EFTA00621054.pdf

Gulfstreant AO CVNAMIC• COMPANY PRELIMINARY INVOICE ParUModel *1: GIV AC Serial No./Tail No.: 1085 / N423W Bldg C.—FAX 561-681-9392 - West Palm Beach. Florida 33406 Mail Remittance To: Overnight Remittance To: Wire Remittance To: Gulfstream Aerospace Corporation Gulfstream Aerospace Corporation (Box VS 730349) Gulfstream Aerospace Corporation Box 730349 do JP Morgan Chase Bank. NA JP Morgan Chase Bank. NA Dallas, Texas 75373-0349 ATTN: Dallas National Wholesale Lockbox TX1-0029 Chicago. IL 60670 14800 Frye Road Account No. 10-15825 Ft. Worth, TX 76155 Fedwire Routing No. (ABA) 021 000 021 S.W.I.F.T. CHASUS33 ACH Credit Routing No. (ABA)071 000 013 Invoice Number. 7113001462 Bill To: JEGE LLC Invoice Date: 4/23/2013 CIO GALAXY AVIATION INC Customer ID: BJ419 ATTN: LARRY VISOSKI 3800 SOUTHERN BLVD, SUITE 204 M . Number: Repair Station: FAA CRS PB8R624N WEST PALM BEACH, Florida 33406 In Date: 05/13/2013 United States Out Date: 06/13/2013 Payment Type: CIA - Wire Payment Terms: Title: JEGE LLC 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: $332,510.64 361,252.00 4/26 400,000.00 6/10 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_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 Part/Model GIV Customer Coordinator: Ray Kraber 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 Completed Inbound/Preliminary Inspection Step: 1.2.2 Waiting Outbound Inspection approval (L) Discrepancy: 1.3 Preflight Inspection Resolution: N/A Discrepancy: 1.4 COMpl) with Debrief Checklist 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 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 Service Chemical Toilet/Clean Galley Resolution: N/A Discrepancy: 1.8 Arrival/Departure Assist & Video Aircraft Resolution: Na 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 Remove Valuables & Secure. Resolution: N/A 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 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. Resolution: N/A Discrepancy: 1.16 Aircraft Cleaning Resolution: Discrepancy: 1.17 Billable Consumables & Shop Supplies Resolution: To be billed as required. Billing Method Hour: Rate Total Parts USD: Flat Rate $4.000.00 Total USD: $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 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. Resolution: N/A 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 fi d. * 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 "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. Resolution: Na Item: 6 Avionics Team Manager. Sean Brown Part/Model g: (;IV Customer Coordinator: Ray Kraber 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 Removed Standby Fuel Qty Indicator P/N I159SCP460-101 S/N 520 for repair. All work accomplished IAW GIV AMM 28-06-00. Step: 6.1.2 Completed 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 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. Step: 6.2.2 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. Step: 6.2.3 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 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. Step: 6.3.2 Completed 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 Removed Standby Engine Indicator P/N 1159SCF412-II S/N 9904598BA for repair. All work accomplished lAW GIV AMM 77-14-00. Step: 6.5.2 Completed 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 WO #: SC13300 Invoice Number: 7113001462 Labor USD: No Charge N/ C Step: 6.6.1 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. Step: 6.6.2 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. Step: 6.6.3 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 Part/Model #: Customer Coordinator: Ray Kraber 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. Description Quantity Sell Price USD Extended USD 7.1 #1 Vendor Supplied Labor 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 WO #: SC13300 Invoice Number: 7113001462 Step: 7.1.1 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. Step: 7.1.2 Completed Re-installed throttle switches and knobs on #1 throttle. All work was done IAW Gulfstream GIV AMM 20-10-01. Step: 7.1.3 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 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 Step: 7.2.2 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 Step: 7.2.3 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 Part/Model #: GIV Customer Coordinator: Ray Kraher 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: No Charge N/ C Parts USD: No Charge N/ C Parts: Ref. No. Part number: Description Quanta • 8.1 #2 GA476-I09 BUSHING 2 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 N/ C Parts USD: No Charge N/ C Services USD: No Charge N/ C Services: Ref. No. Description Quantity 8.2 #1 SERVICE 1.00 Part Ref: 32700022 FIRE BOTTLE, ENGINE - WITHOUT CARTRIGE (HALON 1301) 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: