by date← Dec 12, 2017·Dec 12, 2017 →

EFTA00811205

Dataset 9

December 12, 201763 pages23,789 words

https://www.justice.gov/epstein/files/DataSet%209/EFTA00811205.pdf

Extracted Text

PRELIMINARY INVOICE IlfSfreani t DVNAMIC• COMININV Part/Model G550 AC Serial No./Tail No.: 5173 / N415L111 500 Ciulfstream Rd. - Savannah. Georgia 31407 Mail Remittance To: Overnight Remittance To: Wim Remittance To: Ciulfstream Aerospace Corporation Gulfstream Aerospace Corporation (Box # 730349) Ciulfstream Aerospace Corporation do JP Morgan Chase Bank. NA JP Morgan Chase Bank. NA ATTN: Dallas National Wholesale Lockbox TXI-0029 Chicago, IL 60670 14800 Frye Road Account No. 10-15825 Ft. Wash, TX 76155 Fedwirc Routing No. (ABA) 021 000 021 S.W.I.F.T. CHASUS33 ACH Credit Routing No. (ABA)071 000 013 Invoice Number: 5517132452 Bill To: Plan D, LLC. Invoice Date: 12/12/2017 6100 Red Hook Quarters B3 Customer ID: BP502 St. Thomas. 00802 P.O. Number: Lindsay' Virgin Islands US) Repair Station: FAA CRS CR41221681 In Date: 10/23/2017 Out Date: 03/10/2018 Payment Type: CIA - Wire Payment Terms: Title: Plan D, LLC. INVOICE SUMMARY FOR WORK ORDER NUMBER: SC521661 Time & Materials Flat Rate Total Labor USD: $40,646.72 $684,739.00 5725,385.72 Parts USD: $59,045.30 $674,164.00 $733,209.30 Services USD: $2,384.17 $497,215.90 $499,600.07 Misc Charges USD: 425,000.00 425,000.00 Detail Subtotal USD: $77,076.19 $1,856,118.90 S1,933,195.09 Subtotal USD: $1,933,195.09 Funds on Deposit USD: $392,500.00 Total USD: $1,540,695.09 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page I of 63 Set kl• EFTA00811205 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Quotation ID: 7037536 Quote Number:GAC0717-7536-6550-5173-R00 Complete Exterior Strip And Paint, Photographic Documentation Quotation ID: 7038248 Quote Number:GAC0417-5199-6550-5173-R02 G550 Ka Band Installation Quotation ID: 7039407 Quote Number:GAC1017-9407-6550-5173-R00 Reveneer Woodwork Quotation ID: 7039702 Quotation ID: 7038565 Quote NumberGAC0917-8565-6550-5173-R00 Generic Avionics - Entertaimnent Aircraft 5173: Arrival 10.20.2017 - Departure 01.26.2018 Paint Dates: Induct 12/4/17 (to strip hangar) - Return to SC 12/24/17 Contract # if provided Corporate Care - Yes MSP - No MPP - Yes 4400-84746 HAPP - Yes 4400-82081 PlaneParts - No MedAire - No JSSI - No CASP - No ESP- Yes/No EASA - Yes/No Isle of Man Yes/No *Note to Expeditors - If Yes/ No are both present please contact SCC and/or relevant vendor to determine warranty coverage. Larry Visoski Plan D LLC. e: Ivjet@aol.com o: 561.328.7963 m: 917.868.6145 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 2 of 63 Set 01 EFTA00811206 Bill To: Plan D, LLC. WO SC521661 Invoice Number: 5517132452 Item: 1 Airframe Culfstream C550 Team Manager: Charles Thomas Pan/Model If: G550 Customer Coordinator: Julian Brown AC Serial No/Tail No.: 5173 / N415L111 TSNffSO: CSN/CSO: Aircraft Time: Discrepancy: 1.17 Consumables & Shop Supplies Resolution: For billing purposes only. Billing Method flours Rate Total Parts USD: Flat Rate 55,000.00 Total USD: 55.000.00 Discrepancy: 1.27 Sales Concession Resolution: Billing Method Hours Rate Total Misc Charges USD: Time and Material -525.000.00 Total USD: -525.000.00 Miscellaneous Charge: Ref. No. Miscellaneous Charge Amount USD 1.27 #1 Sales Concession -S25,000.00 Item: 2 ENGINE. BR700-710C4-11 Team Manager: Charles Thomas Pan/Model #: BR700-710C4-11 Customer Coordinator: Julian Brown S/N: 15449 TSNffSO: CSN/CSO: Aircraft Time: Item: 3 ENGINE BR700-710C4-11 Team Manager: Charles Thomas Part/Model 4: gR700-71004-11 Customer Coordinator: Julian Brown S/N: 15448 TSNffSO: CSN/CSO: Aircraft lime: Item: 5 Technical Bulletins (ASC, CB, SB, AD. ACB) Team Manager: Charles Thomas Part/Model #: Customer Coordinator Julian Brown AC Serial No/Tail No.: 5173 / IIANGARA TSNffSO: CSN/CSO: Aircraft Time: Discrepancy: 5.2 CMP 6550 970531 ASC 53A Communications Management Function ARINC Direct - Datalink Service Provider 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). Printed: 3/9/2018 4:29:22PM Page 3 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811207 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: COMPLIED WITH CMP G550 970531 ASC 53A Communications Management Function ARINC Direct - Datalink Service Provider. Gray Disk: PN OFF: N212JE OxAICIBD 28NOV2017 SN OFF: ASC065-123 PN ON: N2I2JE0NAICIBD 02MAR2018 SN ON: ASC053-065-123 Orange Disk: PN OFF: 69001791-505 SN OFF: GDC 04JUL2017 PN ON: 69003236-502 SN ON: ARINC DIRECT 25JAN2018 Billing Method Hours Rate Iotal Labor USD: Time and Material ST 4.00 O! $146.00 $584.00 Pans USD: Time and Material S1.500.00 Total USD: 52.084.00 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 5.2#1 ASC053A-1 G5SP KIT, COMMUNICATIONS 1 $1,500.00 $1,500.00 MANAGEMENT FUNCTION ARINC DIRECT, DATA LINK SERVICE PROVIDER, 5001-9999 Item: 6 Avionics Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNffSO: CSNJCSO: Aircraft Time: Discrepancy: 6.2 Customer request custom checklist be installed on DU. Please hold until receipt of the custom ACL. Resolution: Updated custom check list IAN' CMP G550 319020 Gulfstream, Electronic Checklist Software (Purple Disk) Ref. 11.150 PN OFF: GYPV0105173003L.ecl SN OFF: 5173 I6JAN2015 PN ON: GVPV0105173004LECL SN ON: 5173 0IMAR2018 Billing Method Hours Race Total Labor USD: Time and Material ST 1.00 (a $146.00 $146.00 Total USD: $146.00 Discrepancy: 63 Flight Guidance Panel backlighting does not illuminate for night ops. Confirm IIAAP Covered Item Resolution: Summary: Removed flight guidance panel (pn: 7021852-901 sn: 06030509) and replaced with repaired night guidance panel (pn: 7021852-901 sn: 08080720) and performed Autopilot operational check with no defects noted. All work done ref CMP G550 221002 item 11.10 and 6550 CMP 22100 item 11.8. See steps below for 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 4 of 63 Set 01 EFTA00811208 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Billing Method Hours Rate Total Labor USD: Time and Material ST 4.00 ® $146.00 $584.00 Pans USD: No Charge WC Total USD: $584.00 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 6.3 NI 7021852-901 CONTROLLER, GUIDANCE PANEL 1 $0.00 $0.00 Step: 6.3.1 Completed Removed flight guidance panel (pn: 7021852-901 sn: 06030509) and replaced with repaired flight guidance panel (pn: 7021852-901 sn: 08080720) with no defects noted. All work done per G550 CMP 221001. Ref item 11.8 for CMP R&I. Step: 63.2 Completed Performed Autopilot operational check with no defects noted. All work done ref CMP 6550 221002 item 11.10. Discrepancy: 6.4 DU #4 imp. Swapped with DU #3 and problem followed. Resolution: Removed defective DU and replaced with modified DU (pn: 7028140-905 sn: 09125363) and performed operational check with no defects noted. All work done per 6550 CMP 316024 and CMP 316030. Ref Items 11.7 and 11.9. Billing Method Hours Rate -foal Labor USD: Time and Material ST 3.51 ® $146.00 $512.46 Parts USD: No Charge N/ C Total USD: $512.46 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 6.4 NI 7028140-905 DISPLAY UNIT, FLAT PANEL 1 $0.00 $0.00 (DU-I3I0) Discrepancy: 6.5 Customer request to update RAAS settings. Resolution: Updated RAAS settings IANV CMP GSM 319025 Gulfstream. Setting 1Rigging Software (Grey Disk) Ref. 11.148 PN OFF: N212JE OxAIC1BD 28NOV2017 SN OFF: ASC065-123 PN ON: N212JE 0xAICIBD 02MAR2018 SN ON: ASC053-065-123 Billing Method Hours Rate Total Labor USD: Flat Rate $438.00 ServicesUSD: Flat Rate $762.00 Total USD: $1,200.00 Step: 6.5.1 Completed Created one Settings and Riggings per GER 5767 Discrepancy: 6.6 Customer requests to update the airshow 4000 aircraft photo with the new blue paint scheme and to add the company logo. Logo to be provided by the customer. Ref item 20.1.16 Resolution: Updated the airshow 4000 aircraft photo with the nen blue paint scheme and to add the compans logo. as requested by. customer. Ref. Item 20.1.16 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). Printed: 3/92018 4:29:22PM riAC_RevenueSquawksInvoice.rpt v3 Page 5 of 63 ere. EFTA00811209 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Billing Method Hours Rate Total Labor USD: Time and Material ST 1.50 @ $146.00 $219.00 Labor USD: Time and Material OT 0.75 @ $146.00 $109.50 Parts USD: Time and Material $3,894.00 Total USD: $4,222.50 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 6.6#I 925940-4794-1V2 AIRSHOW SOFTWARE I $3,894.00 $3,894.00 Discrepancy: 6.7 II/II wing static wicks MUM out of tolerance. Resolution: Replaced all 3 Rai wing static wicks pn: 2-16SC-I. Performed functional check with no defects. All maintenance performed using 6550 AMM 23-61-01 Oct 30/08. Megger CN: 557026 Date Due: 02/18 BIRO CN: 560572 Date Due: 02/18 Billing Method Hours Rate Total Pans USD Time and Material $168.75 Total USD: $168.75 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 6.7 NI 2-16SC-I DISCHARGER. STATIC WICK 3 $56.25 S168.75 Discrepancy: 6.8 Left Spoiler Position Transducer has a broken backshell. Resolution: Summary: Replaced Left Spoiler Position Transducer Backshell. Rang out wires with no defects noted. All maintenance performed using WDNI 6550 27-60-00 June 20/13. Performed LII Spoiler RVDT functional check with no defects noted. All maintenance performed using G550 AMM 27-65-00 Dated November 15/ 17. See steps below for more detail. Billing Method Hours Rate Total Labor USD: Time and Material ST 5.90 @ $146.00 S861.40 Parts USD: Time and Material $329.22 Total USD: 31,190.62 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 6.8 NI 447HW151X/.10902 BACKSHELL I $323.22 S323.22 6.8 #2 NI81969/14-01 INSERTION/EXTRACTION TOOL, 5 $1.20 $6.00 GREEN Step: 6.8.1 Completed Replaced Left Spoiler Position Transducer Backshell. Rang out wires with no defects noted. All maintenance performed using WDM (350 27-60-00 June 20/ 13. Step: 6.8.2 Completed Performed LH Spoiler RVDT functional check with no defects noted. All maintenance performed using (350 AMM 27-65-00 Dated Nosrather 15/ 17. Discrepancy: 6.9 Ops check knee panel camera for new radome installation Resolution: Performed operational check of top camera with no defects noted. All work done per CC515050250 Rev -. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.00 @ $146.00 S146.00 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 6 of 63 ut EFTA00811210 Bill To: Plan D, LLC. WO SC521661 Invoice Number: 5517132452 Total USD: $146.00 Item: 7 Interior Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNffSO: CSN/CSO: Aircraft lime: Discrepancy: 7.9 Galley Microwave retainer block cracked. Resolution: Replaced, cracked galley Microwave retainer block, with new GSNI344001014-101 STOP, per GPNI308001581-301 Rev A. Billing Method Hours Rate Total Parts USD: Time and Material $35.63 Total USD: $35.63 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 7.9#I GSM344001014-101 STOP 1 $35.63 $35.63 Discrepancy: 7.13 Grosspoint material behind LII #1 and RH PI table boxes needs to be resecured. Resolution: Resecured grosspoint behind table boxes .Per CCS1136 Rev K. