WORK DONE IAW GULFSTREAM GIV SRM 51-13-10 AND 51-07-10. Step: 14.50.2 Completed ON L/H ELEEVATOR PERFORMED SKN REPAIR INSTL- ELEVATOR TRIM TAB BL 45.799 - 56.0245 IAW GAC BP SE05516001. REPAIR INSTALLED ON UPPER FORWARD SKIN SURFACE APPROXIMATELY BL104. Step: 14.50.3 Waiting ELEVATOR BALANCE CORRECTED AND VERIFIED UNDER ITEM 14.73 Insp Step: 14.50.4 Completed ON L/H ELEEVATOR PERFORMED SKN REPAIR INSTL- ELEVATOR TRIM TAB BL 45.799 - 56.0245 IAW GAC BP 5E05516001. REPAIR INSTALLED ON LOWER FORWARD SKIN SURFACE APPROXIMATELY BLI 24. Step: 14.50.5 Completed ENGINEERING DISPOSITION: ENGINEERING CONSIDERS THE FOLLOWING REWORK TO BE MINOR IN NATURE, NO 8100-9 FAA APPROVALS REQUIRED. REPAIR NOTED DAMEG PER SE05516001 (REV -)'SKIN REPAIR INSTL - ELEVATOR TRIM TAB - BL 45.799-56.0245". CHECK WEIGHT AND BALANCE OF THE REPAIR TAB AND ELEVATOR/TAB ASSY IS REQUIRED, REF NIM27-0I-00 Step: 14.50.6 Waiting MEASURED 1.675 POUNDS AT 18 INCHES AFT OF HINGE #3 CENTERLINE ON Insp LH ELEV TRAILING EDGE OBTAINING 30.15 IN/LB TRAILING EDGE HEAVY MOMENT. WORK PERFORMED IAW GIV AMM 27-01-00 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). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 56 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00808994 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Discrepancy: 14.51 WHILE COMPLYING WITH GIV CMP 552011 LEFT ELEVATOR TRIM TAB HINGE FITTING INSPECTION FOUND LH TRIM TAB INBOARD AND OUTBOARD ATTACH POINT BEARINGS ARE FROZEN. Resolution: RQCI: UPON FUTHUR INVESTIGATION FOUND THE L/H OUTBOARD ELEVATOR TRIM TAB ATTACHMENT BEARING TO BE IN SERVICEABLE CONDITION. REMOVED THE FROZEN L/H ELEVATOR TRIM TAB ATTACHMENT INBOARD BEARING WITH P/N MS14101-4 S/N NSN. INSTALLED A NEW L/H ELEVATOR TRIM TAB ATTACHMENT BEARING WITH PIN MS14101-4 S/N NSN. RECEIVED FROM GULFSTREAM DALLAS REFERENCE PACKING LIST WITH DASH NUMBER 18-08172 DATED 6/2/2018. WORK DONE IAW GULFSTREAM DRAWING# 1159CSM20152, REV. C, AND DOCUMENT# GAB14E. Billing Method Hours Rate Total Labor USD: Time and Material ST 6.92 @ $142.00 $982.64 Pans USD: Time and Material $114.81 Total USD: $1,097.45 Parts: Re. No. Part number: Description Quantity Sell price USD Extended USD 14.51 #1 MS14101-4 BEARING,PLAIN,SELF LUB & ALIGN 3 $13.91 $41.73 14.51 #3 PS870B1-2DAB-KIT SEALANT,50 GRAM KIT,CUP AND 2 536.54 $73.08 SYRINGE Discrepancy: 14.52 WHILE COMPLYING WITH GIV CMP 552011 LEFT ELEVATOR TRIM TAB HINGE FITTING INSPECTION FOUND LH TRIM TAB HOLE INDEX 1-1 IS OUT OF DIMENSIONAL TOLERANCES. Resolution: RQCI: REAMED LH ELEVATOR TRIM TAB HOLE INDEX 1-1 TO THE FIRST OVERSIZE OF .3905. ALSO FOUND LH ELEVATOR TRIM TAB HOLE INDEX 1-3 TO BE OUT OF TOLERANCE. REAMED FITTING TO THE SECOND OVERSIZE OF .4063. ALODINED HOLE AS REQ. INSTALLED A NEW HAT BUSHING WITH P/N SE05000102-912S88-1 NSN . INTO HOLE INDEX 1-1 REFERENCE CERTIFICATE OF CONFORMANCE WITH PACKING LIST # SAP017-17117.1 DATED 4-27-17 FROM GULFSTREAM AEROSPACE CORP. RECIEVED A NEW SLEEVE BUSHING WITH P/N 5E05000102-911P2-5 NSN .REFERENCE R&I LOG INTRY 104 FOR INSTALLATION REFERENCE CERTIFICATE OF CONFORMANCE WITH PACKING LIST # SAP01-64001.1G DATED 5-7-18FROM GULFSTREAM AEROSPACE CORP. . ALL WORK DONE IAW GULFSTREAM DRAWING SE05000102, REV E. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.55 @ $142.00 $504.10 Parts USD: Time and Material $1,076.11 Total USD: $1,580.21 Parts: Ref'. No. Part number: Description Quantity Sell price USD Extended USD 14.52 #1 SE05000102-912588-1 BUSHING, STD REPAIR 1 5321.93 $321.93 14.52 #2 5E05000102-911P2-5 BUSHING, PLAIN 1 $754.18 $754.18 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_WorkOrderPreliminaryInvoicelpt 2011 Page 57 of 117 Printed: 6/28/2018 9:39:11M Rent EFTA00808995 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Step: 14.52.1 Completed RQCI: REAMED LII ELEVATOR TRIM TAB HOLE INDEX 1-1 TO THE FIRST OVERSIZE OF .3905. ALSO FOUND LII ELEVATOR TRIM TAB HOLE INDEX 1-3 TO BE OUT OF TOLERANCE. REAMED FITTING TO THE SECOND OVERSIZE OF .4063. ALODINED HOLE AS REQ. ALL WORK DONE IAW GULFSTREAM DRAWING 5E05000102, REV E. Discrepancy: 14.53 WHILE COMPLYING WITH GIV CMP 552012 RIGHT ELEVATOR TRIM TAB HINGE FITTING INSPECTION FOUND RH TRIM TAB HOLE INDEX 1-3 AND 2-3 ARE OUT OF DIMENSIONAL TOLERANCES. Resolution: RQCI: REAMED RH ELEVATOR TRIM TAB HOLE INDEX 1-3 AND 2-3 TO THE FIRST OVERSIZE OF .3905. ALODINED HOLES AS REQ. RECIEVED TWO NEW SLEEVE BUSHING WITH P/N SE05000102-911P2-5 NSN .REFERENCE R&I LOG INTRY 103 FOR INSTALLATION REFERENCE CERTIFICATE OF CONFORMANCE WITH PACKING LIST # SAP01-64001.1G DATED 5-7-18FROM GULFSTREAM AEROSPACE CORP. WORK DONE IAW GAC DWG SE05000901 REV E. REF STEPS BELOW FOR FURTHER DETAILS. THIS IS A MAJOR REPAIR, REF ITEM 14.70 FOR 8100-9 APPROVAL AND 337 INFO. Billing Method Flours Rate Total Labor USD: Time and Material ST 3.77 ® $142.00 $535.34 Parts USD: Time and Material $2,648.86 Total USD: $3,184.20 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 14.53 #1 5E05000102-911P1-5 BUSHING 2 $1,324.43 $2,648.86 Step: 14.53.1 Completed RQCI: REAMED RH ELEVATOR TRIM TAB HOLE INDEX 1-3 AND 2-3 TO THE FIRST OVERSIZE OF .3905. ALODINED HOLES AS REQ. ALL WORK DONE IAW GULFSTREAM DRAWING 5E05000102, REV E. Discrepancy: 14.54 WHILE COMPLYING WITH GIV CMP CODE 552012 RIGHT ELEVATOR TRIM TAB HINGE FITTING INSPECTION FOUND ALL 3 TRIM RIGHT HAND ELEVATOR TRIM TAB ATTACH POINT BEARING S FROZEN. Resolution: RQCI: UPON FUTHUR INVESTIGATION FOUND THE R/H CENTER ELEVATOR TRIM TAB ATTACHMENT BEARING TO BE IN SERVICEABLE CONDITION. REMOVED THE WORN R/H OUTBOARD ELEVATOR TRIM TAB ATTACHMENT BEARING WITH P/N MS14101-4 S/N NSN. INSTALLED A NEW R/H OUTBOARD ELEVATOR TRIM TAB ATTACHMENT BEARING WITH P/N MS14101.4 S/N NSN. RECEIVED FROM GAC SAVANNAH WITH APPROVAL NUMBER ODA-511131-CE. REFERENCE 8130-3 WITH FORM TRACKING NU,MBER 20111231094508 DATED 12/31/2011. REMOVED THE WORN R/H INBOARD ELEVATOR TRIM TAB ATTACHMENT BEARING WITH P/N MS14101-4 SIN NSN. INSTALLED A NEW R/H INBOARD ELEVATOR TRIM TAB ATTACHMENT BEARING WITH P/N MS14101-4 S/N NSN. RECEIVED FROM GAC LONG BEACH REFERENCE PACKING LIST WITH DASH NUMBER 18-05926 DATED 6/2/2018. WORK DONE IAW GULFSTREAM DRAWING# 1159CSM20152, REV. C, DOCUMENT# GAB14E AND ENGINEERING DISPOSITION SC18654, 14.54.2 Billing Method Flours Rate Total 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 58 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00808996 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Labor USD: Time and Material ST 7.94 @ $142.00 $1,127.48 Labor USD: Time and Material ST 1.00 @ $231.00 $231.00 Parts USD: Time and Material $27.82 Total USD: $1,386.30 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.54 #1 MSI4101-4 BEARING,PLAIN,SELF LUB & ALIGN 2 $13.91 $27.82 Step: 14.54.1 Completed ENGINEERING DISPOSITION REQUEST FOR THE CONTINUE FOR SERVICE ON THE Ftfli ELEVATOR INBOARD TRIM TAB ATTACHMENT POINT BEARING MOUNTING HOLE. THE MOUNT PIN IS 1159CS11120152-1 PER GULFSTREAM DRAWING 1159CSM20152 THE HOLE SHOULD MEASURE .6552 TO .6557. CURRENT MEASUREMENT IS .0013 OVERSIZED. Step: 14.54.2 Completed ENGINEERING DISPOSITION: ENGINEERING REVIEW OF NOTED CONDITION FINDS THE 1159CSM20152-1 BEARING BORE TB STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. CONTINUE WITH MSI4101-4 BEARING PRESS FIT OPERATIONS IAW GABI4E Discrepancy: 14.55 WHILE COMPLYING WITH GIV CMP CODE 552012 RIGHT ELEVATOR TRIM TAB HINGE FITTING INSPECTION, FOUND THE INBOARD RH ELEVATOR TRIM TAB PUSH ROD AFT ROD END GREASE SEALS ARE MISSING. Resolution: RQCI: REMOVED FAULTY ROD END P/N MS21151-8 NSN AND INSTALLED A NEW ROD END P/N MS21151-8 NSN RECEIVED FROM GAC SAV. REF CERTIFICATE OF CONFORMANCE ORDER NUMBER 22013581-0001 P.O. NUMBER WEP017-03885 DATED 8/3/2017. ALL WORK DONE IAW GIV AMM 27-04-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 0.82 @ $142.00 $116.44 Parts USD: Time and Material $89.07 Total USD: $205.51 Parts: Ref'. No. Part number: Description Quantity Sell price USD Extended USD 14.55 kl MS21151-8 BEARING, ROD END, DBL ROW, 235 1 $89.07 $89.07 IN L Discrepancy: 14.56 WHILE COMPLYING WITH GIV CMP CODE 552012 RIGHT ELEVATOR TRIM TAB HINGE FITTING INSPECTIN FOUND CORROSION ON THE RH ELEVATOR UPPER SKIN FWD AND OUTBOARD OF THE TRIM TAB OUTBOARD ATTACH POINT. Resolution: REMOVED LIGHT SURFACE CORROSIONON THE RH ELEVATOR UPPER SKIN FWD AND OUTBOARD OF THE TRIM TAB OUTBOARD ATTACH POINT BY LIGHT HAND SANDING WITH NO MATERIAL LOSS.APPLIED ALODINE AND PRIMER OBTAINED FROM GAC-BAF STOCK. ALL WORK DONE IAW GIV SRM 51-13-21,51-07-10 AND 51-21-21. Billing Method flours Rate Total Labor USD: Time and Material ST 2.12 @ $142.00 $301.04 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 59 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00808997 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Total USD: $301.04 Discrepancy: 14.57 WHILE C/W CMP 273007 L/H ELEVATOR R&I FOUND STATIC WICK ON LH HORIZONTAL STAB PANEL 37-TIP-1 BROKEN. Resolution: REMOVED BROKEN STATIC WICK ON LH HORIZONTAL STAB PANEL 37-TIP-1 NPN NSN AND INSTALLED A NEW STATIC WICK P/N 2-14SC-1 NSN RECEIVED FROM GAC BAF STOCK. PERFORMED RESISTENCE CHECK WITH NO DEFECTS NOTED. ALL WORK DONE IAW GIV AMM 23-05-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 0.68 @ $142.00 S96.56 Total USD: $96.56 Discrepancy: 14.58 WHILE C/W CMP CODE 554015 RUDDER / HINGE INSPECTION FOUND RUDDER BOTTTOM HINGE FITTING HAS AREAS OF SURFACE CORROSION ON ALL EXTERIOR SURFACES. Resolution: REMOVED AREAS OF LIGHT SURFACE CORROSION / STAINING ON AFFECTED EXTERIOR SURFACES OF RUDDER BOTTTOM HINGE FITTING USING GRAY SCOTCHBRITE AND HAND METHOD WITH NO BASE MATERIAL LOSS. CLEANED AND APPLIED EPDXY PRIMER / TOPCOAT AS REQUIRED. WORK DONE IN ACCORDANCE WITH GIV SRM CHAPTER 51-13-20. Billing Method Flours Rate Total Labor USD: Time and Material ST 4.00 @ $142.00 $568.00 Total USD: $568.00 Discrepancy: 14.59 WHILE C/W CMP CODE 554015 RUDDER / HINGE INSPECTION FOUND SKIN ON THE LEFT SIDE OF THE RUDDER NEXT TO THE UPPER HINGE HAS DAMAGE INTO THE COMPOSITE MATERIAL THAT REQUIRES REPAIR Resolution: CAREFULLY REMOVED PAINT AND HIGH BUILD PRIMER FROM DAMAGE AREA AND DETAIL INSPECTED. NOTED TWO MINOR DEPRESSIONS IN COMPOSITE MATRIX WITH NO DISBOND NOTED. PERFORMED CHOPPED FIBER REPAIR TO AREA IAA/ G IV SRM 51-78-00. REPROTECTED AREA WITH 3012 PRIMER AND TOPCOAT TO MATCH. Billing Method Flours Rate Total Labor USD: Time and Material ST 8.20 @ $142.00 $1,164.40 Total USD: $1,164.40 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 60 of 117 Printed: 6/28/2018 9:39:11M Reel EFTA00808998 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Step: 14.59.1 Completed CAREFULLY REMOVED PAINT AND HIGII BUILD PRIMER FROM DAMAGE AREA AND DETAIL INSPECTED. NOTED TWO MINOR DEPRESSIONS IN COMPOSITE MATRIX WITH NO DISBOND NOTED. PERFORMED CHOPPED FIBER REPAIR TO AREA IAW G IV SRM 51-78-00. Discrepancy: 14.60 WHILE C/W CMP CODE 554015 RUDDER / HINGE INSPECTION FOUND RUDDER HINGE INDEX 1-4 HAS PITTING IN THE BORE Resolution: RQCI REMOVED PITTING CORROSION FROM BORE OF RUDDER HINGE INDEX 1.4, BY REAMING TOP HINGE AND FITTING TO FIRST OVERSIZE .3898. NO FURTHER DEFECTS NOTED AT THIS TIME. RECEIVED NEW SLEEVE P/N SE05000901-914P1-28 NSN REFERENCE CERTIFICATE OF CONFORMANCE WITH PACKING LIST # SAP014-14802 DATED 10-1-14 FROM GULFSTREAM AEROSPACE CORP. REF R&I #208 FOR INSTALLATION, WORK DONE IAW GAC DWG SE05000901 REV E. REF STEPS BELOW FOR FURTHER DETAILS. THIS IS A MAJOR REPAIR, REF ITEM 14.70 FOR 8100-9 APPROVAL AND 337 INFO. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.53 ® $142.00 $501.26 Parts USD: Time and Material $2,863.88 Total USD: $3,365.14 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.60 #1 SE0S000901-914P1-28 SLEEVE 1 $2,863.88 $2,863.88 Step: 14.60.1 Step: 14.60.2 Completed REMOVED PITTING CORROSION FROM BORE OF RUDDER HINGE INDEX 1-4, BY REAMING TOP HINGE AND FITTING TO FIRST OVERSIZE .3898. NO FURTHER DEFECTS NOTED AT THIS TIME. WORK DONE IAW GAC DWG NO. 5E05000102, REV E. Completed STEP ENTERED IN ERROR. Discrepancy: 14.61 WHILE C/W CMP CODE 554015 RUDDER / HINGE INSPECTION FOUND RUDDER HINGE INDEX 2-4 IS OUT OF DIMENSIONAL LIMITS. Resolution: RQCI REMOVED PITTING CORROSION FROM BORE OF RUDDER HINGE INDEX 2-4 BY REAMING MIDDLE HINGE AND FITTING TO FIRST OVERSIZE .3898. NO FURTHER DEFECTS NOTED AT THIS TIME. RECEIVED A NEW SLEEVE WITH P/N SE05000901-914P1-2 . REFERENCE CERTIFICATE OF CONFORMANCE WITH PACKING LIST # 100465 DATED JAN-06-2017 FROM DYNAMO AVIATION, INC. REF R&I #208 FOR INSTALLATION. WORK DONE IAW GAC DWG SE05000901 REV E. REF STEPS BELOW FOR FURTHER DETAILS. THIS IS A MAJOR REPAIR, REF ITEM 14.70 FOR 8100-9 APPROVAL AND 337 INFO. Labor USD: Parts USD: Billing Method Flours Rate Total Time and Material ST 3.61 ® $142.00 $512.62 Time and Material $1,123.51 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 61 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00808999 Bill To: JEGE LLC WO SCI8654 Invoice Number: 6918002027 Total USD: $1,636.13 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.61 #1 SE05000901-914P1-2" lit %BING 1 $1,123.51 $1,123.51 Step: 14.61.1 Completed REMOVED PITTING CORROSION FROM BORE OF RUDDER HINGE INDEX 2-4 BY REAMING MIDDLE HINGE AND FITTING TO FIRST OVERSIZE .3898. NO FURTHER DEFECTS NOTED AT THIS TIME. WORK DONE IAW GAC DWG NO. SE05000102 REV E. Discrepancy: 14.62 WHILE C/W CMP CODE 554015 RUDDER / HINGE INSPECTION FOUND RUDDER HINGE INDEX 3-3 HAS PITTING IN THE BORE Resolution: RQCI PERFORMED REPAIR SE05000102-913D3-26 TO RUDDER LOWER HINGE, BORE MEASURES .3755, INSTALLED SE05000901-913D3-26 BUSHING WORK DONE IAW GAC DWG SE05000901 REV E. REF STEPS BELOW FOR FURTHER DETAILS. THIS IS A MAJOR REPAIR, REF ITEM 14.70 FOR 8100-9 APPROVAL AND 337 INFO. Billing Method Flours Rate Total Labor USD: Time and Material ST 3.10 @ $142.00 $440.20 Parts USD: Time and Material $1,565.79 Total USD: $2,005.99 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.62 #1 5E05000901-913D3-26 DOGBONE BUSHING 1 $1,565.79 Step: 14.62.1 Step: 14.62.2 Completed Completed REMOVED PITTING CORROSION FROM BORE OF RUDDER HINGE INDEX 3-3 BY REAMING BOTTOM HINGE AND FITTING TO THIRD OVERSIZE 3755. NO FURTHER DEFECTS NOTED AT THIS TIME. WORK DONE IAW GAC DWG NO. SE05000102 REV E. INSTALLED NEW DOGBONE BUSHING PIN SE05000901-913D3-2 INTO HINGE REF PACKING SLIP SASH#18-82146 FROM GULFSTREAM AEROSPACE CORP. DATED 06/•03/•2018 ALL WORK DONE IAW GAC DWG NO. SE05000102 REV E $1,565.79 Discrepancy: 14.63 WHILE C/W CMP CODE 554015 RUDDER / HINGE INSPECTION FOUND RUDDER HINGE INDEX 4-2 HAS PITTING IN ONE OF THE HAT BUSHINGS Resolution: RQCI REMOVED LH RUDDER TORQUE TUBE HINGE INDEX 4-2 HAT BUSHING WITH P/N UNK, NSN. DIMENSIONALLY MEASURED BORE AND FOUND TO BE NOMINAL. INSTALLED A NEW LH RUDDER TORQUE TUBE HINGE INDEX 4-2 HAT BUSHING WITH P/N GABIOE7-6, NSN. AND LINE REAMED. REFERENCE PACKING SLIP WITH ENTERPRISE TRANSFER NUMBER 000890471 DATED 06/02/2018. RECEIVED FROM GAC SAV. WORK DONE IAW GAC DWG 1159CS20305 REV. J. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.42 @ $142.00 $343.64 Parts USD: Time and Material $156.25 Total USD: $499.89 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 62 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00809000 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.63 #1 GABI0E7-6 BUSHING 1 $156.25 $156.25 Step: 14.63.1 Step: 14.63.2 Completed REMOVED LH RUDDER TORQUE TUBE HINGE INDEX 4-2 HAT BUSHING WITH P/N UNK, NSN. DIMENSIONALLY MEASURED BORE AND FOUND TO BE NOMINAL. INSTALLED A NEW LII RUDDER TORQUE TUBE HINGE INDEX 4-2 HAT BUSHING WITH P/N GABI0E7-6, NSN. REFERENCE PACKING SLIP WITH ENTERPRISE TRANSFER NUMBER 000890471 DATED 06/02/2018. RECEIVED FROM GAC SAV. WORK DONE IAW GAC DWG 1159CS20305 REV. J. Completed LINE REAMED INSTALLED BUSHING TO 0.4372. WORK DONE IAW GAC DWG 1159C520305 REV. J. Discrepancy: 14.64 WHILE C/W CMP CODE 554015 RUDDER / HINGE INSPECTION FOUND VERTICAL ATTACH FITTING INDEX 1-1 IS OUT OF DIMENSIONAL TOLERANCE Resolution: RQCI REMOVED OUT OF TOLERANCE BUSHING P/N 11595B30210-57 FROM UPPER RUDDER HINGE ATTACH FITTING INDEX 1-1 AND INSTALLED A NEW BUSHING P/N 1159SB30210-57. RECEIVED FROM GULFSTREM SAVANNAH WITH AUTHORIZATION # ODA-511131-CE. REFERENCE FAA FORM 8130-3 WITH FORM TRACKING # 20140817034915 DATED 17 AUG 2014. WORK DONE IAW GIV DWG 11595B30210 REV B. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.26 ® $142.00 $462.92 Pans USD: Time and Material $70.50 Total USD: $533.42 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 14.64 #1 1159SB30210-57 BUSHING 1 $70.50 $70.50 Discrepancy: 14.65 WHILE REMOVING L/H WING WEDGE ONE OF THE AFT BOLTS THAT EXTENDS THROUGH THE REAR BEAM IS SEIZED. Resolution: SOAKED FROZEN BOLT WITH PENETRATING OIL AND MILDLY HEATED AREA TO PROMOTE LOOSENING OF BOLT WITH NO EFFECT. RIGGED BUSHING BLOCK IN PLACE AND UNDERSIZE DRILLED BOLT AND PUNCHED OUT REMAINING BOLT. CLEANED BORE AND SURROUNDING AREA. REPROTECTED BORE AND SURROUNDING AREA. ALL WORK IAW G IV SRM 51-41-00 AND 51-13-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.15 ® $142.00 $447.30 Total USD: $44730 Discrepancy: 14.66 WHILE C/W CMP 554015 FOUND UPPER RUDDER HINGE TO HAVE MULTIPLE CORRODED AREAS AND ALL HINGES TO HAVE PITTING CORROSION. 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 63 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00809001 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Resolution: REMOVED MULTIPLE AREAS OF LIGHT SURFACE CORROSION / STAINING ON EXTERIOR SURFACES OF RUDDER UPPER HINGE USING GRAY SCOTCHBRITE AND HAND METHOD WITH NO BASE MATERIAL LOSS. CLEANED AND APPLIED EPDXY PRIMER / TOPCOAT AS REQUIRED. WORK DONE IN ACCORDANCE WITH GIV SRM CHAPTER 51-13-20. REF ITEM 14.60 FOR PITTING CORROSION REMOVAL FROM BORE ON RUDDER HINGE 1 (TOP) REF ITEM 14.61 FOR PITTING CORROSION REMOVAL FROM BORE ON RUDDER HINGE 2 (MIDDLE) REF ITEM 14.62 FOR PITTING CORROSION REMOVAL FROM BORE ON RUDDER HINGE 3 (BOTTOM) Billing Method Flours Rate Total Labor USD: Time and Material ST 6.50 @ $142.00 $923.00 Total USD: $923.00 Discrepancy: 14.67 WHILE PREPPING TO INSTALL RH IB GROUND SPOILER, SPOILER BOARD WAS DROPPED. Resolution: DUE TO EXTENDED DOWN TIME TO REPAIR EXISTING BOARD, REPLACED R/H GROUND SPOILER BOARD WITH A NEW ASSEMBLY. REPLACED THE DAMAGED SPOILER BOARD P/N 1159CSH40070-2 S/N 1091 98897 WITH A NEW BOARD P/N 1159CS40700-10 S/N 1193058. REFERENCE EASA FORM 1 FROM SAFRAN NACELLES LIMITED, APPROVAL # UK.21G.2117, FORM TRACKING # 80298609-1 DATED 27 OCT 2017. WORK DONE IAW ASC454A (REF ITEM 11.8) AND CMP 276076 (REF ITEM 13.69) Parts: Ref. No. Part number: Description Quantity 14.67 #1 1159C540700-10 SPOILER ASSY., GROUND FLT-RII 1 14.67 #2 MSI4183P-C6 WASHER FLAT CTSK-INCONEL,CD I PL 14.67 #3 AN9600616 WASHER I 14.67 #4 GAN512FP6C NUT REDUCED HEX - CSTL, LT 1 WEIGHT 14.67 #5 MS24665-302 COTTER PIN I 14.67 1/6 MS24665-304 COTTER PIN I 14.67 #7 MS27039-081! SCREW-MACHINE, PAN HD, CROSS 2 REC 14.67 #8 MS2I042-08 NUT-SELF LOCKING,RING BASE 2 14.67 #9 MS24665-372 COTTER PIN I 14.67 #10 NAS6703-3 BOLT I 14.67#11 NASII49D0316K WASHER-FLAT ANODIZED ALUM 2 14.67 #12 NAS75-3-008 BUSHING I 14.67 #13 MS2I042L3 NUT I 14.67 #14 NASII49C1063R WASHER-FLAT CRES I 14.67 #15 NASII49FN832P WASHER, FLAT STEEL 2 14.67 #16 NAS1149DN832II WASHER, FLAT 6 14.67 #17 NAS6706D28 BOLT-HEX HEAD, CLOSE I TOLERANCE 14.67#18 GABI0G6PL0625 BUSHING-PLAIN, SLIP FIT 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 64 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809002 Bill To: JEGE LLC Parts: Ref. No. Part number: WO It SC18654 Description Invoice Number: 6918002027 Quantity 14.67 #19 GABI0GI0PL0671 BUSHING-PLAIN, SLIP FIT 14.67 #20 GAB511GGI0D32A BOLT 14.67 #21 NAS1149D1063K WASHER 14.67 #22 GAN512FPI0C NUT REDUCED HEX-CSTL,LT WEIGHT 14.67 #23 MS35338-42 WASHER, LOCK 2 14.67 #24 1159CM30201-21 BUSHING 14.67 #25 NAS1149D1232K WASHER 14.67 #26 MS14144L12 NUT 14.67 #27 NAS6712D33 BOLT 14.67 #28 NAS1149D1216K WASHER-FLAT ANODIZED ALUM 14.67 #29 CM0110701 THINNER 14.67 #30 PR1422B1-2DAB-KIT SEALANT, 50 GRAM KIT (CUP & SYRINGE) Step: 14.67.1 Completed DUE TO EXTENDED DOWN TIME TO REPAIR EXISTING BOARD, REPLACED R./ GROUND SPOILER BOARD WITH A NEW ASSEMBLY. P/N 1159C54700-10 IS APPROVED FOR THIS AIRCRAFT VIA ASC 454A, REF ITEM 11.8 FOR COMPLIANCE. RECEIVED NEW BOARD P/N I159CS40700-10 S/N 1193058 FROM GULFSTREAM SAV, REF PACKING SLIP SHIPMENT # SASH#18-91861 DATED 6-20-18. ROUTED TO PAINT SHOP FOR TOPCOAT. Step: 14.67.2 Completed RECIEVED RAI IB GROUND SPOILER IN PAINT SHOP.SCUFF SANDED TOP AND BOTTOM SIDES.HUNG SPOILER AND WASHED TO REMOVE CONTAMINANTS.TAPED OFF AREA NOT TO BE PAINTED/PRIMED.APPLIED HIGII BUILD PRIMER TO TOP SIDE,AND JET-GLO BLACK TO BOTTOM SIDE.ALL WORK DONE I/A/W GIV SRM 51-07-10 Step: 14.67.3 Completed SANDED PRIMER ON TOP SIDE OF SPOILER BOARD AND MASKED OFF AREAS NOT TO BE PAINTED. SOLVENT CLEANED AREAS AND THEN APPLIED JET GLO BLACK TO PANEL. ALL WORK UMW GIV SRM 51-07-10 Step: 14.67.4 Completed ADDITIONAL CERT INFO FOR NEW SPOILER BOARD: REFERENCE EASA FORM I FROM SAFRAN NACELLES LIMITED, APPROVAL # UK.21G.2117, FORM TRACKING k 80298609-1 DATED 27 OCT 2017. Step: 14.67.5 Completed UNMASKED SPOILER BOARD AND THEN SANDED WITH 2000 TO 3000 GRIT SAND PAPER AND THEN BUFFED AND POLISHED. ALL WORK UAJW GIV SRM 51-07-10 Discrepancy: 14.68 WHILE INSTALL ING XM RADIO SATELLITE ANTENNA FOUND COAX CONECTOR SPINNING WHILE TURNING CABLE CONECTOR. Resolution: REMOVED BROKEN XM ANTENNA WITH P/N CI420-1 SIN 391333.INSTALLED A NEW XM ANTENNA WITH PIN C1420-1 S/N 564266 REFERENCE FAA FORM 8130-3 WITH FORM TRACKING NUMBER 20180203084218 FROM GULFSTREAM AEROSPACE CORPORATION DATED 03 FEB 2018 APPROVAL/AUTHORIZATION NO. ODA-511131-CE.INSTALLED USING 4 ORIGINAL SCREWS AND SEALED IAW GIV AMM 20-42-00 AND 20-70-11. UPDATED GIV CMP 316701 AS REQUIRED.REFERENCE 20.1.4 FOR OPS CHECK. Billing Method Hours Rate Total Labor USD: Time and Material ST 0.17 ® $142.00 524.14 Total USD: $24.14 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_WorkOrderRreliminaryInvoice.rpt 2011 Page 65 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00809003 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 14.69 WHILE C/W CMP GIV 276071 INBOARD FLIGHT SPOILER (LEFT) - REMOVAL/ INSTALLATION NOTED SPOT OF CORROSION ON LH FLAP TOP SKIN AT LOCATION OF SPOILER BOARD CONTACT. Resolution: REMOVED CORROSION ON LH FLAP TOP SKIN AT IB EDGE ABOUT 29" AFT OF LEADING EDGE. ACCOMPLISHED REPAIR AT THE ONE MOST INBD LOCATION ON LH FLAP TOP SKIN AS REQUIRED IN ENGINEERING DISPOSITION. PERFORMED ULTRASONIC THICKNESS INSPECTION AND FOUND THE POST BLEND REMAINING NDT THICKNESS MEASUREMENTS ON THE LH FLAP 1159CS20800-55 SKIN ARE STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. TOUCHED UP BARE METALAND REWORKED AREAS WITH FINISH #213 ALODINE PER GAMPS 6113, #3012 EPDXY PRIMER PER GAMPS 3116 AND TOP COAT TO MATCH CUSTOMER PAINT PER CAMPS 4000. ALL WORK DONE IN ACCORDANCE WITH ENGINEERING DISPOSITION SC18654.14.69 STEP 4 AND GIV CPCM 20-50-01. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.76 ® $142.00 $533.92 Labor USD: Time and Material ST 3.93 ® $231.00 $907.83 Total USD: $1,441.75 Step: 14.69.1 Completed PERFORMED ULTRASONIC THICKNESS INSPECTION ON LEFT FLAP TOP OF SKIN. MEASUREMENTS WRITTEN ON AIRCRAFT. INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL "2.0 ULTRASONIC REVISION 25 DECEMBER 15TH, 2017. Step: 14.69.2 Completed STEP OUT OF ORDER REMOVED CORROSION AS REQUIRED FROM LH FLAP TOP SKIN AT IB EDGE ABOUT 29" AFT OF LEADING EDGE. SINGLE LARGE PIT WAS LEFT IN THIS AREA AND SUBJECT TO ENGINEERING REMEDIATION. A SECOND SPOTOF CORROSION WAS ALSO REMOVED ABOUT 26" AFT OF LEADING EDGE AND 6" OB OF IB EDGE OF FLAP. ALL WORK IAW GIV CPCM 20-50-01. Step: 14.69.3 Completed REQUEST ENGINEERING TO EVALUATE CORROSION ON FLAP SKIN. Step: 14.69.4 Completed ENGINEERING DISPOSITION: THE POST BLEND REMAINING NDT THICKNESS MEASUREMENTS ON THE LH FLAP I159C520800-55 SKIN ARE STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. ENSURE THAT A MINIMUM 20 TO 1 WIDTH TO DEPTH BLEND RATIO AND 125 RIM OR BETTER SURFACE AND EDGE FINISH WAS MAINTAINED. AT THE ONE MOST INBD LOCATION PROTECTTHE SUBSTRUCTURE AND DRILL (I) EA #50 DIA HOLE THROUGH SKIN ONLY AND AERODYNAMICALLY FILL AND FAIR IAW CAMPS 7102. TOUCH BARE METAL AND REWORK WITH FINISH #213 ALODINE PER CAMPS 6113, #3012 EPDXY PRIMER PER GAMPS 3116 AND TOP COAT TO MATCH CUSTOMER PAINT PER GAMPS 4000. 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_WorkOrderPrelintinaryInvoice.rpt 2011 Page 66 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00809004 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Discrepancy: 14.70 ITEM TO TRACK 8100-9 AND 337 FOR FLIGHT CONTROL SURFACE HINGE FITTINGS REPAIRED IAW DWG SE05000102 Resolution: RQCI PERFORMED REWORK OF RUDDER ACTUATOR FORWARD ATTACH FITTING - F.S. 757.562 IN ACCORDANCE WITH GULFSTREAM DRAWING NO. 1159RDB729, NO REVISION, -901 INST. THIS MAJOR REPAIR IS SUBSTANTIATED BY FAA FORM 8100-9, DATED 06/15/2018, PROJECT NO. TR-07-2018-0014, FROM GULFSTREAM SAVANNAH AUTHORIZATION# ODA-511131-CE, CERT 0336099. PERFORMED THE FOLLOWING REPAIRS TO FLIGHT CONTROL HINGE FITTINGS IN ACCORDANCE WITH GULFSTREAM DRAWING NO. SE05000102, REV. E. STD. REPAIR - CONTROL SURFACE HINGE FITTINGS: 1) PERFORMED REPAIR SE05000102-913D6-20 TO L/H #3 AILERON HINGE FITTING P/N 1159WM20202-5. 2) PERFORMED FIRST INCREMENT O/S REPAIR TO L/H AILERON #1 HINGE HOLES (3 PLACES). 3) PERFORMED REPAIR SE05000102-911P5-2I TO L/H ELEVATOR HINGE #4. 4) PERFORMED REPAIR SE05000102-912S88-1 TO L/H ELEVATOR TRIM TAB HINGE# 1 INBOARD LUG. 5) PERFORMED REPAIR SE05000102-911P2-5 TO L/H ELEVATOR TRIM TAB HINGE# 1 OUTBOARD LUG. 6) PERFORMED REPAIR SE05000102-911P1-5 TO R/H ELEVATOR TRIM TAB HINGE# 1 OUTBOARD LUG. 7) PERFORMED REPAIR SE05000102-911P1-5 TO R/H ELEVATOR TRIM TAB HINGE# 2 OUTBOARD LUG. 8) PERFORMED REPAIR SE05000102-914PI-28 TO RUDDER TOP HINGE. 9) PERFORMED REPAIR SE05000102-914PI-27 TO RUDDER MIDDLE HINGE. 