PRELIMINARY INVOICE Gulfstreant AO CVNAMIC• COMPANY

PRELIMINARY INVOICE Gulfstreant AO CVNAMIC• COMPANY Bldg C.—FAX 561-681-9392 - West Palm Beach. Florida 33406 ParUModel *1: GIV AC Serial No./Tail No.: 1085 / N423W Mail Remittance To: Gulfstream Aerospace Corporation Box 730349 Dallas, Texas 75373-0349 Overnight Remittance To: Gulfstream Aerospace Corporation (Box VS 730349) do JP Morgan Chase Bank. NA ATTN: Dallas National Wholesale Lockbox TX1-0029 14800 Frye Road Ft. Worth, TX 76155 Wire Remittance To: Gulfstream Aerospace Corporation JP Morgan Chase Bank. NA Chicago. IL 60670 Account No. 10-15825 Fedwire Routing No. (ABA) 021 000 021 S.W.I.F.T. CHASUS33 ACH Credit Routing No. (ABA)071 000 013 Bill To: JEGE LLC CIO GALAXY AVIATION INC ATTN: LARRY VISOSKI 3800 SOUTHERN BLVD, SUITE 204 WEST PALM BEACH, Florida 33406 United States Title: JEGE LLC Invoice Number. Invoice Date: Customer ID: M. Number: Repair Station: In Date: Out Date: Payment Type: Payment Terms: 7113001462 4/23/2013 BJ419 FAA CRS PB8R624N 05/13/2013 06/13/2013 CIA - Wire INVOICE SUMMARY FOR WORK ORDER NUMBER: SC13300 Time & Materials Flat Rate Total Labor USD: 55,299.97 $204,738.00 $210,037.97 Pans USD: $0.00 $883,018.00 $883,018.00 Services USD: 5706.67 $0.00 $706.67 Detail Subtotal USD: $6,006.64 $1,087,756.00 $1,093,762.64 Subtotal USD: $1,093,762.64 Funds on Deposit USD: $761,252.00 Total USD: 361,252.00 4/26 400,000.00 6/10 $332,510.64 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_WorkOrderPreliminaryInvoicespt Page I of 27 Printed: 6/13/2013 11:53:50AP Rd: I: EFTA00621054 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Item: 1 Airframe Gulfstream GIV Scheduled N423TT Team Manager. Sean Brown Customer Coordinator: Ray Kraber Part/Model GIV AC Serial No./Tail No.: 1085 / N423TT TSN/TSO: CSN/CSO: 3968 Aircraft Time: #573.4 / 3968 Discrepancy: 1.1 Return to Service FAR Part 91. Resolution: ACTT: 8573.4 ACTL: 3968 DATE: I certify that the maintenance listed 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 the work order has been provided to the operator. Signature, Airworthiness Inspector Gulfstream West Palm Beach, FL 33406 FAA CRS PB8R624N Discrepancy: 1.2 Inbound/Outbound Inspection Resolution: Complied with Inbound/Preliminary Inspection IAW Form GAC-PB1-141.001. rev 2. Complied with Outbound Inspections IAW Form GAC-PBI-W-002, rev 9. Labor USD: No Charge NI C Step: 1.2.1 Step: 1.2.2 Completed Inbound/Preliminary Inspection Waiting Outbound Inspection approval (L) Discrepancy: 1.3 Preflight Inspection Resolution: N/A Discrepancy: 1.4 Resolution: COMpl) with Debrief Checklist For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_WorkOrderPreliminaryInvoice.rpt Page 2 of 27 Printed: 6/13/2013 II:53:50AI Rd: I: EFTA00621055 Bill To: JEGE LLC WO If: SC13300 Invoice Number: 7113001462 Step: 1.4.1 Completed ArrivaVDebrief 90 Day Due List Review Accomplished. Step: 1.4.2 Waiting List Operator's Airworthiness Requirements & Special Documentation Requests. approval (L) Step: 1.4.3 Waiting Review Technical Operations Update prior to return to service for newly released approval (L) bulletins and advise operator. Discrepancy: 1.5 Tool Clearance Resolution: Complied with removal of all tools Discrepancy: 1.6 Cover & Protect Resolution: Complied with protection as required to perform maintenance requested. Labor USD: No Charge N/ C Discrepancy: 1.7 Resolution: N/A Service Chemical Toilet/Clean Galley Discrepancy: 1.8 Resolution: Na Arrival/Departure Assist & Video Aircraft Discrepancy: 1.9 Sample Hydraulic Fluids Resolution: N/A 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_WorkOrderPreliminaryInvoicespt Page 3 of 27 Printed: 6/13/2013 11:53:50A1 Rd: I: EFTA00621056 Bill To: JEGE LLC WO SC13300 Invoice Number: 7113001462 Discrepancy: 1.10 Resolution: N/A Remove Valuables & Secure. Discrepancy: 1.11 Comply with Service Team Manager Checklist Resolution: Complied with as required. Discrepancy: 1.12 Fluids Used (Oils/Skydrol) - (Materials Only) Resolution: N/A Discrepancy: 1.13 STM / Quality review of work order and logbook entry prior to departure Resolution: Complied with as required. Discrepancy: 1.14 Towing (Does not include Hangar Moves) Resolution: Complied with towing 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 Page 4 of 27 Printed: 6/13/2013 11 :53:50Ali Rd: I: EFTA00621057 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Discrepancy: 1.15 Resolution: N/A Hathlat - Identify & provide a manifest, and a Shipper's Declaration for Dangerous Goods for all hazardous materials that are loaded aboard any aircraft. FAR Part 121 or 135 Operators will provide a hazardous material notification letter required by FAR 135.505 (e) prior to maintenance at this Repair Station iaw FAR 145.206 (a) (b). If there is to be loading of hazardous materials it shall be complied with by Hazmat trained authorized GDAS-PBI personnel only. Discrepancy: 1.16 Aircraft Cleaning Resolution: Discrepancy: 1.17 Billable Consumables & Shop Supplies Resolution: To be billed as required. Parts USD: Total USD: Billing Method Hour: Rate Total Flat Rate $4.000.00 $4.000.00 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_WorkOrderPreliminaryInvoicespt Page 5 of 27 Printed: 6/13/2013 11 :53:50Ali Rd: I: EFTA00621058 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Discrepancy: 1.18 Resolution: N/A Major Alterations regulatory compliance requirements to be completed by installer as indicated on FAA form 8110-3. Copy and paste from attached statements as needed and edit as required. COMPLY WITH REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d). COMPLIED WITH THE REQUIREMENTS OF FAR 25.1301 (d), 25.1353(a) and 25.1431(c) (d), via GROUND TEST