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.25 ® 5146.00 $474.50 Total USD: $474.50 Discrepancy: 7.14 Acoustic door bearing arc worn and noisy Resolution: Removed existing bearings from acoustic door (4 EACH). Received Ok to install and installed 4 new bearings on acoustic door p/n: SUPER 8-OPN-DD. Work done per GP521400001 REV. C. Billing Method Hours Rate Total Labor USD: Time and Material ST 2.00 Q $146.00 $292.00 Parts USD: Time and Material $216.52 Total USD: $508.52 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 7.14 #1 SUPER S-OPN-DD BEARING, LINEAR, BAI.I.. 4 $54.13 $216.52 ACOUSTIC DOOR Discrepancy: 7.17 Customer request to fabricate new baggage net. (One inboard of the water cabinet) Resolution: Fabricated new baggage net using MIL-T5038GTYPE-IV webbing. All sewing done in accordance ASTM International Standard Practice for Stitches and Seams. Designation 6913-11. All work done per GC525240016 Rev. -. Reference 7.22 for flammability data. Billing Method Hours Rate Total Labor USD: Flat Rate $2,920.00 Paris USD: Time and Material $298.56 Total USD: $3,218.56 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 7 of 63 Set 01 EFTA00811211 Bill To: Plan D, LLC. WO Si: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 7.1782 40044-10 HOOK ASSY, LOOP & KEEPER 6 $2.12 S12.72 7.17 #3 FDA5352 HOOK AND BUCKLE 6 $42.61 S255.66 7.17 #4 MIL-T5038GTYPE-IV WEBBING I" CLASS 1 - BLACK 6 $5.03 $30.18 Discrepancy: 7.18 Acoustic door lower bearings are worn and noisy Resolution: Removed and replaced the acoustical door lower bearings and slides. P/N SRS9XMSS+400LM. All work done PER. CP5210000I Rev.C. Billing Method Hours Rate Total Parts USD: Time and Material $59636 Total USD: $596.36 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 7.1881 SRS9NNISS+4001.M RAIL ASSY 2 S298.18 S596.36 Discrepancy: 7.20 Fwd Lay Ned door pop-up in-op Resolution: Adjusted fwd lay door and pop-up for proper function with all work performed in accordance with GPM412001486-301 Rev - Billing Method Hours Rate Total Labor USD: Time and Material ST 6.62 @ 5146.00 $966.52 Total USD: $966.52 Item: 8 Mechanical Team Manager: Charles Thomas Part/Model N: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNffSO: CSN/CSO: Aircraft Time: Discrepancy: g3 Customer request full cleaning and operational checks of the Lavatory tank and system. Resolution: Summsry: Complied with cleaning of lay systems and toilets/waste tank per O550 AMM 38-31-01 Rev.03/31/17. See below for work performed. Functional operational test for logic control module system performed per CMP 380025 Ref.11.47. No discrepacies noted with logic module. Toilet operation check performed per CMP 380001 Ref.7.15. Operated okay and no leaks noted at this time. Ultrasonic sensors cleaned per CMP 380015/383024. No discrepacies noted with sensors at this time, see below for work performed. Billing Method Hours Rate Total Labor USD: Flat Rate $2,336.00 Parts USD: Time and Material 418,672.83 Total USD: $21,00853 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8381 NA51611-150A ORING 2 $2.25 $4.50 83 #2 MS295I3-226 PACKING, PREFORMED, 2 50.64 $1.28 HYDROCARBON FUEL RESISTANT, 0 RING 8383 7700248 SENSOR, TANK WASTE 1 $16,56330 $16,56330 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). Printed: 3/912018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 8 of 63 Set 01 EFTA00811212 Bill To: Plan D. I.I.C. WO Si: SC52166I Invoice Number: 5517132452 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8384 7600123 GASKET, WASTE TANK SENSOR $2,103.75 $2,103.75 Step: 8.3.1 Completed Removed. cleaned, inspected, and reinstalled ultrasonic sensors PN:7700395-001 1./H SN:07-G-170, and R/H SN:07-G-I67 per CMP 380015/383024. and CMP 380031/380032. Ref. Items. 11.44.11.45,11.46,11.48. Step: 8.3.2 Completed Complied with cleaning of lay systems and toilets/waste tank per 6550 AMM 38-31-01 Rev.03/31/17. Waste tank full light does not go off. Step: 8.3.3 Completed Removed and replaced the Waste tank delta p level sensor on waste tank. OFF: PIN: 7700248. S/N: 0554. ON: P/N: 7700248 S./NI: 1558. Ref. CMP 6550 381059 item /I: 11.157 Waste tank full light now functioning correctly. Discrepancy: 8.4 Customer request to inspect all exterior service door latches for serviceability and replace one discrepant latch on the external MED switch service door Resolution: Summary: Installed New latch P/N 115000-2-102-142 per BP 1159851110 Rev C to the external MED switch service door. Completed inspection of all service door latches per 6550 MM 53-00-00 June 15/16 and found no further discrepancies. (See steps below for a detail of work performed) Billing Method Hours Rate Total Labor USD: Time and Material ST 2.40 Qa 5146.00 $350.40 Pans USD: Time and Material $268.82 Total USD: $619.22 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.4 81 H5000-2-102-142 LATCH, SERVICE DOOR $258.12 $258.12 8.4 82 MS20426AD3-4 RIVET 10 $0.22 42.20 8.4 83 hIS20426AD3-3 RIVET 10 $0.22 42.20 8.4 84 hIS20426AD3-4.5 RIVET 10 $0.41 44.10 8.4 85 hIS20426AD3-5 RIVET- SOLID, CSK 100 DEG 10 $0.22 42.20 Step: 8.4.1 Completed Removed discrepant latch on the external MED switch service door per BP 1159 B5I110 Rev G. Step: 8.4.2 Completed Installed New latch P/N H5000-2-102-142 per BP 1159051110 Rev G to the external MED switch service door. Completed inspection of all exterior service door latches per 6550 MM 53-00-00 June 15/16 and 6550 3131 52-40-00 October 30/06 finding no further discrepancies. Step: 8.43 Completed Request paint on external MED switch service door due to new latch installation. Discrepancy: 8.5 Customer request to check water system indications Resolution: SUMMARY: Serviced water system and performed Water system operational check with no defects noted. All work done per 6550 AMM 38-10-00 dated August 31/05. see steps below for performed. Billing Method Hours Rate Total Labor USD: Time and Material ST 0.90 (a $146.00 S131.40 Total USD: $131.40 Step: 8.5.1 Completed Complied with potable water tank service per 6550 AMM 38-14-01 March 31/17. No indication on external panel noted throughout entire service. Step: 8.5.2 Completed Performed Water system operational check with no defects noted. All work done per 6550 AMM 38-10-00 dated August 31/05. 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 9 of 63 set dm EFTA00811213 Bill To: Plan D, LLC. WO Si: SC521661 Invoice Number: 5517132452 Discrepancy: 8.6 CMP G550 275019 Flap Actuator Travel Nut (Left)- Lubrication Resolution: COMPLIED WITH CMP G550 275019 Flap Actuator navel Nut (Left) - Lubrication Billing Method Hours Rate Total Labor USD: Flat Rate $146.00 Total USD: 5146.00 Discrepancy: 8.7 CMP GSM 275020 Flap Actuator Travel Nut (Right) - Lubrication Resolution: COMPLIED WITH CMP 6550 275020 Flap Actuator navel Nut (Right) - Lubrication Billing Method Hours Rate -total Labor USD: Flat Rate SI 46.00 Total USD: $146.00 Discrepancy: 8.9 CMP G550 491005 APU Enclosure FS 767 - FS 797 - Zonal Inspection Resolution: COMPLIED WITH CMP 6550 491005 APU Enclosure FS 767 - FS 797 - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $438.00 Total USD: $438.00 Discrepancy: 8.10 Customer requests 12 spare aircraft keys. Added during debrief Resolution: Provided 12 spare aircraft keys to customer. Billing Method Hours Rate Total Pans USD: Time and Material $162.00 Total USD: $162.00 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.1041 KEYS KEYS 12 $13.50 $162.00 Discrepancy: 8.11 Blue "R FUEL RETURN FAIL" CAS message appeared one hour into flight. Crew also noted that the right oil temperature was 100 degrees celcius and the left oil temperature was 80 degrees celcius. Added during debrief Resolution: performed heated fuel return operational check with no defects noted. All work done per O550 AMM 28-16-00 dated August 30, 2009. Decade resistor box ID/4 568066 cal due date 11/18 Billing Method Hours Rate Total Labor USD: Flat Rate $584.00 Total USD: $584.00 Discrepancy: 8.19 Cyan "APU Maint Required" Cas message on APU start. CMC fault code 4922222APU (APU Flow Divider Sol Short) 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 10 of 63 recut EFTA00811214 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: Summary: Removed and replaced fuel flow divider P/N WE3883842-2 S/N NSN and solenoid valve P/N WE3883738-1 S/N NSN. Performed operational and leak check with no defects noted at this time per CMP 493011. See steps below for detailed work performed. Billing Method Hours Rate Total Labor USD: Time and Material ST 11.83 ® $146.00 $1,727.18 Labor USD: Time and Material OT 0.02 ® $146.00 52.92 Pans USD: Time and Material 35,574.25 Total USD: 57,30435 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.19 81 WE3883738-1 VALVE, SOLENOID 1 35,572.61 $5,572.61 8.19 #4 M25981U2-904 PACKING 2 50.82 51.64 Step: 8.19.1 Completed Gained access to 181A1PI ( on APU Ceiling). Disconnected plug. inspected and cleaned cannon plug with no defects noted. Returned aircraft to original configuration. All maintenance performed using WDM 49-60-00 June 15/16. Step: 8.19.2 Completed Ran APU and still had constant APU maint. required message for CMC fault code 4922222APU (APU Flow Divider Sol Short) Step: 8.19.3 Completed Removed and replaced with new fuel flow divider PN-WE3883842-2 NSN and solenoid valve PN-WE3883738-1 NSN per CMP G 493011 item 11.153. Discrepancy: 8.22 Horizontal stabilizer Rfil hoist plug stripped. Ref. 13.1 Resolution: Replaced horizontal stabilizer Rill and Lill hoist plugs PN: 1159CSM50558-00I with new horizontal stabilizer R/II and Lill hoist plugs PN: 1159CS3150558-001 per drawing 1159CS3150558 Rev.B. and G550 AMM 20-42-00 Rev. Mar.31/17. Billing Method Hours Rate Total Parts USD. Time and Material $1,145.84 Total USD: $1,145.84 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.22 kl 1159CS3450558-00I PLUG, HORIZONTAL STABILIZER 1 5389.48 $389.48 HOISTING STOP 8.2282 1159CS3450558-00I PLUG, HORIZONTAL STABILIZER 2 5378.18 $75636 HOISTING STOP Discrepancy: 813 L/H Flap "B" Track Aft I/B Roller is worn beyond limits per G550 AMM 27-50-00 Rev. March 31/17 Ref. 13.2 Resolution: Replaced Lill Flap "B" hack Aft 1/B Roller with new roller, P/N KRP233012FT, IAW CMP G550 275037 and Drawing 1159CS54220 Rev G Billing Method Hours Rate Total Labor USD: Flat Rate $1,168.00 Pans USD: Time and Material $999.18 Total USD: $2,167.18 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.23 #1 KRP233012FT ROLLER. FLAP TRACK 1 $703.50 S703.50 8.23 #5 1159C'ShI54233-19 WASHER 2 591.20 S182.40 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). Printed: 3/9/2018 4:29:22PM Page II of 63 Set 01 GAC_RevenueSquawksInvoicc.rpt v3 EFTA00811215 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.23 #6 