10) PERFORMED REPAIR SE05000102-913D3-26 TO RUDDER LOWER HINGE. THIS MAJOR REPAIR IS SUBSTANTIATED BY (2 EA) FAA FORM 8100-9, DATED 06/22/2018, PROJECT NO. TR-07-2018-0014, FROM GULFSTREAM SAVANNAH AUTHORIZATION# ODA-511131-CE, CERT 0336929 AND 0336930. THESE REPAIRS HAVE NO EFFECT ON CURRENT ICA. WEIGHT AND BALANCE EFFECT: NONE AFM SUPPLEMENT: NONE EXECUTED FAA FORM 337 DATED 26 JUN 2018. Billing Method Flours Rate Total Labor USD: Time and Material ST 3.29 ® $142.00 $467.18 Labor USD: Time and Material ST 2.00 ® $231.00 $462.00 Total USD: $929.18 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 67 of 117 Printed: 6/28/2018 939:11A? Reel EFTA00809005 Bill To: JEGE LLC Step: 14.70.1 WO #: SC18654 Invoice Number: 6918002027 Completed (ITEM 14.20) PERFORMED REPAIR SE05000102-913D6-20 TO LH #3 AILERON HINGE FITTING P/N 1159WM20202-5. BORE MEASURES .4065, INSTALLED SE05000901-913D6-20 BUSHING (ITEM 14.21) PERFORMED FIRST INCREMENT OS REPAIR TO LII AILERON #1 HINGE HOLES (3 PLACES). BORES MEASURE 3280, INSTALLED NAS6605D40X, NAS6605D54X, AND NAS6605D66X O/S HARDWARE. (ITEM 14.44) PERFORMED REPAIR SE05000102-911P5-21 TO LII ELEVATOR HINGE #4. BORES MEASURE 3906 - .3911, INSTALLED SE05000102-911P5-2I REPAIR SLEEVE. (ITEM 14.52) PERFORMED REPAIR SE05000102-912588-1 TO Lli ELEVATOR TRIM TAB HINGE 1 INDEX I-I(AS DEFINED IN CMP 552011), BORE MEASURES .3905, INSTALLED SE05000102-912S88-1 BUSHING. (ITEM 14.52) PERFORMED REPAIR SE05000102-911P2-5 TO LII ELEVATOR TRIM TAB HINGE 1 INDEX I-3 (AS DEFINED IN CMP 552011), BORE MEASURES .4063, INSTALLED SE05000I02-9I1P2-5 SLEEVE. (ITEM 14.53) PERFORMED REPAIR SE05000102-91IP1-5 TO RH ELEVATOR TRIM TAB HINGE 1 INDEX 1-3 (AS DEFINED IN CUP 552011), BORE MEASURES .3905, INSTALLED SE05000I02-9I I PI-5 BUSHING. (ITEM 14.53) PERFORMED REPAIR 5E05000102-911P1-5 TO FtlI ELEVATOR TRIM TAB HINGE 2 INDEX 2-3 (AS DEFINED IN CMP 552011), BORE MEASURES .3905, INSTALLED SE05000102-911P1-5 BUSHING. (ITEM 14.60) PERFORMED REPAIR SE05000102-914P1-28 TO RUDDER TOP HINGE AND FITTING, BORES MEASURE .1898, INSTALLED 5E05000901-914P1-28 BUSHING. (ITEM 14.61) PERFORMED REPAIR SE05000102-914P1-27 TO RUDDER MIDDLE HINGE AND FITTING, BORES MEASURE 3898, INSTALLED 5E05000901-914P1-27 BUSHING. (ITEM 14.62) PERFORMED REPAIR SE05000102-913D3-26 TO RUDDER LOWER HINGE, THIRD OVERSIZE, BORE MEASURES 3755, INSTALLED 5E05000901-913D3-26 BUSHING Discrepancy: 14.71 WHILE GIVING AN OK TO INSTALLTHE CARPET FOUND 'C' SHAPED GOUGE IN THE TOP SKIN OF FLR-37 Resolution: ROUTED OUT FIBERGLASS LAYER OF 'C' SHAPE FLOOR BOARD PUNCTURES. FILLED PUNCTURE AREA HONEYCOMB CELLS WITH EA9394 ADHESIVE. APPLIED TWO PLIES OF FIBERGLASS 116 MIXED WITH EA956 RESIN TO REPAIRED PUNCTURE AREAS, AWAITING RESIN TO CURE. WORK PERFORMED IAW GAC SGER-004 53.6 - FLOORBOARD REPAIRS. Billing Method flours Rate Total Labor USD: Time and Material ST 3.49 @ $142.00 $495.58 Parts USD: Time and Material $52.02 Total USD: $547.60 Pans: Ret No. Part number: Description Quantity Sell price USD Extended USD 14.71 #1 EA9394-50G ADHESIVE, EPDXY, E-Z PAK, 50 I S26.01 $26.01 G,AS9277009 14.71 #2 EA9394-50G ADHESIVE, EPDXY, E-Z PAK, 50 1 S26.01 $26.01 G,AS9277009 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 68 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00809006 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Step: 14.71.1 Completed ROUTED OUT FIBERGLASS LAYER OF 'C' SHAPE FLOOR BOARD PUNCTURES. FILLED PUNCTURE AREA HONEYCOMB CELLS WITH EA9394 ADHESIVE. WORK PERFORMED IAW GAC SGER-004 53.6 - FLOORBOARD REPAIRS. Step: 14.71.2 Completed APPLIED TWO PLIES OF FIBERGLASS 116 MIXED WITH EA956 RESIN TO REPAIRED PUNCTURE AREAS, AWAITING RESIN TO CURL WORK PERFORMED IAW GAC SGER-004 53.6 - FLOORBOARD REPAIRS. Discrepancy: 14.72 WHILE INSTALLING R/H ELEVATOR HORN NOTED IB MOST PIVOT BORE TO BE WORN BEYOND LIMITS. Resolution: ITEM ENTERED IN ERROR. BUSHING REPLACED UNDER 14.63.3 Discrepancy: 14.73 WHILE CHECKING ELEVATOR BALANCE DUE TO TRIM TAB REPAIR NOTED ELEVATOR IS OUT OF BALANCE. IS 30 IN LB TRAILING EDGE HEAVY, LIMITS ARE 0 -10 INLB LEADING EDGE HEAVY. Resolution: DETERMINED OVERALL PAINT THICKNESS ON L/H ELEVATOR GREATER THEN THE .005 TOPCOAT BALANCE ALLOWANCE NOTED IN GAC DWG 1159E002 WET SANDED AND BUFFED EXISTING PAINT AS REQUIRED. RE-CHECKED ELEVATOR BALANCE AND FOUND TO BE WITHIN ALLOWABLE LIMITS. WORK DONE IAW GAC DWG 1159E002 REV D. Billing Method Flours Rate Total Labor USD: Time and Material ST 45.67 ® $142.00 $6,485.14 Labor USD: Time and Material ST 1.47 ® $231.00 $339.57 Total USD: $6,824.71 Discrepancy: 14.74 WHILE PERFORMING HYDRAULIC OPERATIONAL CHECKS NOTED HORIZONTAL PRESSURE LINE TO 'T BELOW COMBINED ACCUMULATOR (PN 1159H40016-710CTFtP8) TO BE LEAKING AT THE FITTING. TIGHTENING MADE IT WORSE. Resolution: BLED OFF HYD PRESSURE AND DISCONNECTED LINES TO TEE FITTING BELOW COMBINED ACCUMULATOR. REMOVED TEE FITTING P/N MS21912D8. FOUND TEE FITTING TO BE CRACKED. REPLACED WITH NEW FITTING P/N MS21912D8. INSTALLED WITH NEW PACKING PIN NAS1612-8A AND NEW RETAINER P/N MS28773-08. BOTH RECEIVED FROM BAF GAC STOCK. RECEIVED HYD TEE FITTING FROM GULFSTREAM SAVANNAH. REFERENCE PACKING SLIP WITH ENTERPRISE TRANSFER # 000897482 DATED 06/22/2018. OPS AND LEAK CHECK FOUND GOOD. WORK DONE IAW GIV MM CHAPTER 29-00-00 AND 20-70-10. ALSO COMPLETED COMBINED/FLIGHT HYDRAULIC SYSTEM RESERVIOR - FILLING PROCEDURE 29-01-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 6.67 ® $142.00 $947.14 Parts USD: Time and Material $130.30 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 69 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00809007 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Total USD: Parts: $1,077.44 Ref'. No. Part number: Description Quantity Sell price USD Extended USD 14.74 #1 MS21912D8 TEE FLARELESS TUBE-BIID ON I $92.70 $92.70 RUN 14.74 #2 D 1002IA-08 ELBOW SWIVEL-PERM TO I $35.12 $35.12 FLARELESS 14.74 #3 NASI612-8A SEAL I $0.64 $0.64 14.74 #4 NASI612-8A SEAL I $0.64 $0.64 14.74 #5 MS28773-08 RETAINER 2 $0.60 $1.20 Discrepancy: 14.75 WHILE C/W GIV CMP 271017 AILERON ACTUATOR (RIGHT) REMOVAL AND INSTALLATION NOTED R/H AILERON NOT CONTACTING LOWER STOP BEFORE CONTROL WHEEL STOP Resolution: RQCI VERIFIED RIGGING ON R/H LATERAL CONTROL SYSTEM AND RIGGED R/H AILERON LOWER STOP. ALL WORK DONE IAW GIV MM 27-02-00. OPS CHECK GOOD. Discrepancy: 14.76 WHILE PERFORMING GIV CMP 276030 SPEED BRAKE SYSTEM - RIGGING CHECK FOUND RIH INBOARD FLIGHT SPOILER TO BE PULLING DOWN TO HARD ONTO STOPS Resolution: RQCI SHORTENED FLIGHT SPOILER ACTUATOR INPUT ROD TO ELIMINATE FORCEFUL PULL DOWN OF FLIGHT SPOILER. ALL WORK DONE IAW GIV MM 27-02-00. OPS CHECK GOOD. Item: 15 72 MONTH TASKS (GIV SN 1085) Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes Part/Model #: AC Serial No/Tail No.: TSN/TSO: CSNICSO: 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 70 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809008 Bill To: JEGE LLC Discrepancy: 15.1 72 MONTH TASKS WO It SC18654 Invoice Number: 6918002027 Resolution: Labor USD: Total USD: ACCOMPLISH MISCELLANEOUS 72 MONTH CMP TASKS. (SEE EXHIBIT 2) NOTES: - CORRECTION OF DISCREPANCIES IS NOT INCLUDED IN THE QUOTED PRICE. - MATERIALS/OUTSIDE SERVICES WILL BE AS REQUIRED. - PRICING INCLUDES LABOR REQUIRED FOR TOUCH UP PAINT ON AREA AFFECTED BY THE WINGLET ATTACH HARDWARE INSPECTION. IN THE EVENT THE CUSTOMER REQUESTS A "BLOWN-IN" PAINT FINISH APPLIED, ESTIMATED COST CAN BE $5,000 - $7,000 IN LABOR AND MATERIALS AND WILL BE QUOTED THROUGH THE WORK CHANGE REQUEST PROCESS. RE: PROPOSAL# 7042687 R00 (GAC0218-2687-GIV-1085-R00)-1.2 *** LABOR ONLY Billing Method Hours Rate Total Flat Rate 533.232.00 533.232.00 Discrepancy: 15.2 Resolution: Parts USD: Total USD: Pans: ACCOMPLISH THE 72 MONTH SERVICE CMP TASKS BELOW: Billing Method Hours Rate Total Time and Material $4,024.90 $4,024.90 Ret No. Part number: Description Quantity Sell price USD Extended USD 15.2 #1 GAS55IB3C I2 SCREW 1 $4.93 $4.93 15.2 #2 GAS55IB3C7 SCREW 3 S0.78 $2.34 15.2 #3 BAF500B4QT SKYDROL 500B4 OIL IN QUART 2 $33.88 $67.76 CANS 15.2 44 MS24694549 SCREW 10 S0.23 $2.30 15.2 #5 MS24694-547 SCREW 10 S0.23 $230 15.2 #6 GAS550E3S8 SCREW-WASHER HEAD,SELF 24 $2.02 $48.48 LOCKING 15.2 #7 NAS1149D0363Il WASHER 2 S0.23 $0.46 15.2 #8 NASI202-2 BOLT I S0.25 $0.25 15.2 #9 MS24694-S50 SCREW, MACHINE, FLAT CTSK HD, 2 $0.23 $0.46 100 DEG, STRL, CROSS RECESSED 15.2 #10 MS24694S5I SCREW 2 S0.23 $0.46 15.2 #11 AS3510-02181C SAFETY CABLE KIT (AP) II CABLE 4 $27.02 $108.08 & I FERRULEI 15.2 #12 CIO-218 WIRE, SAFETY CABLE .032 x 6 53.52 S21.12 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 71 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00809009 Bill To: JEGE LLC Pans: Ref'. No. Part number: WO #: SCI8654 Description Invoice Number: 6918002027 Quantity Sell price USD Extended USD 15.2 #13 44GN011-3OZ TOUCHUP KIT,DEFT EPDXY SPRAY 1 $54.53 $54.53 PRIMER 15.2 #14 40945 BONDER, LOCTITE SUPER 409 GEL 1 525.05 $25.05 15.2 #I5 1159CSM20203-17 BOLT (LOW ALLOY) 2 5250.00 $500.00 15.2 #17 1159CSM20203-13 BOLT, LOW ALLOY, VERTICAL FIN 2 5204.92 $409.84 15.2 #19 GAN5I I B720 NUT 1 S35.11 $35.11 15.2 #20 NASI611-028A SEAL I S1. 15.2 #21 61524693552 S24693S52 SCREW, 100 DEGREE 2 S1.25 50.4525 $0.90 COUNTERSINK 15.2 #22 M524693529 SCREW 2 50.38 $0.76 15.2 #23 CAIOOOX6OZ COMPOUND, 6 OUNCE CORROSION 1 $145.95 $145.95 INHIBITIVE 15.2 #24 MS24693S34 SCREW, COUNTERSINK-100 2 $0.22 $0.44 DEGREE 15.2 #25 MS20002-10 WASHER 2 50.38 $0.76 15.2 #26 CORBAN35 COMPOUND,CORRISION I $20.64 $20.64 INHIBITOR QUART,I2 OZ 15.2 #27 MS29513-12I PACKING 4 50.31 $1.24 15.2 #28 61529513-1255 PACKING 4 50.42 $1.68 15.2 #29 MS24694-S50 SCREW, MACHINE, FLAT CTSK HD, 100 DEG, STRL, CROSS RECESSED 20 $0.23 $4.60 15.2 #30 15.2 #31 M524694C6 MS24694-C25 SCREW SCREW, MACHINE, FLAT 10 1 50.22 $ $2.20 $37.08 COUNTERSUNK HEAD, 100 DEG., CROSS RECESSED, UNC-2A AND UNF-2A 15.2 #32 GAB5IIGA3-5 BOLT 25 $1.84 $46.00 15.2 #33 GAB5IIGA3-4 BOLT I0 $1.87 $18.70 15.2 #34 GAB5IIGA3-7 HI-BOLT I 0 $2.07 $20.70 15.2 #35 515X333-2OZ KIT, TOUCH UP, EPDXY PRIMER, 2 I $29.26 $29.26 OZ, GREEN 15.2 #36 PS870B1-2-654 SEALANT, 6 OZ CARTRIDGE 654 I $60.56 $60.56 SEMKIT, 3.5 FL. OZ 15.2 #37 PR1776B1-2-654 SEALANT, 6 OZ SEM KIT (MEETS 2 $69.33 $138.66 SPEC ANIS3281 REV E) 15.2 #38 PRI440B1-2-654 SEALANT, 6 OUNCE #654 SEMKIT 3 $26.67 $80.01 1/2 HOUR WORK LIFE 15.2 #39 GAS551B3C11 SCREW 2 52.35 $4.70 15.2 #40 15.2 #41 61524694548 MS24694-S52 SCREW SCREW, MACHINE, FLAT CTSK HD, 20 4 S0.22 $0.23 $4.40 $0.92 100 DEG, STRL, CROSS RECESSED 15.2 #42 AN315-3R NUT 2 $0.23 $0.46 15.2 #43 CIO-218 WIRE, SAFETY CABLE .032 x I8" 4 53.52 $14.08 15.2 #44 NASI310-56D BOLT I $157.25 $157.25 15.2 #45 S24665-302 61524665-302 $0.92 COTTER PIN 4 50.23 15.2 #46 MS24665-153 PIN, COTTER 5 50.22 $1.10 15.2 #47 II59CM20264-13 PIN, CRANK ASSY - LAT SYS 1 $515.00 $515.00 15.2 #48 220 LUBRICANT, 12 OUNCE AIR DRY I $31.56 $31.56 SOLID FILM 15.2 #49 AN320C8 NUT 10 55.64 $56.40 15.2 #50 M524665-302 COTTER PIN 18 $0.23 $4.14 15.2 #52 NAS6605D40X BOLT I $93.82 $93.82 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_WorkOrderPreliininaryInvoice.rpt 2011 Page 72 of 117 Printed: 6/28/2018 9:39:11M Reel EFTA00809010 Bill To: JEGE LLC Pans: Ref. No. Part number: WO It: SCI8654 Description Invoice Number: 6918002027 Quantity Sell price USD Extended USD 15.2 #53 NAS6605D54X BOLT, OVERSIZED 1 $174.02 $174.02 15.2 #54 NAS6605D66X BOLT 1 $240.00 $240.00 15.2 #55 PRI440B1-2-654 SEALANT,6OZ #654 SEMKIT I $26.67 $26.67 15.2 #56 MS24665-302 COTTER PIN 5 $0.23 S1.15 15.2 #57 MS24665-153 PIN, COTTER 22 $0.22 $4.84 15.2 #58 NA56608D23 BOLT 1 $16.93 $16.93 15.2 #59 1159CSNI20095-15 BUSHING 2 $90.91 $181.82 15.2 #60 1159CSNI20094-7 SLEEVE I $63.64 $63.64 15.2 #61 MSI7825-7 NUT SELF I $5.25 $5.25 LKG-CASTELLATED,STEEL 15.2 #62 AN960D716L WASHER FLAT-ALUM,I/64 TIM 1 $0.76 $0.76 15.2 #63 MS24665-304 COTTER PIN 2 $0.23 $0.46 15.2 #66 MS24693-C25 SCREW 2 $1.13 $2.26 15.2 #68 MS24693S26 SCREW,MACHINE,FLAT CNTRSNK 3 $0.23 $0.69 HD,100 DEG 15.2 #69 CI0-218 WIRE, SAFETY CABLE .032 x 18" 4 $3.52 $14.08 15.2 #70 PRI440B1-2-654 SEALANT,6OZ #654 SEMKIT 4 $26.67 $106.68 15.2 #71 PRI440B1-2-654 SEALANT,6OZ #654 SEMKIT 2 $26.67 $53.34 15.2 #72 MS24694-S50 SCREW,MACHINE,FLAT CTSK 32 $0.23 $736 FID,100DEG,STRL 15.2 #73 MS24665-306 COTTER PIN 1 $0.23 S0.23 15.2 #74 MS24665-372 COTTER PIN 2 $0.23 50.46 15.2 #75 MS24665-I53 PIN, COTTER 4 $0.22 $0.88 15.2 #76 PR1440B1-2-654-6OZ SEALANT, 6 OUNCE #654 SEMKIT i $0.00 50.00 15.2 #78 PRI440B1-2-654 SEALANT,6OZ #654 SEMKIT I $26.67 $26.67 15.2 #79 NASI580C3T4 BOLT IS $0.75 $11.25 15.2 #80 MS20002C4 WASHER 2 $0.23 $0.46 15.2 #81 NA51149F0432P WASHER, FLAT STEEL (SAME AS 3 50.23 $0.69 AN960-416L) 15.2 #82 MSI7826-4 NUT 2 $1.60 $3.20 15.2 #83 MS24694-S52 SCREW,MACHINE,FLAT CTSK 30 50.23 $6.90 HD,100DEG,STFtL 15.2 #84 MS24694S51 SCREW 6 $0.23 $138 15.2 #85 MS24694S7 SCREW 30 $0.23 $6.90 15.2 #86 NAS620CI0L WASHER, FLAT, REDUCED OUTSIDE 4 50.23 $0.92 DIAMETER 15.2 #87 NAS620CI0L WASHER, FLAT, REDUCED OUTSIDE 4 50.23 $0.92 DIAMETER 15.2 #88 500B4-55GAL SKYDROL OIL (55 GAL DRUM) 12 $19.77 $237.24 15.2 #89 NASI919B05S03 RIVET- BLIND, PROTRUDING HEAD 4 51.95 $7.80 15.2 #90 NASI919B05-04 RIVET BLIND-PROTRUDING HEAD 1 $4.96 $4.96 15.2 #91 MS24694-S52 SCREW,MACHINE,FLAT CTSK 10 50.23 $230 FID,100DEG,STRL 15.2 #92 MS24694-S52 SCREW,MACHINE,FLAT CTSK 20 50.23 $4.60 FID,100DEG,STRL 15.2 #93 NASI581F3T2 BOLT 10 $0.53 $5.30 15.2 #94 MS24665-I53 PIN, COTTER 10 $0.22 $2.20 15.2 #95 CIO-218 WIRE, SAFETY CABLE .032 x 18" 5 $3.52 $17.60 15.2 #96 AN525-10R8 SCREW 8 $0.31 $2.48 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 73 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00809011 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Step: 15.2.1 Completed PERFORMED INITIAL OK TO CLOSE FOR THE FOLLOWING FUEL PANELS, 531BZ, 54IAB-3, 631BZ, 641AB-3. Step: 15.2.2 Completed COMPLETED 1ST INSPECT FOR AN OK TO CLOSE LM WING FUEL PANELS 2I-FT-2,3 AND 15. Discrepancy: 15.3 CMP GIV 291091 Combined Hydraulic Filter (Main Pressure) - Inspection Resolution: COMPLIED WITH CMP GIV 291091 Combined Hydraulic Filter (Main Pressure) - Inspection Billing Method flouts Rate Total Parts USD: Time and Material $152.71 Total USD: $152.71 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 153 #1 AC-B45I F-12 FILTER ELEMENT 1 5152.71 $152.71 Discrepancy: 15.4 CMP GIV 291011 Combined System Manifold Filter and Filter Bowl (Main Pressure) - Removal / Installation Resolution: REMOVED THE TIME CHANGED MAIN PRESSURE HYDRAULIC FILTER P/N ACB451F12 SIN NSN. INSTALLED A NEW MAIN PRESSURE HYDRAULIC FILTER P/N ACB451F12 SIN NSN. RECEIVED FROM PALL CORPORATION REFERENCE COC WITH DOCUMENT NUMBER 8000380530 DATED 10/30/2015. WORK DONE JAW CMP GIV 291011 COMBINED SYSTEM MANIFOLD FILTER AND FILTER BOWL MAIN PRESSURE REMOVAL AND INSTALLATION. REFERENCE ITEM 20.1 STEP 20.1.1 FOR LEAK CHECKS. Discrepancy: 15.5 CMP GIV 291057 Combined / Flight Hydraulic System Reservoir - Filling Procedures Resolution: Discrepancy: 15.6 CMP GIV 291092 Combined Hydraulic Filter (Main Return) - Inspection Resolution: COMPLIED WITH CMP GIV 291092 Combined Hydraulic Filter (Main Return) - Inspection Billing Method flouts Rate Total Parts USD: Time and Material $212.16 Total USD: $212.16 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 74 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809012 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Pans: Ref'. No. Part number: Description Quantity Sell price USD Extended USD 15.6 #1 AC-B45I F-16 FILTER ELEMENT 1 $212.16 $212.16 Discrepancy: 15.7 CMP GIV 291013 Combined System Manifold Filter and Filter Bowl (Main Return) - Removal / Installation