REPORT -REPORT No. CEXXXXXXXX REV. X, ( IN SUPPORT OF STC XXXXXXXXX ) and GR4R216M REPAIR STATION INTERFERENCE TESTING REQUIREMENTS POST MAJOR ALTERATIONS COMPLIANCE FORM. COMPLY WITH REQUIREMENTS OF FAR 25.1529, INSTRUCTIONS FOR CONTINUED AIRWORTHINESS. REF XXXXX MANUAL, P/N XXXXXXX REV. X, FOR INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AND BLOCK 8 OF FAA FORM 337, DATED XX/XX/XXXX. COMPLY WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01-04 AND FAR 25.1353 (B) COMPLIED WITH THE WIRE ROUTING REQUIREMENTS OF FAA POLICY ANM-01.04 AND FAR 25.1353 (B) BY ENSURING ROUTING WAS IN ACCORDANCE AC43.13-1B, CHANGE 1 CHAPTER 11, SECTION 8. Discrepancy: 1.19 Update Weight & Balance 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_WorkOrderPreliminaryInvoicespt Page 6 of 27 Printed: 6/13/2013 II:53:50AP Rd: I: EFTA00621059 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Discrepancy: 1.20 Exterior Paint and Weight & Balance Requirements. Review scope of aircraft exterior paint touch-up/repairs, and skin replacements resulting in paint reapplication, and determine affect on weight and balance. For surfaces where paint is stripped and reapplied or added on top of existing paint on an area greater than 36 square feet the thickness values will be documented before and after painting. If average thickness values remain the same, weight and balance revision is not required. For surfaces painted with an area greater than 36 square feet and before and after paint thickness average varies, QC review for possible weight and balance revision will be required. * Thickness will be plotted on an aircraft drawing derived from AMM chapter 6 or other suitable sketch, attached to the work order and measurements taken on a two square foot grid. * Reference GAMPS 4000, paragraph 3.5.1 for paint restrictions to flight control surfaces and RVSM certified aircraft. * Reference GAMPS 4000, total average thickness shall not exceed 6 mils. * Per GAC Mass Properties Engineering, paint thickness of 5 mils equals .055 pounds per square fid. * If after QC review, weight change is greater than 2 pounds or .05% of MAC, the weight and balance report will require recomputation. Resolution: N/A Discrepancy: 1.21 Resolution: Na "Advise customer of preservation requirements per ATA Chapter 10 of the relevant maintenance manuals for Airframe, Engines, and APU; review requirements in relation to scheduled Date Promised and later potential Date Completed; and perform maintenance or preservation actions as directed by the customer and documented as a Work Order Squawk. Item: 6 Avionics Team Manager. Sean Brown Customer Coordinator: Ray Kraber Part/Model g: (;IV AC Serial No./Tail No.: 1085 / N423TT TSN/TSO: CSNICSO: Aircraft Time: 8573.4 / 3968 Discrepancy: 6.1 Squawk from flight test - Standby fuel gauge totalizer is indicateing 2001bs lower than the LT and RT fuel gauges and there is a 150Ibs difference between total fuel on EICAS primary and systems page compared to STBY totalizer gauge - EICAS and SYSTEMs page ind same Ref. SC13175 6.7 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 Page 7 of 27 Printed: 6/13/2013 II:53:50AP Rd: I: EFTA00621060 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Resolution: Removed Standby Fuel Qty indicator P/N 1159SCP460-101 S/N 520 for repair. All work accomplished JAW GIV AMM 28-06-00. Installed a REPAIRED Dual Standby Fuel Quantity Indicator PN.: 1159SCP460-101, SN.: 520 obtained from Parker Hannifin Corp., Hauppauge, NY, FAA App./Cert.# FX1R 156K. Complied with Sections B and C of Gulfstream GIV CUP 284042 Fuel Quantity Dual Standby Indicator - Removal / Installation. Additionally complied with Gulfstream GIV CMP 284029 Fuel Low Level Warning System - Operational Test and CMP 284044 Fuel Quantity Indication System - Operational Check. System Ops. Checks Good. Work done IAW Gulfstream GIV AMM Chs. 28.06.00 and 28-07-00. Step: 6.1.1 Completed Step: 6.1.2 Completed Removed Standby Fuel Qty Indicator P/N I159SCP460-101 S/N 520 for repair. All work accomplished IAW GIV AMM 28-06-00. Installed a REPAIRED Dual Standby Fuel Quantity Indicator PN.: 1159SCP460-101, SN.: 520 obtained from Parker Hannifin Corp., Hauppauge, NY, FAA App./Cert.# FXIR 156K. Complied with Sections B and C of Gulfstream GIV CMP 284042 Fuel Quantity Dual Standby Indicator - Removal / Installation. Additionally complied with Gulfstream GIV CMP 284029 Fuel Low Level Warning System - Operational Test and CMP 284044 Fuel Quantity Indication System - Operational Check. System Ops. Checks Good. Work done IAN' Gulfstream GIV AMM Chs. 28-116.011 and 28-07-00. Discrepancy: 6.2 Squawk from flight test - LED light burned out on Rate of Climb / FPM (3 digit from LT) on pressurization controller ref. SC13175 6.8 Resolution: Removed Cabin Press/Rate Of Climb Indicator P/N Pressurization indicator P/N 1159SCF407-7 S/N 168DB was removed and sent out for repair. Reinstalled repaired cabin pressure ind assy P/N 1159SCF407-7 S/N 168DB. Complied with Pressure Indicator - Operational Test. System Ops. Checks Good. All work performed IAW Gulfstream GIV AMM Chapter 21.02.00 and 21.00.00. Reference item SC13300.8.4 for Pressurization Ground Delta P Functional check. Step: 6.2.1 Step: 6.2.2 Step: 6.2.3 Completed Removed, wrapped, and tagged upholstered overhead panel from night deck. Removed Center Overhead Panel immediately aft of Overhead Instrument panel. Removed circuit breaker panel overlays ( L/R ) temporarily to gain access to Overhead Instrument Panel attaching screws. Removed screws and dropped Overhead Instrument Panel. Removed Cabin Press/Rate Of Climb Indicator P/N 1159SCF407-7 S/N 168DB to be sent out for repair. Temporarily re-installed