hIS17826-8 NUT 2 $2.42 $4.84 8.23 47 hIS24665-370 COTTER PIN 2 $0.22 $0.44 8.23 48 NA56704L13 BOLT $108.00 $108.00 Discrepancy: 8,24 Rft1Flap "B" Track Aft DB Roller is worn beyond limits per 6550 A6161 27-50-00 Rev. March 31/17 Ref. 13.2 Resolution: Summary: Removed R/11 Flap "B" *hack Aft outboard bracket Replaced FUR Flap "B" Track Aft 1/B roller with new roller, P/N KRP233012FT. Installed R/H Flap "B" Track Aft outboard bracket. Work performed per CMP O550 275038 and Drawing 1159CS54220 Rev G. See steps below for detailed work performed. Billing Method Hours Rate Total Labor USD: Time and Material ST 8.92 ® $146.00 $1,302.32 Pans USD: Time and Material 31,056.60 Total USD: $2,358.92 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.24 #1 KRP233012FT ROLLER. FLAP TRACK I $703.50 $703.50 8.24 #2 NAS6704LII BOLT 1 $117.70 $117.70 8.24 #3 NAS67041,11 BOLT 2 $117.70 $235.40 Step: 8.24.1 Completed Removed RAI Flap "B" Track Aft outboard bracket. Replaced Rai Flap "B" Track Aft I/B roller with new roller. FIN KRP233012FT. per ChIP G550 275038 and Drawing 1159CS54220 Rev G Step: 8.24.2 Completed Recieved ok to install and installed R 11 Flap Track "B" AFT O/B roller fitting. Bolts still require torque and fitting requires sealant per 1159CS54220 Rev G. Step: 8.243 Completed Bolts require torque and fitting requires sealant per 1159C'S54220 Rev G. Discrepancy: 8.27 Rh i Pylon leading edge seal torn Resolution: Replaced R/11 Pylon leading edge seal per DWG 1159P57911 rev. C Billing Method Hours Rate Total Labor USD: Time and Material ST 3.47 @ $146.00 $506.62 Pans USD: Time and Material $2,044.87 Total USD: $2,551.49 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.27 #1 1159SCP510-18E SEAL, LEADING EDGE. R/H 1 52,027.56 $2,027.56 8.27 #2 NAS8802-3 BOLT 3 $2.72 $8.16 8.27 #3 MS21043-04 NUT-SELF LKG,CRES,RING BASE 3 $2.06 $6.18 8.27 #4 NASI149DN816K WASHER 3 50.22 $0.66 8.27 #5 MS21043-08 NUT, SELF LOCKING. REDUCED H 3 $0.77 42.31 Discrepancy: 8.29 NLG %%ire harness Is contacting hydraulic lines in aft NLC wheel well when gear is retracted. Found while accomplishing clearance check. REF 13.1.1 paint traveler 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawkslnvoice.rpt v3 Page 12 of 63 wt EFTA00811216 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: Adjusted AFTsection of NLG wire harness (P/N: 1159SCAV516-5) to clear hydraulic lines and repositioned teflon protective wrap (P/N: GAP105F2C2). Retracted NLG and verified NLG harness does not contact hydraulic lines. All work performed per AMM 655032-26-03 Dated MArch 31/17 Billing Method Hours Rate Total Labor USD: Flat Rate 5876.00 Total USD: 5876.00 Discrepancy: 8.30 L/11 MLG brake harness has tear in insulation located near upper hydraulic brake swivel. Found while accomplishing clearance check. REF 13.1.1 paint traveler Resolution: Summary : Complied with LH MIA: brake harness insulation tear repair 1AW SR1052 Rev-B. No defects noted. Sec steps below for details of work performed. Billing Method flours Rate Total Labor USD: Flat Rate 5584.00 Pans USD: Time and Material 535.44 Total USD: $619.44 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.30#1 GAC501K400H1 BANDCLAMP I $32.99 $32.99 8.30 #3 GAS830CV150-0 SLEEVING I $1.76 $1.76 8.30 Al GAS830CV100-0 SLEEVE I $0.69 $0.69 Step: 830.1 Completed Replaced upper broken clamp on Left 311.6 strut. All maintenance performed using DWG 1159130300 REV K. Torque Wrench CN: 562086 Date Due: 09118 Step: 830.2 Completed Complied with I.H 311.(i brake harness insulation tear repair LAW SR1052 Rev-B. No defects noted. Discrepancy: 831 LAI hal: brake harness is kinked near upper hydraulic brake swivel when gear is retracted. Found while accomplishing clearance check. REF 13.1.1 paint traveler Resolution: Summaary : Added heat shrink to harness to move the bending point of the harness. Placed mulct-jai butted up to repaired area extending up toward the plug end and heat in place. See steps below for details of work performed. Engineering disposition complete. See item 8.31.2 Billing Method flours Rate Labor USD: Flat Rate $1,168.00 Parts USD: Time and Material $6.28 Total USD: $1,174.28 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 83181 GAS830CV100-0 SLEEVE 4 $0.69 $2.76 831#2 GAS830CV150-0 SLEEVING 2 $1.76 $3.52 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 13 of 63 Set 01 EFTA00811217 Bill To: Plan D, LLC. WO fl: SC521661 Invoice Number: 5517132452 Step: 831.1 Completed Request Engineering Disposition Step: 831.2 Completed ENGINEERING DISPOSITION: Add heat shrink to harness to move the bending point of the harness to a desired location (gear up), similarly: add apmx. 4 inches heat shrink. Place material butted up to repaired area extending up toward the plug end and heat in place. Center a 4-6" piece of heat shrine on top of that butt joint, and heat in place. Add or remove heat shrink shrink material to increase or decrease flexibility of impingement. Discrepancy: 832 LAI #5 Flap pillow block assembly is worn and making a loud grinding sound when operated with 3000 psi mule. Ref. 11.99 Located at RBS 260 Resolution: Removed Lill #5 pillow block assembly PN-I159SCC504-15 SN-3924 and installed new block PN-1159SCC504-15 SN-7992 per 6550 AMM 27-53-05 Aug 30/09. Complied with flap system operational with no defects noted per 6550 AMNI 27-50-00 Nov 15/17. Billing Method Hours Rate Total Labor USD: Time and Material ST 14.84 @ $146.00 $2,166.64 Pans USD: Time and Material $1,811.89 Total USD: $3,978.53 Pans: Rd: No. Pan number: Description Quantity Sell price USD Extended USD 832#1 1159SCC504-15 PILLOW BLOCK, FLAPCONTROL I $1,758.99 $1,758.99 DRIVE 832 #2 NAS6404U6D BOLT 2 50.00 $0.00 832 #3 NASI 587-4C WASHER 2 $1.69 $338 832#4 NASI149D0463K WASHER 2 $0.23 $0.46 832#5 202-16I26-4L NUT, SELF LOCKING 2 $23.62 $47.24 832#6 NIS24665-153 PIN, COTTER 2 $0.22 S0.44 832 #7 MS24665-86 COTTER PIN 6 $0.23 5138 Discrepancy: 833 R/I1 #5 Flap pillow block assembly is worn and making a loud grinding sound when operated with 3000 psi mule. Ref. 11.99 Located at RBS 260 Resolution: Removed R/11 #5 pillow block assembly PN-1159SCC504-15 SN-3945 and installed new block PN-1159SCC504-15 SN-7995 per 6550 ANIM 27-53-05 Aug 30/09. Complied with flap system operational with no defects noted per 6550 AMM 27-50-00 Nov 15/17. Billing Method I lours Rate Total Labor USD: Time and Material ST 14.05 (a 5146.00 $2,05130 Labor USD: Time and Material OT 0.35 ;tit 5146.00 $51.10 Pans USD: Time and Material $1,810.51 Total USD: $3,912.91 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 833 #1 1159SCC504-15 PILLOW BLOCK, FLAP CONTROL I $1,758.99 $1,758.99 DRIVE 833#2 NAS6404U6D BOLT 2 50.00 50.00 833#3 NASI 587-4C WASHER 2 $1.69 5338 833#4 NASI149D0463K WASHER 2 $0.23 50.46 833#5 202-16I26-4L NUT, SELF LOCKING 2 $23.62 $47.24 833 #6 MS24665-153 PIN, COTTER 2 $0.22 50.44 Discrepancy: 836 RAH NLG door step is out of limits .060. (0.035 Max)) Ref. 13.1.1 Paint Travel Section D Line NI 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). Printed: 3/9/2018 4:29:22PM Page 14 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811218 Bill To: Plan D. LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: Removed cotter pins (2ea.). loosened jam nuts and adjusted R/II and Lilt NIG door control rod P/N: 159L10085-9. 1/2 turn out to achieve proper door fit stated per CV-GER-313 Rev. P Adjusted R./II SIC aft door stop until contact was made with bumper stop. Installed new cotter pins and tightened control rod jam nuts. Cycled doors and checked for proper operation and indications with no faults noted. Work done per GV-GER-313 Rev. P Billing Method Hours Rate Total Labor USD: Time and Material ST 6.00 @ S146.00 5876.00 Total USD: $876.00 Discrepancy: 8.38 RAI #2 E-window upper heat contactor showing signs of arcing. Re(Item 19.1.12 Resolution: Removed contactor P/N 1159F50236-22 from RAI #2 E-window frame and installed new contactor P/N 1159F50236-22 as per GAC Drawing 1159F50236 Rev B. Ref item 19.1.12 for heat check following window installation Bitting Method Hours Rate Total Labor USD: Flat Rate $146.00 Parts USD: Time and Material $250.00 Total USD: $396.00 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.38#1 1159150236-22 CONNECTOR ASSY. M DO-R1L 1 $250.00 S250.00 GVFS490 Discrepancy: 8.40 Lill engine has Fire-loop B fault, during and after fireloop test in cockpit. Resolution: Removed L/H Fire control box PN: 51653-154 SN: 3305 and installed repaired Fire control box PN: 51653-154 SN: 2763. Performed operational check with no defects noted. All work done per 6550 ChIP 261201 (Ref 11.151) and CMP G550 261211 (Ref 11.154) Billing Method Hours Rate Total Labor USD: Time and Material ST 1.13 ® S146.00 5164.98 Labor USD: Time and Material OT 1.50 @ S146.00 5219.00 Parts USD: Time and Material 57.922.87 Total USD: 58.306.85 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.40 #1 51653-154 CONTROLLER, FIREWIRE I $7,921.03 $7,921.03 8.40#2 MS35207-264 SCREW 4 50.23 $0.92 8.40#3 NAS1149D0316H WASHER 4 50.23 $0.92 Item: 9 Paint Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 15 of 63 Set 01 EFTA00811219 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Item: 10 Outstanding Pans, Materials, and / or Services Team Manager: Charles Thomas Pan/Model Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNffSO: CSN/CSO: Aircraft Time: Item: Follow on CMP Codes / Maintenance Tasks Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNffSO: CSN/CSO: Aircraft Time: Item: 12 WCR's - Work Change Requests Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNffSO: CSN/CSO: Aircraft Time: Discrepancy: 12.3 WCR 3- APPROVED: Customer requests to remove the two (2) console tables and lids from the cabin side ledges. Resolution: Removed Ltl #2 and RII #2 console tables and lids from the cabin side ledges Per CE522280107 Rev - Reveneered Revennered with Dark Eucalyptus Veneer part# CSE150717-1LP Lt 17-366384. Reference RSQCT-400 Rev.-, Index #9 for details of work done. Ref. 19.24 for flammability data. Billing Method Hours Rate Total Labor USD: Flat Rate 510.840.00 Pans USD: Flat Rate 5207.00 Total USD: 5'1.047.00 Step: 123.1 Completed Wood Labor Only Step: 123.2 Completed INT Support (R&R) Labor Only Step: 123.3 Completed Inspection Labor Only Step: 123.4 Completed Electrical Engineering Step: 123.5 Completed Mechanical Engineering Step: 123.6 Completed Removed the two (2) console tables and lids from the cabin side ledges per drawing # CE522280I07-0I Rev.