Resolution: REMOVED THE TIME CHANGED MAIN RETURN HYDRAULIC FILTER WITH P/N ACB451F16 S/N NSN. INSTALLED A NEW MAIN RETURN HYDRAULIC FILTER WITH P/N ACB451F16 S/N NSN RECEIVED FROM PALL CORPORATION REFERENCE COC WITH DOCUMENT NUMBER 8000380253 DATED 10/30/2015. WORK DONE IAW CMP GIV 291013 COMBINED SYSTEM MANIFOLD FILTER AND FILTER BOWL (MAIN RETURN) - REMOVAL AND INSTALLATION. REFERENCE ITEM 20.1 STEP 20.1.1 FOR LEAK CHECKS. Discrepancy: 15.8 CMP GIV 291093 Combined Hydraulic Filter (Engine-driven Pump Bypass) - Inspection Resolution: COMPLIED WITH CMP GIV 291093 Combined Hydraulic Filter (Engine-driven Pump Bypass) - Inspection Billing Method flours Rate Total Parts USD: Time and Material $89.53 Total USD: $89.53 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.8 #1 AC-B451F-8 FILTER ELEMENT 1 $89.53 $89.53 Discrepancy: 15.9 CMP GIV 291009 Combined System Manifold Filter and Filter Bowl (Engine-driven Pump Bypass) - Removal / Installation Resolution: REMOVED THE TIME CHANGED ENGINE DRIVEN PUMP BYPASS HYDRAULIC FILTER PIN ACB451F8 S/N NSN. INSTALLED A NEW ENGINE DRIVEN PUMP BYPASS HYDRAULIC FILTER P/N ACB451F8 S/N NSN. RECEIVED FROM PALL CORPORATION REFERENCE COC WITH DOCUMENT NUMBER 8001374737 DATED 12/29/2016. WORK DONE IAW CMP GIV 291009 COMBINED SYSTEM MANIFOLD FILTER AND FILTER BOWL ENGINE DRIVEN PUMP BYPASS REMOVAL INSTALLATION. REFERENCE ITEM 20.1 STEP 20.1.1 FOR LEAK CHECKS. Discrepancy: 15.10 CMP GIV 291094 Flight Hydraulic Filter (Main Pressure) - Inspection Resolution: COMPLIED WITH CMP GIV 291094 Flight Hydraulic Filler (Main Pressure) - Inspection 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 75 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00809013 Bill To: JEGE LLC WO It: SC18654 Invoice Number: 6918002027 Billing Method Parts USD: Time and Material Total USD: Pans: Ref. No. Part number: Flours Rate Total $152.71 $152.71 Description Quantity Sell price USD Extended USD 15.10 #1 AC-B451F-12 FILTER ELEMENT 1 $152.71 $152.71 Discrepancy: 15.11 CMP GIV 291012 Flight System Manifold Filter and Filter Bowl (Main Pressure) - Removal / Installation Resolution: REMOVED THE TIME CHANGED MAIN PRESSURE HYDRAULIC FILTER P/N ACB451F12 S/N NSN. INSTALLED A NEW MAIN PRESSURE HYDRAULIC FILTER P/N ACB451F12 S/N NSN. RECEIVED FROM PALL CORPORATION REFERENCE COC WITH DOCUMENT NUMBER 8000380530 DATED 10/30/2015. WORK DONE IAW CMP GIV 291012 FLIGHT SYSTEM MANIFOLD FILTER AND FILTER BOWL MAIN PRESSURE REMOVAL AND INSTALLATION REFERENCE ITEM 20.1 STEP 20.1.1 FOR LEAK CHECKS. Discrepancy: 15.12 CMP GIV 291096 Flight Hydraulic Filter (Main Return) - Inspection Resolution: COMPLIED WITH CMP GIV 291096 Flight Hydraulic Filter (Main Return) - Inspection Billing Method flouts Rate Total Parts USD: Time and Material $212.16 Total USD: $212.16 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.12 #1 AC-B451F-16 FILTER ELEMENT 1 $212.16 $212.16 Discrepancy: 15.13 CMP GIV 291014 Flight System Manifold Filter and Filter Bowl (Main Return) - Removal / Installation Resolution: REMOVED THE TIME CHANGED MAIN RETURN HYDRAULIC FILTER WITH P/N ACB451F16 S/N NSN. INSTALLED A NEW MAIN RETURN HYDRAULIC FILTER WITH P/N ACB451F16 S/N NSN RECEIVED FROM PALL CORPORATION REFERENCE COC WITH DOCUMENT NUMBER 8000380253 DATED 10/30/2015. WORK DONE IAW CMP GIV 291014 FLIGHT SYSTEM MANIFOLD FILTER AND FILTER BOWL MAIN RETURN REMOVAL AND INSTALLATION. REFERENCE ITEM 20.1 STEP 20.1.1 FOR LEAK CHECKS. Discrepancy: 15.14 CMP GIV 291097 Flight Hydraulic Filter (Engine-driven Pump Bypass) - Inspection 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 76 of 117 Printed: 6/28/2018 9:39:11A? Reel EFTA00809014 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Resolution: COMPLIED WITH CMP GIV 291097 Flight Hydraulic Filter (Engine-driven Pump Bypass) - Inspection Billing Method flours Rate Total Parts USD: Time and Material $89.53 Total USD: $89.53 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.14 #1 AC-B45IF-8 FILTER ELEMENT 1 $89.53 $89.53 Discrepancy: 15.15 CMP GIV 291010 Flight System Manifold Filter and Filter Bowl (Engine-driven Pump Bypass) - Removal / Installation Resolution: REMOVED THE TIME CHANGED ENGINE DRIVEN PUMP BYPASS HYDRAULIC FILTER PIN ACB451F8 S/N NSN. INSTALLED A NEW ENGINE DRIVEN PUMP BYPASS HYDRAULIC FILTER P/N ACB451F8 S/N NSN. RECEIVED FROM PALL CORPORATION REFERENCE COC WITH DOCUMENT NUMBER 8001374737 DATED 12/29/2016. WORK DONE IAW CMP GIV CMP GIV 291010 FLIGHT SYSTEM MANIFOLD FILTER AND FILTER BOWL ENGINE DRIVEN PUMP BYPASS REMOVAL AND INSTALLATION. REFERENCE ITEM 20.1 STEP 20.1.1 FOR LEAK CHECKS. Discrepancy: 15.16 CMP GIV 292010 Auxiliary Hydraulic Filter (Pressure) - Inspection I Replacement Resolution: COMPLIED WITH CMP GIV 292010 Auxiliary Hydraulic Filter (Pressure) - Inspection / Replacement Billing Method flours Rate Total Parts USD: Time and Material $89.53 Total USD: $89.53 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.16 #1 AC-B451F-8 FILTER ELEMENT 1 589.53 $89.53 Discrepancy: 15.17 CMP GIV 292026 Auxiliary Hydraulic System Filter Element and Bowl (Pressure) - Removal / Installation Resolution: COMPLIED WITH CMP GIV 292026 Auxiliary Hydraulic System Filter Element and Bowl (Pressure) - Removal / Installation 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 77 of 117 Printed: 6/28/2018 939:11AI Rent EFTA00809015 Bill To: JEGE LLC WO tt: SCI8654 Invoice Number: 6918002027 Discrepancy: 15.18 CMP GIV 292012 Auxiliary Hydraulic Filter (Return) - Inspection / Replacement Resolution: COMPLIED WITH CMP GIV 292012 Auxiliary Hydraulic Filter (Return) - Inspection / Replacement Billing Method flours Rate Total Parts USD: Time and Material $89.53 Total USD: $89.53 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 15.18 #1 AC-B451F-8 FILTER ELEMENT 1 $89.53 $89.53 Discrepancy: 15.19 CMP GIV 292027 Auxiliary Hydraulic System Filter Element and Bowl (Return) - Removal / Installation Resolution: REMOVED THE TIME CHANGED AUXILIARY HYDRAULIC RETURN FILTER P/N ACB45IF8 S/N NSN. INSTALLED A NEW AUXILIARY HYDRAULIC RETURN FILTER P/N ACB451F8 S/N NSN. RECEIVED FROM PALL CORPORATION REFERENCE COC WITH DOCUMENT NUMBER 8001374737 DATED 12/29/2016. WORK DONE IAW CMP GIV 292027 AUXILIARY HYDRAULIC SYSTEM FILTER ELEMENT AND BOWL (RETURN) - REMOVAL/ INSTALLATION REFERENCE ITEM 20.1 STEP 20.1.1 FOR LEAK CHECKS. Discrepancy: 15.20 CMP GIV 351021 Crew Oxygen Mask / Regulator (Pilot) - Overhaul Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.21 CMP GIV 351005 Crew Oxygen System (Pilot) - Operational Test Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.22 CMP GIV 351022 Crew Oxygen Mask / Regulator (Copilot) - Overhaul Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW 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 78 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00809016 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 15.23 CMP GIV 351006 Crew Oxygen System (Co-Pilot) - Operational Test Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.24 CMP GIV 351023 Crew Oxygen Mask / Regulator (Observer) - Overhaul Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.25 CMP GIV 351007 Crew Oxygen System (Jumpseat) - Operational Test Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.26 CMP GIV 510075 Composite Components - Visual / NDT Inspection Resolution: COMPLIED WITH CMP GIV 510075 Composite Components - Visual / NDT Inspection Discrepancy: 15.27 CMP GIV 510405 Wing To Fuselage Attachments (Left) - Radiographic Inspection Resolution: COMPLIED WITH CMP GIV 510405 Wing To Fuselage Attachments (Left) - Radiographic Inspection Step: 15.27.1 Completed PERFORMED X-RAY INSPECTION TO CHECK FOR FAYING SURFACES OF REAR BEAM WEB I CAP ANGLES AND ATTACH FITTING FORWARD VERTICAL FLANGES (AREA COVERED BY ATTACH FITTINGS: LEFT AND RIGHT - FS 452, BL 33).. INSPECTION PERFORMED IN ACCORDANCE WITH CMP GIV 510405 PROCEDURE B FIGURE 2 AND GULFSTREAM GIV NONDESTRUCTIVE TESTING PROCEDURES MANUAL, PART II, PROCEDURE NO. 57-00-011. WING TO FUSELAGE ATTACHMENT- RADIOGRAPHIC INSPECTION. NO DEFECTS NOTED AND RADIOGRAPH PROVIDED TO ENGINEERING. 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 79 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00809017 Bill To: JEGE LW WO #: SC1865.1 Invoice Number: 6918002027 Discrepancy: 15.28 CMP GIV 280010 Deluding Procedures Resolution: COMPLIED WITH CMP GIV 280010 Deluding Procedures Discrepancy: 15.29 CMP GIV 280018 Fuel Tank (Left) - Leak Check Resolution: COMPLIED WITH CMP GIV 280018 Fuel Tank (Left) - Leak Check Discrepancy: 15.30 CMP GIV 282015 Fuel Boost Pump (Left Main) - Removal / Installation Resolution: N/A ALTERNATE (OB) BOOST PUMP IS REMOVED FOR WING LINK INSPECTION Discrepancy: 15.31 CMP GIV 282038 Fuel Pump Auto Change - Operational Test Resolution: Discrepancy: 15.32 CMP GIV 510410 Wing To Fuselage Attachments (Right) - Radiographic Inspection Resolution: COMPLIED WITH CMP GIV 510410 Wing To Fuselage Attachments (Right) - Radiographic Inspection Step: 15.32.1 Completed PERFORMED X-RAY INSPECTION TO CHECK FOR RAYING SURFACES OF REAR BEAM WEB I CAP ANGLES AND ATTACH FITTING FORWARD VERTICAL FLANGES (AREA COVERED BY ATTACH FITTINGS: LEFT AND RIGHT - FS 452, BL 33).. INSPECTION PERFORMED IN ACCORDANCE WITH CMP GIV 510410 PROCEDURE B FIGURE 2 AND GULFSTREAM GIV NONDESTRUCTIVE TESTING PROCEDURES MANUAL, PART II, PROCEDURE NO. 57-00-011. WING TO FUSELAGE ATTACHMENT- RADIOGRAPHIC INSPECTION. NO DEFECTS NOTED AND RADIOGRAPH PROVIDED TO ENGINEERING. Discrepancy: 15.33 CMP GIV 280019 Fuel Tank (Right) - Leak Check Resolution: COMPLIED WITH CMP GIV 280019 Fuel Tank (Right) - Leak Check 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 80 of 117 Printed: 6/28/2018 939:11M Reel EFTA00809018 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 15.34 CMP GIV 282016 Fuel Boost Pump (Right Main) - Removal / Installation Resolution: N/A ALTERNATE (OB) BOOST PUMP IS REMOVED FOR WING LINK INSPECTION Discrepancy: 15.35 CMP GIV 537010 Aft Wing / Fuselage Fairing (Left) Corrosion - Inspection Resolution: COMPLIED WITH CMP GIV 537010 Aft Wing / Fuselage Fairing (Left) Corrosion - Inspection Discrepancy: 15.36 CMP GIV 537011 Aft Wing/ Fuselage Fairing (Right) Corrosion - Inspection Resolution: COMPLIED WITH CMP GIV 537011 Aft Wing / Fuselage Fairing (Right) Corrosion - Inspection Discrepancy: 15.37 CMP GIV 539472 Aft Pressure Bulkhead - Inspection Resolution: COMPLIED WITH CMP GIV 539472 Aft Pressure Bulkhead - Inspection Discrepancy: 15.38 CMP GIV 539505 Below Emergency Window (Left No. I) Corrosion - Inspection Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.39 CMP GIV 562007 Emergency Exit and Cabin Windows - Leak Check Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW 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 81 of 117 Printed: 6/28/2018 939:11M Reel EFTA00809019 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Discrepancy: 15.40 CMP GIV 562050 Emergency Window (Left No. I) - Removal / Installation Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.41 CMP GIV 539506 Below Emergency Window (Left No. 2) Corrosion - Inspection Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.42 CMP GIV 562051 Emergency Window (Left No. 2) - Removal / Installation Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.43 CMP GIV 539507 Below Emergency Window (Right No. 1) Corrosion - Inspection Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.44 CMP GIV 562052 Emergency Window (Right No. 1) - Removal i Installation Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.45 CMP GIV 539508 Below Emergency Window (Right No. 2) Corrosion - Inspection Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW 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 82 of 117 Printed: 6/28/2018 939:11A? Reel EFTA00809020 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Discrepancy: 15.46 CMP GIV 562053 Emergency Window (Right No. 2) - Removal / Installation Resolution: CUSTOMER DOESN'T WANT THIS CODE COMPLIED WITH NOW Discrepancy: 15.47 CMP GIV 552025 Elevator Leading Edge and Ballast Weight (Left) - Inspection Resolution: COMPLIED WITH CMP GIN' 552025 Elevator Leading Edge and Ballast Weight (Left) - Inspection Discrepancy: 15.48 CMP GIV 552026 Elevator Leading Edge and Ballast Weight (Right) - Inspection Resolution: COMPLIED WITH CMP GIV 552026 Elevator Leading Edge and Ballast Weight (Right) - Inspection Discrepancy: 15.49 CMP GIV 553010 Vertical Stabilizer Attach Fitting - Alternative Inspection Resolution: RQCI REMOVED 2 OLD AFT VERTICAL STABILIZER ATTACH HARDWARE WITH P/N 1159CSM20203-13. NSN. REPLACED WITH 2 NEW AFT VERTICAL STABILIZER ATTACH HARDWARE WITH P/N 1159CSM20203-13. NSN. ALL PARTS RECEIVED FROM GAC BAF STOCK. REMOVED 2 OLD FWD VERTICAL STABILIZER ATTACH HARDWARE WITH P/N 1159CSM20203-17. NSN. REPLACED WITH 2 NEW FWD VERTICAL STABILIZER ATTACH HARDWARE WITH P/N 1159CSM20203-17. NSN. REFERENCE PACKING SLIUP WITH SHIPMENT NUMBER MESG#18-10882 DATED 05/30/2018. FROM GAC SAVANNAH. ALL WORK DONE JAW WITH CMP GIV 553010 VERTICAL STABILIZER ATTACH FITTING - ALTERNATIVE INSPECTION 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_WorkOrderPrelintinaryInvoice.rpt 2011 Page 83 of 117 Printed: 6/28/2018 9:39:11M Reel EFTA00809021 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 15.50 ( 'M P 275001 Wing Flap Stabilizer - Operational Test Resolution: Discrepancy: 15.51 CMP GIV 275013 Emergency Flap System - Operational Test Resolution: Discrepancy: 15.52 CMP GIV 571033 Wing Sponson Rib (Left) - Inspection Resolution: COMPLIED WITH CMP GIV 571033 Wing Sponson Rib (Left) - Inspection Discrepancy: 15.53 CMP GIV 571034 Wing Sponson Rib (Right) - Inspection Resolution: COMPLIED WITH CMP GIN' 571034 Wing Sponson Rib (Right) - Inspection Discrepancy: 15.54 CMP GIV 572001 Wing Wedge (Left) - Inspection Resolution: COMPLIED WITH CMP GIN' 572001 Wing Wedge (Left) - Inspection Step: 15.54.1 