Overhead Instrument Panel and I../R circuit breaker panel overlays to facilitate the access of power to the aircraft. All work performed IAW Gulfstream GIV AMM Chapter 21.00.00. Completed Reinstalled repaired cabin pressure ind assy P/N 1159SCF407-7 SIN 168DB. Awaiting ops check. All work done IAW GIV MM AMM Chapter 21.00.00. Completed IAN? Gulfstream GIV CMP 213022 Cabin Pressure Indicator - Removal / Installation item B. (6); performed Cabin Pressure Indicator - Operational Test. System Ops. Checks Good. Work done IAW Gulfstream GIV AMM Ch. 21-02-00. NOTE: A/C stills needs Gulfstream GIV CMP 213086 Pressurization Ground Delta P - Functional Check when A/C is outside and APU running. Discrepancy: 6.3 Squawk from flight test - With both engines and APU running and both converters on DC volts on the Right-Left-AUX or ESS selected indicate 47.8VDC 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_WorkOrderPreliminaryinvoicespt Page 8 of 27 Printed: 6/13/2013 I 1:53:50Ali Rd: I: EFTA00621061 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Step: 6.3.1 Step: 6.3.2 Completed Completed C/W CMP 245060 from steps A. to steps B.(6). Removed EPMP P/N 159SCAV373-1007 S/N N1069 for service. Work performed IAW GAC GIV MM 24-03-02. Installed repaired EPMP PN: I I59SCAV337-1007 SN: N1069. Installed overlay next to EPMP. Awaiting ops check. All work done IAW GIV AMM 24-03-02. Discrepancy: 6.4 Squawk from flight test - On RNAV approach VNAV worked and then became unavailable on approach Ref. SC 13175 6.12 Also crew states Predictive Raim fail Resolution: Removed defective #2 VHF Nay Receiver P/N 622-7194-201, S/N 3647 to be sent out for repair. Installed modified #2 VHF Nav Receiver PIN 622-7194-201, S/N 3647. Op ck good. Work done IAW GIV MM 34-02-02, with no defects noted. Updated CMP 345006 NOTE predictive RAIM fail is addressed in item 6.10 Step: 6.4.1 Completed Removed suspected bad #2 VHF Nay Receiver P/N 622-7194-201, S/N 3647 to be sent out for repair 3-15-13. All work performed IAN' Gulfstream GIV AMM Chapter 34-03.00. Step: 6.4.2 Completed Installed modified #2 VHF Nay Receiver P/N 622-7194-201, S/N 3647. Op ck good. Work done IAW GIV MM 34-02-02, with no defects noted. Discrepancy: 6.5 Squawk from flight test - Standby engine instrument gauge is indicating all "8888"s on RT HP gauge Resolution: Removed Standby Engine Indicator P/N 1159SCF412-11 S/N 9904598BA for repair. All work accomplished IAW GIV AMM 77-14-00. Installed an OVERHAULED Standby Engine Instruments Indicator PN.: 1159SCF412-11, SN.: 9904598BA obtained from Aero-Mach Labs, Inc., Wichita, KS, FAA App./Cert.# NU2R 044L. Complied with Gulfstream GIV CMP 770009 Standby Engine Instruments Indicator - Removal / Installation Sections "C" and "D". Additionally complied with Gulfstream GIV CMP 770001 Standby Engine Instruments - Operational Test. System Ops. Checks Good. Work done IAW Gulfstream GIV AMM Ch. 77-14-00. Step: 6.5.1 Completed Step: 6.5.2 Completed Removed Standby Engine Indicator P/N 1159SCF412-II S/N 9904598BA for repair. All work accomplished lAW GIV AMM 77-14-00. Installed an OVERHAULED Standby Engine Instruments Indicator PN.: I 159SCF412-11, SN.: 9904598BA obtained from Aero-Mach Labs, Inc., Wichita, KS, FAA App../Cert.# NU2R 044L. Complied with Gulfstream GIV CMP 770009 Standby Engine Instruments Indicator - Removal / Installation Sections "C" and "D". Additionally complied with Gulfstream GIV CMP 770001 Standby Engine Instruments - Operational Test. System Ops. Checks Good. Work done IAW Gulfstream GIV AMM Ch. 77-14-00. Discrepancy: 6.6 TCAS processor stuck in air mode. Unable to test from processor or load data. Resolution: Found pin 62 recessed on Avionics Interface Unit connector. Locked in recessed pin 62. TCAS system ops checks good. All work done IAW Gulfstream GIV AMM 34-47-00. See steps for further details of work performed. 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_WorkOrderPreliminaryInvoicespt Page 9 of 27 Printed: 6/13/2013 I I :53:50Ali Rd: I: EFTA00621062 Bill To: JEGE LLC Labor USD: No Charge Step: 6.6.1 Step: 6.6.2 Step: 6.6.3 WO #: SC13300 Invoice Number: 7113001462 N/ C Completed Verified TCAS connector RMP-13F and Rh1P-5K grounds. Pin 5K is reading 250 ohms to ground. Researched GAC WDM and found that the WDM does not have prints for this S/N aircraft. Contacted GAC techops. Techops researched but could not find the prints for this aircraft. Awaiting customer's completion prints to troubleshoot system. Work performed IAW ACSS SB 8008558-001. Completed Researched A/C drawings and found that WCI DIM 08069372 dated 9-8-93 shows that originally PN.: 4066010-902 was installed. The TCAS computer has been updated to PN.: 4066010-910 in 2001. Performed TCAS - Functional Check and found that TCAS ops. checks good every time and all proper indications are present. However noticed that the computer's front panel LEDs did not illuminate. Researched this system's manufacturer's MM and found Honeywell TCZ-910 TCAS System Description and Installation Manual Pub. No. A15-3840-001 online. The computer's LED illumination conditions are as follows: la. Power-on Self-test, lamps on for a 3 sec. self-test (lamps only flashed momentarily), lb. Test OK, green TCAS PASS lamp on for 10 sec. (this does not happen0. Ic. Fault Found, a fault i8ndicator will illuminate for 10 sec. (PTT through tall always PASSES). 2. Continuous Self-Test, if fault is stored, data may be re-called on ground (no data apparent, computer PTT button appears inactive). 