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FBI VOL00009
EFTA00811141
64 pages
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Bill To: Plan D, LLC. Pans: Ref. No. Part number: WO #: SC521661 Description Invoice Number: 5517132452 Quantity 13.1 #88 M524694-C7 SCREW. MACHINE, FLAT CTSK HD, 7 100 DEG, STRI, CROSS RECESSED 13.1 #89 MS21043-08 NUT, SELF LOCKING, REDUCED H 36 13.1 #90 M524694-C7 SCREW, MACHINE, FLAT CTSK HD, 24 100 DEG, STRI, CROSS RECESSED 13.1.1 #1 NA51581K4R5 BOLT 22 13.1.1 #2 NA51580V3R6 SCREW I50 Services: Ref. No. Description Quantity 13.1 #3 Vendor Supplied Labor 1.00 13.1 #1 IAS. Carders. 13.1.6.8 hrs. 2/5-2/11 1.00 13.1 #2 1AS, Carders. 13.1.6.8 hrs, 2/12-2/18 1.00 13.1.2 #1 1AS Graf, David 20.0 HRS item 13.1.2 1.00 13.13 #1 1AS Biddle. Brett 40.0 IIRS and 4.0 HRS OT item 13.1.3 on 1.00 12/11/17-12/14/17 13.13 #2 1AS Graft. David 11.O IIRS item 13.13 on 12/13/17 1.00 13.1.5 #1 1AS Blanton 40 hrs + 5Inrs ot 13.1.5 12/17 1.00 13.1.6 #1 IASSIKES,12/25-12/31.13.1.6.„16 HOURS 1.00 13.1.6 #2 1AS , Sikes ,13.1.6 , 46hrs. , 1/8 - 1/13 1.00 13.1.6 #3 1AS, Johnson,I3.1.6, 2 hrs. 1/29-2/4 1.00 Step: 13.1.1 Completed Mechanical Paint Traveler Step: 13.1.1.1 Completed Temporarely install of panel 325AT. and panel 337CT for paint traveler per G550 AMM 55-30-00 Rev.Nov 15/17. Ref.13.1.1 Step: 13.1.1.2 Completed Remove panel 325AT. and panel 337CT after completion of paint traveler per G550 AMM 55-30-00 Rev.Nov 15/17. Ref.17.1 Step: 13.1.1.3 Completed Complied with landing gear cycling operational checks. No faults noted at this time. Work done per G550 MOM 3240-00. Nov 15117 Step: 13.1.1.4 Completed Panel 325AT installed. needs sealant, panel 337C1 waiting for ops checks prior to final installation Step: 13.1.1.5 Completed Complied with Aircraft paint traveler RSQCT-330Rev.8. Ftetpaper copy for work performed. Step: 13.1.2 Completed Strip Aircraft Step: 13.13 Completed Prep Aircraft Step: 13.1.4 Completed Layout Aircraft Step: 13.1.5 Completed Paint Aircraft Step: 13.1.6 Completed Detail Aircraft Step: 13.1.7 Waiting approval Weight and balance (L/P/S) Step: 13.1.7.1 Waiting lnsp Complied with the physical weighing of the aircraft as outlined in the steps of RSQCT 15 Rev 17 and the 6550 Weight and Balance Manual. Step: 13.1.7.2 Completed Competed the weight and balance report and insert into the customer's weight and balance manual. Step: 13.1.8 Completed customer support Step: 13.1.9 Completed engineering support Discrepancy: 133 Radome to structure perimeter steps- detail inspection Rill side negative step of .053 out of limits, marked with masking tape with arrows per 6550 AMM 53-02-01 Rev. Nov 15/17. Ref.Piant traveler II A. Resolution: Complied with engineering disposition on item 133.1.1 see steps below for all work preformed Billing Method Hours Rate Total Labor USD: Time and Material ST 0.45 @ $146.00 $65.70 Labor USD: Time and Material ST 0.25 @ $222.00 $55.50 Total USD: $121.20 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_RevenueSquawkslnvoice.rpt v3 Page 21 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811161
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Step: 133.1 Step: 133.1.1 Step: 133.2 Step: 13.3.3 Completed Request engineering disposition to correct R/Ii side negative step on radome that is out of limits. Completed Engineering Disposition: It is acceptable to repair the out-of-tolerance radome steps in accordance with Gulfstream Service Letter CR.005300001 Rev. - ."Aerodynamic Filler Sweep - Fair Procedure - Radome Steps". This Gulfstream Service Letter (GSL) is classified as a Manufacturer's Service Document and is governed by Advisory Circulars 20-176A and AC 120-77. Completing a repair per a Gulfstream Service Letter is similar to completing a repair per the Structural Repair Manual (SRM): No serial number specific FAA Form 8100-9 is required and will not be provided in support of a GM. repair. The Engineering (Source) Data for this Service Letter has been shown to comply with the applicable FAR's and is FAAApproved. Engineering source data is retained by Gulfstream as proprietary data. Completed Request paint to comply with engineering dispo during full strip and paint, ref item 13.1 Completed Comply with post-paint radome to fixed structure perimeter steps and gap measurements. Discrepancy: 133 Replace MED belicrank cover hardware where attaches at airstair riser rail with unpainted screws and washers per customer request. Resolution: Replaced MED hardware with correct hardware PN:AN525-832-7 per Drawing 159B140023 Revd]. Billing Method Hours Rate Total Parts USD: Time and Material $126.65 Total USD: $126.65 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 13.541 AN525-832-1I SCREW I $7.27 $7.27 13.542 NA51149DN816H WASHER, FLATALUMINUM 10 $0.23 42.30 13.543 MS210421.08 NUT, SELF LOCKING 10 $0.44 $4.40 13.514 AN525-832R11 SCREW I $0.22 $0.22 13.545 AN525-8321211 SCREW 5 $0.22 $LI0 13.546 AN525-8321211 SCREW I $0.22 $0.22 13.547 AN525-8321211 SCREW I 50.22 $0.22 13.548 WH832RIIDGI3WH SCREW 14 $7.87 $110.18 13.549 AN525-8321211 SCREW I $0.74 $0.74 Discrepancy: 13.7 One drain dlverter missing just forward of tail compartment door. Resolution: Replaced drain diverter PN:1159B4147517-13 just forward of tall compartment door per G550 AMM 53-51-00 RevJan 15/10. Time adhesive GAA100BD04 was applied 14:00 PM, set in 6 hours. Parts USD: Total USD: Billing Method Hours Rate Total Time and Material $11235 $11235 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 13.781 115981O47517-B DIVERTER DRAIN, AFT LOWER 1 $11235 4112.35 PANEL Discrepancy: 13.8 Customer Requests to polish and swap I.JH and FUR eventing E-light lenses. Resolution: •**Summan.*** Removed 6 et erwing emergency light lenses. Polished lenses. Reinstalled 6 °venting emergency light lenses. Sealed 6 overwing emergency light lenses. See steps below for 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). riAC_RevenueSquawksInvoice.rpt v3 Page 22 of 64 Printed: 3/7/2018 3:15:05PM tit W. EFTA00811162