Completed PERFORMED EDDY CURRENT INSPECTION PER GIV 572001 WING WEDGE LEFT WITH NO DEFECTS NOTED. INSPECTION PERFORMED IN ACCORDQANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL 3.0 EDDY CURRENT REVISION 7- SEPTEMBER 16TH. 2015. Discrepancy: 15.55 CMP GIV 572002 Wing Wedge (Right) - Inspection Resolution: COMPLIED WITH CMP GIN' 572002 Wing Wedge (Right) - Inspection 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 84 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00809022 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Step: 15.55.1 Completed PERFORMED EDDY CURRENT INSPECTION PER GIV 572002 WING WEDGE RIGHT WITH NO DEFECTS NOTED. INSPECTION PERFORMED IN ACCORDQANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL 3.0 EDDY CURRENT REVISION 7- SEPTEMBER 16TH, 2015. Discrepancy: 15.56 CMP GIV 573013 Winglet Attach Hardware (Left) - Inspection Resolution: COMPLIED WITH CMP GIV 573013 Winglet Attach Hardware (Left) - Inspection Step: 15.56.1 Completed PERFORMED EDDY CURRENT INSPECTION PER CMP GIV 573013 WINGLET ATTACH HARDWARE (LEFT) - INSPECTION AND GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL 3.0 EDDY CURRENT REVISION 7- SEPTEMBER 16TH, 2015.. NO DEFECTS NOTED. Discrepancy: 15.57 CMP GIV 573014 Winglet Attach Hardware (Right) - Inspection Resolution: COMPLIED WITH CMP GIV 573014 Winglet Attach Hardware (Right) - Inspection Step: 15.57.1 Completed PERFORMED EDDY CURRENT INSPECTION PER CMP GIV 573014 WINGLET ATTACH HARDWARE (RIGHT) - INSPECTION AND IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL 3.0 EDDY CURRENT REVISION 7- SEPTEMBER 16TH, 2015.NO DEFECTS NOTED. Discrepancy: 15.58 CMP GIV 783007 Engine Thrust Reverser Hot Short To Ground (Left) - Inspection Resolution: COMPLIED WITH CMP GIV 783007 Engine Thrust Reverser Hot Short To Ground (Left) - Inspection Discrepancy: 15.59 CMP GIV 346025 FMS CDU No. 1- Removal / Installation Resolution: REMOVED FMS CDU NO. 1, P/N 7007549-902 S/N 87010183. REINSTALLED A SERVICEABLE FMS CDU NO. 1, P17007549-902 S/N 87010183. ALL WORK DONE IN ACCORDANCE WITH CMP CODE 340200. Discrepancy: 15.60 CMP GIV 349800 Flight Management System No. 1 - Operational Check Resolution: COMPLIED WITH CMP GIV 349800 Flight Management System No. 1 - Operational Check 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 85 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809023 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 15.61 CMP GIV 783008 Engine Thrust Reverser Hot Short To Ground (Right) - Inspection Resolution: COMPLIED WITH CMP GIV 783008 ENGINE THRUST REVERSER HOT SHORT TO GROUND (RIGHT) - INSPECTION, CHECKED GOOD AT THIS TIME. Item: 16 72 MONTH TASKS DISCREPANCIES Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes ParVModel #: AC Serial NolTail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 16.1 WHILE C/W CMP 783008 ENGINE THRUST REVERSER HOT SHORT TO GROUND (RIGHT) - INSPECTION FOUND R/H TR SWITCH (S10) PINS J TO I TO HAVE HIGH RESISTANCE (>200 OHM) Resolution: RECHECKED R/H T/R SWITCH (S10) CONTINUITY RESISTANCE AT PIN J* AND I* WHILE T/R IN STOW POSITION FOUND GOOD (5 OHMS). CYCLED IT MANY TIMES FOUND GOOD AT THIS TIME. WORK DONE JAW GIV A.M.M. 3141-00 - T/R CONTROL SWITCH ADJUSTMENT/TEST, PAGE 510. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.75 @ $142.00 $390.50 Total USD: $390.50 Discrepancy: 16.2 WHILE C/W CMP GIV 572001 WING WEDGE (LEFT) - INSPECTION NOTED BUBBLING PAINT / CORROSION AT THE WINGLET TO WING, LOWER SKIN SEAM. Resolution: REMOVED CORROSION FROM NOTED AREAS AT MI LOWER WINGLET TO WING SKIN SEAM. PERFORMED THICKNESS CHECKS AND EVALUATED BY ENGINEERING, FOUND TO BE STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. PEENED WING PLANK WHERE REWORKED, APPLIED ALODINE, PRIMERED, AND TOPCOATED AS REQUIRED. REF STEPS FOR FURTHER DETAILS. WORK DONE IAW ENGINEERING DISPOSITION SC18654.16.2.4 AND GIV SRM 51-13-20, Billing Method Hours Rate Total Labor USD: Time and Material ST 5.27 @ $142.00 $748.34 Labor USD: Time and Material ST 2.47 @ $231.00 $570.57 Parts USD: Time and Material $29.26 Total USD: $1,348.17 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_WorkOrderPrelintinarylnvoice.rpt 2011 Page 86 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809024 Bill To: JEGE LLC WO it: SC18654 Invoice Number: 6918002027 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 16.2 #1 515X333-2OZ KIT, TOUCH UP, EPDXY PRIMER, 2 1 $29.26 829.26 OZ, GREEN Step: 16.2.1 Completed REMOVED BUBBLING PAINT TO FIND HEAVY PITTED CORROSION, REMOVED PITTED CORROSION BY MECHANICAL MEANS IAW GIV SRM 51-13-20 Step: 16.2.2 Completed PERFORMED ULTRASONIC THICKNESS MEASUREMEXTSS PER MAINTENANCE REQUEST AFTER MAINTENANCE REMOVED HEAVY PITTED CORROSION BY MECHANICAL MEANS FROM Lli WING AREA AND FUSELAGE IAW GIV SRM 51-13-20.INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL 2.0 ULTRASONIC REVISION 7 - SEPTEMBER 16TH, 2015. Step: 16.2.3 Completed REQUEST ENGINEERING EVALUATION OF REMAINING SKIN THICKNESS WHERE REWORKED. Step: 16.2.4 Completed ENGINEERING DISPOSITION: GAC CLASSIFIES THIS AS A MINOR REPAIR. THE REMAINING POST BLEND THICKNESSES FOLLOWING CORROSION BLENDING ON THE 1159W30701 WINGLET ASSY, 1I59WM40001, AND 1159WM40002 LOWER WING SKINS HAVE BEEN ANALYZED AND FOUND TO BE STRUCTURALLY ACCEPTABLE. ENSURE A 20:1 (WIDTH TO DEPTH) BLEND RATIO AND A I25RA SURFACE FINISH OR SMOOTHER WAS MAINTAINED WHILE BLENDING. IF ADDITIONAL BLENDING IS REQUIRED TO OBTAIN TILE BLEND RATIO OR SURFACE FINISH DO NOT DEEPEN THE BLENDED AREAS. INSPECT THE FASTENER HEADS IN THE AREAS OF CORROSION REMOVAL IF NO IDENTIFICATION MARKINGS ARE VISIBLE ON THE HEAD, REMOVE AND REPLACE FASTENER. PERFORM ROTO PEENING ON ALL REWORKED WING PLANKS SKINS PER CAMPS 2102 REQUIREMENTS; INTENSITY TO BE 0.002A TO 0.004A. TOUCH UP REWORKED BARE METAL WITH FINISH #213 (ALODINE PER CAMPS 6113), #3012 (EPDXY PRIMER PER GAMPS 3116), AND CUSTOMER TOPCOAT TO MATCH PER CAMPS 4000. Step: 16.2.5 Completed INSPECTED REWORK AREA AND NOTED NO FASTENERS WITH MISSING HEAD MARKINGS. PERFORMED ROTO PEENING ON ALL REWORKED WING PLANKS SKINS PER CAMPS 2102 REQUIREMENTS. ALLMAN GAUGE ID # 1452Z00 DUE MAY 2019. TOUCHED UP REWORKED BARE METAL WITH FINISH #213 (ALODINE PER CAMPS 6113)AND #3012 (EPDXY PRIMER PER CAMPS 3116) Discrepancy: 16.3 WHILE C/W CMP GIV 57200R WING WEDGE (RIGHT) - INSPECTION NOTED BUBBLING PAINT/ CORROSION AT THE WINGLET TO WING, LOWER SKIN SEAM. Resolution: REMOVED CORROSION FROM NOTED AREAS AT R/H LOWER WINGLET TO WING SKIN SEAM. PERFORMED THICKNESS CHECKS AND EVALUATED BY ENGINEERING, FOUND TO BE STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. PEENED WING PLANK WHERE REWORKED, APPLIED ALODINE, PRIMERED, AND TOPCOATED AS REQUIRED. REF STEPS FOR FURTHER DETAILS. WORK DONE IAW ENGINEERING DISPOSITION SC18654.16.3.4 AND GIV SRM 51-13-20, 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 87 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809025 Bill To: JEGE LLC WO ti: SCI8654 Invoice Number: 6918002027 Billing Method Hours Rate Total Labor USD: Time and Material ST 530 @ $142.00 $752.60 Labor USD: Time and Material ST 2.48 @ $231.00 $572.88 Parts USD: Time and Material 556.51 Total USD: $1,381.99 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 163 #1 PR1440B1-2DAB-KIT SEALANT, 50 GRAM KIT (CUP & 1 $27.25 $27.25 SYRINGE) 163 #2 515X333-2OZ KIT, TOUCH UP, EPDXY PRIMER, 2 1 $29.26 $29.26 OZ, GREEN Step: 163.1 Completed REMOVED BUBBLING PAINT TO FIND HEAVY PITTED CORROSION, REMOVED PITTED CORROSION BY MECHANICAL MEANS IAW GIV SRM 5I-I3-20. Step: 163.2 Completed PERFORMED ULTRASONIC THICKNESS MEASUREMENTSS PER MAINTENANCE REQUEST AFTER MAINTENANCE REMOVED HEAVY PITTED CORROSION BY MECHANICAL MEANS FROM RH WING AREA AND FUSELAGE IAW GIV SRM 51-13-20.INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL 2.0 ULTRASONIC REVISION 7 - SEPTEMBER 16TH, 2015. Step: 16.3.3 Completed REQUEST ENGINEERING EVALUATION OF REMAINING SKIN THICKNESS WHERE REWORKED. Step: 16.3.4 Completed ENGINEERING DISPOSITION: Step: 163.5 GAC CLASSIFIES THIS AS A MINOR REPAIR. THE REMAINING POST BLEND THICKNESSES FOLLOWING CORROSION BLENDING ON THE 1159W30701 WINGLET ASSY, 1159W11140001, AND 1159WM40002 LOWER WING SKINS HAVE BEEN ANALYZED AND FOUND TO BE STRUCTURALLY ACCEPTABLE. ENSURE A 20:1 (WIDTH TO DEPTH) BLEND RATIO AND A 125RA SURFACE FINISH OR SMOOTHER WAS MAINTAINED WHILE BLENDING. IF ADDITIONAL BLENDING IS REQUIRED TO OBTAIN TILE BLEND RATIO OR SURFACE FINISH DO NOT DEEPEN THE BLENDED AREAS. INSPECT THE FASTENER HEADS IN THE AREAS OF CORROSION REMOVAL IF NO IDENTIFICATION MARKINGS ARE VISIBLE ON THE HEAD, REMOVE AND REPLACE FASTENER. PERFORM ROTO PEENING ON ALL REWORKED WING PLANKS SKINS PER CAMPS 2102 REQUIREMENTS; INTENSITY TO BE 0.002A TO 0.004A. TOUCH UP REWORKED BARE METAL WITII FINISH #213 (ALODINE PER CAMPS 6113), #3012 (EPDXY PRIMER PER GAMPS 3116), AND CUSTOMER TOPCOAT TO MATCII PER GAMPS 4000. Completed INSPECTED REWORK AREA AND NOTED NO FASTENERS WITH MISSING HEAD MARKINGS. PERFORMED ROTO PEENING ON ALL REWORKED WING PLANKS SKINS PER CAMPS 2102 REQUIREMENTS. ALLMAN GAUGE ID # 1452Z00 DUE MAY 2019. TOUCHED UP REWORKED BARE METAL WITH FINISH #213 (ALODINE PER GAMPS 6113)AND #3012 (EPDXY PRIMER PER CAMPS 3116) 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 88 of 117 Printed: 6/28/2018 939:11M Ref: EFTA00809026 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Discrepancy: 16.4 WHILE C/W CMP 572001 LEFT WING WEDGE REMOVAL FOUND SPINNING RIVNUTS (6 EA) Resolution: COMPLIED WITH GAC BP SE05803901 TO GAIN ACCESSS TO SPINNING RIVNUT. REMOVED 1 RIVNUT P/N GAN512B3-166 AND INSTALLED 1 NEW RIVNUT WET PIN GAN5I2Et3-166. RECEIVED RIVNUTS FROM GAC STOCK. WORK DONE IAW GIV DWG 1159W40166 REV D AND SE05803901 REV B. REMOVED 5 SPINNING RIVNUTS P/N GAN512B3-166 AND INSTALLED 5 NEW RIVNUTS WET P/N GAN512B3-166. RECEIVED RIVNUTS FROM GAC STOCK. WORK DONE IAW GIV DWG 1159W40166 REV D. Labor USD: Parts USD: Total USD: Parts: Ref. No. Billing Method Hours Rate Total Time and Material ST 9.54 @ $142.00 $1,354.68 Time and Material Pan number: $178.26 $1,532.94 Description Quantity Sell price USD BLIND NUT COLLAR COLLAR COLLAR 16.4 #1 16.4 #2 16.4 #3 16.4 #4 Step: 16.4.1 Step: 16.4.2 Step: 16.4.3 GAN512B3-166 GAN512B3-116 GAN512B3-116 GAN512B3-116 Completed Completed Completed Extended USD 2 53.55 2 $15.56 I $15.56 8 $15.56 REMOVED S SPINNING RIVNUTS P/N GAN512B3-166 AND INSTALLED 5 NEW RIVNUTS WET PIN GAN5I2B3-166. RECEIVED RIVNUTS FROM GAC STOCK. WORK DONE IAW GIV DWG 1159W40166 REV D. COMPLIED WITH GAC BP SE05803901 TO GAIN ACCESSS TO SPINNING RIVNUT. REMOVED 1 RIVNUT P/N GAN5I2B3-166 AND INSTALLED 1 NEW RIVNUT WET PIN GAN512,33-166. RECEIVED RIVNUTS FROM GAC STOCK. WORK DONE IAW GIV DWG 1159W40166 REV D AND SE05803901 REV B. PERFORMED PRELIMINARY INSPECTION IN FUEL PANELAREAS 22FT-2, 22FT-3 AND 22FT-1S. $7.10 $31.12 $15.56 $124.48 Discrepancy: 16.5 WHILE VW 572002 RIGHT WING WEDGE REMOVAL FOUND SPINNING RIVNUTS (6 EA) Resolution: REMOVED 6 SPINNING RIVNUTS P/N GAN5I2B3-166 AND INSTALLED 6 NEW RIVNUTS WET PIN GAN512B3-166. RECEIVED RIVNUTS FROM GAC STOCK. REMOVED 1 SPINNING RIVNUTS P/N GAN512B3-366 AND INSTALLED 1 NEW RIVNUT WET P/N GAN512B3-166. RECEIVED RIVNUT FROM GAC STOCK WORK DONE IAW GIV DWG 1159W40166 REV D. Billing Method Hours Rate Total Labor USD: Time and Material ST 4.98 @ $142.00 $707.16 Parts USD: Time and Material $126.76 Total USD: $833.92 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 16.5 #1 GAN512B3-166 BLIND NUT 1 $3.55 16.5 #2 GAN512B3-116 COLLAR 3 S15.56 16.5 #3 GAN512B3-366 COLLAR 1 S14.29 16.5 #4 GAN51263-116 COLLAR 2 S15.56 16.5 #5 GAN512B3-116 COLLAR 2 S15.56 For detail description of the work complied with see the Work Order Detail report. $3.55 $46.68 $14.29 $31.12 $31.12 Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminarylnvoice.rpt 2011 Page 89 of 117 Printed: 6/28/2018 9:39:11.41 Reel EFTA00809027 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 16.6 WHILE C/W CMP CODE 573013 LEFT WINGLET ATTACH HARDWARE INSPECTION FOUND LJH WINGLET ATTACH FITTING VERTICAL HOLE 1 OUTBD AND 3 OUTBD, HORIZONTAL HOLE LOWER 4 HAVE TOOLING / CHATTER MARKS IN THE HOLE BORES. Resolution: NOTED TOOLING MARKS DEEMED INSIGNIFICANT IN NATURE AND WELL WITHIN SURFACE ROUGHNESS CRITERIA: 125 RMS AS PER GAC BP 1159WM40700. NOTED AREAS ABSENT HIGH METAL AND NO INTERFERENCE WITH ATTACH HARDWARE. CLEANED AND PRIMED ALL BARE AREAS AS REQUIRED. ALL WORK IAW G IV SRM 51-11-00. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.71 ® $142.00 $242.82 Total USD: $242.82 Discrepancy: 16.7 WHILE C/W CMP CODE 573013 LEFT WINGLET ATTACH HARDWARE INSPECTION FOUND LJH WINGLET ATTACH FITTING VERTICAL HOLE 2 OUTBOARD, 1, 2, 3 INBOARD, AND HORIZONTAL HOLE 1 LOWER HAVE CORROSION IN THE HOLE BORES. Resolution: CLEANED BORES OF ALL IMPERFECTIONS BY HAND WITH SCOTCH BRITE. NO MEASURABLE MATERIAL LOSS NOTED. CONFIRMED NO CORROSION PRESENT DURING FOLLOWING NDT INSPECTION. NO FURTHER DEFECTS NOTED. ALL WORK IAW G IV SRM 51-13-21. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.55 ® $142.00 $220.10 Total USD: $220.10 Discrepancy: 16.8 WHILE C/W CMP CODE 573014 RIGHT WINGLET ATTACH HARDWARE INSPECTION FOUND R/H WINGLET ATTACH FILLING VERTICAL HOLE 1, 3 OUTBOARD, 2, 3 INBOARD, AND HORIZONTAL HOLE 3, 5 LOWER, 4 UPPER HAVE CORROSION IN THE HOLE BORES. Resolution: CLEANED BORES OF ALL IMPERFECTIONS BY HAND WITH SCOTCH BRITE. NO MEASURABLE MATERIAL LOSS NOTED. CONFIRMED NO CORROSION PRESENT DURING FOLLOWING NDT INSPECTION. NO FURTHER DEFECTS NOTED. ALL WORK IAW G IV SRM 51-13-21. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.47 ® $142.00 $208.74 Total USD: $208.74 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 90 of 117 Printed: 6/28/2018 939:11.41 Reel EFTA00809028 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 16.9 WHILE CM CMP GIV 572001 WING WEDGE (LEFT) - INSPECTION NOTED SURFACE CORROSION ON TOP AFT OB SCREW LINE OF THE WING WEDGE. Resolution: REMOVED LIGHT SURFACE CORROSION WITH SCOTCH BRITE. CLEANED ALODINED, PRIMED AND TOP COATED AFFECTED AREAS. ALL WORK DONE IAW GIV SRM 51-13-20 AND 51-07-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.10 @ $142.00 $298.20 Parts USD: Time and Material $104.32 Total USD: $402.52 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 16.9#1 GAS55 I B3C7 SCREW 7 S0.78 $5.46 16.9 #2 GAS550E3S8 SCREW-WASHER HEAD,SELF 1 $2.02 S2.02 LOCKING 16.9 #3 GAS55IB3Cl2 SCREW 2 $4.93 $9.86 16.9#4 NAS583-I6 BOLT 2 $13.60 $27.20 16.9 #5 NAS583-14 BOLT 2 S29.89 $59.78 Step: 16.9.1 Completed REMOVED CORROSION WITH SCOTCH BRITE. CLEANED ALODINED AND PRIMED AFFECTED AREA& ALL WORK DONE IAW GIV SRM 51-13-20 AND 51-07-10. Discrepancy: 16.10 DURING INSPECTION OF RH SPEED BRAKE SECTOR TO GROUND SPOILER CONTROL ROD NOTED OB ROD END SEAL FAILURE ON ROD END BEARING. Resolution: USED CONTROL ROD END FIXTURE TO MEASURE ORIGINAL LENGTH OF CONTROL ROD BEFORE REMOVAL OF FAILED OB ROD END. REMOVED FAILED OB ROD END WITH PART NUMBER MS21151-8. NSN. REPLACED WITH NEW OB ROD END WITH PART NUMBER MS21151-8. NSN. CONTROL ROD ASSEMBLED TO ORIGINAL LENGTH PRIOR TO REMOVAL. ALL WORK DONE IAW 1159C20260 REV E. ALL PARTS RECEIVED FROM GAC BAF STOCK. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.08 @ $142.00 $295.36 Parts USD: Time and Material $89.07 Total USD: $384.43 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 16.10 #1 MS2I151-8 BEARING, ROD END, DBL ROW, 235 I $89.07 $89.07 IN L 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 91 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00809029 Bill To: JEGE LW WO It SC18654 Invoice Number: 6918002027 Item: 17 ANTENNA INTERFACE INSPECTION (GIV-SP SN 1085) Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes Part/Model AC Serial No./Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 17.1 ANTENNA INTERFACE - INSPECTION Resolution: ACCOMPLISH THE ANTENNA INTERFACE - INSPECTION (CMP TASK 539516). NOTES: - REMOVAL OF ALL PRODUCTION AND OUTFITTING INSTALLED ANTENNAS, PENETRATIONS OF FUSELAGE SKIN, EXTERNAL SKIN DOUBLERS (EXCEPT AS NOTED BELOW) TO PERFORM THE INSPECTION AS WELL AS ANY REQUIRED FOLLOW ON CHECKS ARE INCLUDED IN THE QUOTED AMOUNT. - ANTICIPATED INTERIOR ACCESS TO COMPLETE THIS INSPECTION IS INCLUDED, HOWEVER ADDITIONAL CHARGES MAY BE INCURRED BASED ON NON-GULFSTREAM INSTALLED INTERIORS OR SPECIFIC AIRCRAFT INTERIOR CONFIGURATIONS WHICH WOULD REQUIRE REMOVAL OF GALLEYS, LAVATORIES, BULKHEADS, CLOSETS, DOORS AND ACOUSTICAL LINER PANELS. UPON AIRCRAFT ARRIVAL AND EVALUATION AN ESTIMATE WILL BE PRESENTED FOR APPROVAL IF ADDITIONAL ACCESS IS DEEMED TO BE REQUIRED. - EXTERNAL SKIN DOUBLERS, ADAPTER OR CONTOUR PLATES THAT ARE RIVETED ON THE AIRCRAFT SKIN (OR OTHER MEANS OF PERMANENT ATTACHMENT) ARE NOT INCLUDED IN THE QUOTED PRICE AND WILL BE WORKED ON A TIME AND MATERIALS BASIS. - SATCOM ANTENNAS MOUNTED ON THE AIRCRAFT FUSELAGE, ANTENNA PODS, NON-OPERATIONAL EQUIPMENT, OR BLANKING PLATES FROM REMOVED ANTENNAS AND ANY NON-GULFSTREAM INSTALLED EQUIPMENT ARE NOT INCLUDED IN THE QUOTED AMOUNT. - SOME AIRCRAFT AND INSTALLATIONS MAY REQUIRE "POLYURETHANE SELF-LEVELING ANTENNA GASKETS" TO BE INSTALLED BETWEEN THE ANTENNA FACE AND THE AIRCRAFT EXTERNAL SKIN. FOR BUDGETARY AND PLANNING PURPOSES, ESTIMATED COST FOR REPLACEMENT GASKETS FOR A STANDARD EQUIPPED AIRCRAFT IS S9,000. - ANY LABOR OR MATERIALS REQUIRED FOR CLEARING OF DISCREPANCIES IS NOT INCLUDED IN THE QUOTED AMOUNT. RE: PROPOSAL# 7042687 ROO (GACO218-2687-GIV-1085-R00)-1.3 *** LABOR ONLY Billing Method Hours Rate Total Labor USD: Flat Rate S19,500.00 Total USD: S19,500.00 Discrepancy: 17.2 ACCOMPLISH THE ANTENNA INTERFACE - INSPECTION CMP CODES BELOW: Resolution: 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 92 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00809030 Bill To: JEGE LLC Billing Method WO It: SC18654 Hours Rate Invoice Number: 6918002027 Total Parts USD: Time and Material 52.01151 Total USD: 52.01351 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 17.2 #1 PRI440B1-2-654 SEALANT,6OZ #654 SEMKIT 1 $26.67 $26.67 17.2 #2 IIL19PB5-5 111-1OK 10 $1.64 $16.40 17.2 #3 IILI9PB5-3 111-1OK 10 S3.91 $39.10 17.2 #4 NASI581C3T4 SCREW 10 $0.60 $6.00 17.2 #5 IIT3326-5FR-50 SEALANT, SELF-LEVELING GREEN, 3 $77.62 $232.86 FLAME RETARDANT 17.2 #6 PR1440B1-2-654 SEALANT,6OZ #654 SEMKIT 8 $26.67 $213.36 17.2 #7 06408 TAPE, 3M 1/2 INCH BLUE VINYL I0 $16.29 $162.90 17.2 #8 C1420-I XM ANTENNA ( COMANT/DAC ) 1 $1,056.73 $1,056.73 17.2 #9 NASII49D031611 WASHER 17 $0.23 S3.91 17.2 #10 PR1422B2-654 SEALANT, 3.5 OUNCE SEMKIT 2 $51.71 $103.42 17.2 #11 II59SCF457-15 VINYL DOTS, SCREW HEAD RECESS 50 $0.45 $22.50 COVER 17.2 #12 PRI440B1-2-654 SEALANT,6OZ #654 SEMKIT 2 $26.67 $53.34 17.2 #13 1159SCF457-1I VINYL DOTS, SCREW HEAD RECESS 50 $0.45 $22.50 COVER 17.2 #14 I159SCF457-13 VINYL DOTS,SCREW HEAD RECESS 50 $0.45 $22.50 COVER 17.2 #15 515X333-2OZ KIT, TOUCH UP, EPDXY PRIMER, 2 I $29.26 $29.26 OZ, GREEN 17.2 #16 NASI149F0432P WASHER, FLAT STEEL (SAME AS 2 $0.23 S0.46 AN960-4161) 17.2 #17 MSI7826-4 NUT I $1.60 S1.60 17.2 #18 NA56604D45 BOLT, DRILLED SHANK 1 $0.00 S0.00 Discrepancy: 17.3 CMP G1V 539516 Antenna Interface - Inspection Resolution: COMPLIED WITH CMP GIV 539516 Antenna Interface - Inspection Step: 173.1 Completed ACCOMPLISHED ANTENNA INSPECTION AND SKIN SURFACE INSPECTION EXCEPT UNDER UPPER TCAS ANTENNA DOUBLE IAW CMP GIV 539516 ANTENNA INTERFACE - INSPECTION. Discrepancy: 17.4 CMP GIV 231015 VHF COMM SYS- OPS CHECK Resolution: COMPLIED WITH CMP GIV 231015 VHF COMM SYS- OPS CHECK 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 93 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00809031 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Discrepancy: 17.5 CMP GIV 231035 ANTENNA, VHF COMM (TOP FWD) Resolution: COMPLIED WITH CMP GIV 231035 ANTENNA, VHF COMM (TOP FWD) TEST EQUIPMENT USED: MODEL: FLUKE 77 IV S/N: 22870351 DATE CAL: 07/14/2017 CAL. DUE DATE: 07/14/2018 MILLI OHM METER I.D. 1560G00, DUE 4/10/2019 Discrepancy: 17.6 CMP GIV 231036 ANTENNA, VHF COMM (BOT FWD) Resolution: COMPLIED WITH CMP GIV 231036 ANTENNA, VHF COMM (BOT FWD) TEST EQUIPMENT USED: MODEL: FLUKE 77 IV S/N: 22870351 DATE CAL: 07/14/2017 CAL. DUE DATE: 07/14/2018 MILLI OHM METER I.D. 1560600. DUE 4/10/2019 Discrepant:). 17.7 CMP GIV 231037 ANTENNA, VHF COMM (BOT AFT) Resolution: COMPLIED WITH CMP GIV 231037 ANTENNA, VHF COMM (BOT AFT) TEST EQUIPMENT USED: MODEL: FLUKE 77 IV S/N: 22870351 DATE CAL: 07/14/2017 CAL. DUE DATE: 07/14/2018 MILLI OHM METER I.D. 1560600, DUE 4/10/2019 Discrepancy: 17.8 CMP GIV 231456 ANTENNA, 800 MGHZ #1 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 94 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809032 Bill To: JEGE LLC WO It SC18654 Resolution: COMPLIED WITH CMP GIV 231456 ANTENNA, 800 MGHZ #1 Invoice Number: 6918002027 REMOVED 800 MGHZ ANTENNA PIN N129-18-1, SIN 0494. RECIEVED O.K. TO INSTALL AND INSTALLED SERVICABLE 800 MGHZ ANTENNA P/N N129-18-1, SIN 0494. Discrepancy: 17.9 CMP GIV 237107 ANTENNA, SECURITY SYSTEM Resolution: COMPLIED WITH CMP GIV 237107 ANTENNA, SECURITY SYSTEM Discrepancy: 17.10 CMP GIV 238056 Antenna LH (Aircell / Iridium). Resolution: COMPLIED WITH CMP GIV 238056 Antenna LH (Aircell / Iridium). Discrepancy: 17.11 CMP GIV 238076 Antenna, ABS ATG (Forward) Resolution: COMPLIED WITH CMP GIV 238076 Antenna, ABS ATG (Forward) Discrepancy: 17.12 CMP GIV 238077 Antenna, ABS ATG (Aft) Resolution: COMPLIED WITH CMP GIV 238077 Antenna, ABS ATG (Aft) Discrepancy: 17.13 CMP GIN. 256130 Emergency Locator Transmitter Antenna - Removal / Installation 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 95 of 117 Printed: 6/28/2018 939:11M Reel EFTA00809033 Bill To: JEGE LLC WO it SC18654 Invoice Number: 6918002027 Resolution: COMPLIED WITH CMP GIV 256130 EMERGENCY LOCATOR TRANSMITTER ANTENNA - REMOVAL / INSTALLATION COAX CABLE CENTER CONDUCTOR CHECK. TEST EQUIPMENT USED: MODEL: FLUKE 77IV S/N: 22870351 CAL DATE: 07/14/2017 CAL. DUE DATE: 07/14/2018 Discrepancy: 17.14 CMP GIV 334029 Anti-collision Beacon Assembly (Top) - Removal / Installation Resolution: COMPLIED WITH CMP GIV 334029 Anti-collision Beacon Assembly (Top) - Removal / Installation Discrepancy: 17.15 CUP GIN' 334030 .kriticollision Beacon Assembly (Bottom) - Removal r Installation Resolution: Discrepancy: 17.16 CMP GIV 341035 ANTENNA, #1 RADIO ALT XMITTER Resolution: COMPLIED WITH CMP GIV 341035 ANTENNA, #1 RADIO ALT XMITTER MILLI-OHM METER I.D. 1560G00, DUE 4/10/2019 Discrepancy: 17.17 CMP GIV 341036 Radio Altimeter Receiver Antenna No. 1 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 341036 RADIO ALTIMETER RECEIVER ANTENNA NO. 1 - REMOVAL/ INSTALLATION MILLI-OHM METER I.D. 1560G00, DUE 4/10/2019 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 96 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00809034 Bill To: JEGE LW WO if: SCI8654 Invoice Number: 6918002027 Discrepancy: 17.18 CMP GIV 341037 Radio Altimeter Receiver Antenna No. 2 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 341037 RADIO ALTIMETER RECEIVER ANTENNA NO. 2 - REMOVAL/ INSTALLATION MILLI-OHM METER I.D. 1560G00, DUE 4/10/2019 Discrepancy: 17.19 CMP GIV 341038 ANTENNA, #2 RADIO ALT XMITTER Resolution: COMPLIED WITH CMP GIV 341038 ANTENNA, #2 RADIO ALT XMITTER MILLI-OHM METER I.D. 1560G00, DUE 4/10/2019 Discrepancy: 17.20 CMP GIV 343014 Marker Beacon Antenna - Removal / Installation Resolution: COMPLIED WITH CMP GIV 343014 MARKER BEACON ANTENNA - REMOVAL / INSTALLATION FLUKE METER - 1804U00 CAL DATE - 5/7/2018 CAL DUE - 5/7/2019 Discrepancy: 17.21 CMP GIV 343015 Marker Beacon System - Operational Check Resolution: COMPLIED WITH CMP GIV 343015 MARKER BEACON SYSTEM - OPERATIONAL CHECK EQUIPMENT USED: IFR 4000 ITEM--1753N00 CAL DATE-6/17/I7 CAL DUE DATE--6/30/2018 Discrepancy: 17.22 CMP GIV 343016 ANTENNA, MARKER BEACON Resolution: COMPLIED WITH CMP GIV 343016 ANTENNA, MARKER BEACON 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 97 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00809035 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 17.23 CMP GIV 344315 Traffic Collision Avoidance System Top Antenna - Removal / Installation Resolution: COMPLIED WITH CMP GIV 344315 TRAFFIC COLLISION AVOIDANCE SYSTEM TOP ANTENNA - REMOVAL / INSTALLATION TEST EQUIPMENT USED: MODEL: FLUKE 77IV S/N: 22870351 CAL DATE: 07/14/2017 CAL. DUE DATE: 07/14/2018 Discrepancy: 17.24 CMP GIV 344316 Traffic Collision Avoidance System Bottom Antenna - Removal / Installation Resolution: COMPLIED WITH CMP GIV 344316 TRAFFIC COLLISION AVOIDANCE SYSTEM BOTTOM ANTENNA - REMOVAL / INSTALLATION TEST EQUIPMENT USED: MODEL: FLUKE 77IV S/N: 22870351 CAL DATE: 07/14/2017 CAL. DUE DATE: 07/14/2018 Discrepancy: 17.25 CM l' GIN 344341 TCAS - Functional Check Resolution: COMPLIED WITH (MP GIV 344341 TCAS - Functional Check Discrepancy: 17.26 CMP GIN 345141 Distance Measuring Equipment Antenna No. I - Removal Installation 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 98 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00809036 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Resolution: COMPLIED WITH CMP GIV 345141 DISTANCE MEASURING EQUIPMENT ANTENNA NO. 1- REMOVAL / INSTALLATION TEST EQUIPMENT USED: MODEL: FLUKE 77 IV S/N: 22870351 DATE CAL: 07/14/2017 CAL. DUE DATE: 07/14/2018 MILLI-OHM METER I.D. 1560G00, DUE 4/10/2019 COMPLIED WITH CMP GIV 345141 Distance Measuring Equipment Antenna No. 1 - Removal / Installation Discrepancy: 17.27 CMP GIV 345142 Distance Measuring Equipment Antenna No. 2 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 345142 DISTANCE MEASURING EQUIPMENT ANTENNA NO. 2 - REMOVAL/ INSTALLATION TEST EQUIPMENT USED: MODEL: FLUKE 77 IV S/N: 22870351 DATE CAL: 07/14/2017 CAL. DUE DATE: 07/14/2018 MILLIOHM METER I.D. 1560600, DUE 4/10/2019 Discrepancy: 17.28 CMP GIV 345246 ANTENNA, ADF #2 Resolution: N/A THERE IS ONY ONE ADF ANTENNA INSTALLED ON THE AIRCRAFT, TRACKED UNDER CMP 345250. Discrepancy: 17.29 C N1P GIN 345250 ADF Dual Antenna - Removal / Installation 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_WorkOrderPrelintinaryInvoice.rpt 2011 Page 99 of 117 Printed: 6/28/2018 939:11.41 Reel EFTA00809037 Bill To: JEGE LLC WO #: SCI8654 Invoice Number: 6918002027 Resolution: COMPLIED WITH CMP GIV 345250 AUTOMATIC DIRECTION FINDING DUAL ANTENNA - REMOVAL / INSTALLATION MULTIMETER ID-1695C00 DATE CAL-7/14/2017 CAL DUE DATE--7/14/2018 MILLIOHM METER I.D. 1560G00, DUE 4/10/2019 Discrepancy: 17.30 CMP GIV 345311 ATC Transponder No. 1- Test / Inspection (FAR91.413) Resolution: COMPLIED WITH CMP GIV 345311 ATC NO. 1 - FUNCTIONAL TEST / INSPECTION (FAR 91.413). ATC TRANSPONDER TESTS WERE PERFORMED IN ACCORDANCE WITH 14 CFR PART 43, APPENDIX FAS REQUIRED BY 14 CFR PART 91.413. #1 TRANSPONDER P/N: 622-9210-409, S/N: 364 DATE TESTED: 06/26/2018 EXPIRATION DATE: 06/26/2020 TRANSPONDER TEST EQUIPMENT USED FOR TRANSPONDER CERTIFICATIONS: MODEL: IFR-6000 S/N: 1000685211 CAL DATE: 11/10/2017 CAL DUE DATE: 11/10/2018 THIS AIRCRAFT MEETS THE REQUIREMENTS STIPULATED IN THE REGULATION THAT AUTHORIZES NAVIGATION IN REDUCED VERTICAL SEPARATION MINIMUM (RVSM) AIRSPACE, IN ACCORDANCE WITH APPLICABLE AIRCRAFT MAINTENANCE MANUAL. Discrepancy: 17.31 CMP GIV 345312 ATC Transponder No. 2 - Test / Inspection (FAR91.413) Resolution: COMPLIED WITH CMP GIV 345312 ATC NO. 2 - FUNCTIONAL TEST / INSPECTION (FAR 91.413). ATC TRANSPONDER TESTS WERE PERFORMED IN ACCORDANCE WITH 14 CFR PART 43, APPENDIX FAS REQUIRED BY 14 CFR PART 91.413. #2 TRANSPONDER P/N: 622-9210-409, S/N: ICBM DATE TESTED: 06/26/2018 EXPIRATION DATE: 06/26/2020 TRANSPONDER TEST EQUIPMENT USED FOR TRANSPONDER CERTIFICATIONS: MODEL: IFR-6000 S/N: 1000685211 CAL DATE: 11/10/2017 CAL DUE DATE: 11/10/2018 THIS AIRCRAFT MEETS THE REQUIREMENTS STIPULATED IN THE REGULATION THAT AUTHORIZES NAVIGATION IN REDUCED VERTICAL SEPARATION MINIMUM (RVSM) AIRSPACE, IN ACCORDANCE WITH APPLICABLE AIRCRAFT MAINTENANCE MANUAL. 