3a. Commanded Self-Test. push unit's PTT for lamp and fault/pass indications ( pushing PTT creates no output), 3b. PTT during self-test second time should recall faults (PTT Inactive). With this system returning TCAS SYSTEM TESTS OK every time tested through RTUs, it appears that the computers PTT is inoperative. Lamps only flash briefly when power is initially applied to A/C. Also, can we determine "Why the TCAS appeared to be stuck in 'AIR' mode?" Work done JAW Gulfstream GIV AMM Ch. 34.47.00 and Honeywell TCAS TCZ-910 System Description and Installation Manual Pub. No. A15-3840-001. Completed Found pin 62 recessed on Avionics Interface Unit connector. Locked in recessed pin 62. TCAS system ops checks good. All work done 'ANY Gulfstream GIV AMM 34-47-00. Discrepancy: 6.7 Radome has delamination and moisture. Resolution: Repaired/Modified Radome Assembly P/N 1159B21040-S7K as per B/P SE05204902-1,. CE443356002. Rev-. 03 Radome Mod, Engineer Dispos 1.2.2 and 1.4.1. Work order RC329452/1.1 Discrepancy: 6.8 Per customer's request, chrome plate the T/R knobs. Resolution: Duplicate Squawk, reference 7.1 for work performed. Discrepancy: 6.9 APU EGT indication on DU #4 shows 0, RPM indication is normal. Overhead APU indicator is normal. Resolution: Billing Method Flours Rate Total Labor USD: Time and Material ST 0.50 @ $118.00 $59.00 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_WorkOrderPreliminaryInvoicespt Page 10 of 27 Printed: 6/13/2013 11 :53:50Ali Rd: I: EFTA00621063 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Total USD: $59.00 Discrepancy: 6.10 Crew states Predictive Raim fail Resolution: Could not duplicate discrepancy. After GPSs had acquired satellites, I entered info in to FMSsfor each of the GPSs to display RAIM for at least 3 different locations and different times. Predictive RAIM was computed every time. Both GPSs op ck good. Work done IAW GIV MM 34-52-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 1.00 @ $118.00 $118.00 Total USD: $118.00 Item: 7 Interior N423TT Team Manager: Sean Brown Customer Coordinator: Ray Kraber Part/Model #: AC Serial No./Tail No.: TSN/TSO: CSNICSO: Aircraft Time: 8573.4 / 3968 Discrepancy: 7.1 Customer requests to remove and send out the both engine throttle knobs and both thrust reverser knobs for chrome plating. Note: Prior to knob removal, visual inspection revealed the No.1 throttle knob housing is cracked on the inboard side (pies in G drive). Also, multiple scratches on both knobs. Resolution: Re-installed previously removed throttle switches and knobs #land #2 do to unavailability of new knobs P/N na S/N na and TR knob's P/N na S/N na. Op's check all switches all check good. All work was done IAW Gulfstream GIV AMM 20-10-01. No defects noted. Billing Method Flours Rate Total Labor USD: Time and Material ST 22.13 @ $118.00 $2,611.34 Labor USD: Time and Material OT 0.07 @ $177.00 $12.39 Parts USD: No Charge N/C Services USD: No Charge N/C Total USD: $2.623.73 Services: Ref. No. 7.1 #1 Description Vendor Supplied Labor Quantity Sell Price USD Extended USD 1.00 $0.00 $0.00 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 Page I I of 27 Printed: 6/13/2013 II :53:50A? Rd: I: EFTA00621064 Bill To: JEGE LLC Step: 7.1.1 Step: 7.1.2 Step: 7.1.3 WO #: SC13300 Invoice Number: 7113001462 Completed Removed throttle switches and knobs on #1 and #2 throttles P/N na S/N na and TR knob's P/N na S/N na. Note: Prior to knob removal, visual inspection revealed the No.1 throttle knob housing is cracked on the inboard side and needs to be replaced (pies in G drive), and the No.2 Takeoff/Go Around switch wouldn't physically click to operate. All work was done IAW Gulfstream GIV AMM 20-10-01. Completed Re-installed throttle switches and knobs on #1 throttle. All work was done IAW Gulfstream GIV AMM 20-10-01. Completed Re-installed throttle switches and knobs on #2 throttle. All work was done IAW Gulfstream GIV AMM 20-10-01. Discrepancy: 7.2 Remove Cabin switch panels, Galley switch panels and all other plated components and Ship to: International jet Interiors do Eric Roth / Jay Massar 2221 Smithtown Ave Ronkonkoma NY 11779 Ref 1085 GIV NOTE: 2 Panels previously removed before Aircraft came in. Interior company is going to change the plating color. Resolution: Per customer request, removed Cabin switch panels, Galley switch panels and all other plated components and shipped as requested to International jet Interiors. Billing Method Hours Rate Total Labor USD: Time and Material ST 17.45 @ $118.00 $2,059.10 Labor USD: Time and Material OT 032 @ $177.00 $56.64 Total USD: $2.115.74 Step: 7.2.1 Completed Step: 7.2.2 Step: 7.2.3 Removed through out cabin all Galley Switch Panels and all other plated components and Ship to: All work was done IAW Gulfstream GIV AMM 20-10-01. International jet Interiors do Eric Roth / Jay Massar 2221 Smithtown Ave Ronkonkoma NY 11779 Completed Removed through out cabin, galley, aft lav and sliding baggage door latches, strikers, cabinet latches and lea. cigar holder for plating. Components to be shipped to: AU work was done IAW Gulfstream GIV AMM 20-10-01. International jet Interiors do Eric Roth / Jay Massar 2221 Smithtown Ave Ronkonkoma NY 11779 Completed Removed pilot, co-pilot overhead panel, center overhead panels and breaker closeout panel. Removed (2ea.) switch assy's, (3ea.) cold air vents and (7ea.) light ass'ys to be sent out for plating. All work performed IAW GIV AMM 25-10-00. International jet Interiors do inn. S Mechanical 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 Page 12 of 27 Printed: 6/13/2013 II :53:50AP Rd: I: EFTA00621065 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Team Manager. Sean Brown Customer Coordinator: Ray Kraher Part/Model #: GIV AC Serial No./Tail No.: 1085 / N423TT TSN/TSO: CSN/CSO: Aircraft Time: 8573.4 / 3968 Discrepancy: 8.1 While complying with Radome removal, found radome hinge bushing