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Billing Method Hours Rate Total Labor USD: lime and Material ST 18.00 @ $146.00 $2,628.00 Total USD: $2,628.00 Step: 13.8.1 Completed Step: 13.8.2 Completed Removed 6 overwing emergency light lease covers. Sealent required for 6 overwing emergency light loose coven Item: 14 Photographic Documentation - (Ref. Item D 2.1 of Proposal 104 7037536. ROO) Team Manager: Charles Thomas Customer Coordinator: Julian Brown Part/Model #: AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Item: 15 Jet ConneX (Ka-band) High -Speed Data System Installation - (Ref. Item B 2.2 of Proposal ID# 7038248 R02) Team Manager: Charles Thomas Customer Coordinator: Julian Brown Part/islodel #: AC Serial No/Tail No.: TSWISO: CSN/CSO: Aircraft Time: Discrepancy: 15.1 Jet ConneX (Ka-band) I firth-Speed Data System Installation Gulfstream will install this latest version of high-speed Broad-Band data system. One (1) Modem Manager (MODMAN) will be installed in the aft baggage compartment in a new cabinet. If Sat TV is installed, the existing cabinet will be modified and reused unless the cost exceeds the new cabinet installation. As the overall manager for the system, the MODMAN is responsible for providing the user interfaces to the aircraft/passengers. One (I) Aeronautical Personality Module (APN1) will be located in the baggage compartment equipment cabinet and holds the configuration data for the system. One (I) Ka-band Aircraft Network Data Unit (KANDU) will be installed in the boiler room. The KANDU receives commands front the MODMAN through an Ethernet Interface to configure the antenna/KRFU and reports status over this Ethernet interface One (I) Ka-band Frequency Unit (KRFU) will be installed in the proximity of the TMA assembly on top of the tail empennage. The KRFU contains a Block-Down Converter (BDC) to convert the received Ka-band frequencies to IF frequencies and also is made up of a Block-Up Convener (BUC) to convert the IF frequencies to Ka-band frequencies. A Iligh- Potter Amplifier (IIPA) increases the signal strength for transmission by the antenna. One (I) Tail Mounted Antenna (TMA) will be mounted on top of the tail empennage underneath the radome. The antenna system is to acquire and establish communications with satellites in various orbits to enable beyond lineof- sight communications between airborne, ground fixed, and ground transportable terminals. The Radome will be removed and replaced by a new Ka-band capable radome. Certification: The Jet ConneX (Ka-band) High-Speed Data System along with the Satcom Direct Router will be installed via Gulfstream STC; expected, availability of STC, 4th Quarter 2017. n* SEE APPENDIX *** 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_RevenueSquawksInvoicc.rpt v3 Page 23 of 64 Printed: 3/7/2018 3:15:05PM tit W. EFTA00811163
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: Complied with installation of Jet ConneX (Ka-band) High-Speed Data System per STC ST03238AT-D Index List GC413038007 Rev R. Configuration Lists 6C513038031 Rev A, GC513038034 Rev A, and GC513038035 Rev —. Reference Custom Electrical Drawing List CE51 496???? Rev ?? and Custom Mechanical Drawing List CE5200???? Rev ?? for deviations. Complied with GC41 429G002 Rev — and GC51 303G007 Rev — Ground Test Plans with no defects noted. Instructions for Continued Airworthiness GC51 303A004 Rev F applicable to this installation and incorporated into maintenance program. Airplane Flight Manual Supplement GC51 303M005 Rev F incorporated into Flight Manual Reference GWBR000000160 Rev — for Weight and Balance Supplement. Reference GC51 4696768 Rev — for Electrical Load Analysis Ref 15.30 for Cockpit Storage Box upuolstered with Grospoint Poster P/N GPFR0242 (Ref work 15.20) Reference CE51 4696543 Rev -- for Electrical Load Supplement. One ( I ) SDR will be installed in the aft baggage and interfaced with the existing aircraft internet capable systems. New wiring for the 3C cellular antenna will be installed in the cabin in an engineering approved location. If the aircraft has an existing Gogo system installed, the SDR will be integrated with the Gogo utilizing existing Ethernet provisions for single MID, unless otherwise directed by Ow ner/Operator. If provisions are not present, Ethernet cabling will be quoted as a separate item. New Components: One (1) 90400012-0001 - Honeywell Modem Manager (MODMAN) One (I) 90401121 - Honeywell Aeronautical Personality Module (APM) One (I) 90401202 - Honeywell Ka-band Frequency Unit (KRFU Convection Cooled) One (1) 90400013-0001 - Honeywell Tail Mounted Antenna (TMA) One (I) 90401566 - Honeywell Ka-band Aircraft Network Data Uolt (KANDU) One (I) 1233-F-2191-10 - Satcom Direct Router (SDR) One (I) Radome Various Installation Kits Certification: The Jet ConneX (Ka-band) High-Speed Data System along with the Satcom Direct Router will be installed via Gulfstream STC: expected. availability of STC. 4th Quarter 2017. Notes: If an existing Sat TV system is removed to accommodate the Ka band system the CMS software may be modified to remove the Satellite Television. This modification is not included in the sell price of the Ka band system and will be provided after a detailed engineering review is completed. estimated charges approximately 518,000. Changes to the Aircraft's Completion Center Maintenance Handbook (COUR), or Cabin Operating Manual (COM) are not included as part of this Proposal. Should a modified CCMH or COM be requested by the Customer, it may be provided at additional charge. Gulfstream may require assistance front the Customer's Information Technologies (IT) department for the configuration of the high speed data system. Notes: (continued) This involvement will verify proper system configuration as well as provide system simplicity to the operator. This will be coordinated at the time of installation and will be completed prior to delivery of the aircraft. The Customer must establish and maintain a service subscription for the Ka-band system. Quote assumes sufficient space is available for the equipment above and does not include relocation of equipment to provide space. This installation is a managed program. Please contact your Regional Sales Manager to coordinate the availability of components and installation. Billing Method Hours Rate Total Labor USD: Flat Rate 5192.054.00 Pans USD: Flat Rate 5492.946.00 Semites USD: No Charge N/ C 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_RevenuaquawksInvoice.rpt v3 Page 24 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811164