- Discrepancy: 12.4 WCR 4- APPROVED: Customer requests to remove all cabin dual cupholders and replace with single cupholders. No cupholders will be required al the divan or the area where the two console tables are removed. Resolution: Removed all cabin dual cupholders and replaced with single cupholders.RII #1, 2 and LII #1, 2, and 3 Ledges.Removed cupholders al the divan area and Res ennered with Dark Eucalyptus Veneer part# GSE150717-1LP Lt 17-366384 All work done per CE522280108 Rev - Reference RSQCT-400 Index #9 for details of work done. Billing Method Hours Rate Total Labor USD: Fiat Rate 513,322.00 Parts USD: Fiat Rate 54105.00 Total USD: 514,427.00 Pans: Ref. No. Pan number: Description Quantity 12.4 #1 2123X2.43NEC CUPHOLDER 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 16 of 63 Set 01 EFTA00811220 Bill To: Plan D, LLC. WO C. SC521661 Invoice Number: 5517132452 Step: 12.4.1 Completed INT Sheet Metal Labor Only Step: 12.4.2 Completed Wood Labor Only Step: 12.4.3 Completed Inspection Labor Only Step: 12.4.4 Completed Nlechaincal Engineering Step: 12.4.5 Completed Bonded hardwood to fill-in unwanted cup holes using DP-420 per CE522280108-0I Rev.- Discrepancy: 12.6 WCR 6- APPROVED: Customer requests to replace the galley and gaffe!, annex counter top nosings with hardwood. The current nosings will be removed. The new nosings will be fabricated of hardwood and veneer. Resolution: Removed existing nosing and installed new galley and galley annex counter top nosings with Hardwood P/N 8-4QTR-SAWN-MOZAMBIQUEILOT # LT17-365416 LAI Galley Veneer P/N GSE 150717-1LP LOTS/ LT17-366384 Bonded per CCS 1136 TYPE 1 REV K. & CCS1109 Rev A Ref. Ref 19.24 for flammability & Ref 12.6.7 for work performed) Billing Method Hours Ratc Total Labor USD: Flat Rate $7,884.00 Pans USD: Flat Rate $1,338.00 Total USD: $9,222.00 Pans: Ref. No. Pan number: Description Quantity 12.6 #1 GSM344001007-101 STOP 2 12.6 #2 AN525-10R10 SCREW 10 12.6 #3 AN525-10R11 SCREW 10 12.6 #4 AN525-10R12 SCREW 10 Step: 12.6.1 Completed Wood Labor Only Step: 12.6.2 Completed INT Finish and Paint Labor Only Step: 12.6.3 Completed Inspection labor Only Step: 12.6.4 Completed Mechanical Engineering Step: 12.6.5 Completed Stress Engineering Step: 12.6.6 Completed Verify material for R/H Galley annes.,and LEH Galley Veneer P/N GSE 150717-1LP LOT# LTI7-366384. Hardwood P/N 8-4QTR-SAWN-MOZAMBIQUE ILOT # LT17-365416. Bonded veneer per CCS 1136 TYPE 3 REV J. Bonded hardwood per CCS 1136 TYPE 1 REV J. Received okay to send to finish. Step: 12.6.7 Completed Hardwood P/N 8-4QTR-SAWN-MOZAMBIQUE ILOT # LTI7-365416. Bonded hardwood nosing on I/H GalleyMay per CCS 1136 TYPE 1 REV K. Ref. GPM308001581-301 rev ne. Step: 12.6.8 Completed Finish- Lai Galley hardwood nosing Step: 12.6.9 Completed Finish - Rut Galley annex Item: 13 Option 1- Full Paint - (Ref. Item D 1.1 of Proposal ID8 7037536, ROD) Team Manager: Charles Thomas Pan/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNffSO: CSN/CSO: 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). Printed: 3/9/2018 4:29:22PM Page 17 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811221 Bill To: Plan D. LLC. WO It: SC521661 Invoice Number: 5517132452 Discrepancy: 13.1 Option I- Full Paint The preparation and application of the exterior paint will be applied in accordance with the procedures and specifications outlined in the Culfstream Aerospace Material and Process Specification (CAMPS 4000) and will include the following Customer specified elements: The existing paint will be removed from the aircraft. Composite surfaces will be scuff sanded to remove the gloss front the existing paint. The main entrance Airstair door, Airstair door jamb. and baggage door jamb will be painted to match the primary fuselage color. C. The inside of the landing gear doors will be painted with the same base color as the outside surface. O The landing gear will be cleaned. O Wing walks will be applied in accordance with approved data. O A new radome boot will be applied. MI antenna leading edges will have erosion tape applied. O Previously polished metal surfaces will be huffed. ❑ The inside surfaces of the airbrakes will be painted. r. After completion of the exterior paint, a weight and balance will be performed on the aircraft. Any items not listed above will be quoted on a per item basis by the Culfstream facilities Paint Operations Manager. including labor and materials on a Work Change Request (WCR). """ SEE APPENDIX FOR ADDITIONAL INFO *** Resolution: Complied with full paint. See steps below for details of all work accomplished. In addition to the paint specifications listed above, the following standard Culfstream Aerospace Paint Specifications will be incorporated: The existing paint will be removed from the aircraft. Composite surfaces will be scuff sanded to remove the gloss from the existing paint. The main entrance Airstair door. Airstair door jamb, and baggage door jamb will be painted to match the primary fuselage color. The inside of the landing gear doors will be painted with same base color as the outside surface. The landing gear will be cleaned. Wing walks will be applied in accordance with approved data. A new radome boot will be applied. All antenna leading edges will have erosion tape applied. Previously polished metal surfaces will be buffed. The inside surfaces of the air brakes will he painted. After completion of exterior paint, a weight and balance will be performed on the aircraft. Any items not listed above will be quoted on a per item basis by the Culfstream facility's Paint Operations Manager. including labor and materials on a Work Change Request (WCR). Billing NIethod flours Rate Total Labor USD: Flat Rate 4223,060.00 Pans USD: Flat Rate S'25,294.00 Services USD: Flat Rate $'21,108.00 Total USD: 4269,462.00 Pans: Ref. No. Pan number: Description Quantity 13.1 HI PAINT KIT GV 6550 PAINT KIT FOR GV, G550 I 13.1 #2 CA18050C GAL SOLVENT REDUCER 6 13.1 #3 P10010-155 LACQUER, ACRYLIC -FLAT BLACK 4 13.1 #4 J328 DEGREASER, ZONE DEFENSE (I EA- I 5 GL PAIL) 13.1 #5 P12144081-2-654 SEALANT, 6 OUNCE #654 SENIKIT 24 1/2 HOUR WORK LIFE 13.1 #6 CA8905HP CLEAR COAT KIT GL I 13.1 #7 AN525-832-8 SCREW 5 13.1 #8 NASI149DN816K WASHER 5 13.1 #9 MS210421.08 NUT, SELF LOCKING 2 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). Printed: 3/9/2018 4:29:22PM DAC_RevenueSquawkfinvoice.rpt v3 Page IS of 63 Set 01 EFTA00811222 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity 13.1 #10 738651E5-01 PAINT, ELITE BLUE IMRON AF700 40 13.1 #11 137755-01GL THINNER 20 13.1#12 AF740 PAINT, CLEAR COAT 40 13.1 #13 131105 CATALYST 1 13.1 #14 137655 REDUCER I 13.1 #15 131105 CATALYST I 13.1 #16 131105 CATALYST I 13.1 #17 131105 CATALYST I 13.1 #18 131105 CATALYST I 13.1 #19 131105 CATALYST I 13.1 #20 131105 CATALYST I 13.1 #2I 131105 CATALYST I 13.1 #22 131105 CATALYST I 13.1 #23 131105 CATALYST I 13.1 #24 131105 CATALYST I 13.1 #25 131105 CATALYST I 13.1 #26 131105 CATALYST I 13.1 #27 131105 CATALYST I 13.1 #28 131105 CATALYST I 13.1 #29 131105 CATALYST I 13.1 #30 131105 CATALYST I 13.1 #31 131105 CATALYST I 13.1 #32 131105 CATALYST I 13.1 #33 131105 CATALYST I 13.1 #34 137655 REDUCER I 13.1 #35 137655 REDUCER I 13.1 #36 137655 REDUCER I 13.1 #37 13765.5 REDUCER I 13.1 #38 13765.5 REDUCER I 13.1 #39 13765.5 REDUCER I 13.1 #40 13765.5 REDUCER I 13.1 #41 13765.5 REDUCER I 13.1 #42 13765.5 REDUCER I 13.1 #43 13765.5 REDUCER I 13.1 #44 13765.5 REDUCER I 13.1 #45 13765.5 REDUCER I 13.1 #46 13765.5 REDUCER I 13.1 #47 13765.5 REDUCER I 13.1 #48 13765.5 REDUCER I 13.1 #49 13765.5 REDUCER I 13.1 #50 13765.5 REDUCER I 13.1 #51 13765.5 REDUCER I 13.1 #52 13765.5 REDUCER I 13.1 #54 CA1805CX GAL SOLVENT REDUCER 8 13.1 #55 PR1440B1-2-654 SEALANT, 6 OUNCE #654 SEMKIT 14 1/2 HOUR WORK LIFE 13.1 #56 CA8905HP CLEAR COAT KIT GL I 13.1 #57 D9001 CONVERTER 2 13.1 #58 D8003 SURFACER, SANDING 2 13.1 #59 400 EVERCOAT EVERCOAT FILLER 3 13.1 460 140N2022S1 FUSELAGE DRAIN VALVE 1 13.1 #61 GASI3AN-1-41 SEAL, BUTTONED STRIP, WHEEL 9 WELL DOOR (5' SECTION) 13.1 #62 MS27039C0807 SCREW-MACHINE, CRES PAN HD, 34 STRL 13.1 #63 NAS1149DN816K WASHER 46 13.1 #64 MS27039C0808 SCREW, PAN HEAD, X RECESSED 8 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). Printed: 3/9/2018 4:29:22PM Page 19 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811223 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity 13.1 #65 MS24693S26 SCREW, MACHINE. FLAT 18 COUNTERSUNK HD. 100 DEG. CROSS RECESS 13.1 #66 MS24693-528 SCREW 6 13.1 #67 AN525832R7 BOLT 12 13.1 #68 AN525-832R11 SCREW 10 13.1#69 NAS1149DN816H WASHER, FLAT ALUMINUM 10 13.1 #70 MS21042108 NUT, SELF LOCKING 10 13.1 #7I AN525-832R5 SCREW 21 13.1 #72 MS27039-0809 SCREW, MACHINE 9 13.1 #73 NA51149CN816R WASHER-FLAT CRES 14 13.1 #74 140N2022S1 FUSELAGE DRAIN VALVE I 13.1 #75 MS24665-155 COTTER PIN 2 13.1 #78 NIS27039C0807 SCREW-MACHINE, CRES PAN HD, 10 STRL 13.1 #79 NAS43DD3-36FC SPACER SLEEVE 2 13.1 #80 SJ8665FP021-I RADOME BOOT I 13.1 #81 MS24665-302 COTTER PIN 24 13.1 #84 GAS18h1-1-1440 SEAL 12 13.1 #85 MS24694-C7 SCREW, MACHINE, FLAT CTSK HD, 30 100 DEG, STRI, CROSS RECESSED 13.1#86 NIS24694C7 SCREW, CSK - 100 DEGREE - 5 STRUCTURAL -ST 13.1 #87 NAS1149CN816R WASHER-FLAT CRES 36 13.1 #88 MS24694-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 MS24694-C7 SCREW, MACHINE, FLAT CTSK HD, 24 100 DEG, STRI, CROSS RECESSED 13.1.1 #1 NAS1581K4R5 BOLT 22 13.1.1 #2 NAS1580V3R6 SCREW ISO Services: Ref. No. Description 13.1 #3 Vendor Supplied Labor 1.00 13.1 #1 IAS. Cardoza, 13.1.6.8 hrs. 2/5-2/11 1.00 13.1 #2 IAS, Cardoza, 13.1.6.8 hrs.2/12-2118 1.00 13.1.2 #1 IAS Graf. David 20.0 HRS item 13.1.2 1.00 13.13 #1 IAS Biddle, Brett 40.O !IRS and 4.0 HRS OT item 13.1.3 on 1.00 121I1117-12/14/17 13.13 #2 IAS Graft. David 11.0 IIRS item 13.13 on 12/13/17 1.00 13.1.5 #1 IAS Blanton 40 hrs + 5hrs 01 13.1.5 12/17 1.00 13.1.6 #1 IAS,SIKE.S.,12/25-12/31..13.1.6.„16 HOURS 1.00 13.1.6 #2 IAS , Sikes ,13.1.6 , 46hrs. , 1/8 - 1/13 1.00 13.1.6 #3 IAS, Johnson,13.1.6, 2 brs, 1/29-214 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). Printed: 3/9/2018 4:29:22PM Page 20 of 63 Wet 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811224 Bill To: Plan D, LLC. WO SC521661 Invoice Number: 5517132452 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 6550 AMM 55-3040 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 6550 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 6550 AMM 32-0040. Nov 15/17 Step: 13.1.1.4 Completed Panel 325AT installed. needs sealant, panel 337CT waiting for ops checks prior to final installation Step: 13.1.13 Completed Complied with Aircraft paint traveler RSQCT-330 Rev.8. Ref.paper 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 Completed Weight and balance Step: 13.1.7.1 Completed 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: 13.3 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.Plant traveler 11A. Resolution: Complied with engineering disposition on item 13.3.1.1 see steps below for all work preformed Billing Method Flours 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 Step: 133.1 Completed Request engineering disposition to correct Rill side negative step on radome that is out of limits. Step: 133.1.1 Completed Engineering Disposition: It is acceptable to repair the out-of-tolerance radome steps in accordance with Gulfstream Service Letter 651.005300001 Rev. - ."Aerodynamic Filler Sweep - Fair Procedure - Radome Steps". This Gulfstream Service Letter (GSL) is classified as a Manufacturer's Sen ice 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 651. 