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 100 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00809038 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 17.32 CMP GIV 345335 ANT, #1 ATC UPPER(A/C 1360-SUB Resolution: COMPLIED WITH CMP GIV 345335 ANT, #1 ATC UPPER(A/C 1360-SUB TEST EQUIPMENT USED: MODEL: FLUKE 77 IV S/N: 22870351 DATE CAL: 07/14/2017 CAL. DUE DATE: 07/14/2018 MILLIOHM METER I.D. 1560600, DUE 4/10/2019 Discrepancy: 17.33 CMP GIV 345336 ANT, #2 ATC UPPER(A/C 1360-SUB Resolution: COMPLIED WITH CMP GIV 345336 ANT, #2 ATC UPPER(A/C 1360-SUB TEST EQUIPMENT USED: MODEL: FLUKE 77 IV S/N: 22870351 DATE CAL: 07/14/2017 CAL. DUE DATE: 07/14/2018 MILLIOHM METER I.D. 1560600, DUE 4/10/2019 Discrepancy: 17.34 CMP GIV 345341 ANTENNA, #1 ATC (LWR FORWARD) Resolution: COMPLIED WITH CMP GIV 345341 ANTENNA, #1 ATC (LWR FORWARD) TEST EQUIPMENT USED: MODEL: FLUKE 77 IV S/N: 22870351 DATE CAL: 07/14/2017 CAL. DUE DATE: 07/14/2018 MILLIOHM METER I.D. 1560600, DUE 4/10/2019 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 101 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809039 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 17.35 CMP GIV 345342 ANTENNA, #2 ATC (LOWER AFT) Resolution: COMPLIED WITH CMP GIV 345342 ANTENNA, #2 ATC (LOWER AFT) TEST EQUIPMENT USED: MODEL: FLUKE 77 IV S/N: 22870351 MILLIOHM METER I.D. 1560600, DUE 4/10/2019 Discrepancy: 17.36 CMP GIV 345805 GPS SYSTEM-OPS TEST Resolution: COMPLIED WITH CMP GIV 345805 GPS SYSTEM—OPS TEST Discrepancy: 17.37 CMP GIN' 345815 ANTENNA, GPS #1 Resolution: COMPLIED WITH CMP GIV 345815 ANTENNA, GPS #1 FLUKE METER - 1804U00 CAL DATE - 5/7/2018 CAL DUE - 5/7/2019 MILLIOHM METER I.D. 1560600, DUE 4/10/2019 Discrepancy: 17.38 CMP GIV 346049 ANTENNA, POSITIONING #1 Resolution: COMPLIED WITH CMP GIV 346049 ANTENNA, POSITIONING #1 Discrepancy: 17.39 CMP GIV 346050 ANTENNA, POSITIONING #2 Resolution: COMPLIED WITH CMP GIV 346050 ANTENNA, POSITIONING #2 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 102 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00809040 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 17.40 CMP GIV 232226 ANTENNA, SATELLITE COMMUNICATI Resolution: COMPLIED WITH CMP GIV 232226 ANTENNA, SATELLITE COMMUNICATI Discrepancy: 17.41 CMP GIV 231005 TRANSCEIVER, #1 VHF COMM Resolution: COMPLIED WITH CMP GIV 231005 TRANSCEIVER, #1 VHF COMM Discrepancy: 17.42 CMP OW 231006 TRANSCEIVER, #2 VHF COMM Resolution: COMPLIED II CMP GIV 231006 TRANSCEIVER, #2 VHF COMM Discrepancy: 17.43 CMP GIV 345205 Automatic Direction Finding Receiver No. 1 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 345205 AUTOMATIC DIRECTION FINDING RECEIVER NO. 1- REMOVAL/ INSTALLATION REMOVED AND REINSTALLED SAME ADF RECIEVER #1 P/N 622-7382-101 SN 495. ALL WORK COMPLIED WITH IAW GIV MM 34-02-03 OPERATIONAL TEST DUE. SEE ITEM 17.47 Discrepancy: 17.44 CMP GIV 345206 Automatic Direction Finding Receiver No. 2 - Removal / Installation Resolution: COMPLIED WITH CMP GIV 345206 AUTOMATIC DIRECTION FINDING RECEIVER NO. 2 - REMOVAL / INSTALLATION INSTALLED SAME ADF RECIEVER #2 P/N 622-7382-101 SN 498. ALL WORK COMPLIED WITH IAW GIV MM 34-02-03. OPERATIONAL TEST DUE. SEE ITEM 1747 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 103 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809041 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 17.45 CMP GIV 345305 TRANSPONDER, #1 ATC Resolution: COMPLIED WITH CMP GIV 345305 TRANSPONDER, #1 ATC Discrepancy: 17.46 CMP GIV 345306 TRANSPONDER, #2 ATC Resolution: COMPLIED WITH CMP GIV 345306 TRANSPONDER, #2 ATC Discrepancy: 17.47 CMP GIV 345219 AUTOMATIC DIRECTION FINDING SYSTEM - OPERATIONAL CHECK SEE ITEM 17.44 AND 17.45 Resolution: COMPLIED WITH CMP GIV 345219 AUTOMATIC DIRECTION FINDING SYSTEM - OPERATIONAL CHECK, CHECKED GOOD AT THIS TIME. Discrepancy: 17.48 CMP GIV 344305 TCAS Computer- Removal / Installation Resolution: COMPLIED WITH CMP GIV 344305 TCAS Computer - Removal / Installation Item: 18 ANTENNA INTERFACE INSPECTION DISCREPANCIES Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes Part/Model #: AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 18.1 WHILE REMOVING ANTENNAS FOR CMP GIV 539516 ANTENNA INTERFACE - INSPECTION NOTED ALL RAD ALT ANTENNAS ARE PAINTED OVER. Resolution: PERFORMED REMOVAL / INSTALLATION OPERATION TESTS (REF ITEMS 17.16 THRU 17.19). CUSTOMER ELECTS NO FURTHER ACTION AT THIS 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 104 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809042 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 18.2 ADDITIONAL TIME REQUIRED TO REMOVE LOWER TCAS DOUBLER. IT IS ATTACHED TO AIRCRAFT SKIN. Resolution: REMOVED LOWER TCAS ANTENNA CONTOUR PLATE TO FACILITATE ANTENNA INTERFACE INSPECTION. INSTALLED LOWER TCAS ANTENNA CONTOUR PLATE WORK REF GAC BP SC44129001 REV (J) - TCAS HONEYWELL (STC). & ENGINEERING DISPO 18654.18.2.1 Labor USD: Labor USD: Parts USD: Total USD: Pans: Ref. No. 18.2 #2 18.2 #3 18.2 #4 Billing Method Time and Material Time and Material Time and Material Part number: IIL82-5APBW 11140-4-2 11197-4 Step: 18.2.1 Completed ST ST Flours Rate 15.57 @ $142.00 1.00 @ $231.00 Total $2,210.94 $231.00 $984.11 $3,426.05 Description Quantity Sell price USD III LOC COLLAR PIN, HILOK COLLAR, HILOK ENGINEERING DISPOSITION: 100 33 33 $5.00 $3.76 $10.91 Extended USD AT NOTED LOCATIONS COMMON TO THE 159F10906 SUPPORT ASSY & INSTL STA 133-168, IT IS PERMISSIBLE TO SUBTITUTE SOLID AD RIVETS WITH HL40-4-(XX) HI-LOKS AND HL94-4 OR IIL97-4 COLLARS. ENSURE HOLE(S) ARE CLEAN AND ROUND AT 0.138 - 0.141 INCH DIA. MAINTAIN A MINIMUM OF 2X DIA EDGE DISTANCE FOR III - LOK INSTALLATION AND INSTALL PER GAMPS2206 WET WITH MIL-PRF-81733 OR EQUIVALENT SEALANT PER CAMPS 7115. $500.00 $124.08 $360.03 Discrepancy: 18.3 ADDITIONAL TIME REQUIRED TO REMOVE UPPER TCAS DOUBLER. IT IS ATTACHED TO AIRCRAFT SKIN. Resolution: REMOVED UPPER TCAS ANTENNA CONTOUR PLATE TO FACILITATE ANTENNA INTERFACE INSPECTION. RE-INSTALLED UPPER TCAS ANTENNA CONTOUR PLATE WORK REF GAC BP SC44129001 REV (J) - TCAS HONEYWELL (STC). Billing Method Flours Rate Total Labor USD: Time and Material ST 19.30 @ $142.00 $2,740.60 Parts USD: Time and Material $666.25 Total USD: $3,406.85 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 18.3 #9 IILI9PB5-5 HI-LOK 10 $1.64 $16.40 183 #15 IILI9PB6-5 HI-LOK 10 $1.77 $17.70 183 #10 IILI9PB5-6 HILOK 20 $1.74 $34.80 183 #8 IILI9PB-5-7 BOLT 20 S3.44 $68.80 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 105 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00809043 Bill To: JEGE LLC Pans: Ref. No. Part number: WO It SC18654 Description Invoice Number: 6918002027 Quantity Sell price USD Extended USD 18.3 47 IlL82-6APBW III LOC / COLLAR 20 $16.50 $330.00 183014 GAB5I0B3-6 BOLT 5 $1.00 S5.00 18.3 kll NASI581C3T5 BOLT, 100 DEC FRI', OFS 10 $1.25 $12.50 CRUCIFORM, 95 ICSI 183 013 NAS1581C3T3 SCREW 10 $0.44 $4.40 183 012 NAS1581C3T6 BOLT, 100 DEG FLUSH REDUCED 10 $1.25 $12.50 HEAD, OFS CRUCIFORM, 95 ICSI FSU 183 016 MS2I042L3 NUT 17 $0.24 $4.08 183 PI IlLI9PB5-2 HILOK 17 $3.09 $52.53 183 #2 IILI9PB5-8 HILOK 20 $3.00 S60.00 183 #3 IILI9PB5-5 III-LOK 9 $1.64 S14.76 183 44 IILI9PB6-10 HI-LOK I $1.76 $1.76 183 45 IILI9PB6-10 HI-LOK 1 $1.76 $1.76 183 #6 515X333-20Z KIT, TOUCH UP, EPDXY PRIMER, 2 1 $29.26 $29.26 OZ, GREEN Discrepancy: 18.4 WHILE C/W CMP 539516 ANTENNA INTERFACE INSPECTION NOTED MULTIPLE LOWER ANTENNA FUSELAGE LANDINGS TO HAVE MINOR SURFACE CORROSION. Resolution: REMOVED SURFACE CORROSION ON LOWER ANTENNA INTERFACES, SEE STEPS FOR DETAILS. PERFORMED NDT THICKNESS CHECKS. PER ENGINEERING DISPOSITION STEP 18.4.4 REMAINING SKIN THICKNESS IS STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. CLEANED AND ALODINED BARE SURFACES AS REQUIRED. WORK DONE LAW SRM 15-13-10 AND GSL405300001 (REV -) Billing Method Hours Rate Total Labor USD: Time and Nlaterial ST 5.15 ® $142.00 $73130 Labor USD: Time and Nlaterial ST 1.00 ® $231.00 $231.00 Total USD: $96230 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_WorkOrderPreliminarylnvoice.rpt 2011 Page 106 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809044 Bill To: JEGE LLC Step: 18.4.1 Step: 18.4.2 Step: 18.43 WO #: SC18654 Invoice Number: 6918002027 Completed REMOVED CORROSION ON LOWER ANTENNA INTERFACES. CLEANED ALL AFFECTED AREAS. ALL WORK DONE JAW GIV SRM 51-13-10. Completed PERFORMED ULTRASONIC THICKNESS MEASUREMENTS PER MAINTENANCE REQUEST AFTER MAINTENANCE REMOVED CORROSION FROM LOWER ANTENNA INTERFACES IAW GIV SRM 51-13-20. INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL 2.0 ULTRASONIC REVISION 7 - SEPTEMBER 16TH, 2015.MEASUREMENTS MARKED ON TAPE ON AIRCRAFT. Completed REQUEST ENGINEERING EVALUATION OF REMAINING SKIN THICKNESS WHERE REWORKED: DME NO. 1 ANTENNA, .040 MIN NOTED RAD ALT NO. 1 XMIT, .066 MIN NOTED ATC NO. 1 ANTENNA, .039 MIN NOTED RAD ALT NO.2 REC, .067 MIN NOTED DME NO.2 ANTENNA, .041 MIN NOTED RAD ALT NO.1 FtECV - .060 MIN NOTED ATC NO.2 ANTENNA - .042 MIN NOTED VHF NO.2 ANTENNA - .040 MIN NOTED VHF NO. 3 (LOCATED ON PANEL) - .070 MIN NOTED L BAND ANTENNA AT FS 565 -.039 MIN NOTED LH MARKER BEACON ANTENNA - .062 MIN NOTED Step: 18.4.4 Completed ENGINEERING DISPOSITION: THE NOTED POST BLEND THICKNESS MEASUREMENTS ARE STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. CONTINUE REWORK OPERATIONS IAW GSL405300001 (REV -) "ALLOWABLE DAMAGE - FUSELAGE SKIN AT ANTENNA LOCATIONS" Discrepancy: 18.5 WHILE REMOVING FWD LOWER TCAS ANTENNA DOUBLER NOTED FUSELAGE DEFORMATION CAUSED BY DOUBLER REMOVAL Resolution: COLD STRAIGHTENED DISCREPANT AREA OF THE 1159B20223-47 FUSELAGE SKIN. LIGHTLY SCOTCH-BRITE/BLENDED DISCREPANT AREAS. NDT VERIFID NO CRACKS AND POST BLEND SKIN THICKNESS IS WITHIN ALLOWABLE LIMITS. TOUCHED UP REWORK WITH FINISH #213 ALODINE PER GAMPS 6113 AND REINSTALLED TCAS ANTENNA PER GAC BP SC44129001. WORK DONE IAW ENGINEERING DISPOSITION SC18654.18.5.2. REF STEPS BELOW FOR FURTHER DETAILS AND COMPONENTS REMOVED AND INSTALLED FOR ACCESS TO SKIN. 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 107 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809045 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Step: 18.5.1 Completed REQUEST ENGINEERING EVALUATION OF SKIN DEFORMATION UNDER FWD LOWER TCAS DOUBLER Step: 18.5.2 Completed ENGINEERING DISPOSITION: COLD STRAIGHTEN DISCREPANT AREA OF THE II 59B20223-47 FUSELAGE SKIN TO BRING BACK TO WITHIN APPROXIMATELLY 0.002 INCH OF B/P CONTOUR; (REF SR 1077). LIGHTLY SCOTCH-BRITEIBLEND DISCREPANT AREAS 0.004 MAX TO ENSURE A SMOOTH AND GRADUAL TRANSITION WITH A MINIMUM 20 TO 1 WIDTH TO DEPTH BLEND RATIO AND 63 RIM OR BETTER SURFACE FINISH. NDT VERIFY NO CRACKS AND POST BLEND SKIN THICKNESS (REF. 2024-T42, 0.040 THK). A 10% REDUCTION IN SKIN THICKNESS WILL BE STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. TOUCH REWORK WITH FINISH #213 ALODINE PER CAMPS 6113 AND REINSTALL TCAS ANTENNA PER B/P, MUM REQT'S. Step: 18.53 Completed GAINED ACCESS TO AND REMOVED THE HMG CONTROL UNIT PN:752502176I SN: III, AUDIO JUNCTION BOX PN:UNK SN: UNK, DC EXTERNAL REMOTE CIRCUIT BREAKER PN: UNK SN: UNK, LIGHT DIMMER POWER SUPPLY #1 PN:LT-52A SN: 8854, LIGHT DIMMER POWER SUPPLY #2 PN:LT-52A SN: 8855, LIGHT DIMMER POWER SUPPLY #3 PN:LT-52A SN: 8856, STANDBY GENERATOR AC POWER RELAY PN: IIT-A4A-002 SN: UNK. Step: 18.5.4 Completed COLD STRAIGHTENED DISCREPANT AREA AROUND LOWER TCAS CONTOUR PLATE MOUNTING INTERFACE ON 1159620223-47 FUSELAGE SKIN. LIGHTLY BLENDED COLD STRAIGHTENED AREA WITII SCOTCIIBRITE PAD. DONE PER ENGINEERING DISPOSITION SCI8654.18.5.2 Step: 18.5.5 Completed PERFORMED EDDY CURRENT INSPECTION FOR CRACKS PER MAINTENANCE REQUEST AFTER MAINTENANCE COLD STRAIGHTENED DISCREPANTAREA AROUND LOWER TC AS CONTOUR PLATE MOUNTING INTERFACE ON 1159B20223-47 FUSELAGE SKIN. INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL 3.0 EDDY CURRENT REVISION 7- DECEMBER 15TH, 2017. NO DEFECTS NOTED. Step: 18.5.6 Completed PERFORMED ULTRASONIC THICKNESS MEASUREMENTS PER MAINTENANCE REQUEST ON AREA AROUND LOWER TC AS CONTOUR PLATE MOUNTING INTERFACE ON 1159620223-47 FUSELAGE SKIN AFTER MAINTENANCE LIGHTLY BLENDED COLD STRAIGHTENED AREA WITH SCOTCIIBRITE PAD. MEASUREMENTS WRITTEN ON AIRCRAFT BARE METALMINIMUM READING RECORDED .037. Step: 18.5.7 Completed PER ENGINEERING STEP 18.5.2 THE NOTED MINIMUM SKIN THICKNESS OF .037 NOTED IS WITHIN ALLOWABLE LIMITS. (1159B20223-47 FUSELAGE SKIN) Step: 18.5.8 Completed RECEIVED OK TO INSTALL AND INSTALLED THE FOLLOWING SERVICABLE UNITS: HMG CONTROL UNIT PN:7525021761 SN: III, AUDIO JUNCTION BOX PN:UNK SN: UNK, DC EXTERNAL REMOTE CIRCUIT BREAKER PN: UNK SN: UNK, PEDESTAL LIGHT DIMMER POWER SUPPLY #1 PN:LT-52A SN: 8854, PEDESTAL LIGHT DIMMER POWER SUPPLY #2 PN:LT-52A SN: 8855, PEDESTAL LIGHT DIMMER POWER SUPPLY #3 PN:LT-52A SN: 8856, STANDBY GENERATOR AC POWER RELAY PN: IIT-A4A-002 SN: UNK. ALL WORK PERFORMED IN ACCORDANCE WITH GIV MUM 24-01-05 STANDBY ELECTRICAL POWER AND WIRING DIAGRAMS 23-52-00 AUDIO CONTROL SYSTEM. 