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Bill To: Plan D, LLC. Total USD: WO #: SC521661 Invoice Number: 5517132452 5685,000.00 Parts: Ref. No. Part number: Description SATCOM DIRECT ROUTER ANTENNA ANTENNA ADAPTER, TNC TO SMA TERRETRIAL MODEM ANTENNA INSTALLATION OF SATCOM (HIGH SPEED DATA HD-I28) SYSTEM PEDESTAL SWITCH PANEL ASSY SLEEVE SPACER CONNECTOR PLUG, D-SUB, 25-PIN RCPT, SOCKET, D-SUB, 25-20 GA BACKSHELL SPACER KA PED OVERLAY SLEEVE SPACER CONNECTOR BACKSHELL CONNECTOR BACKSHELL CONNECTOR BACKSHELL SWITCH KIT, SDR COAX CABLE REMOTE WIFI ANTENNA RING RING CLIP CABLE, ONE CONTINUOUS LENGTH ON SPOOL BOLT, PROTRUDING SHEAR HEAD, TITANIUM BOLT BOLT BOLT, PROT SHEAR HEAD, TI BOLT BOLT, PROTRUDING SHEAR HEAD, TITANIUM COLLAR, SHEAR BOLT, PROTRUDING SHEAR HEAD. TITANIUM BOLT, PROTRUDING SHEAR HEAD. TITANIUM SOLDER SLEEVE (BRAID) SOLDER SLEEVE (PIG TAIL) LUG,TERMINAL,YELLOW,H8 TERMINAL TERMINAL LUG, TERMINAL, RED, #8 CAP END TERMINAL TERMINAL CLIP ASSEMBLY. 90 DEG. ANGLE HINGE BASE (BLUM LARGE) Quantity 15.1 #1 15.1 #2 15.1 #3 15.1 #4 15.1 #5 15.1 #6 15.1 #7 15.1 #8 15.1 #9 15.1 #10 15.1 #11 15.1 #12 15.1 #13 15.1 #14 15.1 #15 15.1 #16 15.1 #17 15.1 #18 15.1 #19 15.1 #20 15.1 #2I 15.1 #22 15.1 #23 15.1 #24 15.1 #25 15.1 /426 15.1 #27 15.1 #28 15.1 #29 15.1 #30 15.1 #3I 15.1 #32 15.1 #33 15.1 #34 15.1 #35 15.1 #36 15.1 #37 15.1 #38 15.1 #39 15.1 #40 15.1 #4I 15.1 #42 15.1 #43 15.1 #44 15.1 #45 15.1 /446 15.1 #47 15.1 #48 15.1 #49 15.1 #51 I233-F-2191-I0 100-1021-30 100-1021-50 PE9079 PI8350-001 ST03238AT-D GPM004001402-301 27498-001 27498-006 GAC830T3 M24308/4-3F M24308/2-3F DB115339-22 27498-006 GPM004001714-301 27498-001 27498-008 hIS27473T12F3S M85049/49-2-12N N1S27473T16F55S M85049/49-2-161C N1S27473T18F35S M85049/49-2-181C 27500-010 500-35750-101 PI6917-001 GAR540BY16 GAR540BY22 D20419 GAC861AH424S GAB511AB6B5 GAB511AB6B6 GAB511AB6B7 GAB511AB6B8 GABSIIAB6B4 GAB5I [ABM GAN510AA6 GAB511AB6B5 GAB511AB6B5 GAS830AJ2 GAS830All I GA11051110-08 GAT8051118-3B GA11051118-36 GA11051118-08 324484 GAT805P8-08 GAT8051110-3A 5684-01 173H7100 2 2 6 100 100 41 30 40 20 IS 4 70 41 41 I00 100 50 50 50 50 100 20 75 50 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_RevenueSquawksInvoice.rpt v3 Page 25 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811165
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Bill To: Plan D, LLC. Pans: Ref. No. Pan number: WO #: SC521661 Description Invoice Number: 5517132452 Quantity 15.1 #52 GA436-5/3 PANEL ASSY-CONSOLE BLANK 2 (COLOR GREY) 15.1 #53 NAS1581K4R6 BOLT 2 15.1 #54 110872 TNC CONNECTOR, STRAIGHT PLUG 3 15.1 #55 M24308/2-1F RCPT, D-SUB, 9-SOCKET I 15.1 #56 GAR835NK1 RELAY I 15.1 #57 65009-001-513 SOCKET I 15.1 #58 CTJ716E01D-513 DEU COMPOSITE TERMINATION 1 SYSTEM 15.1 #59 1-480698-0 PLUG 1 15.1 #60 ABMM-A-C CABLE, TIE MOUNT 20 15.1 #61 1032.119-24 B/R INSERT, THREADED 50 15.1 #62 225791-3 INSERT, SIZES FOR RG188 2 15.1 #63 P18350-001 TERRETR1AL MODEM ANTENNA I 15.1 #64 D38999/26FD19SN CONNECTOR, PLUG I 15.1 #65 D38999/26FC4PN CONNECTOR I 15.1 #66 AS21919WDG23 CLAMP I 15.1 #67 M53367-1-9 STRAP. TY WRAP 1.000 15.1 #68 NAS1802-3-13P SCREW, HEX HD, CRUCIFORM REC. 10 FULL THD, A286 CRES 15.1 #69 NAS1802-3-8P SCREW 10 15.1 #70 hIS210421.3 NUT 20 15.1 #71 NA51149F0332P WASHER. FLAT STEEL 30 15.1 #72 NAS1802-3-10P SCREW. HEX HD, CRUCIFORM REC, 10 FULL THD. A286 CRES 15.1 #73 hIS27039C0807 SCREW-MACHINE. CRES PAN HD, 10 STRI. 15.1 #74 NA51149FN832P WASHER. FLAT STEEL 10 15.1 #75 M525083-7BB11 JUMPER, BONDING CNT I 15.1 #76 310701 CABLE, COAX 50 15.1 #77 CTR002 PLUG, TNC, 90 DEGREE I 15.1#78 BTS002 RCPT,TNC BULKHEAD I 15.1 #79 2-139N602-70 0 -RING 2 15.1 #80 E1257-70/2-0I5 0 RING RUBBER 2 15.1 #81 NAS1580C3T12 BOLT 10 15.1 #82 BTS002 RCPT,TNC BULKHEAD I 15.1 #83 CTR022 CONNECTOR I 15.1 #84 27500-044 SWITCH I 15.1 #85 C75-520/20 CONTACT 30 15.1 #86 XP-610 PRINTER, EPSON I 15.1 #87 ABMM-A-C CABLE, TIE MOUNT 15 15.1 #88 M24308/4-1F CONNECTOR I 15.1 #89 MS35207-269 SCREW 6 15.1 #90 D436-36 SLEEVE 200 15.1 #91 GAC860K-1 END CAP, WHITE 300 15.1 #92 324485 WIRE END CAPS 150 15.1 #93 GAC860K-3 END CAP-BLUE 100 15.1 #94 GAC860K-4 END CAP (YELLOW) 100 15.1 #95 CTS002 PLUG, TNC, STRAIGHT I 15.1 #96 CTS022 CONNECTOR I 15.1 #97 GARI00B2B0031 RUBBER .031 SHEET 9 15.1 #98 MS35207-260 SCREW 50 15.1 #99 MS35207-262 SCREW 50 15.1 #100 MS35207-264 SCREW 50 15.1 #101 MS35207-266 SCREW, MACH, PAN HEAD, CROSS 50 REC, CARBON STL, CADMIUM PLD 15.1 #102 GANIOW1032 NUT 100 15.1 #103 NAS1149D0316H WASHER 100 15.1 #104 NAS1149F0363P WASHER. FLAT STEEL 100 For detail description of the work complied with sec the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). GAC_RevenueSquawksInvoice.rpt v3 Page 26 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811166
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Bill To: Plan D, LLC. Pans: Ref. No. Pan number: WO #: SC521661 Description Invoice Number: 5517132452 Quantity 15.1 4105 NAS1149F0332P WASHER. FLAT STEEL 100 15.1 4106 GAS805K3 SPLICE 30 15.1 #107 GAC860N08 CAP D300-08 30 15.1 #108 GAC860N12 CAP 30 15.1 #109 GAC860N18 CAP, SPLICE 30 15.1 #110 VS-08-RJ45-5-(//1P20 CONNECTOR, RJ45 (GRAY) 15 15.14/111 M81969-1-01 INSERT/EXTRACT GREENAYHITE 8 METAL 15.1 #112 91066-4 EXTRACTOR TOOL 8 15.1#113 M81969-14-0I EXTRACTOR, GREENPNHITE 12 PLASTIC 15.1 #114 M81969/14-10 TOOL, ORANGE/RED INSERTION 15 AND EXTRACTION 15.1 #115 M15570-22-I TOOL 15 15.1 #116 hIS27039C1-12 SCREW. PAN HEAD, X RECESSED 4 15.1#117 294-541 EXTRACTOR, AMOHENOL I 15.1 WI III GARI00B2B0063 RUBBER .063 SHEET 5 15.1 #119 1159AV33022-5 CIRCUIT BREAKERASSEMBLY 1 (ESDS MATERIAL) 15.1 #120 58T-101 EATON EXTRACTION TOOL 1 15.1 #121 43031-0009 PIN 15 15.1 #122 90401566 KA-BAND AIRCRAFT NETWORK I DATA UNIT (KANDU) 15.1.5#1 GC524980001-121 BRACKET ASSEMBLY 2 15.1.5 #2 14524694555 SCREW, 100 DEGREE CSK 30 STRUCTURAL 15.1.5 43 M527039-I-04 SCREW, PAN HEAD MACHINE 30 15.1.5 44 GSM805001267-10 I ANGLE 2 15.1.5 45 GSM806002351-101 BRACKET 2 15.1.5 46 CB200-40 ADHESIVE, ACRYLIC (DUAL PACK 3 CARTRIDGE) PLUNGER PLA050-10 40 ML 15.1.5 47 021200-50009 NOZZLE, STATIC MLXER, SHORT 100 GOLD NOZZLE FOR 1.5OZ 15.1.5 48 CCS1005-09-48.00 ANGLE 1 15.1.5 49 CCS1005-33-48.00 ANGLE 1 15.1.5 410 NAS1836-06-10 INSERT 20 15.1.5 411 MS35206-226 SCREW 20 15.1.5 412 TC141 BRACKET, TIE -DOWN 20 15.1.5 413 MS21266-7T GROMMET, PLASTIC, EDGING 2 15.1.5 414 M53339-4-9 PLATE MOUNTING 5 15.1.5 415 NIS20470A4-5N RED RIVET 25 15.1.5 416 NASI149DN832J WASHER 25 15.1.5 417 GAB51IGA3-4 BOLT 100 15.1.5 418 GAB51IGA3-6 BOLT 100 15.1.5 419 GAB51IGA3-7 HI-BOLT 100 Services: Ref. No. Description Quantity 15.1.1 41 REF.. M. Eddy, 15.1.1, 3.0 hrs, 11/27 -12103/2017 1.00 15.1.1 42 REF.. Eddy. 15.1.1, 3 HRS, 11/27 - 12/03 1.00 15.1.2 41 AETS. Molnar. .15.1.2, 1.0 hrs, 1)22 -112812018 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_RevenueSquawksInvoice.rpt v3 Page 27 of 64 Printed: 3/712018 3:15:05PM tit W. EFTA00811167