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. Step: 133.2 Completed Request paint to comply with engineering dispo during full strip and paint. ref item 13.1 Step: 1333 Completed Comply with post-paint radome to fixed structure perimeter steps and gap measurements. Discrepancy: 13.5 Replace MED helicrank 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 159BP10023 Rev.Il. Billing Method Hours Rate Total Parts USD: Time and Material $126.65 Total USD: $126.65 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). Printed: 3/9/2018 4:29:22PM Page 21 of 63 Set 01 riAC_RevenueSquawksInvoice.rpt v3 EFTA00811225 Bill To: Plan D, LLC. WO tol: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 13.5 #1 AN525-832-1I SCREW 1 $7.27 $7.27 13.542 NAS1149DN816H WASHER, FLAT ALUMINUM 10 $0.23 42.30 13.5#3 NIS210421.08 NUT, SELF LOCKING 10 $0.44 44.40 13.5#4 AN525-832R11 SCREW 1 $0.22 $0.22 13.5#5 AN525-832R11 SCREW 5 $0.22 S1.10 13.5#6 AN525-832R11 SCREW 1 50.22 S0.22 13.5 #7 AN525-832R11 SCREW 1 $0.22 S0.22 13.5#8 WH832R11D613WH SCREW 14 $7.87 $110.18 13.5#9 AN525-832R11 SCREW 1 $0.74 $0.74 Discrepancy: 13.7 One drain diverter missing just forward of tail compartment door. Resolution: Replaced drain diverter PN:1159BM47517-13 just forward of tail compartment door per G550 AMM 53-51-00 RevJan 15/10. Time adhesive GAA100BD04 was applied 14:00 PM, set in 6 hours. Billing Method Hours Rate Total Pans USD: Time and Material $11235 Total USD: $11235 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 13.7 #1 1159BM47517-13 D1VERTER DRAIN, AFT LOWER 1 $11235 $11235 PANEL Discrepancy: 13.8 Customer Requests to polish and swap L/H and Rill overwing E-light lenses. Resolution: ***summary*** Removed 6 overwing emergency light lenses. Polished lenses. Reinstalled 6 overwing emergency light lenses. Sealed 6 overwing emergency light lenses. See steps below for details of work perforated. Billing Method Hours Rate Total Labor USD: Time and Material ST 18.00 (a 5146.00 $2,628.00 Total USD: $2,628.00 Step: 13.8.1 Completed Removed 6 overwing emergency light tense covers. Step: 13.8.2 Completed Sealent required for 6 overwing emergency light lease coven Item: 14 Photographic Documentation - (Ref. Item D 2.1 of Proposal ID4 7037536, R00) Team Manager: Charles Thomas Part/Modci N: Customer Coordinator: Julian Brown 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 Parttivlodcl Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSN/TSO: CSN/CSO: 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 22 of 63 Set 01 EFTA00811226 Bill To: Plan D, LW. WO Ft: SC521661 Invoice Number: 5517132452 Discrepancy: 15.1 Jet ConneX (Ka-band) HighSpeed 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 (APM) will be located in the baggage compartment equipment cabinet and holds the configuration data for the system. One (1) Ka-band Aircraft Network Data Unit (KANDU) will be installed in the boiler room. The KANDU receives commands from the MODMAN through an Ethernet interface to configure the antenna/KRFU and reports status over this Ethernet interface One (1) Ka-band Frequency Unit (KRFU) will be installed in the proximity of the TMA assembly on top of the tall 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 Converter (BUC) to convert the IF frequencies to Ka-band frequencies. A High- Power 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. .•• SEE APPENDIX *fl Resolution: Complied with installation of Jet ConneX (Ka-band) High-Speed Data System per STC ST03238AT-D Index List GC413038007 Rev R, Configuration Lists GC513038031 Rev A, GC513038034 Rev A, and GC513038035 Rev —. Reference Custom Electrical Drawing List CESI 4960797 Rev E and Custom Mechanical Drawing List CE52005173 Rev C 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 Pewter P/N GPFR0242 (Ref work 15.20) Reference CE51 4696543 Rev -- for Electrical Load Supplement. 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 23 of 63 Set 01 EFTA00811227 Bill To: Plan D, LLC. WO Ii: SC521661 Invoice Number: 5517132452 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 Cogo system installed, the SDR will be integrated with the Cogo utilizing existing Ethernet provisions for single SSID, unless otherwise directed by Owner/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 (1)90401121 - Honeywell Aeronautical Personality Module (APM) One (I) 90401202 - Honeywell Ka-band Frequency Unit (KRFU Convection Cooled) One (1)90409013-0001 - Honeywell Tail Mounted Antenna (TMA) One (I) 90401566 - Honeywell Ka-band Aircraft Network Data Unit (KANDU) One (I) I233-F-2191-10 - Satcont Direct Router (SDR) One (I) Radome Various Installation Kits Certification: The Jet ConneX (Ka-band) High-Speed Data System along with the Salcom Direct Router will be installed via Culfstream 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 $18,000. Changes to the Aircraft's Completion Center Maintenance handbook (CCNIII), 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 al additional charge. Culfstream may require assistance from 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 ay ailabilit of components and installation. Billing Method Hours Raw Total Labor USD: fl at Rale S192.054.00 Parts USD: Flat Rate $492.946.00 Services USD: No Charge 's; t Total USD: S685.000.00 Pans: Ref. No. Pan number: Description Quanta> 15.1 #1 1233-F-2191-I0 SATCOM DIRECT ROUTER 1 15.1 #2 100-1021-30 ANTENNA I 15.183 100-1021-50 ANTENNA I 15.1 #4 PE9079 ADAPTER, TNC TO SMA 2 15.185 P18350-001 TERRETRIAL MODEM ANTENNA I 15.1 #6 ST03238AT-D INSTALLATION OF SATCOM (HIGH I SPEED DATA HD-I28) SYSTEM 15.187 GPM004001402-301 PEDESTAL SWITCH PANEL ASSY I 15.1 #8 27498-4101 SLEEVE 2 15.189 27498-006 SPACER I 15.1810 GAC830T3 CONNECTOR I 15.1 #I1 M24308/4-3F PLUG, D-SUB, 25-PIN I 15.1812 M2430812-3F RCPT, SOCKET, D-SUB. 25-20 GA I 15.1813 DBI15339-22 BACKSHELL I 15.1814 27498-006 SPACER I 15.1815 GPM004001714-301 KA PED OVERLAN I For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). Printed: 3/9/2018 4:29:22PM GAC_RevenuaquawksInvoice.rpt v3 Page 24 of 63 Set 01 EFTA00811228 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity 15.1 #16 27498-001 SLEEVE 1 15.1 #17 27498-008 SPACER 1 15.1 #18 N1S27473T12F3S CONNECTOR I 15.1 #19 M85049/49-2-I2N BACKSHELL I 15.1 #20 N1S27473T16F55S CONNECTOR I 15.1 021 M85049/49-2-I6N BACKSHELL I 15.1 #22 N1S27473T18F35S CONNECTOR I 15.1 #23 M85049/49-2-I8N BACKSHELL I 15.1 #24 27500-010 SWITCH ' 15.1 #25 500-35750-101 KIT, SDR COAX CABLE I 15.1 #26 P16917-001 REMOTE WIFI ANTENNA I 15.1 #27 GAR540BY16 RING 8 15.1 #28 GAR540BY22 RING 6 15.1 #29 D20419 CLIP l00 15.1 #30 GAC861A11424S CABLE, ONE CONTINUOUS LENGTH 100 ON SPOOL 15.1 #32 (;ABSIIAB6B6 BOLT 30 15.1 #33 (;ABSIIAB6B7 BOLT 40 15.1 #34 GAB511AB6B8 BOLT, PROT SHEAR HEAD. TI 20 15.1 #35 GABSIIAB6B4 BOLT IS 15.1 #36 GAB5IIAB8B8 BOLT, PROTRUDING SHEAR HEAD. 4 TITANIUM 15.1 #37 GANSIOAA6 COLLAR, SHEAR 70 15.1 #39 GAB5HAB6B5 BOLT, PROTRUDING SHEAR HEAD. 41 TITANIUM 15.1#411 GAS830AJ2 SOLDER SLEEVE (BRAID) 100 15.1#41 GAS830AHI SOLDER SLEEVE (PIG TAIL) 100 15.1 #42 GAT805H10-08 LUG.TERMINAL.YELLOW1/8 50 15.1 #43 GAT805H18-38 TERMINAL 50 15.1 #44 GAT805H18-3B TERMINAL 50 15.1 #45 GAT805H18-08 LUG, TERMINAL, RED, #8 50 15.1 #46 324484 CAP END 100 15.1 #47 GAT805P8-08 TERMINAL 20 15.1 #48 GAT805H10-3A TERMINAL 75 15.1#49 5684-01 CLIP ASSEMBLY, 90 DEG. ANGLE 50 15.1 #51 I73H7100 HINGE BASE (BLUM LARGE) 12 15.1 #52 GA436-5B 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-IF RCPT, D-SUB. 9-SOCKET I 15.1 #56 GAR835NKI RELAY I 15.1 #57 65009-001-513 SOCKET I 15.1 #58 (7.1716E0ID-513 DEU COMPOSITE TERMINATION i SYSTEM 15.1 #59 1-480698-0 PLUG I 15.1#611 ABMM-A-C CABLE, TIE MOUNT 20 15.1 #61 1032JI9-24 B/R INSERT, THREADED 50 15.1#62 225791-3 INSERT, SIZES FOR RGI88 2 15.1 #63 P18350-001 TERRETRIAL MODEM ANTENNA I 15.1 #64 D38999/26FDI9SN CONNECTOR. PLUG I 15.1 #65 D38999/26FC4PN CONNECTOR I 15.1 #66 AS21919WDG23 CLAMP I 15.1#67 M53367-I-9 STRAP. TY WRAP 1.000 15.1 #68 NASI802-3-13P SCREW, HEX HD, CRUCIFORM REC, 10 FULL THD, A286 CRE.S 15.1 #69 NASI802-3-8P SCREW 10 15.1 #70 MS210421.3 NUT 20 15.1#71 NAS1149F0332P WASHER. FLAT STEEL 30 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). Printed: 3/9/2018 4:29:22PM Page 25 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811229 Bill To: Plan D, LW. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity 15.1 #72 NASI802-3-10P SCREW. HEX HD, CRUCIFORM REC, 10 FULL THD, A286 CRES 15.1 #73 NIS27039C0807 SCREW-MACHINE, CRES PAN HD, 10 STRL 15.1#74 NASI149FN832P WASHER, FLAT STEEL 10 15.1 #75 MS25083-7BBI I 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 O-RING 2 15.1 #80 E1257-70/2-015 0 RING RUBBER 2 15.1 #81 NASI580C3T12 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 CT.S-S20/20 CONTACT 30 15.1 #86 XP-610 PRINTER, EPSON I 15.1#87 ABMM-A-C CABLE, TIE MOUNT IS 15.1 #88 M24308/4-IF CONNECTOR I 15.1 #89 MS35207-269 SCREW 6 15.1 #90 D436-36 SLEEVE 200 15.1 #91 GAC860K-I 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 1 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 GAN10%1032 NUT 100 15.1 #103 NASI149D0316H WASHER 100 15.1 #104 NA51149F0363P WASHER. FLAT STEEL 100 15.1 #105 NA51149F0332P WASHER. FLAT .STEEL 100 15.1 #106 GAS805K3 SPLICE 30 15.1#107 GAC860N08 CAP D300-08 30 15.1 #108 GAC860NI2 CAP 30 15.1#109 GAC860NI8 CAP, SPLICE 30 15.1#110 VS-08-RJ45-5-Q/IP20 CONNECTOR, RJ45 (GRAY) 15 15.1 #111 M81969-1-01 INSERT/EXTRACT GREEN/WHITE 8 METAL 15.1 #112 91066-4 EXTRACTOR TOOL 8 15.1#113 M81969-14-0I EXTRACTOR, GREEN/WHITE 12 PLASTIC 15.14114 N181969/14-10 TOOL, ORANGE/RED INSERTION 15 AND EXTRACTION 15.1 #115 NII5570-22-I TOOL 15 15.1 #116 NIS27039C1-12 SCREW, PAN HEAD, X RECESSED 4 15.1#117 294-541 EXTRACTOR, AMOHENOL 1 15.1 #118 GAR100B2B0063 RUBBER .063 SHEET 5 15.1 #119 1159AV33022-5 CIRCUIT BREAKER ASSEMBLY 1 (ESDS MATERIAL) 15.1 4120 58T-101 EATON EXTRACTION TOOL 1 15.1 #121 43031-0009 PIN IS 15.1.5#1 GC524980001-121 BRACKET ASSEMBLY 2 15.1.5 #2 MS24694555 SCREW. 100 DEGREE CSK 30 STRUCTURAL 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). Printed: 3/9/2018 4:29:22PM Page 26 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811230 Bill To: Plan D, LW. WO 4: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity 15.1.5 #3 M527039-1-04 SCREW. PAN HEAD MACHINE 30 15.1.5 #4 GSM805001267-101 ANGLE 2 15.1.5 85 GSIM806002351-101 BRACKET 2 15.1.5 #6 CB200-40 ADHESIVE, ACRYLIC (DUAL PACK 3 CARTRIDGE) PLUNGER PLA050-10 40 ML 15.1.5 #7 021200-50009 NOZZLE, STATIC MIXER, SHORT 100 GOLD NOZZLE FOR 1.5OZ 15.1.5 #8 CCSI005-09-48.00 ANGLE I 15.1.5 #9 CCSI005-33-48.00 ANGLE I 15.1.5 #10 NASI836-06-10 INSERT 20 15.1.5 #11 MS35206-226 SCREW 20 15.1.5 #12 TC141 BRACKET, TIE-DOWN 20 15.1.5 #13 MS21266-77 GROMMET, PLASTIC, EDGING 2 15.1.5 #14 MS3339-4-9 PLATE MOUNTING 5 15.1.5 #15 1.41520470AI-5N RED RIVET 25 15.1.5 #16 NAS1149DN832J WASHER 25 15.1.5 #17 GAB51IGA3-4 BOLT 100 15.1.5 #18 GAB51IGA3-6 BOLT 100 15.1.5 #19 GAB511GA3-7 HI-BOLT 100 Services: Ref. No. Description Quantity 15.1.1 #1 RFE. M. Eddy. 15.1.1, 3.0 hrs, 11/27 - 12/03/2017 1.00 15.1.2 #1 AETS. Molnar. 