seized will require replacement. (PN: GA476-109) Resolution: Labor USD: Parts USD: Parts: Ref. No. No Charge No Charge Part number: Description 8.1 #2 GA476-I09 BUSHING Quanta • 2 N/ C N/ C Step: 8.1.1 Completed Researched part number and placed two (2) bushing on order. No shipping status at this time. Discrepancy: 8.2 #1 Left engine fire bottle was discharged into right engine. Resolution: Removed LT engine fire bottle P/N 32700022, S/N 06758C2 with LT AFT cartridge P/N M30903823, S/N 05662 and LT FWD cartridge P/N M30903823, S/N 05676. Installed an Overhauled LT engine fire bottle P/N 32700022, S/N 06758C2 with a NEW LT AFT cartridge P/N M30903823, S/N 06643 with a MFG Date of 03/2012 and a NEW LT FWD cartridge P/N M30903823, S/N 06724 with a MFG Date of 05/2012 IAW GIV MM 26-02-00. Overhaul, Hydro test, weight check and cartridge install performed by AMERON GLOBAL PRODUCT SUPPORT, CRS RU2R148L W.O. 279829 This updates CMPs 262025, 262115, 262116, 262117, 262118, 262065 and 262045 Labor USD: No Charge Parts USD: No Charge Services USD: No Charge Services: Ref. No. Description Quantity 8.2 #1 SERVICE 1.00 Part Ref: 32700022 FIRE BOTTLE, ENGINE - WITHOUT CARTRIGE (HALON 1301) N/ C N/ C N/ C Discrepancy: 8.3 The APU alternator's thermal switch has a broken wire Resolution: New harness installed by CMP GIV 974653 ASC 465C APU 36-150(G) Installation.(REF 12.1) no further action required Parts USD: No Charge N/ C Discrepancy: 8.4 CMP GIV 213086 Pressure Ground Delta P-Function Test, reference item SC13300.6.2 Resolution: COMPLIED WITH CMP GIV 213086 Pressure Ground Delta P-Function Test. No defects noted. Work done I.A.W. GIV M. chap. 21.02.00. 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_WorkOrderPreliminaryinvoicespt Page 13 of 27 Printed: 6/13/2013 II :53:50A) Rd: I: EFTA00621066 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Discrepancy: 8.5 When converting from a -100 to a -150 APU the CMP code 490055 APU Alternator Bearing Discard came up as Overdue. Resolution: Updated CMP Code 490055 - APU Alternator Bearing Discard. The APU Alternator P/N 1159SCAV373-105, S/N 129-A0171, was installed overhauled on 5/11/05 at 4355.0 TSN (APU). No further action is required. Discrepancy: 8.6 Comply with GIV CMP 262631 Portable Halon Fire Extinguisher (Right Cockpit) - Inspection Resolution: Complied with GIV CMP 262631 Portable Halon Fire Extinguisher (Right Cockpit) - Inspection. No defects noted IAW GIV MM 26-03-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 0.25 @ $118.00 $29.50 Total USD: $29.50 Discrepancy: 8.7 Comply with GIV CMP 262632 Portable Halon Fire Extinguisher (FWD Cabin) - Inspection Resolution: Complied with GIV CMP 262632 Portable Halon Fire Extinguisher (FWD Cabin) - Inspection. No defects noted JAW GIV MM 26-03-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 0.25 @ $118.00 $29.50 Total USD: $29.50 Discrepancy: 8.8 Comply with GIV CMP 262633 Portable Halon Fire Extinguisher (AFT Cabin) - Inspection. Resolution: Complied with GIV CMP 262633 Portable Halon Fire Extinguisher (AFT Cabin) - Inspection. No defects noted LAW GIV MM 26-03-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 0.25 @ $118.00 $29.50 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_WorkOrderPreliminaryInvoicespt Page 14 of 27 Printed: 6/13/2013 I 1:53:50A? Rd: I: EFTA00621067 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Total USD: $29.50 Discrepancy: 8.9 Comply with GIV CMP 262621 Portable Halon Fire Extinguisher (Right Cockpit) - Weight Check. Resolution: Complied with GIV CMP 262621 Portable Halon Fire Extinguisher (Right Cockpit) - Weight Check. No defects noted IAW GIV MM 26.03.00. Extinghuisher weighed 31bs. 12.6oz. Billing Method Flours Rate Total Labor USD: Time and Material ST 0.25 @ $118.00 529.50 Total USD: $29.50 Discrepancy: 8.10 Comply with GIV CMP 320004 Main Landing Gear (Left) - Lubrication Resolution: Complied with GIV CMP 320004 Main Landing Gear (Left) - Lubrication IAW GIV MM 32-10-00. Billing Method Flours Rate Total Labor USD: Time and Material ST 0.75 @ $118.00 S88.50 Total USD: $88.59 Discrepancy: 8.11 Comply with GIV CMP 320005 Main Landing Gear (Right) - Lubrication Resolution: Complied with GIV CMP 320005 Main Landing Gear (Right) - Lubrication IAW GIV MM 32.10.00. Billing Method Flours Rate Total Labor USD: Time and Material ST 0.75 @ $118.00 588.50 Total USD: $88.50 Discrepancy: 8.12 Comply with GIV CMP 320006 Nose Gear - Lubrication Resolution: Complied with GIV CMP 320006 Nose Gear - Lubrication IAW GIV MM 32-20-00. 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_Work0rderPreliminaryInvoicespt Page 15 of 27 Printed: 6/13/2013 I 1:53:50A? Rd: I: EFTA00621068 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Billing Method Hours Rate Total Labor USD: Time and Material ST 0.75 @ $118.90 588.50 Total USD: $88.50 Item: 10 Outstanding Parts, Materials, and / or Services Team Manager: Sean Brown Customer Coordinator: Ray Kraber ParVModel 0: AC Serial No./Tail No.: TSN/TSO: CSNICSO: Aircraft Time: 8573.4 / 3968 Discrepancy : 10.1 Resolution: Parts from items Parts USD: No Charge N/ C Discrepancy: 10.2 Service fur APU Resolution: Discrepancy: 10.3 ASC Kit for ASC 468A. Kit is unavailable at this time. Resolution: Parts USD: No Charge Pans: Ref. No. Pan number: Description NI C Quantity Sell price USD Extended USD 103 #1 A.SC468A-1 G4 KIT, COCKPIT SWITCH INDICATOR 1 $0.00 LIGHTING, 1000-1535" $0.00 Item: 12 ASC 465C Honeywell GTCP -36-150 Upgrade - Proposal GAC0413-293-GIV.1085-R00 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_WorkOrderPreliminaryInvoicespt Page 16 of 27 Printed: 6/13/2013 I I :53:50Ali Rd: I: EFTA00621069 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Team Manager. Sean Brown Customer Coordinator: Ray Kraber ParVModel #: AC Serial No./Tail No.: TSN/ISO: 7047.11 CSN/CSO: N/.