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Step: 15.1.1 Waiting approval Avionics Engineering Labor Avionics (L/P/S) Step: 15.1.2 Waiting approval Mech Engr Labor Avionics (L/P/S) Step: 15.13 Waiting approval AVI Systems Test Labor Only (L/P/S) Step: 15.1.4 Waiting approval AVI /Electrical Labor Only (L/P/S) Step: 15.1.5 Waiting approval AVI Sheet Metal Labor Only (L/P/S) Step: 15.1.5.1 Completed Lightly scuff sanded 5" area around routed area. then cleaned area with cheese cloth and isopropyl alcohol. Cut and impregnated 3 plies of 120 style fiberglass cloth with 828 resin. Applied impregnated fiberglass on routed area and vacuum bagged and 24 inches of mercury. Let dwell for 1 hour and heat cured at 140 for 4 hours. After cure sanded excess resin smooth to blend new plies into original contour. Reference engineers dispo ## 15.8.1.1 Step: 15.1.6 Completed INT Support (R&R) Labor Only Step: 15.1.7 Waiting approval SC Ntaintenancefflangar / Primary Codes /Touch Labor Only (L/P/S) Step: 15.1.8 Waiting approval SC Paint Labor Only (L/P/S) Step: 15.1.9 Waiting approval Inspection Labor Only (L/P/S) Step: 15.1.10 Waiting approval Weight and Balance Labor Only (L/P/S) Item: 16 KA BAND HARNESS FABRICATION Team Manager: Customer Coordinator: Charles Thomas Julian Brown Part/Model 8: AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Item: 17 ASC 085A X61 Weather Installation - (Ref. Item B 2.3 of Proposal ID# 7038248 R02) Team Manager: Charles Thomas Customer Coordinator: Julian Brown Pan/Model ft: AC Serial No/Tail No.: TSN/TSO: CSNJCSO: 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_RevenueSquawksinvoice.rpt v3 Page 28 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811168
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Bill To: Plan D, LLC. WO #: SC52166I Invoice Number: 5517132452 Discrepancy: 17.1 ASC 085A XN1 Weather Installation This Service Change installs an antenna, receiver, two (2) data ports and associated wiring for the XM satellite weather system. Either a fore or an aft installation may be selected based on aircraft configuration. Aircraft that are provisioned for XM installation may require an engineering review to complete the installation. Provisions may include wiring, antenna, receiver, data ports or any combination of these components and are typically installed during completion. Prerequisites: ASC 908 - PlaneView Master Operating Software System Software Update (Cert Fox) Prior to. or at the time this ASC is ordered, operators will be required to supply a configuration report of the Central Maintenance Computer (CMC). The CMC report can be stored on the aircraft PC laptop then electronically submitted to Culfstream at asc.softwareCrgulfstream.com. Allow three (3) to five (5) days for the CMC report review and up to twenty-one (21) days for the creation of a new Options Data disk. Effectivity: This Service Change is applicable to aircraft Serial Numbers 5001 - subsequent. Notes: Interior access to perform this installation is not included in the kit price. Aircraft configuration. installation location of the system and availability of spare wiring may impact labor hours, amount of access required and could necessitate additional engineering. This ASC is a managed program. Incorporation must be coordinated through Culfstream Aircraft Scheduling at 800-810-GULF (4853) or 912-965-4178. If not scheduled, aircraft downtime could increase significantly. This Service Change may only be installed at a Culfstream Aerospace facility. Resolution: Complied with ASC 085A XM Weather Installation Ref Item 17.2 CN1P 970851 Billing Method Hours Rate Total Labor USD: Flat Rate $16,060.00 Pans USD: Flat Rate 563,940.00 Total USD: 480,000.00 Parts: Ref. No. Pan number: Description Quantity 17.1 #1 A.SC0S5A-1 GSSP KIT, XM SATELLITE WEATHER I INSTALLATION, 5001-SUB(KIT ONLY) 17.182 RGI42Bill COAX 35 17.1#3 HET-A-02C FERRULE, SHIELD 6 17.1 #4 PLC1.51-58 TYRAP 10 17.1 #5 BTS722 RCPT, RFTNC I 17.1 #6 CTS722 CONNECTOR 1 17.1 #8 M24308/4-IF CONNECTOR I 17.189 GAC835MR20S CONTACT 10 17.1#10 CSS722 PLUG, ShIA, STRAIGHT 1 17.1 #11 CSR722 PLUG, SMA,90° I 17.1 #12 CTS722 CONNECTOR I 17.1 #13 NIS21919WDG2 CLAMP 4 17.1 #14 NIS21919WDG4 CLAMP PTYPE-CUSHIONED,IM IN 4 17.1#15 NIS21919WDG3 CLAMP PTYPE-CUSHIONED,3116 4 INCH 17.1 #16 DCR-IA-05 RAIL I 17.1 #18 GAN IOW 1032 NUT 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_RevenueSquawksInvoice.rpt v3 Page 29 of 64 Printed: 3/7/2018 3:15:05PM tit kW EFTA00811169
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Bill To: Plan D, LW. Pans: Ref. No. Part number: WO #: SC521661 Description Invoice Number: 5517132452 Quantity 17.1 819 GATIIF-BR3-I0A TERMINAL INSTALL, ELEC 2 GROUNDING AND BONDING 17.1821 ABI4-SA LUG,TERMINAL-ELEC 5 17.1822 GATIIF-BR3-I0A TERMINAL INSTALL, ELEC 4 GROUNDING AND BONDING 17.1 823 A10086 TIE-DEX BAND 10 17.1824 AS21919WDG08 CLAMP. LOOP 8 17.1 825 NASI802-3-14P SCREW (AP) 2 17.1826 NASI802-3-8P SCREW 3 17.1 #27 58T-101 EATON EXTRACTION T(Xli. 1 Item: 18 ASC 912 and ASC 123 Planeview MOS Upgrade - (Ref. Item B 2.4 of Proposal ID# 7038248 R02) Team Manager: Customer Coordinator: Charles Thomas Julian Brown ParttModcl #: AC Serial No/Tail No.: TSWISO: CSN/CSO: Aircraft Time: Discrepancy: 18.1 ASC 912 and ASC 123 Planeview MOS Upgrade ASC 912: This Service Change (ASC 912) installs the Planeview Master Operating System (MOS) software Media Part Number (PN) MM7031235-024. ASC 123: This Service Change (ASC 123) loads a combination of new and existing software based on current aircraft configuration. Prerequisites: Submit an APN1 Settings & Riggings form ASC 910 - Planeview MOS Software Update or later; or production equivalent is the minimum cert level required. Prior to. or at the time this ASC is ordered, operators will be required to supply a configuration report of the Central Maintenance Computer (CMC). The CMC report can be stored on the aircraft PC laptop then electronically submitted to C airstream at asc.software(it gulfstream.com. Operators utilizing Custom Electronic Checklist (ECL) must order new software. Prior to. or at the time this ASC is ordered, software may be ordered from the Custom ECL page on NlyCulfstream.com Concurrent Requirements: ASC 912 and ASC 123 are complied with in conjunction. Effectivity: This Service Change is applicable to aircraft Serial Numbers 5001 - 5549. This, or a similar change. will be installed during initial phase manufacturing on aircraft Serial Numbers 5550 and subsequent. Notes: Aircraft that do not meet the prerequisite minimum level for modification may utilize drawing 11595857083 to meet the requirements of ASC 107 and ASC 910. This drawing may only be used concurrently with ASC 123 and ASC 912. Aircraft utilizing drawing 1159SB57083 to meet the prerequisite minimum requirements of ASC 107 and AM' 910 are part of a managed program conducted by Product Support Program Management (PSPM). Resolution: COMPLIED WITH ASC 912 and ASC 123 Planeview MOS Upgrade Billing Method Flours Rate Total Labor USD: Flat Rate 53,306.00 Parts USD: No Charge N/ C Total USD: 53,306.00 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_RevenueSquawksInvoice.rpt v3 Page 30 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811170