15.1.2, 1.0 hrs, 1/22 - 1/28/2018 1.00 Step: 15.1.1 Completed Avionics Engineering Labor Avionics Step: 15.1.2 Completed Mech Engr 1.abor Avionics Step: 15.1.3 Completed AVI Systems Test Labor Only Step: 15.1.4 Completed AVI /Electrical Labor Only Step: 15.1.5 Completed AVI Sheet Metal Labor Only 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 I 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 88 15.8.1.1 Step: 15.1.6 Completed LNT Support (R&R) Labor Only Step: 15.1.7 Completed SC Maintenance/Hangar / Primary Codes /Touch Labor Only Step: 15.1.8 Completed SC Paint Labor Only Step: 15.1.9 Completed Inspection Labor Only Step: 15.1.10 Completed Weight and Balance Labor Only Item: 16 KA BAND HARNESS FABRICATION Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Item: 17 ASC 085A X94 Weather Installation - (Ref. Item B 2.3 of Proposal 'DM 7038248 R02) Team Manager: Charles Thomas Pan/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSN/TSO: CSN/CSO: 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). Printed: 3/9/2018 4:29:22PM Page 27 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811231 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Discrepancy: 17.1 ASC 085A XM 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 XN1 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 Gulfstream at asc.softwareCtgulfstream.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 Gulfstream Aircraft Scheduling at 800-810-GULF (4853) or 912-965—$178. 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 CMP 970851 Billing Method Hours Rate Total Labor USD: Flat Rate $16,060.00 Pans USD: Flat Rate $63,940.00 Total USD: $80,000.00 Pans: Ref. No. Pan number: Description Quantity 17.1 #1 ASC085A-1 GSSP KIT, XM SATELLITE WEATHER 1 INSTALLATION, 5001-SUB(KIT ONLY) 17.1 #2 RGI42B/U COAX 35 17.1#3 HET-A-02C FERRULE, SHIELD 6 17.1 #4 PLC131-58 TYRAP 10 17.1 #5 BTS722 RCPT, RFTNC I 17.1 #6 CTS722 CONNECTOR I 17.1 #8 M24308/4-IF CONNECTOR I 17.1 #9 GAC835MR20S CONTACT 10 17.1#10 C55722 PLUG, SMA, STRAIGHT I 17.1#11 CSR722 PLUG, SMA,90° I 17.1 #12 CTS722 CONNECTOR I 17.1 #13 MS21919WDG2 CLAMP 4 17.1 #14 MS21919WDCA CLAMP PTYPE-CUSHIONED,1/4 IN 4 17.1#15 MS21919WDG3 CLAMP P TYPE-CUSHIONED, 3416 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 28 of 63 Set 01 EFTA00811232 Bill To: Plan D, LW. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Part number: Description 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 TOOL 1 Item: 18 ASC 912 and ASC 123 Planeview MOS Upgrade - (Ref. Item B 2.4 of Proposal ID# 7038248 R02) Team Manager: Charles Thomas Pan/Model 8: Customer Coordinator: Julian Brown 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 29 of 63 Set 161 EFTA00811233 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 18.1 81 ASC912-I GSSP KIT, INDICATING/ RECORDING 1 $0.00 $0.00 PLANEVIEW MOS UPDATE, 5001-5549 18.1 82 ASC123-I GSSP 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 Gulfstream 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. Gulfstream 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 $163,510.00 Parts USD: Flat Rate $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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 30 of 63 Set 01 EFTA00811234 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 &niers USD: Flat Rate $470,155.00 Total USD: 5702,649.00 Pans: Ref. No. Part number: Description Quantity 19.1 #1 M520-01437 STAIN, RAW UMBER PENETRATING 2 19.1 #2 NI520-2247 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 911.1 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 IMAGECAST, 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 S-4QTR-SAWN-MOZAMBI( 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 31 of 63 ucw EFTA00811235 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: 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 1453 929-91-3.51 HARDENER,GLASURIT FINISH 1 19.1 1454 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawkslnvoice.rpt v3 Page 32 of 63 ucw EFTA00811236 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Part number: Description 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). Printed: 3/9/2018 4:29:22PM Page 33 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811237 Bill To: Plan D, LLC. WO tt: 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 2/4 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). Printed: 3/9/2018 4:29:22PM Page 34 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811238 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Step: 19.1.9.10 Completed Labor to Veneer - FWD Pocket Door. Step: 19.1.9.11 Completed Labor to Veneer - FWD LH and RH Bulkheads. Step: 19.1.9.12 Completed Labor to Veneer - PSU Hand Rails. Step: 19.1.9.13 Completed Labor to Veneer - FWD Crew Refresh Cabinet. Step: 19.1.9.14 Completed Labor to Veneer - FWD RH Lay. Step: 19.1.9.15 Completed Labor to Veneer - LEER and Reer Panels. Step: 19.1.9.16 Completed Labor to Veneer - Acoustic Doors. Step: 19.1.9.17 Completed Labor to Veneer - Entry Bulkheads (2) Step: 19.1.9.18 Completed Labor to Veneer -AFT Lav Door. Step: 19.1.9.19 Completed Labor to Veneer - FWD Lay Door. Step: 19.1.9.20 Completed Labor to Veneer - Console Tables. Step: 19.1.9.21 Completed 1.abor to Veneer - Magazine Racks. Step: 19.1.10 Completed Wood Shop Labor to Assemble Cabinets. Step: 19.1.10.1 Completed Labor to Assemble - LH and RH 680 Bulkheads and Door. Step: 19.1.10.2 Completed 1.abor to Assemble -AFT Lay Niche and Shroud. Step: 19.1.10.3 Completed Labor to Assemble - AFT Lay Vanity. Step: 19.1.10.4 Completed Labor to Assemble -AFT LH Closet. Step: 19.1.10.5 Completed 1.abor to Assemble - AFT RH Closet. Step: 19.1.10.6 Completed Labor to Assemble - AFT LH Galley. Step: 19.1.10.7 Completed Labor to Assemble - AFT RH Galley Annex. Step: 19.1.10.8 Completed 1.abor to Assemble - 4 Divan End Cabinets. Step: 19.1.10.9 Completed Labor to Assemble - Cabin Ledges. Step: 19.1.10.10 Completed 1.abor to Assemble - Console tables. Step: 19.1.10.11 Completed 1.abor to Assemble - FWD Pocket Door. Step: 19.1.10.12 Completed 1.abor to Assemble - FWD LH and RH Cabin Bulkheads. Step: 19.1.10.13 Completed Labor to Assemble - FWD Crew Refresh Cabinet. Step: 19.1.10.14 Completed Labor to Assemble - FWD RH Lim Step: 19.1.10.15 Completed Labor to Assemble - Leer and Reer Panels. Step: 19.1.10.16 Completed Labor to Assemble - Acoustic Doors. Step: 19.1.10.17 Completed Labor to Assemble - AFT Lay Door. Step: 19.1.10.18 Completed Labor to Assemble - FWD Lay Door. Step: 19.1.11 Completed ***Entered in Error******* Flammability Data. Step: 19.1.12 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. R/H #1 P/N 1159SCCE500-23 S/N 0702030 R/H #2 P/N 1159SCCE500-23 S/N 0701885 Step: 19.1.12.1 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 Step: 19.1.12.2 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 Step: 19.1.12.3 Completed CMP G550 562115 Cabin Windows- Leak Check Ref.11.143 Step: 19.1.12.4 Completed CMP G550 560001 Emergency Window Release Mechanism - Functional Test Ref.11.144 Step: 19.1.12.5 Completed CMP 6550 304110 CABIN WINDOW HEAT - 0PS TEST Ref.11.145 Step: 19.1.12.6 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. Step: 19.1.13 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). Printed: 3/9/2018 4:29:22PM Page 35 of 63 Set 01 GAC_RevenueSquawksinvoicc.rpt v3 EFTA00811239 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. AA 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 Part/Model Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSN/TS0: CSN/CS0: 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 #13A 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 S15.30 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 36 of 63 urns EFTA00811240 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: Charles Thomas Pan/Model 8: Customer Coordinator: Julian Brown 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). Printed: 3/9/2018 4:29:22PM Page 37 of 63 Set 01 liAC_RevenueSquawksInvoice.rpt v3 EFTA00811241 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 38 of 63 Set 01 EFTA00811242 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: Charles Thomas ParUModel #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Item: 23 Miscellaneous CMP Tasks (Exhibit 3) - (Ref. Item C 1.3 of Proposal ID# 7039702 ROO) Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 23.1 Accomplish Miscellaneous CMP Tasks (Exhibit 3) Notes: Correction of discrepancies is not included in the quoted price. Materials! Outside Services will be billed as required. Resolution: Complied with Customer Requested Miscellaneous CMP Tasks. See squawks below for details of all work accomplished. Billing Method Hours Rate Taal Labor USD: Flat Rate 58.953.00 Total USD: 58.953.00 Discrepancy: 23.12 CMP G550 282651 Main Fuel Boost Pump (Left) - Fuel Leak Check Resolution: COMPLIED WITH CMP 6550 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 Parts USD: Time and Material $1.88 Total USD: 51.88 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 23.12 #1 NASI612-3A 0 -RING, 0.188 INCH OD TUBING 4 50.47 51.88 Discrepancy: 23.17 CMP 6550 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 Charge N/ C Pans USD: Time and Material $2.86 Total USD: 52.86 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 23.17#1 NASI612-4A SEAL, 0.250 INCH OD TUBING 2 5030 $0,60 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 39 of 63 Set 01 EFTA00811243 Bill To: Plan D, LW. WO Si: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 23.1782 2-212 E0540-80 SEAL-0 RING 2 $1.13 $2.26 Discrepancy: 23.34 CMP G550 262620 Portable Halon Fire Extinguisher (Aft Cabin) - Removal / Installation Resolution: COMPLIED WITH CMP G550 262620 Portable Helen Fire Extinguisher (Aft Cabin) - Removal / Installation Billing Method Hours Rate Total Parts USD: Time and Material S3.15 Total USD: S3.15 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 2334 01 14776 STRAP AND CLAMP ASSY 1 $3.15 $3.15 Discrepancy: 23.43 CMP G550 351222 Passenger Oxygen Cylinder (No. 2)- Removal / Installation Resolution: COMPLIED WITH CMP 6550 351222 Passenger Oxygen Cylinder (No. 2)- Removal / Installation Billing Method Hours Rate Total Labor USD: No Charge N/C Parts USD: Time and Material S531 Total USD: S531 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 23.43 01 hIS21044C08 NUT SELF LICG-CRES.FASSIVATED $0.41 $0.41 23.43 