\ Aircraft Time: 8573.4 / 3968 Discrepancy: 12.1 CMP GIV 974653 ASC 465C APU 36-150(G) Installation. ASC 465C APU 36-150 Installation (without MSP) Having ASC 470. Resolution: Removed Honeywell Loaner GTCP36-100(GIV) APU P/N 3800062-9-1, S/N P-115-C with 7047.0 TSN. Installed the Customers Modified GTCP36-150(G) APU P/N 3800826-1, S/N P-465C with 6449.0 TSN, (0.0 Hrs Hobbs). Removed APU Electronic Control Unit (ECU) P/N 2118478.1, S/N 63, and installed new APU Electronic Control Unit (ECU) P/N 2119584-6002, S/N 32-W03312. Operational checks good. All work was performed IAW GIV AMM chapter 49-10-00, ASC 465C, and GIV-GER-9957. REF steps for actual work performed Labor USD: Parts USD: Services USD: Total USD: Parts: Ref. No. Billing Method Flours Flat Rate Flat Rate No Charge Pan number: Description Rate Total $27,967.00 5183,046.00 N/ C $211,013.00 Quantity 12.1 #1 12.1 #2 12.1 #3 12.1 #4 12.1 #5 12.1 #6 12.1 #7 12.1 #8 12.1 #9 12.1 #I0 Services: 2119584-6002 2025598-1 ASC465C-2 G4 1159SB21515-11 AMS3374C TYPES 1 & M.S20615.4M5 NAS43HT4-24 K11707 1595443-I 1159SB40637-1 CONTROL UNIT, ELECTRONIC, APU CABLE, LAPTOP/ECU MAINT INTERFACE KIT, AUXILARY POWER UNIT (APU) 36-1501G] INSTALLATION, 1000-1535 HAVING ASC470 DOUBLER 3 SEALANT KIT, 6 OUNCE FIREWALL RIVET SPACER WASHER VESTIBULE INSERT GROUND STRAP 6 1 12 1 Ref. No. Description Quantity 12.1 #3 REPAIR 1.00 Part Ret: GTCP36-I00G APU (3800062-9-1) 12.1 #1 Vendor Supplied Labor Loo Part Ret: 3800826-1 AUXILIARY POWER UNIT (CIMS) 12.1 #2 SERVICE Part Ret: 1159B2I638-103 NOZZLE ASSY 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_WorkOrderPreliminaryInvoicespt Page 17 of 27 Printed: 6/13/2013 II :53:50A? Rd: I: EFTA00621070 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Step: 12.1.1 Completed Performed GIV CMP code 490001 removal and install of APU steps B-I through B4 complete. Remove exhaust pipe from APU or access. All work performed IAW GIV NIM 49-00-00. Step: 12.1.2 Completed Complied with CMP 490001 APU GTCP36-100(G)-Removal/Installation step B.(5) through (13). Removed APU P/N 3800062-9-1, SN P-115-C with APUTT. 7047. All maintenance performed IAW GIV AMM 49-10-00. Step: 12.1.3 Completed Removed existing Doubler P/N 1159SB2I416-75 from APU upper enclosure between BL 1.84 and BL 10.97. Located, fitted and match drilled and installed new Doubler P/N 1159SB21515-11, and new Doubler P/N 11595B21515.I3. All maintenance performed IAW Gulfstream Doubler Installation , APU Enclosure Rework Drawing No. I I59SB21515. Removed existing APU ECU PIN 2118478-1, SN 63. Located, fitted and match drilled and installed new support Angle's (2ea.) P/N 115951140041.I7, and new Zee support P/N I I59SB40041-31 at RBL 26.510 of upper APU enclosure. Located, fitted and match drilled and installed new Support Assembly P/N 1159SB40041.5, with new NICI: Tray P/N T600-2-S-R-A-100. and new Bracket Assembly P/N I I59SB40041-9. Located, fitted and match drilled and installed new Support Assembly P/N 1159SB40041-7 at RBL 19.5 of upper APU enclosure. Located, fitted and match drilled and installed new Support Bracket (lea.) P/N 1159SB40017-19, and new Support Bracket's (2ea) P/N 11595B40017-17 onto new APU exhaust nozzle welded Assembly P/N 11595B40017-1, and installed on reworked nozzle Assembly P/N 1159SB21638-103. Located, fitted and match drilled and installed new Deflector P/N I I59SB40920-19 on APU exhaust nozzle. All maintenance performed IAW Gulfstream GIV APU Modernization-GTCP36-150(G) Intl Drawing No. 1159ASC41465. Step: 12.1.4 Completed Removed APU Pallet assembly from 36-100 APU and installed on 36-150 APU. Ilnstalled new apu alternator spline adapter (PN: 1595443.1). Installed APU Alternator Mount (PN: 1159SCAV373-203, SN: 29361. Installed apu Alternator (PN: II59SCAV373-105, SN: 129-A0171). All maintenance accomplished in reference to GIV & GIV-MSG3 Maintenance Manual Chapter 49-10-00 Steps C.(1)(a) through C.(1)(g) and Aircraft Service Change No. 465C.Grounding Strap (PN: 11595B40637 -I) placed on order. No shipping status at this time. Step: 12.1.5 Completed Completed the internal modification of the 339A1 Aux Power Relay Box and performed continuity check with no defects noted. Also, terminated and mounted APU enclosure connector 48A IJ4. All work done IAW Gulfstream GIV APU Retrofit Wiring Diagram I I59SB49006, Rev L, sheet 3.001, for aircraft effectivity 1001, 1006-1182. Step: 12.1.6 Completed Installed exhaust assembly on APU with new V-clamp, P/N NM102422G0700. Work accomplished referencing GIV M/M 49-10-00. Step: 12.1.7 Completed Installed modified APU GTCP36-I50(G) P/N 3800826-1, SN P-465C 'ASV ASC 465C. Installed new Ground Strap PN 1159SB40637-1, IAW ASC No. 249. Complied with the following CMP's 490051 APU GTCP36-150(G) Removal/Installation, 491305 Auxiliary power Unit Drains System GTCP36-150(G)-Inspection, APU Pallet Assembly and Vibration Isolators GTCP36-150(G)-Inspection, APU Enclosure GTCP36-150(G)- Inspection, and 491306 APU Fuel Control and Air Inlet Plenum Drains GTCP36-150(G)- Operational Check. Step: 12.1.8 Completed Completed the external modification of the 339A1 Aux Power Relay Box and terminated all other remaining mod wiring. Performed continuity check with no defects noted. Still need to reconnect exisitng ground wires adjacent to the APU enclosure firewall connectors and final dress and protect wiring. All work done IAW Gulfstream CIV APU Retrofit Wiring Diagram I159SB49006, Rev L, sheet 3.001, for aircraft effectivity 1001, 1006-1182. Step: 12.1.9 Completed Reconnected ground wires adjacent to the APU enclosure