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Bill To: Plan D, LLC. Pans: WO #: SC521661 Invoice Number: 5517132452 Ref. No. Pan number: Description Quantity Sell price USD Extended USD 18.1 81 ASC912-I GSSP 18.1 82 ASC123-I GSSP KIT, INDICATING/ RECORDING 1 $0.00 $0.00 PLANEVIEW MOS UPDATE, 5001-5549 KIT, INDICATING/RECORDING 1 $0.00 $0.00 PLANEV1EW AVIONICS ENHANCEMENTS. 5001-5549 Item: 19 Reveneer Woodwork - (Ref. Item A 1.1 of Proposal ID# 7039407 ROO) Team Manager: Charles Thomas Part/Model 8: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNffSO: CSN/CSO: Aircraft Time: Discrepancy: 19.1 Reveneer Woodwork The existing veneer covered components will be removed from the aircraft and stripped of all veneer surfaces, hardwood caps. and nosing. All substrate will be cleaned and prepped for application of new selected veneer with corresponding hardwood caps and nosing. Modifications or repairs to any substrate material or structural hardware will be evaluated and addressed on a time and material basis. All the existing latches will be cleaned and retained. New hardware. if requested. will be addressed on a time and materials basis. New Customer Selected Veneer will be applied to the existing substrates. The new veneer will be finished with Gulfstreant standard III-BIL clear coat finish and polished to a predetermined luster. All applicable internal surfaces will be cleaned and retained in existing condition. Painting or recovering of the internal surfaces will he addressed on a time and materials basis. Inlays of any type such as wood. metal. or stone inlays are not included in this proposal. Existing inlays will be evaluated on a case-by-case basis and addressed on a time and materials basis. Burn certification is predicated upon the existing substrates meeting all the FAA flammability requirements. Gu[(stream is not responsible for any existing materials meeting burn requirements. The recovered doors, panels, and cabinetry will be reassembled and installed in aircraft. All adjustments will be made to ensure correct fit and function. Equipment relocation is not part of this proposal and will be addressed on a time and materials basis. ***SEE APPENDIX FOR ADDITIONAL INFO*" Resolution: Ref steps 19.2 thru 19.23, For details of veneer covered components that were removed from the aircraft and stripped of all veneer surfaces, hardwood caps, and nosing. Reveneered and new hardwood caps and nosings were completed with customer approved materials. Ref R&I for details of reinstallation REF 19.24 and 19.30 for Veneer & Hardwood Flammability Notes: Staining or Tinting Finish to achieve a specific color or grain pattern is not included in this proposal. Any finish other than natural will be evaluated and addressed on a time and materials basis. This proposal includes Natural Wood Veneer. Composite Veneer (due to ordering limitations) may require Gulfstream to purchase additional sheets of that product. Should additional sheets will be required: the Customer will be advised of the additional charges. Sharp radiuses on ledges and other cabinetry that are covered with veneer will require additional labor charges and will be accomplished on a time and materials basis. Proposal is based on reusing all applicable substrate and componentry. All plating will be accomplished on a time and materials basis. Billing Method Hours Rate Total Labor USD: Flat Rate Parts USD: Flat Rate 5169.036.00 $68.984.00 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_RevenueSquawksInvoice.rpt v3 Page 31 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811171
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 &niers USD: Total USD: Pans: Ref. No. Flat Rate Part number: Description 5470,155.00 5706,175.00 Quantity 19.1 #1 M520-01437 STAIN, RAW UMBER PENETRATING 2 19.1 #2 M520-2247 MOHAWK BLACK ULTRA 2 PENETRATING STAIN 19.1 #3 M520-00017 REDUCER, ULTRA PENETRATING 2 STAIN, GALLON 19.1 #4 P63563A LEX EDGE OUTDOR SOYD. 1 19.1 45 P77709A INTENSE RED (FOIL) 1 19.1 #6 P77685A 91M FX BLACK SPOT FOIL GERBER 1 EDGE GSP 19.1 #7 P77753A PLACARD, RUBY RED GERBER I FOIL 19.1 kt1 T1310-14 TRANSFER RITE 1310 UTRACLEAR 1 TAPE 14" x 100 VD 19.1 #9 GSE150717-1LP QTR FIG DARK EUCALYPTUS 1,139 19.1 #10 P65580A GERBER 1MAGECAST, CLEAR, IS 50 IN/38CM-P 19.1 #11 1357 NEUTRAL 5GAL ADHESIVE CEMENT, 5GAL, I GAA100AU1 19.1 #12 923450GL CLEARCOAT, MULTI-TEMP BAKING 26 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #13 929-91-3.5L HARDENER,GLASURIT FINISH 15 19.1 #14 352-91 GAL REDUCER 15 19.1 #15 8-4QTR-SAWN-MOZAMBK HARD WOOD QTR SAWN 150 MOZAMBIQUE 19.1 #20 MS2469456 SCREW 3 19.1 #21 NIS24694S6 SCREW 15 19.1 #22 hIS35206-226 SCREW 50 19.1423 222S PAINT-MID-COAT ADHESION 2 PROMOTER 19.1 #24 NAS1149FN832P WASHER, FLAT STEEL 100 19.1425 GSE150717-1LP QTR FIG DARK EUCALYPTUS 126 19.1 #26 DMA50 DISPENSING GUN KIT FOR 50hIL 1 EPDXY CARTRIDGES 19.1427 hIEGM10001 PRO SPEED COMPOUND 5 19.1 #28 P65580A GERBER IMAGECAST, CLEAR, IS 50 IN/38CM-P 19.1 #29 1357 NEUTRAL 5GAL ADHESIVE CEMENT, SGAL, 1 GAA100AU1 19.1 430 923450GL CLEARCOAT, MULTI-TEMP BAKING 6 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1432 923450GL CLEARCOAT, MULTI-TEMP BAKING 4 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #33 923450GL CLEARCOAT, MULTI-TEMP BAKING 6 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #34 929-93 GLASURIT HARDNER (35 LITER) 3 19.1#35 929-91-3.5L HARDENER,GLASURIT FINISH 2 19.1 #36 P77788A WHITE (FOIL! I 19.1 #37 DPIOOFR EPDXY ADHESIVE, 1.7 OZ 2 19.1 #38 CA40 ADHESIVE I OZ 2 19.1#39 PRONTO SURFACE ACTIVATOR 3 19.1 #45 923460GL CLEARCOAT, MULTI-TEMP BAKING I URETHANE ACRYLIC, GLASURIT (35 LITER) 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_RevenueSquawksInvoice.rpt v3 Page 32 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811172