33-12-00 COCKPIT LIGHTS SYSTEM, 24-24-00 STANDBY ELECTRICAL POWER Step: 18.5.9 Completed PERFORMED OPERATIONAL CHECK OF HMG CONTROL UNIT (PERFORMD UNDER ITEM 11.12), AUDIO JUNCTION BOX IAW GIV MM 23-50-00 AUDIO INTEGRATING SYSTEM OPERATIONAL CHECK, DC EXTERNAL REMOTE CIRCUIT BREAKER IAW GIV MM 24-02-00 DC POWER SUPPLY AND DISTRIBUTION, AND PEDESTAL LIGHT DIMMER POWER SUPPLY 1-3 IAW GIV MM 33-01-00 WARNING LIGHTS SYSTEM 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 IO8 of 117 Printed: 6/28/2018 939:11AI Reel EFTA00809046 Bill To: JEGE LW WO SC18654 Invoice Number: 6918002027 Discrepancy: 18.6 WHLIE C/W CMP 539516 UPPER ANTENNA INTERFACE NOTED SEVERAL ANTENNA FUSELAGE LANDINGS TO HAVE LIGHT SURFACE CORROSION / TOOLING MARKS Resolution: REMOVED LIGHT SURFACE CORROSION AND TOOLING MARKS FROM SEVERAL ANTENNA LANDINGS: XM ANTENNA@ FS 193, VHF NO. 1 ANTENNA, BLADE ANTENNA @ FS 315, ANTI COLLISON LIGHT ON UPPER FUSELAGE SURFACE BY HAND SANDING AND MECHANICAL MEANS. PERFORMED ULTRASONIC THICKNESS MEASUREMENTS FOR ENGINEERING FOUND TO BE WITHIN STRUCTUAL SERVICABLE LIMITS. CLEANED AND ALODINED REWORKED AREAS IAW GIV SRM-21-21. Billing Method Hours Rate Total Labor USD: Time and Material ST 5.23 @ $142.00 $742.66 Labor USD: Time and Material ST 1.00 @ $231.00 $231.00 Total USD: $973.66 Step: 18.6.1 Completed REMOVED LIGHT SURFACE CORROSION AND TOOLING MARKS FROM SEVERAL ANTENNA LANDINGS ON THE UPPER FUSELAGE SURFACE BY HAND SANDING AND MECHANICAL MEANS. ALL WORK DONE IAW GIV SRM 51-13-21. Step: 18.6.2 Completed PERFORMED ULTRASONIC THICKNESS MEASUREMENTS PER MAINTENANCE REQUEST AFTER MAINTENANCE REMOVED LIGHT SURFACE FROM SEVERAL ANTENNA LANDINGS ON THE UPPER FUSELAGE SURFACE IAW GIV SRM 51-13-20. INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL 2.0 ULTRASONIC REVISION 7 - SEPTEMBER 16TH, 2015.MEASUREMENTS MARKED ON TAPE ON AIRCRAFT. Step: 18.63 Completed REQUEST ENGINEERING EVALUATION OF REMAINING SKIN THICKNESS WHERE REWORKED: XM ANTENNA ® FS 193- .040 MIN NOTED VHF NO. 1 ANTENNA - .040 MIN NOTED BLADE ANTENNA (i) FS 315 - .040 MIN NOTED ANTI COLLISON LIGHT - .040 MIN NOTED Step: 18.6.4 Completed ENGINEERING DISPOSITION: THE NOTED POST BLEND THICKNESS MEASUREMENTS ARE STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. CONTINUE REWORK OPERATIONS IAW GSIA05300001 (REV -) "ALLOWABLE DAMAGE - FUSELAGE SKIN AT ANTENNA LOCATIONS" Discrepancy: 18.7 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND MULTIPLE UPPER AND LOWER FUSELAGE ANTENNA SURFACES TO BE PAINTED. Resolution: FOUND 3 UPPER (GPS #1, GPS #2 AND ELT) AND 1 LOWER (ATC) ANTENNA SURFACES TO HAVE PAINT ON AIRFRAME SURFACES. REMOVED PAINT WITH NO MATERIAL LOSS NOTED AND CLEANED, ALODINED THESE ANTENNA SURFACES. WORK DONE IAW GIV SRM 51-21-21. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.02 @ $142.00 $144.84 Total USD: $144.84 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 109 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00809047 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 18.8 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE #2 VHF ANTENNA TO BE CORRODED. Resolution: REMOVED SURFACE CORROSION FROM ANTENNA BONDING SURFACE (BASE).. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE IAW GIV SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.06 ® $142.00 $292.52 Total USD: $292.52 Step: 18.8.1 Completed ENTERED IN ERROR Discrepancy: 18.9 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE #3 VHF ANTENNA TO BE CORRODED. Resolution: REMOVED SURFACE CORROSION FROM ANTENNA BONDING SURFACE (BASE).. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE IAW GIV SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.04 ® $142.00 $289.68 Total USD: $289.68 Step: 18.9.1 Completed ENTERED IN ERROR Discrepancy: 18.10 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE RADIO ALTIMETER #1 RECEIVE ANTENNA TO BE CORRODED. Resolution: REMOVED SURFACE CORROSION FROM ANTENNA BONDING SURFACE (BASE).. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE IAW GIV SRM 51-13-10. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.99 ® $142.00 $282.58 Total USD: $282.58 Step: 18.10.1 Completed ENTERED IN ERROR Discrepancy: 18.11 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE AIRPHONE ANTENNA TO BE CORRODED. Resolution: REMOVED SURFACE CORROSION FROM ANTENNA BONDING SURFACE (BASE).. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE IAW GIV SRM 51-13-10. 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 110 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00809048 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Billing Method flours Rate Total Labor USD: Time and Material ST 1.86 @ $142.00 $264.12 Total USD: $264.12 Discrepancy: 18.12 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE L BAND ANTENNA DME/ATC TRANSPONDER ANTENNA DOUBLER TO BE CORRODED. Resolution: REMOVED SURFACE CORROSION FROM ANTENNA DOUBLER.. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE IAW GIV SRM 51-13-10. Billing Method flours Rate Total Labor USD: Time and Material ST 1.98 @ $142.00 $281.16 Total USD: $281.16 Discrepancy: 18.13 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE #1 DME ANTENNA TO BE CORRODED. Resolution: REMOVED SURFACE CORROSION FROM ANTENNA BONDING SURFACE (BASE).. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE JAW GIV SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.99 @ $142.00 $282.58 Total USD: $282.58 Discrepancy: 18.14 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE #2 ATC LOWER ANTENNA TO BE CORRODED. Resolution: REMOVED SURFACE CORROSION FROM ANTENNA BONDING SURFACE (BASE).. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE JAW GIV SRM 51-13-10. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.84 @ $142.00 $261.28 Total USD: $261.28 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 111 of 117 Printed: 6/28/2018 939:11A? Reel EFTA00809049 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 18.15 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE RADIO ALTIMETER #2 TRANSMIT ANTENNA TO BE CORRODED. Resolution: REMOVED SURFACE CORROSION FROM ANTENNA BONDING SURFACE (BASE).. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE IAW GIV SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.15 @ $142.00 $305.30 Total USD: $30530 Discrepancy: 18.16 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE LOWER BEACON LIGHT TO BE CORRODED. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 0.48 @ $142.00 $68.16 'total USD: $68.16 Discrepancy: 18.17 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE TOP GPS ANTENNA TO BE CORRODED. Resolution: REMOVED SURFACE CORROSION FROM ANTENNA BONDING SURFACE (BASE).. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE IAW GIV SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.12 @ $142.00 $301.04 Total USD: $301.04 Discrepancy: 18.18 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE L/H MARKER BEACON ANTENNA TO BE CORRODED. 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 112 of 117 Printed: 6/28/2018 939:11A1 Rent EFTA00809050 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Resolution: REMOVED SURFACE CORROSION FROM ANTENNA BONDING SURFACE (BASE).. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE JAW GIV SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.10 @ $142.00 $156.20 Labor USD: Time and Material OT 1.03 @ $213.00 $219.39 Total USD: $375.59 Discrepancy: 18.19 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE AFT AIRCELL ANTENNA BASE TO BE CORRODED. Resolution: REMOVED SURFACE CORROSION FROM ANTENNA BONDING SURFACE (BASE).. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE JAW GIV SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.10 @ $142.00 $298.20 Total USD: $298.20 Discrepancy: 18.20 WHILE C/W CMP 539516 ANTENNA INTERFACE - INSPECTION FOUND THE FWD AIRCELL ANTENNA BASE TO BE CORRODED. Resolution: REMOVED SURFACE CORROSION FROM ANTENNA BONDING SURFACE (BASE).. ALODINED BARE ALUMINUM AS REQUIRED. WORK DONE JAW GIV SRM 51-13-10. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.08 @ $142.00 $295.36 Total USD: $295.36 Discrepancy: 18.21 WHILE C/W CMP 539516 ANTENNA INTERFACE INSPECTION, FOUND FUSELAGE SKIN AT UPPER TCAS ANTENNA HAS SHARP DEEP GRINDING MARKS. Resolution: BLENDED NOTED TOOLING GOUGE MARKS ON UPPER TCAS CONTOUR PLATE/AIRCRAFT SKIN INTERFACE. PERFORED NDT THICKNESS AND CRACK CHECKS WITH NO CRACKS NOTED. REMAINING SKIN THICKNESS IS STUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. ALODINED AND REINSTALLED DOUBLER PLATE (ITEM 18.2) AS REQUIRED. SEE STEPS FOR FURTHER DETAILS. WORK DONE lAW GIV SRM 51-77-11 AND ENGINEERING DISPOSITION 18.21.4 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 113 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00809051 Bill To: JEGE LLC WO It SC18654 Invoice Number: 6918002027 Billing Method Hours Rate Total Labor USD: Time and Material ST 5.63 @ $142.00 $799.46 Labor USD: Time and Material ST 1.00 @ $231.00 $231.00 Parts USD: Time and Material $82.17 Total USD: $1,112.63 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 18.21 #1 PRI440B1-2-654 SEALANT,6OZ #654 SEMKIT 1 $26.67 $26.67 18.21 #2 IILI9PB5-5 111-1OK 10 $1.64 $16.40 18.21 #3 IILI9PB5-3 111-1OK 10 $3.91 $39.10 Step: 18.21.1 Step: 18.21.2 Step: 18.21.3 Step: 18.21.4 Completed Completed Completed Completed BLENDED NOTED TOOLING GOUGE MARKS ON UPPER TCAS CONTOUR PLATE/AIRCRAFT SKIN INTERFACE WITH SCOTCH BRITE DISC IAW GIV SRN1 51-77-1I. PERFORMED EDDY CURRENT INSPECTION FOR CRACKS ON BLENDED TOOLING GOUGE . NO DEFECTS NOTED.INSPECTION PERFORMED IN ACCORDANCE WITH GULFSTREAM PRODUCT SUPPORT NON-DESTRUCTIVE PROCEDURES MANUAL "3.0 EDDY CURRENT REVISION 25 DECEMBER 15TH, 2017. EDDY CURRENT MACHINE SN 1797Z00 CAL DUE DATE 9/2012018.. REQUEST ENGINEERING EVALUATION OF REMAINING SKIN THICKNESS ENGINEERING DISPOSITION: THE NOTED POST BLEND THICKNESS MEASUREMENTS ON THE 1159B40225-11 SKIN ARE STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. CONTINUE REWORK OPERATIONS IAW GSL405300001 (REV -) "ALLOWABLE DAMAGE - FUSELAGE SKIN AT ANTENNA LOCATIONS" Item: 19 ASC501B & CB236B GUST LOCK THROTTLE INTERLOCK - RETROFIT Team Manager: Charles Helwig ParVModel #: Customer Coordinator: Shannon Sykes AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 19.2 CMP GIV 982362 CB 236B GUST LOCK THROTTLE INTERLOCK - RETROFIT (ASC 501B) *** WARRANTY CB - NO CHARGE LABOR AND MATERIAL Resolution: COMPLIED WITH CMP GIV 982362 CB 236B Gust Lock Throttle Interlock - Retrofit (ASC 501B) Discrepancy: 19.3 CMP GIV 994041 AD 2017-13-11 - GULFSTREAM AEROSPACE - (PART 2)RETROFIT OF GUST LOCK THROTTLE INTERLOCK *** RELATED TO ASC501B & CB236B Resolution: COMPLIED WITH CMP GIV 994041 AD 2017-13-11 - Gulfstream Aerospace - (Part 2)Retrofit of Gust Lock Throttle Interlock 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 114 of 117 Printed: 6/28/2018 9:39:11A1 Reel EFTA00809052 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 19.4 CMP GIV 251109 SEAT ASSEMBLY, PILOT *** RELATED TO ASC501B & CB236B Resolution: COMPLIED WITH CMP GIV 251109 SEAT ASSEMBLY, PILOT Discrepancy: 19.5 CMP GIV 251110 SEAT ASSEMBLY, COPILOT *** RELATED TO ASC501B & CB236B Resolution: COMPLIED WITH CMP GIV 251110 SEAT ASSEMBLY, COPILOT Discrepancy: 19.6 CMP GIV 277010 GUST LOCK HANDLE - REMOVAL / INSTALLATION *** RELATED TO ASC501B & CB236B Resolution: COMPLIED WITH CMP GIV 277010 GUST LOCK HANDLE - REMOVAL / INSTALLATION REMOVED GUST LOCK HANDLE P/N UNK WITH NSN FOR MODIFICATION. INSTALLED NEW GUST LOCK HANDLE P/N 11595B40859-1 NSN. PARTS RECEIVED FROM GAC SAV. REFERENCE FAA FORM 8130-3 WITH TRACKING # 20160904161242, APPROVAL # ODA-511131-CE, DATED 04 SEP 2016. ALL WORK DONE IAW GIV CMP 277010. Discrepancy: 19.7 CNIP GIN. 2770 I I GUST LOCK SYS-OPS TEST *** RE I E 1) ASC501B & CB236B Resolution: Discrepancy: 19.8 CMP GIV 277015 GUST LOCK SYSTEM - RIGGING PROCEDURE *** RELATED TO ASC501B & CB236B Resolution: 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 II 5 of 117 Printed: 6/28/2018 939:11M Reel EFTA00809053 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Discrepancy: 19.9 CMP GIV 344020 MODE SELECT UNIT - REMOVAL / INSTALLATION *** RELATED TO ASC501B & CB236B Resolution: COMPLIED WITH CMP GIV 344020 MODE SELECT UNIT - REMOVAL / INSTALLATION REMOVED AND REINSTALLED MSU WITH P/N CG1227AC01, S/N 097. ALL WORK PERFORMED IAIV GIV MM 34-02-01 MODE SELECT UNIT - REMOVAL / INSTALLATION. SEE ITEM 19.10 FOR OPERATIONAL CHECK. Discrepancy: 19.10 CMP GIV 344086 ATTITUDE AND HEADING REFERENCE SYSTEM / INERTIAL REFERENCE UNIT - OPERATIONAL CHECK *** RELATED TO ASC501B & CB236B Resolution: COMPLIED WITH CMP GIV 344086 Attitude and Heading Reference System / Inertial Reference Unit - Operational Check Discrepancy: 19.11 CMP GIV 346026 FMS CDU NO. 2 - REMOVAL / INSTALLATION *** RELATED TO ASC501B & CB236B Resolution: COMPLIED WITH CMP GIV 346026 FMS CDU NO. 2 - REMOVAL / INSTALLATION REMOVED AND REINSTALLED FMS NO. 2 WITH P/N 7007549-902, S/N 99113632. ALL WORK PERFORMED IAW GIV MM 34-0240 FMS CDU NO. 2 - REMOVAL / INSTALLATION. SEE ITEM 19.12 FOR OPERATIONAL CHECK Discrepancy: 19.12 CMP GIV 349801 FLIGHT MANAGEMENT SYSTEM NO. 2 - OPERATIONAL CHECK *** RELATED TO ASC501B & CB236B Resolution: COMPLIED WITH CMP GIV 349801 Flight Management System No. 2 - Operational Check 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 116 of 117 Printed: 6/28/2018 9:39:11AI Reel EFTA00809054 Bill To: JEGE LLC WO #: SC18654 Invoice Number: 6918002027 Item: 20 ITEM FOR FOLLOW ON OPS AND LEAK CHECKS Team Manager: Charles Helwig Customer Coordinator: Shannon Sykes ParVModel #: AC Serial No/Tail No.: N/A / N/A MN/MO: N/A CSN/CSO: N/A Aircraft Time: N/A Discrepancy: 20.1 ITEM TO TRACK FOLLOW ON OPS AND LEAK CHECKS Resolution: Step: 20.1.1 Open LEAK CHECK REQUIRED ON ALL HYDRAULIC FILTERS ON THE LJH AND Ft/II MANFOLDS AND WHEEL WELLS, CHECK DPI'S AFTER HYDRAULIC POWER APPLICATION. Step: 20.1.2 Completed OPS CHECK PERFORMED FOR L/H AND R/H FUEL TEMP SENSORS - RI-154 IAW GIV MM 28-08-00 FUEL TANK TEMPERATURE INDICATING SYSTEM - INSPECTION / CHECK WITII NO DEFETS NOTED. Step: 20.1.3 Open OPEN ITEM FOR COMPLETION OF RSQCT-71 REV. 06 FLIGHT CONTROL THROWS TRAVELLER Step: 20.1.4 Open OPS CHECK FOR XM ANTENNA ITEM 11.6. Communications concerning disputed debts, including a check or other instrument tendered as full satisfaction of a debt, must be forwarded to: Gulfstream Aerospace Atm: Credit Manager M/S B-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 are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt 2011 Page 117 of 117 Printed: 6/28/2018 939:11A1 Reel EFTA00809055