firewall connectors and final dressed and protected the wiring. Perfomed power and ground check for the new APU Electronic Control Unit (ECU) with no defects noted. Installed new APU Electronic Control Unit (ECU) P/N 2119584-6002,5/N 32-W03312. Ops check to be performed when aircraft gets relocated outside the hangar. All work done IAW Gulfstream GIV APU Retrofit Wiring Diagram 11595B49006. Rev L. sheet 3.001, for aircraft effectivity 1001, 1006.1182 and GIV AMM 49-60-00. Step: 12.1.10 Completed Complied with GIV-GER-9957 APU operational test after install of ASC 465. See item 6.9 for squawk. All other indications and operations normal. Work done I.A.W. GIV-GER-9957. Item: 13 PlaneDeck DU-885 - GAC0313-223-GIV.1085-R00 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_WorkOrderPreliminaryInvoicespt Page 18 of 27 Printed: 6/13/2013 I 1:53:50Ali Rd: I: EFTA00621071 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Team Manager. Sean Brown Customer Coordinator: Ray Kraber ParVModel #: AC Serial No./Tail No.: TSN/TSO: N/A CSN/CSO: N/A Aircraft Time: 8573.4 / 3968 Discrepancy: 13.1 CMP GIV 974761 ASC 476A Electronic Display System - DU-885 Liquid Crystal Display (LCD) Installation (PlaneDeck). Resolution: COMPLIED WITH CMP GIV 974761 ASC 476A Electronic Display System - DU-885 Liquid Crystal Display (LCD) Installation (PlaneDeck). All work performed IAW ASC 476A, 1159ASC41476 Rev "E", Top Drawing - Honeywell DU-885 Cockpit Display and Gulfstream MM Chapter 21-00-00, 23.00.00, 31-00-00, and 34-00-00. Deviations shown on Customer Engineering Drawing List DL No. CE41 4960458 Approved by FAA Form 8100.9 dated 06**/2013. No defects noted. Reference Gulfstream Airplane Flight Manual Supplement No. GIV-2011.01. Updated the following CMP Codes: 316021, 316022, 316022, 316023, 316024, 316025, 316026, 316075, 316074, 316073, 316072, Labor USD: Pans USD: Services USD: Total USD: Pans: Ref. No. 316071, 316070, 348000, Billing Method 316301, 316300, 316700, 316701, 316040, Hours Rate 346019, 346020, 346021 Total Flat Rate Flat Rate No Charge Pan number: $113,540.00 S576,460.00 N/ C Description 5690.000.00 Quantio. 13.1 #1 K9321061A02 BLACK LCD DISPLAY UNIT I 13.1 #2 K9321061A02 BLACK LCD DISPLAY UNIT I 13.1 #3 K9321061A02 BLACK LCD DISPLAY UNIT I 13.1 #4 K9321061A02 BLACK LCD DISPLAY UNIT I 13.1 #5 K9321061A02 BLACK LCD DISPLAY UNIT I 13.1 #6 K9321061A02 BLACK LCD DISPLAY UNIT I 13.1 #7 G7228-02 DATA LOADER -1000 BLACK (CIMS) I 13.1 #8 ASC476A-1 G4 KIT, DU885 LCD MODERNIZATION, I AC WITH BLACK COCKPIT,1000-1252 13.1 #9 M22520/2-37 TOOL ( DANIEL DIE SET) 1 13.1 #10 M22520/2-37 TOOL ( DANIEL DIE SET) 1 13.1 #11 Y776 Die, Danlals HX4 1 13.1 #13 GAC860K-I END CAP, WHITE 100 13.1 #14 NF24Q100 CABLE 81 13.1 #16 D436-37 SLEEVE 100 13.1 #17 7003155.902 CIRCUIT CARD ASSY 1 13.1 #18 GAC861AD224S CABLE 20 13.1 #19 TV06RGQW25.8S CONNECTOR 1 13.1 #2I PR 1440-B-2 SEALANT, PRC, CARTRIDGE 6oz 1 13.1 #22 73E-8203 GRIP ASSEMBLY, CURSOR 1 CONTROL FOR DU885 BLACK LI I PILOT 13.1 #23 CT.1122E04F513 BLOCK ASSEMBLY 1 13.1 #24 M81714-60-22-04 MODULE 1 13.1 #25 PR1422-B-1/2 SEALANT,PRC,CARTRIDGE 1 13.1 #26 GA436-I PANEL ASSY (BLACK) 1 13.1 #27 PRI440-B-1/2 SEALANT, PRC,CARTRIDGE 1 13.1 #28 GAS805BB-36 SPLICE,ENVIRO.(RED) D436-36 100 13.1 #29 TC92 PLATE 100 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 Page 19 of 27 Printed: 6/13/2013 I 1:53:50Ali Rd: I: EFTA00621072 Bill To: JEGE LLC Pans: Ref. No. Pan number: WO #: SC13300 Invoice Number: 7113001462 Description Quantity 13.1 830 M8I969-14-11 EXTRACTOR, RED & WHITE 100 PLASTIC 13.1831 M81969/14-01 INSERTION/EXTRACTION TOOL 100 Services: Ref. No. Description S( t. 13.181 ELECTRICAL / STRUCTURAL ENG. (SAV.) 1.00 13.182 Vendor Supplied Labor 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 Page 20 of 27 Printed: 6/13/2013 11 :53:50A/, Ref: EFTA00621073 Bill To: JEGE LLC Step: 13.1.1 Completed WO #: SC13300 Invoice Number: 7113001462 Removed copilot circuit breaker (CB) panel overlay NPN, NSN, and sent out for engraving. All work done IAW Gulfstream GIV AMM 20-28-00. Step: 13.1.2 Completed Removed #1 DU-880 P/N 4053000-901 S/N 88020674,#2 DU-880 P/N 4053000-901 S/N 90011270,#3 DU-880 P/N 4053000-901 SIN 88090305,#4 DU-880 P/N 4053000-901 S/N 99033336,#5 DU-880 P/N 4053000-901 S/N 01014136 and #6 DU-880 P/N 4053000-901 S/N 88100930. All were removed for MOD. ASC 476 A Electronic Display System - DU-885 Liquid Crystal Display (LCD) Installation (PlaneDeck). Each DU removed weighed 30.4 lbs, and removed from Sta 73. Updated the following CMP's for permanent DU removal; 316021. 316022, 316023, 316024, 316025, and 316026. All work was done JAW Gulfstream GIV AMM 20-28-00. Step: 13.1.3 Completed Removed LH, Center and RH DU filters (6ea.) behind cockpit electronic displays. All work performed IAW G1V MM 39-10-00. Step: 13.1.4 Completed Removed LH, RH cockpit side panel carpet, and storage units, removed pilot, co-pilot seats, removed 101 LH, RH #1,2,3 console closeout panels, RH cockpit fire extinguisher S/N-732449, RH cockpit entry trim. LH, RH cockpit junction box closeouts, RH,LH radiorack covers, LH jepp storage box a.ts'y. All work performed lAW G1V MM 25.20.00. Step: 13.1.5 Completed Removed fwd and aft MED door hinge covers, cockpit step box, floor panels FLR15 and FI.R16. All work performed lAW GIV MM 25-20-00. Step: 13.1.6 Completed Removed DAU#2 PN: 7007580-901 SN: 88100296, Symbol Generator #2 PN:7008570-905 SN: 91090754, 5 VLT Test PN: UNK SN: UNK, Performance Computer #2 PN: 7004609-925 SN: 94039666, Fault Warning Computer #2 PN: 7007484-905 SN: 88090300, and Nay Computer #2 PN: 7018879-03 SN: 95120678. All work done IAW GIV MM 31-20-00. Step: 13.1.7 Completed Removed LH, RH cockpit