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Bill To: Plan D, LLC. Pans: Ref. No. Pan number: WO #: SC521661 Invoice Number: 5517132452 Description Quantity 19.1 #47 437-2263 PRIMER, IN WC EXTUFF (5 GAL PAIL) 19.1 #46 923-4S0GL CLEARCOAT, MULTI-TEMP BAKING 6 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #48 923-45061 CLEARCOAT, MULTI-TEMP BAKING URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #49 923-450GL CLEARCOAT, MULTI-TEMP BAKING URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #50 923-450GL CLEARCOAT, MULTI-TEMP BAKING URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1#51 923-450GL CLEARCOAT, MULTI-TEMP BAKING URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #52 923-450 ;L CLEARCOAT, MULTI-TEMP BAKING 4 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1#53 929-91-3.51 HARDENER,GLASURIT FINISH 1 19.1 #54 929-91-3.51 HARDENER, GLASURIT FINISH 1 19.1 #55 929-91-3.51 HARDENER,GLASURIT FINISH 2 19.1 #56 832J16-2IBR INSERT 12 19.1 #57 400 EVERCOAT EVERCOAT FILLER 1 19.1 #58 GMS5005-I QT EPDXY PRIMER COATING (TYPE I) 3012 QUART KIT (44GN011 QK) 19.1 #59 282.01.701 SUPPORT, SHELF 20 19.1#611 PRONTO SURFACE ACTIVATOR 2 19.1 #63 923450GL CLEARCOAT, MULTI-TEMP BAKING 10 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #64 DMD1684/GL PAINT, DELTRON BASECOAT WHITE 19.1 #65 DMD1683IGL PAINT, DELTRON BASECOAT BLACK 19.1 #66 CA8000KICKER QT PAINT KICKER 2 19.1 #67 929-91-3.51 HARDENER, GLASURIT FINISH 1 19.1 #68 929-91-3.51 HARDENER, GLASURIT FINISH 1 19.1 #69 929-91-3.51 HARDENER, GLASURIT FINISH 6 19.1 #70 522-10 ACCELERATOR, DRYING ADDITIVE 19.1 #71 522-10 ACCELERATOR, DRYING ADDITIVE 4 19.1 #72 352-91 GAL REDUCER 6 19.1 #73 GMS5005-I QT EPDXY PRIMER COATING (TYPE I) 2 3012 QUART KIT (44GN011 QK) 19.1 #74 hIEGNI10001 PRO SPEED COMPOUND 4 19.1 #75 M524693-C26 SCREW, MACHINE, FLAT 12 COUNTERSUNK HD. 100 DEG. CROSS RECESS 19.1 #76 MS24694-53 SCREW, MACHINE, FLAT CTSK HD, 8 100 DEG, STRL, CROSS RECESSED 19.1 #77 22001-15 ISOLATOR 2 19.1 #78 MS27039-1-6 SCREW 143 19.1 #79 MS27039-1-09 SCREW, MACHINE PAN HEAD 150 STRUCTURAL 19.1 #80 NAS1149F0332P WASHER. FLAT STEEL 100 19.1 #81 NAS6603-7 BOLT-HEX HEAD, CLOSE 25 TOLERANCE 19.1 #82 AN970-3 WASHER. FLAT 50 19.1 #83 M527039-1-06 SCREW-MACHINE,PAN HEAD 7 19.1 #84 1032J19-24 B/R INSERT. THREADED 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_RevenueSquawkslnvoice.rpt v3 Page 33 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811173
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Bill To: Plan D, LLC. Pans: Ref. No. Part number: WO #: SC521661 Description Invoice Number: 5517132452 Quantity 19.1 #ss NAS6603-6 BOLT, HEX HEAD, CLOSE 24 TOLERANCE 19.1 #86 CA40 ADHESIVE I OZ 2 19.1 #87 PRONTO SURFACE ACTIVATOR 2 19.1 #88 GAPIO5A15C KYDEX 100(#62015) IVORY-.060 I 19.1 #89 151.01.710 FLUSH HANDLE I 19.1 #90 NAS1149D0332K WASHER. FLAT ANODIZED 8 ALUMINUM 19.1 #91 NAS1149D0363H WASHER 8 19.1 #92 1159F57355-3 BRACKET AS.SY 1 19.1 #94 GAG8106H3 GASKET, U.S. 100% INSPECTED 10 19.1 #95 GAG8106H3 GASKET, U.S. 100% INSPECTED 10 19.1 #96 MS24693-530 SCREW, MACHINE, FLAT 10 COUNTERSUNK HD, 100 DEG, CROSS RECESS 19.1 #97 MS24693-532 SCREW, COUNTERSINK-I00 10 DEGREE 19.1 #98 MS24665-300 COTTER PIN 4 19.1 #99 NAS1580C3T17 BOLT 2 19.1.5 #2 NAS1611-015A 0 -RING 8 19.1.5 #3 NASM24665-I53 COTTER PIN 4 19.1.5#4 NAS1611-013A 0 -RING ' 19.1.5 #8 DPIOOFR EPDXY ADHESIVE, 1.7 OZ 1 19.1.5#9 DPIOOFR EPDXY ADHESIVE, 1.7 DZ 1 19.1.5 #10 DPIOOFR EPDXY ADHESIVE, 1.7 OZ 1 19.1.5 #11 DPIOOFR EPDXY ADHESIVE, 1.7 OZ 1 19.1.5 #12 DPIOOFR EPDXY ADHESIVE, 1.7 OZ 1 19.1.5 #13 DPIOOFR EPDXY ADHESIVE, 1.7 OZ 1 19.1.5 #14 DPIOOFR EPDXY ADHESIVE, 1.7 OZ 1 19.1.5 #15 DPIOOFR EPDXY ADHESIVE, 1.7 OZ 1 19.1.5 #16 DPIOOFR EPDXY ADHESIVE, 1.7 OZ 1 19.1.5 #17 DPIOOFR EPDXY ADHESIVE, 1.7 OZ I 19.1.8.6 #1 M52469456 SCREW 2 19.1.8.6 #2 M52469456 SCREW IS Services: Ref. No. Description Quantity 19.1 #1 Vendor Supplied Labor 1.00 19.13 #1 Vendor Supplied Labor SAPS 1.00 19.1.4 #1 Vendor Supplied Labor 1.00 19.1.4 #2 Vendor Supplied Labor 1.00 19.1.4 #3 Vendor Supplied Labor 1.00 19.1.4 #4 Vendor Supplied Labor 1.00 19.1.4 #5 Vendor Supplied Labor 1.00 19.1.4 #6 Vendor Supplied Labor 1.00 19.1.4 #7 Vendor Supplied Labor 1.00 19.1.4 #8 Vendor Supplied Labor 1.00 19.1.4 #9 Vendor Supplied Labor 1.00 19.1.4 #11 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_RevenueSquawksInvoice.rpt v3 Page 34 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811174
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Bill To: Plan D, LLC. WO it: SC521661 Invoice Number: 5517132452 Step: 19.1.1 Completed AV1 /Electrical Labor Only Step: 19.1.2 Completed INT Sheet Metal Labor Only Step: 19.13 Completed Wood Labor Only (270 ) Deducted 270 hours from the original 1897 hours for vendor supplied labor (SAPS) Step: 19.1.4 Completed INT Finish and Paint Labor Only Total Hours 1186 Outside Labor for 11/27 to 12/6 197 hrs Outside Labor for 12/4 to 12/10 208 hrs Outside Labor for 12/11 to 12/17 58 hrs Outside Labor for 12118 to 12124 40 hrs Outside Labor for 1/2 to 1/7 90 hrs Outside Labor for 1/8 to 1/14 180 hrs Outside Labor for 1/15 to 1/21 120hrs Outside Labor for 1122 to 1/28 180hrs Outside Labor for1/29 to 214 60 hrs Outside Labor for2/5 to VII 50 hrs Step: 19.1.5 Completed NT Support (R&R) Labor Only Step: 19.1.5.1 Completed ****VOID**** Entere din wrong section Removed all old sealant from the outboard edges of the MED entn way fwd and aft bulkhead veneer pieces per .A3134 G550 20-4240 March 31/17. The edges are taped and are ready to be scaled. Step: 19.1.5.2 Completed *****VOID*** ENT in wrong section ref Applied PR 1440 BI/2 sealant to M.E.D. aft bulkhead veneer closeout at 01:00 on 3/1/2018 per 6550 AMM 20-42-00 March 31/17. Step: 19.1.6 Completed Inspection Labor Only Step: 19.1.7 Completed Flammability t Placards Labor Only Step: 19.1.8 Completed Wood Shop Labor to Strip Existing Veneer. Step: 19.1.8.1 Completed Strip Veneer - RH and LH 680 Bulkheads and Door. Step: 19.1.8.2 Completed Strip Veneer -AFT LAN' Niche and Shroud. Step: 19.1.8.3 Completed Strip Veneer -AFT Lay Vanity Step: 19.1.8.4 Completed Strip Veneer -AFT LH Closet. Step: 19.1.8.5 Completed Strip Veneer -AFT RH Closet. Step: 19.1.8.6 Completed Strip Veneer -AFT LH Galley. Step: 19.1.8.7 Completed Strip Veneer -AFT RH Galley Annex. Step: 19.1.8.8 Completed Strip Veneer - 4 Divan End Cabinets. Step: 19.1.8.9 Completed Strip Veneer -Cabin Ledges. Step: 19.1.8.10 Completed Strip Veneer - Console Tables. Step: 19.1.8.11 Completed Strip Veneer- FWD Pocket Door. Step: 19.1.8.12 Completed Strip Veneer - FWD RH and 1.11 Cabin Bulkheads. Step: 19.1.8.13 Completed Strip Veneer - PSU Handrails. Step: 19.1.8.14 Completed Strip Veneer - FWD Crew Refresh Cabinet. Step: 19.1.8.15 Completed Strip Veneer - FWD RH Lay. Step: 19.1.8.16 Completed Strip Veneer - REER and LEER panels. Step: 19.1.8.17 Completed Strip Veneer -Acoustic Door. Step: 19.1.8.18 Completed Strip Veneer - Entry Panels (2) Step: 19.1.8.19 Completed Strip Veneer - AFT LAV Door. Step: 19.1.8.20 Completed Strip Veneer - FWD Lav Door. Step: 19.1.8.21 Completed Strip Veneer - Magazine Racks. Step: 19.1.9 Completed Wood Shop Labor to Reveneer Cabinets. Step: 19.1.9.1 Completed Labor to Veneer -1.11 and RH 680 Bulkheads and Door. Step: 19.1.9.2 Completed Labor to Veneer - AFT LAV Niche and Shroud. Step: 19.1.9.3 Completed Labor to Veneer -AFT Lay Vanity. Step: 19.1.9.4 Completed Labor to Veneer -AFT LH Closet. Step: 19.1.9.5 Completed Labor to Veneer -AFT RH Closet. Step: 19.1.9.6 Completed Labor to Veneer -AFT LH Galley. Step: 19.1.9.7 Completed Labor to Veneer -AFT RH GalleyAnnex. Step: 19.1.9.8 Completed Labor to Veneer - 4 Divan End Cabinets. Step: 19.1.9.9 Completed Labor to Veneer -Cabin Ledges. 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_RevenueSquawksInvoice.rpt v3 Page 35 of 64 Printed: 3/7/2018 3:15:05PM tit W. EFTA00811175