02 hIS21044C3 NUT $4.90 $430 Item: 24 Discrepancies related to Miscellaneous CMP Tasks (Exhibit 3) - (Ref. Item C 13 of Proposal ID# 7039702 ROO) Team Manager: Charles Thomas Part/Modcl te: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 24.3 2 Bruce Batts failed cap check and require replacement. Refer to items 31.1 and 33.1. Resolution: Ordered and recieved New Bruce Batts. Ref Items 23.35 and 23.37 Billing Method Hours Rate Total Pans USD: Time and Material $2,810.64 Total USD: $2,810.64 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 243 91 2013-BR BATTERY, EMERGENCY LIGHTS 2 51,40532 $2,810.64 Discrepancy: 24.4 (I) passanger 02 mask has a broken valve and (I) passenger 02 mask has a broken lanyard. Ref 23.44 Resolution: Removed and replaced (2ea.) o2 masks. PN On/Off: 289-601-224-1 Ref. G550 AMM 35-25-01 dated June 15, 2016 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). Printed: 3/9/2018 4:29:22PM riAC_RevenuaquawksInvoice.rpt v3 Page 40 of 63 Set 161 EFTA00811244 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Billing Method Hours Rate Total Labor USD: Time and Material ST 6.50 @ $146.00 $949.00 Pans USD: Time and Material S159.46 Total USD: 51,108.46 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 24.4 #1 289-601-224-1 MASK 2 $79.73 S159.46 Discrepancy: 24.5 One light bulb from "No smoking" light on cabin PSU #5 LH and One light bulb from "No smoking" light on cabin PSU #1 RH did not illuminate during test Ref. 23.44 Resolution: Removed and replaced light bulb from "No smoking" light on cabin PSU #5 LH and light bulb from "No smoking" light on cabin PSU #1 Rif. Ops ck good. PN on/off GE387 Billing Method Hours Rate Total Pans USD: Time and Material $3.50 Total USD: $3.50 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 24.5#1 GE387 BULB SlA GE387 10 5035 53.50 Discrepancy: 24.7 Cabin drop down 02 mask has a tear in rubber .Re 24.6 Resolution: Removed and installed new cabin oxygen mask PN 289-601-224-1 during operational test. Ref item 11.156 Billing Method Hours Rate Total Pans USD: Time and Material $79.73 Total USD: $79.73 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 24.7 #1 289401-224-1 MASK 1 $79.73 519.73 Item: 25 Replace all Main and Nose tires - (Ref. Item C 1.5 of Proposal ID# 7039702 ROO) Team Manager: Charles Thomas Pan/Model Of: Customer Coordinator: Julian Brown AC Serial No./Tail No.: TSN/TSO: CSNJCSO: Aircraft Time: Discrepancy: 25.1 Remove and Replace all main and nose landing gear tires. Resolution: Summary: Removed all MIA: wheel assemblies (4ea.) and NLG (2ca.) and routed to back shop for tire changes and NDT, reference items 34,35,3637,38 and 39 for work performed in the back shop. Received wheels after tire change and installed on aircraft, Reference items 11.58 thru 11.61 for MLG wheel assembly WI CMPs and 11.93 and 11.94 for NLG wheel assy. WI CMPs See steps below Billing Method Hours Rate Total Labor USI) Flat Rate $2,686.00 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). Printed: 3/9/2018 4:29:22PM Page 41 of 63 Set 01 riAC_RevenueSquawksInvoice.rpt v3 EFTA00811245 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans USD: Flat Rate 415,350.00 Total USD: 418,036.00 Step: 25.1.1 Completed Removed main wheels (4) and routed to back shop. Ref items 11.58 thru 11.61 Step: 25.1.2 Completed Removed nose wheels per 6550 ChIP 324001 and 6550 CMP 324002 and routed to back shop for tire replacement. Step: 25.1.3 Completed Installed red wheels on NW per AMM 6550 32-41-01 rev 3/31117 TW: 560296 Cal Due: 04/18 Step: 25.1.4 Completed Removed 1./11 and R/H NW red wheels. Received ok to install and Installed L/H NLG Wheel Assy P/N 1159150400-37 S/N 508117 per CMP (350 324002. Received ok to install and installed R/11 NLG Wheel Any P/N 1159130400-37 S/N 5082F2 per ChIP (350 324003. Serviced LAI and RAI NLG Wheels to 120PS1 per 6550 AMM 12-33-01 Rev. June 20/13. Step: 25.1.5 Completed Installed main wheels (4) LAW 6550 CMPs 324003,324004,324005. and 324006. Ref items 11.58 thru 11.61 Item: 26 CUSTOMER PROPERTY OUT TO VENDOR Team Manager: Charles Thomas Customer Coordinator: Julian Brown S/N: N/A TSN/TSO: N/A CSN/CSO: N/A Aircraft Time: N/A Discrepancy: 26.1 SEND BLOW DOWN BOTTLE TO SUPPLIER FOR HYDROSTATIC TEST AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N4I5LM REQUESTED RETURN DATE - 11/9 Resolution: Hecieved Blow Down Bottle Billing Method Hours Rate Total Services USD: Flat Rate $270.60 Total USD: $270.60 Services: Ref. No. Description Quantity 26.1 #1 HYDROSTATIC TEST 1.00 Part Ref: 1159SCH233-1I BOTTLE, NITROGEN - BLOW DOWN BOTTLE Discrepancy: 26.2 SEND 02 BOTTLE TO SUPPLIER TO COMPLY WITH HYDROSTATIC TEST AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N4I5LM REQUESTED RETURN DATE - II/II Resolution: Recto ed O2 Bottle. Billing Method Hours Rate Total Services USD: Flat Rate 52.527.80 Total USD: 52.527.80 Services: Ref. No. Description Quanti”, 26.2 #1 HYDROSTATIC TEST 1.00 Part Ref: 805983-15 BOTTLE. OXYGEN 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). Printed: 3/9/2018 4:29:22PM Page 42 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811246 Bill To: Plan D, LLC. WO SC52166I Invoice Number: 5517132452 Discrepancy: 26.3 SEND 02 MASK TO SUPPLIER FOR RESTORE/RECERTIFYAND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N415LM REQUESTED RETURN DATE 11/24 Resolution: Recieved O2 Mask Billing Method Hours Rate Total Services USD: Flat Rate $2,392.50 Total USD: $2,392.50 Services: Ref. No. Description Quantity 263 #1 REPAIR 1.00 Part Ref: MC10-15-158 MASK, OXYGEN, CREW Discrepancy: 26.5 SEND 18 EA LIFE VEST TO THE SUPPLIER FOR RESTORE AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N415LM REQUESTED RETURN DATE - 2/20 PN - 63600-105 SN - L784996, L748997, L784998, L784999, L785000, L785001. L785002, L785003, L785004, L785006, L785007, L785008, L785009, L785010 AND L785011 PN - 63600-505 SN - L785711, L745141. L785710 Resolution: Received 18 each repaired life vests Billing Method Hours Rate Total Services USD: Time and Material $884.17 Total USD: $884.17 Services: Ref. No. Description Quantity Sell Price USD Extended USD 263 HI REPAIR 1.00 5884.17 S884.17 Part Ref: AC5173LIFEVESTKIT LIFE VEST KIT Discrepancy: 26.6 SEND CUP HOLDERS AND DOOR HANDLE TO QUAKER CITY TO BE PLATED QCPSSS SATIN BLUSHED WHITE GOLD AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N415LM REQUESTED RETURN DATE - 2/26/2018 Resolution: Received plated cup holders. 222/18- Per the PO in Corridor It is tracking for 2-26 confirmed by Courtney. CC Billing Method Hours Rate Total Services USD: Time and Material 31,500.00 Total USD: 31,500.00 Services: Ref. No. Description Quantity Sell Price USD Extended USD 26.6 #1 PLATING 1.00 S0.00 50.00 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 43 of 63 Set 161 EFTA00811247 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Services: Ref. No. Description Quantity Sell Price USD Extended USD Part Ref: AC5173PLATINGKIT KIT 26.6 #2 EXPEDITE FEE 1.00 $1,500.00 $1,500.00 26.603 PLATING 1.00 50.00 $0.00 Part Ref: AC5173PLATINGKIT KIT Item: 27 AIRCRAFT BATTERY (FCS EBHA BATTERY & MAIN SHIP BATTERY) Team Manager: Charles Thomas Pan/Model #: 1159SCAY519-1 Customer Coordinator: Julian Brown S/N: 0905200069DDF TSNEIS0: N/A CSN/CS0: N/A Aircraft Time: N/A Item: 28 AVIATION BATTERY TYPE - CORE (FCS EBHA BATTERY & MAIN SHIP BATTERY) Team Manager: Charles Thomas Part/Model #: 5317C11-I Customer Coordinator: Julian Brown S/N: 09052001067B3 TSNfIS0: N/A CSN/CS0: N/A Aircraft Time: N/A Item: 29 FAIRING ASSY, BULLET, FWD Team Manager: Charles Thomas Part/Model #: 1159CSII52024-405 Customer Coordinator Julian Brown S/N: N/A TSN/TS0: N/A CSN/CS0: N/A Aircraft Time: N/A Discrepancy: 29.1 FWD BULLET FAIRING (KNEE PANEL) HAS EVIDENCE OF EROSION AT FWD EDGE AROUND FWD EDGE AROUND FWD LOOKING CAMERA AND A PUNCTURE INSIDE OF FAIRING. AREAS !WAKED WITH BLUE GREASE PENCIL. IRAN AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N4I5LM REQUESTED RETURN DATE - 11/17 Resolution: Repaired satcom radome. Reference: Engineering dispo in step 29.2.1.1 and B/P 1159C51152024 Rev.D 1/17/06 Engineering dispos in steps 29.3.8 and 29.3.10. FWD BULLET FAIRING Part# ->1159CSII52024-405 Ser# Final finish will apply at service center. Billing Method I lours Rate Total Labor USD: Time and Material ST 68.78 (it $146.00 $10,041.88 Labor USD: Time and Material ST 1.02 (a $222.00 S226.44 Parts USD: Time and Material 42,318.91 Total USD: $12,587.23 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 29.101 ISSQW00-0460 LIGHTNING D1VEFtTER I $772.97 S772.97 29.102 ISSQW00-0460 LIGHTNING D1VERTER I $772.97 $772.97 29.103 ISSQW00-0460 LIGHTNING DIVERTER I $772.97 $772.97 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). Printed: 3/9/2018 4:29:22PM DAC_RevenueSquawksInvoice.rpt v3 Page 44 of 63 Set 01 EFTA00811248 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Step: 29.1.1 Completed Incoming Inspection Step: 29.1.2 Completed Teardown Step: 29.1.3 Completed Inspection Step: 29.1.4 Completed Rework Step: 29.1.5 Completed Assembly Step: 29.1.6 Completed Test Step: 29.1.7 Completed Refinish Step: 29.1.7.1 Completed Made Mytar Step: 29.1.7.2 Completed Apply IOP2-3 anti-static coating Step: 29.1.7.3 Completed Strip-Sand and prime with 3012 / D-8003 Hi-Bu0d.Apply 10P2-3 Anti-Static.Re-prime with 3012. Step: 29.1.7.4 Completed Apply IOP2-3 Anti-Static. Perform resistivity test. Step: 29.1.8 Completed Outgoing Imagery Discrepancy: 29.2 Erosion along the leading edge and diverter strips. Resolution: Repaired erosion along the leading edge and replaced all diverter strips. Reference: Engineering dispo in step 29.2.1.1 and B/P 1159CSII52024 Rev. D.U17/06. Billing Method Hours Rate Labor USD: lime and Material ST 2.00 @ 5222.00 5444.00 Total USD: 5444.