carpet, panels 107-LH-1, LH-2, LH DU fan PIN 508617, SIN ST4809, RH DU fan PN 508617, 5/N ST4811. All work performed lAW G1V MM 39-20-00. Step: 13.1.5 Completed Removed and discarded CRT fan commutating modules (FWD) PIN 508534 S/N ST2634 1.135 station 147.5, weight 1.5 LBS and AFT module PIN 508534 S/N ST4821 FUS station 151, weight 1.5 LBS also Cap stow commutating module wiring. All work was done lAW Gulfstream GIV AMM 21-10-01 and dwg 1159SB40743. Step: 13.1.9 Completed Permanently removed left and right display unit plenum assemblies, hoses, ducting, filters, fans, clamps and hardware. Total weight of DU equipment permanently removed from FS 73 totals 11.65 lbs. Performed this work lAW ASC 476A. Step: 13.1.10 Completed Removed Passenger Briefing Box P/N:114000B S/N8904288. Removed GPWS PIN 965.0976.003.218.218 S/N 1601. Removed No. 3 VHF arr P/N 822-1116-001 S/N 1609. Removed No. 3 VOR arr P/N 622-7194-201 S/N 975. Removed No. 1 Performance/ Autothrottle Computer P/N 7004609-925 S/N 90120389. Removed No.1 Nay Computer P/N 7018879-03014 S/N 95120669. Parts removed for wire routing access. All work performed 1A1V GAC GIV MM 20-28-00. Step: 13.1.11 Completed Removed the following equipment front RJR and LAi radio racks for wiring access. SELCAL P/N 120000-000 S/N 003 Airshow P/N 920050 S/N 1395 Audio Amplifier P/N 990-3070-014 S/N 9611112 . All work performed IAW GIV MM 31.00.00. AFIS D111U P/N 400-045500-0003 S/N 402 #1 Fault Warning Computer P/N 7007484-905 S/N 88090305 #1 Data Acquisition Unit P/N 7007580-901 S/N 87060191 #1 Symbol Generator PIN 7OO8570.905 S/N 88090405 #3 Symbol Generaror P/N 7008570-905 SIN 90010585 Annunciator Dim/test Box P/N 1159SCF422-7 SIN 0087 Performed this work lAW GIV AMM 20-28-00. Step: 13.1.12 Completed Removed micellaneous panels in Pedestal, Pilot's and co-Pilot's side console area. Refer to RI log book for P/N and S/N. All work was done IAW Gulfstream GIV AMM 20-10-01. Step: 13.1.13 Completed Terminated wires for Left Cockpit Junction Panel and Right Cockpit Junction Panel IAW ASC 476A Elect Display wiring DWG 115951140743. Step: 13.1.14 Completed Removed copilot's main circuit breaker panel, and stored in avionics shop for wiring/cb modifications. Permanently removed all six display unit connector hardware and square connector mounting bracket. Total weight removed eqauLs .62 lbs from FS 75. Performed this work lAW ASC 476A. 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 Page 21 of 27 Printed: 6/13/2013 I I :53:50Ali Rd: I: EFTA00621074 Bill To: JEGE LLC WO #: SC13300 Invoice Number: 7113001462 Step: 13.1.15 Completed Routed pull wires thru conduits thruout RH Radio rack and side console, terminated TJ blocks ASC48ITJI and ASC48ITJ2 also routed wire harness from ATC #1 and ATC #2 on to cockpit area. All work was done IAW Gulfstream GIV dwg 11595641481. Step: 13.1.16 Completed Located pilot's audio control panel connector S0AIPI. Spliced pilot's cursor control device (CCD) wires IRA1.312CC22. IRAI3566622, L807WW22(blu), and I.168FF22(wht) to pilot's audio control panel existing wires. Routed these wires to the new CCD location on Pilots side console. Located copilot's audio control panel connector 80A2P1. Spliced copilot's CCD wires 2RA1312CC22, 2RA1356BB22, I.8056622(blu), and L1916622(wht) to copilot's audio control panel existing wires. Routed these wires to the new CCD location on copilots side console. Performed this work IAW ASC 476A DWG 11595B40743 REV F. Step: 13.1.17 Completed OW Installation and ring out of Plt.s, and CopIts CCD and XM Weather 2 amp CB P/N-1159AV33013.2, 1 each, to respective connectors. No defects noted. All work performed LA. W. GIV XM-W/D-11595B40468 sht-2, and Primus Elite EDS / DU-885 ASC ) W/D. Step: 13.1.18 Completed Treminated wires at the #1 and #2 GPS connectors 503A1P1 and 5503A2PI also terminated wires at connector 315A1J2, 306A1P11 and routed wires thruout Co-pilot's side console. All work was done IAW Gulfstream GIV DWG 11595840743 and11595641481. Step: 13.1.19 Completed Permanetly removed the existing EMS Data Loader DL-950 P/N G7226-02 SIN 1678. The data loader came of FS 169 R, and weighed 1.17 lbs (Aux RR). This data loader will be replaced with DL-I000 for ASC 476A. Updated GIV CMP 346040 for permanent removal of this part. Performed this work IAW GIV AMM 34-02-00. Step: 13.1.20 Completed Working IAW ASC476A and Gulfstream drawing CE540040002 worked items F8/F9 and figures 2.0-2.1. Step: 13.1.21 Completed Working IAW Gulfstream drawing 11595B40470 Antenna installation XM Weather. located and drilled -II doubler, -05 nutplate holder assy. Cutout foot print of antenna 01420.1 from M/F5C34114001-235, creating -15 contour doubler. All parts ready for installation. Step: 13.1.22 Completed Completed assembly and dress of ASC 476A wiring harness on avionics wire harness board. Harness weighed 7.2 lbs. and routes from FS 85.0 through FS 174.3. Loosely installed and routed harness. Currently inwork on routing breakouts to their respective equipment locations. All work done IAW Gulfstream DU-885 Wire Routing Dnvaing No. 11595640471. Step: 13.1.23 Completed Working IAW Gulfstream drawing 11595640470 installed one -11 doubler, two -05 nutplate holder assy, one -15 contour doubler and one new XM Antenna PN C1420-1, SN 393565 at ES 174.25 and 1.B1.. 3.77. Combined total weight of install is 0.420 lbs. Seperate weights are as followed antenna 0.2 lbs. and structure materials 0.22 lbs. Related item CMP 316701 XM Weather Antenna complied with. Step: 13.1.24 Completed Terminated wires at the Avionics shelf #2 372A1 TJ2, Avionics shelf #1 372A1 TJI, ASC476TJ9, Data loader 95A5PI and annun dim test box 140A1 connector 140A1P2A. All work was done IAN' Gulfst