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Completed Labor to Veneer - FWD Pocket Door. Completed Labor to Veneer - FWD LH and RH Bulkheads. Completed Labor to Veneer - PSU Hand Rails. Completed Labor to Veneer - FWD Crew Refresh Cabinet. Completed Labor to Veneer - FWD RH Lay. Completed Labor to Veneer - LEER and Reer Panels. Completed Labor to Veneer - Acoustic Doors. Completed Labor to Veneer - Entry Bulkheads (2) Completed Labor to Veneer -AFT Lav Door. Completed Labor to Veneer - FWD Lay Door. Completed Labor to Veneer - Console Tables. Completed 1.abor to Veneer - Magazine Racks. Completed Wood Shop Labor to Assemble Cabinets. Completed Labor to Assemble - LH and RH 680 Bulkheads and Door. Completed 1.abor to Assemble -AFT Lay Niche and Shroud. Completed Labor to Assemble - AFT Lay Vanity. Completed Labor to Assemble -AFT LH Closet. Completed 1.abor to Assemble - AFT RH Closet. Completed Labor to Assemble - AFT LH Galley. Completed Labor to Assemble - AFT RH Galley Annex. Completed 1.abor to Assemble - 4 Divan End Cabinets. Completed Labor to Assemble - Cabin Ledges. Completed 1.abor to Assemble - Console tables. Completed 1.abor to Assemble - FWD Pocket Door. Completed 1.abor to Assemble - FWD LH and RH Cabin Bulkheads. Completed Labor to Assemble - FWD Crew Refresh Cabinet. Completed Labor to Assemble - FWD RH Lim Completed Labor to Assemble - Leer and Reer Panels. Completed Labor to Assemble - Acoustic Doors. Completed Labor to Assemble - AFT Lay Door. Completed Labor to Assemble - FWD Lay Door. Completed ***Entered in Error******* Flammability Data. Completed Removal/Install of R/H #1 and R/H #2 E-windows required for access for interior installation. As per 6550 AMM 52-22-00 Rev Nov 15/17. Step: 19.1.9.10 Step: 19.1.9.11 Step: 19.1.9.12 Step: 19.1.9.13 Step: 19.1.9.14 Step: 19.1.9.15 Step: 19.1.9.16 Step: 19.1.9.17 Step: 19.1.9.18 Step: 19.1.9.19 Step: 19.1.9.20 Step: 19.1.9.21 Step: 19.1.10 Step: 19.1.10.1 Step: 19.1.10.2 Step: 19.1.10.3 Step: 19.1.10.4 Step: 19.1.10.5 Step: 19.1.10.6 Step: 19.1.10.7 Step: 19.1.10.8 Step: 19.1.10.9 Step: 19.1.10.10 Step: 19.1.10.11 Step: 19.1.10.12 Step: 19.1.10.13 Step: 19.1.10.14 Step: 19.1.10.15 Step: 19.1.10.16 Step: 19.1.10.17 Step: 19.1.10.18 Step: 19.1.11 Step: 19.1.12 Step: 19.1.12.1 Step: 19.1.12.2 Step: 19.1.12.3 Step: 19.1.12.4 Step: 19.1.12.5 Step: 19.1.12.6 Step: 19.1.13 R/H #1 P/N 1159SCCE500-23 S/N 0702030 R/H #2 P/N 1159SCCE500-23 S/N 0701885 Completed Removed FUH #1 and R/H #2 E-windows for access for interior installation. As per 6550 .AMM 52-22-00 Rev Noy 15/17. FUN #1 P/N II 59SCCE500-23 S/N 0702030 FUN #2 P/N 1159SCCE500-23 S/N 0701885 Completed Install of R/H #1 and Rill #2 E-windows for access for interior installation. As per G550 AMM 52-22-00 Rev Nov 15/17. Ref.11.141. 11.142 Rill #1 P/N 1159SCCE500-23 S/N 0702030 RAF #2 P/N 1159SCCE500-23 SIN 0701885 Completed CMP G550 562115 Cabin Windows- Leak Check Ref.11.143 Completed CMP G550 560001 Emergency Window Release Mechanism - Functional Test Ref.11.144 Completed CMP 6550 304110 CABIN WINDOW HEAT - 0PS TEST Ref.11.145 Completed E-window #2 is out of limits on emergency window release mechanism - fuctional test. inside pull is at 42. and outside pull is at 65. Completed Summary: Removed all old sealant from the outboard edges of the MED entry way fwd and aft bulkhead veneer pieces per AMM G550 20-42-00 March 31/17. The edges are taped and are ready to be scaled. see sub-steps below 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_RevenueSquawksinvoicc.rpt v3 Page 36 of 64 Printed: 3/7/2018 3:15:05PM tit W. EFTA00811176
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Bill To: Plan D, LLC. WO SC521661 Invoice Number: 5517132452 Step: 19.1.13.1 Completed Applied PR 1440 8112 sealant to M.E.D. aft bulkhead 'veneer closeout at 01:00 on 3/1/2018 per 6550 AMM 20-42-00 March 31/17. Step: 19.1.13.2 Completed Applied PR 1440 B1/2 sealant to M.E.D. fwd bulkhead veneer closeout at 4:30pm on 3/1/2018 per 6550 AMM 20-42-00 March 31/17. Step: 19.1.14 Completed Permanently install MED airstair upper handrail bolts where handrails attach to bulkheads (NA and aft). Item: 20 Registration Change Team Manager: Charles Thomas Customer Coordinator: Julian Brown Part/Model AC Serial No/Tail No.: TSNITSO: CSN/CSO: Aircraft Time: Discrepancy: 20.1 Comply with registration change as outlined in RSQCT-115 Rev. 12. Registration change to N2I2JE. Resolution: Complied with registration change as outlined in RSQCT-115 Rev. 12. Reference steps below and traveler paper copy index 013A for details of work performed. Billing Method Hours Rate Total Labor USD: Time and Material ST 37.64 @ $146.00 $5,495.44 Labor USD: Time and Material OT 4.46 ® $146.00 $651.16 Labor USD: Time and Material ST 4.63 @ $222.00 $1,027.86 Parts USD: Time and Material $31.80 Total USD: $7,206.26 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 20.181 CTS-S22/22 CONTACT 30 $0.51 $15.30 20.182 GAS805IC2 SPLICE 30 50.22 $6.60 20.1 83 GAC860K-2 END CAP-RED 30 $033 49.90 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_RevenueSquawksInvoice.rpt v3 Page 37 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811177
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Bill To: Plan D, LLC. WO St: SC521661 Invoice Number: 5517132452 Step: 20.1.1 Completed Customer requests that the Gulfstream (WA issue a replacement standard airworthiness certificate due to registration change. Provide to the ODA the following items: A. A copy of the workorder cover sheet with current hours and landings. B. Standard Airworthiness Certificate. FAA Form 8100-2. C. Certificate of Aircraft Registration. AC Form 8050-3. Step: 20.1.2 Completed Require a written original statement signed by the registered owner or certificate opreator to request a replacement airworthiness certificate. The request shall include the registration number. serial number. make and model of the aircraft as well as the reason for the request. Step: 20.1.3 Completed Review the aircraft records and inspect the aircraft to ensure the request is justified and the aircraft is eligible for the certification requested. Records review consists of verification that there are no open maintenance due actions or airworthiness directives. Aircraft inspection consists of a data plate and registration marking examination. with a visual review of the aircraft for obvious conditions impacting aircraft safety. Step: 20.1.4 Completed Verify current aircraft registration. reference 14 CFR 47: Hard copy Registration AC: form 8050-3 for new registration number or Assignment of Special Registration Number AC form 81)50-64 alnd hard copy of old Registration AC Form 8050-3 8050-3 or Dealer Registration AC Form K050-6. Step: 20.1.5 Completed Verify new registration number is installed on the aircraft. Ref: I4CFR 45.23, 45.25. 45.29 & 4533. Step: 20.1.6 Completed Verify aircraft ID plate installation. Ref: 14 CFR Part 45. Step: 20.1.7 Completed FAA form 8100-2 issued for new registration number by Gulfstream ODA. Step: 20.1.8 Completed If the customer defers Gulfstream ()DA issuance of a replacement airworthiness certificate. a Corridor squawk will be signed as deferred by the customer. Rref : 14 CFR 91.203 (a) (1) 1 Step: 20.1.9 Completed Re-strap/ Re-program transponders to new registration. (Transponders with Mode S) Step: 20.1.10 Completed Re-Strap/Re- program SEI.CAl. to new code if ownership changes. Step: 20.1.11 Completed Commission SATCOM for new ownership / or Re-Strap SDU for new registration number change. Step: 20.1.12 Completed Reconfigure Magnastar. Aircell. & Iridium systems. Step: 20.1.13 Completed Configure AFIS. New installation or registration number change. Re-strap via Laptop. Step: 20.1.14 Completed Install new registration number placards in cockpit. Step: 20.1.15 Completed Install(if new) SELCAL number in cockpit. Step: 20.1.16 Completed Change logo on Airshow / Cabinview. if ownership changes. Step: 20.1.17 Completed Re-strap or re-program ELT's (406MHZ) in aircraft ( As required to new registration and / or country code). Step: 20.1.18 Completed Reconfigure High Speed Data Units or BBML. Step: 20.1.19 Completed Reconfigure Display Controllers Tail number ISELCAL. Step: 20.1.20 Completed Verify proper registration of ELT's (406MHZ) ( if installed in life rafts). Step: 20.1.21 Completed Reconfigure the Enhanced Flight Identification Code to the current registration Step: 20.1.22 Completed ()plain a copy of the Export Certificate of Airworthiness. Foreign Airworthiness Certificates. all Foreign Registration Documents and archive with the workorder. Item: 21 12 Month CNIP Tasks (Exhibit 1)-(Ref. Item C 1.1 of Proposal ID4 7039702 ROO) Team Manager: Customer Coordinator: Charles Thomas Julian Brown Pan/Model 8: AC Serial No/Tail No.: TSN/TSO: CSNJCSO: Aircraft Time: Discrepancy: 21.1 Accomplish 12 Month CNIP Tasks (Exhibit 1) Notes: Correction of discrepancies is not included in the quoted price. Materials / Outside Services will be billed as required. Resolution: Complied with 12 Month CMP Tasks. See squawks below for details of all work accomplished. (Complied with all required tasks for a 12 months/1C check) 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). liAC_RevenueSquawksInvoice.rpt v3 Page 38 of 64 Printed: 3/7/2018 3:15:05PM tit kW EFTA00811178
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Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Labor USD: Flat Rate $9,298.00 Total USD: $9,298.00 Discrepancy: 21.32 CMP G550 312003 BATTERY, PILOT CLOCK Resolution: COMPLIED WITH CMP G550 312003 BATTERY, PILOT CLOCK Billing Method Hours Rate Total Pans USD: Time and Material $2.63 Total USD: $2.63 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 21.32 #1 MN9I00 BATTERY, LW SIZE N, DURACELL 1 $2.63 52.63 Discrepancy: 21.33 CMP G550 312004 BATTERY, COPILOT CLOCK Resolution: COMPLIED WITH CMP G550 312004 BATTERY, COPILOT CLOCK Billing Method Hours Rate Total Pans USD: Time and Material $2.63 Total USD: $2.63 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 2133 #1 MN9100 BATTERY, I.5V SIZE N. DURACELL 1 $2.63 52.63 Discrepancy: 21.65 CMP G550 381039 WATER STERILIZER Resolution: COMPLIED WITH CMP G550 381039 WATER STERILIZER Billing Method Hours Rate Total Labor USD: No Charge N/C Pans USD: Tittic and Material $40.50 Total USD: $40.50 Pans: Ref. No. Part number: Description Quantity Scll price USD I:mended l'til) 21.65 #1 02-190002-012 WATER FILTER 0 -RIM; 3 513.50 $40.50 Discrepancy: 21.67 CAW G550 382002 Water Sterilizer Filter - Removal I Installation Resolution: COMPLIED WITH CMP G550 382002 Water Sterilizer Filter - Removal / Installation Billing Method Hours Rate Total Labor USD: No Charge N/ C Parts USD: Time and Material $119.25 Total USD: $119.25 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 21.67 #1 06-133802-001 FILTER, WATER 1 $92.25 $92.25 21.67#2 02-190002-018 WATER FILTER 0 -RING 1 $13.50 $13.50 21.67 #3 02-190002-019 WATER SYSTEM 0 -RING, FILTER 1 $13.50 $13.50 SPACER 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_RevenueSquawksInvoice.rpt v3 Page 39 of 64 Printed: 3/7/2018 3:15:05PM tat W. EFTA00811179
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Bill To: Plan D, LLC.
WO #: SC521661
Invoice Number: 5517132452
Item: 22
Discrepancies related to 12 Month CMP Tasks (Exhibit 1) - (Ref. Item C 1.1 of Proposal ID# 7039702 ROO)
Team Manager:
Customer Coordinator:
Charles Thomas
Julian Brown
ParUModel #:
AC Serial No/Tail No.:
TSN/TSO:
CSN/CSO:
Aircraft Time:
Item: 23
Miscellaneous CUP Tasks (Exhibit 3) - (Ref. Item C 1.3 of Proposal ID# 7039702 ROO)
Team Manager:
Customer Coordinator:
Charles Thomas
Julian Brown
Pan/Model #:
AC Serial No/Tail No.:
TSN/TSO:
CSN/CSO:
Aircraft Time:
Discrepancy: 23.1
Accomplish Miscellaneous CMP Tasks (Exhibit 3)
Notes:
O Correction of discrepancies is not included in the quoted price.
O Materials / Outside Services will be billed as required.
Resolution:
Billing Method
flours
Rate
Total
Labor USD:
Flat Rate
$8,953.00
Total USD:
$8,953.00
Discrepancy: 23.12
CMP G550 282651 Main Fuel Boost Pump (Left) - Fuel Leak Check
Resolution: COMPLIED WITH CMP G550 282651 Main Fuel Boost Pump (Left) - Fuel Leak Check
TW 558064
Date Due 08/18
Billing Method
Hours
Rate
Total
Labor USD:
No Charge
N/ C
Pans USD:
Time and Material
51.88
Total USD:
$1.88
Pans:
Ref. No.
Pan number:
Description
Quantity
Sell price USD
Extended USD
23.12#1
NAS1612-3A
0 -RING. 0.188 INCH OD TUBING
4
50.47
41.88
Discrepancy: 23.17
CMP G550 323012 Landing Gear Emergency Extension Nitrogen Blow-down Bottle (Right) - (Hydrostatic)
Functional Test
Resolution: COMPLIED WITH CMP G550 323012 Landing Gear Emergency Extension Nitrogen Blow-down Bottle (Right) -
(Hydrostatic) Functional Test
Billing Method
Hours
Rate
Total
Labor USD:
No ('barge
N/ C
Pans USD:
Time and Material
$2.86
Total USD:
$2.86
Parts:
Ref. No.
Pan number:
Description
Quantity
Sell price USD
Extended USD
23.17#1
NAS1612-4A
SEAL, 0.250 INCH OD TUBING
2
5030
50.60
23.17 #2
2-212 E0540-80
SEAL-0 RING
2
$1.13
52.26
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).
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