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document arc in US Dollars (USD). Printed: 3/92018 4:29:22PM tiAC_RevenuaquawksInvoice.rpt v3 Page 45 of 63 &tot EFTA00811249 Bill To: Plan D, LLC. WO 4: SC521661 Invoice Number: 5517132452 Step: 29.2.1 Completed Request engineering evaluation for repair of erosion. Step: 29.2.1.1 Completed Engineering disposition: Remove lightning diverter and hardware as required. Sand eroded areas smooth. Scuff sand minimum 1.50in around areas to be repaired. removing all glossy surfaces, to prepare for wet lay up. Fabricate two plies using plies of 161/181sts le dry fiberglass cloth. Size plies to ensure coverage of eroded and sanded regions. Ply #1 should extend at least 1.00in beyond the reworked area and Ply #2 should extend at least .50in beyond Ply al. except plies may end at edge of part where applicable. Saturate Plies 1 and 2 with Shell Epon 828/DTA or Hysol EA956A/B mixed per manufacturer's instructions. Lay up rework areas with Ply #1 and Ply #2 ensuring adequate overlap as specified above. Cure plies under vacuum bag at 75-95°F for at least 12 hours, or under vacuum bag at 75-95°F for at 2-3 hours followed by 3 hours at 130-140°F. Remove vacuum hag and sand smooth. Visually inspect reworked area: if required. fill and fair using 11>sol EA960F and sand to contour. If required, install lightning diverter as described below. Touch up with primer and paint to match customer topcoat, as required. Lightning diverter installation: Prepare surface to be bonded per CAMPS 8210: scuff sand then solvent wipe with MEN or acetone followed by isopropyl alcohol. Apply GAA100BDI0 or GAAI00BD03 adhesive and position diverter per 1159C5H52024. Cure under vacuum bag for 7 days at room temperature, or 2-3 hours at room temperature followed by 2 hours at 130-140°F. Step: 29.2.2 Completed REMOVED PAINT/PRIMER FROM DISCREPANT FWD AREAS AND SOLVENT CLEANED. THEN FABRICATED AND INSTALLED 2 PLIES OF STYLE 181 FIBERGLASS WET USING EPON 828fDTA. VACUUM BAGGED AND CURED. REF ENGINEERING DISPO STEP 29.2.1.1 Step: 29.2.3 Completed Removed and replaced all diverter strips(P/N LSSQW00-0460). Reference: B/P 1159O:1152024 Rev. D Released 1/17/06. Discrepancy: 29.3 Puncture on Lill Inner surface. Resolution: Repaired puncture on Lill Inner surface. Reference: Engineering dispos in steps 29.3.8 and 29.3.10. Billing Method Hours Rate Total Labor USD: Time and Material ST 18.00 €2; 5222.00 53,996.00 Total USD: 53,996.00 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). Printed: 3/9/2018 4:29:22PM Page 46 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811250 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Step: 293.1 ( moulded Request engineering evaluation for repair of inner skin puncture. Step: 293.2 ( moult:Ertl Request NDT to perform tap test of inner skin puncture. Step: 2933 ( moult:Ertl Preliminary Engineering Disposition: Refer to pic in the "files" tab for suspect location of contact area. Place a soft compressible material (clay, repro-rubber. etc.) that will retain location and determin if this is the contact area. Install fwd bullet fairing and attach with B/P hardware. Remove fairing and take pits of suspect contact area. Resubmit pies via Corridor to engineering for evaluation. MRB No. E064 Step: 29.3.4 ompleted Per preliminary engineering disposition placed a soft compressible material (repro-rubber) on the contact area. Installed fwd bullet fairing and attach with B/P hardware. Removeed fairing and took pits of suspect contact area. Resubmited pies to engineering. Step: 29.3.5 ompleted Preliminary Engineering Disposition: Refer to pic in the" Files" tab drill a No. 30 at the location shown. Take a measurement from the inner surface of outer skin to the outer surface of inner skin. Resubmit results to engineering for Final disposition. MRS No. F.064 Step: 293.6 Completed Resubmit engineering after measurement from the inner surface of outer skin to the outer surface of inner skin is .240" Step: 293.7 Completed Preliminary Engineering Disposition: Refer to attachment in the "Files" tab: using the smallest clean up diameter. represented by the red dash line, trim out the discrepant section of inner skin and associated core down to the bond surface of outer skin. Do not undercut the outer skin or incorporate core ramp at this time. Measure, document, and resubmit resulting clean up dia. MRB E064 Step: 293.8 Completed Final Engineering Disposition: Rework per Steps I thru 13. NOTE. -Steps 9 thru 13 are in 29.3.9. Cutout of the inner skin and core removal is acceptable. Proceed with following rework: I. Refer to "Files" Powerpoint attachment Section A-A in 29.3.7. Incorporate core ramp that starts from edge of cutout extending .25 to .35 inches beyond cutout. At the lower EOP it is acceptable for the chamfer to extend onto the solid laminate. 2. Straighten out folded over core cells and remove loose cells. Vacuum out debris. 3. Pot core ramp with Magnobond 68-3. Cure at 70 to 95F' until potting has a harden surface. Do not touch sanded surfaces with bare hands. wear clean cotton gloves. 4. Solvent clean using fresh cheesecloth wipers wet with MEK or Isopropyl Alcohol an area extending at least 2.0 inches beyond cutout or to EOP. whichever is closer. Continue until wipers remain clean. Do not use synthetic or shop towel wiper materials. Also solvent clean a corresponding area on outer skin. 5. Sand off excess potting. Sand inner bond surface to remove core stubble and any glossy surface finish, also extend sanding around skin cutout over an area extending from lower EOP or at least 2.0 inches beyond edge of cutout to expose the outer fiberglass (F/G) ply. Vacuum out debris. Traces of paint, primer. etc. remaining within the F/G weave shall be acceptable. 6. Sand correspond outer skin surface in the same way. 7. On inner skin add two plies of dry Style 181 (F/C). Orientation of both plies is optionaL It is acceptable to dart F7G to allow working out wrinkles. Stagger darts so they do not overlap onto each other. Saturated plies with Epon 828 / DTA or EA956 MB. Refer to SRM 51-34-00 Table 1 and SRM 51078-10 Repair Technique 7. 8. Refer to Files tab in 29.3.7. Ply I shall overlap .50 to .80 inch onto the inner surface. Ply 2 shall overlap Ply 1 by .50 to .80 inches. Disposition continues in 29.3.9 MRB No. E064 Step: 29.3.9 Completed Final Engineering Disposition Continued from 29.3.8. 9. On outer surface add like plies centered over cutout. 10. Install a breather pack and vacuum bag. refer to SRM51-78-10 Repair Technique 8. Perform a vacuum leak check by pulling full vacuum (min 21 inches of Hg) until bag is pulled tight. Disconnect vacuum source and verify max leakage rate does not exceed 5 inches of Hg within 5 minutes. II. Cure at 70 to 95F until adhesive gels which should take at least 4 hours. 12. After cure remove bag and sand off excess adhesive and F'/G. Tap test outer and inner skin within repair area to verify no voids and I or disbands exist. Also visually verify no ply separations exist. 13. On outer surface apply Finish 3012 (CAMPS 3116) followed by anti-static paint and customer topcoat. Ensure applied anti-static paint overlaps onto the existing anti-static paint. On inner surface no finish is required unless dry surfaces exist and if so apply Finish 3012 to entire repaired surface. This is a minor repair. MRB No. E064 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). Printed: 3/9/2018 4:29:22PM Page 47 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811251 Bill To: Plan D, LLC. WO tr: SC521661 Invoice Number: 5517132452 Step: 293.10 Completed Made core ramp and potted core with Magnobond 68-3. Cured at 70 to 95F until potting has a harden surface. Solvent cleaned, sanded off excess potting. Sanded inner bond surface and extend sanded around skin cutout over an area. On inner and outer skin added two plies of dry Style 181 (FIG). Saturated plies with Epon 828 / DTA. Install vacuum bag, performed a vacuum Ink cheek and cured at 70 to 95F. After cured remove bag and sand off excess adhesive and F/C. Tap tested outer and inner skin within repair area to verified no voids and I or disbands exist. Also visually verified no ply separations exist. Work reference:Engineering dispo in steps 29.3.8 and 29.3.10. item: 30 Addition of a SIIADE MASTER at the Right-Hand #2 VIP Seat - (Ref. Item B 1.1 of Proposal ID#7038565 ROO ) Team Manager: Charles Thomas Part/Model #: Customer Coordinator Julian Brown AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Item: 31 BATTERY, EMERGENCY LIGHTS Team Manager: Charles Thomas Part/Model #: 2013-BR Customer Coordinator: Julian Brown S/N: B8662 TSWISO: N/A CSN/CSO: N/A Aircraft Time: N/A Item: 32 BATTERY, EMERGENCY LIGHTS Team Manager: Charles Thomas Part/Model /I: 2013-BR Customer Coordinator Julian Brown S/N: B8663 TSN/TSO: N/A CSN/CSO: N/A Aircraft Time: N/A Item: 33 BATTERY, EMERGENCY LIGHTS Team Manager: Charles Thomas Part/Model If: 2013-BR Customer Coordinator: Julian Brown S/N: B8660 TSWISO: N/A CSN/CSO: N/A Aircraft Time: N/A Item: 34 MAIN WHEEL Team Manager: Charles Thomas Pan/Model 1159SCL503-9 Customer Coordinator Julian Brown S/N: 5159FX TSN/TSO: N/A CSN/CSO: N/A Aircraft Time: 5402.8 / 1725 Item: 35 MAIN WHEEL ASSEMBLY Team Manager: Charles Thomas Part/Modcl 1159SCL503-7 Customer Coordinator: Julian Brown S/N: 5167FP TSNffSO: N/A CSN/CSO: N/A Aircrafaime: 5402.8 / 1225 Item: 36 MAIN WHEEL Team Manager: Charles Thomas Part/Model 1159SCL503-9 Customer Coordinator Julian Brown S/N: 5175GC TSNEISO: N/A CSN/CSO: N/A Aircraft lime: 5402.8 / 1225 For detail description of the work complied with see the \Vora. Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoicc.rpt v3 Page 48 of 63 Jet dm EFTA00811252 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Item: 37 MAIN WHEEL ASSEMBLY Team Manager: Charles Thomas Pan/Model 1159SCL503-7 Customer Coordinator. Julian Brown S/N: 5188FP TSNffS0: N/A CSN/CS0: N/A Aircraft Time: 5402.8 11225 Item: 38 NOSE WHEEL/TIRE ASSEMBLY-MOUNTED 1159L50400-37 Team Manager: Charles Thomas Part/Model #: 1159SCL505-7MTD Customer Coordinator: Julian Brown S/N: 5082FZ TSWIS0: N/A CSN/CS0: N/A Aircraft Time: 5402.8 Item: 39 NOSE WHEEL/TIRE ASSEMBLY-MOUNTED 1159L50400-37 Team Manager: Charles Thomas Pan/Model 1159SCL505-7MTD Customer Coordinator Julian Brown S/N: 508IFZ TSNfIS0: N/A CSN/CS0: N/A Aircraft lime: 5402.8 Item: 40 Customer Requested Due List Items as of 02/15/18 Team Manager: Charles Thomas Part/Model ft: Customer Coordinator Julian Brown AC Serial No/Tail No.: N/A / N/A TSN/TS0: N/A CSN/CS0: N/A Aircraft Time: N/A Discrepancy: 40.1 CMP G550 231108 Airshow 4000 Sys Components - VI Resolution: COMPLIED WITH CMP G550 231108 Airshow 4000 Sys Components - GVI Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 40.2 CMP G550 231113 Securaplane 500 Components - GV1 Resolution: COMPLIED WITH CMP G550 231113 Securaplane 500 Components - GVI Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.3 CMP G550 232158 Airshow 4000 Above Floor - Visual Inspection Resolution: COMPLIED WITH CMP G550 232158 Airshow 4000 Above Floor - Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.4 CMP G550 240108 Fwd Emergency Battery - BITE / Battery Level Test Resolution: COMPLIED WITH CMP G550 240108 Fwd Emergency Battery - BITE / Battery Level Test 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 arc in US Dollars (USD). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 49 of 63 Set 01 EFTA00811253 Bill To: Plan D, LLC. WO #: SC52166I Invoice Number: 5517132452 Labor USD: fl at Rate 5152.00 Total USD: $152.00 Discrepancy: 40.5 CMP G550 240109 Aft Emergency Battery - BITE J Battery Level Test Resolution: COMPLIED WITH CMP G550 240109 Aft Emergency Battery - BITE Battery Level Test Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: $152.00 Discrepancy: 40.6 CMP €550 251006 Crew Scats Inertia Reel (Pilot) - Operational Test Resolution: COMPLIED WITH CMP G550 251006 Crew Seats Inertia Reel (Pilot) - Operational Test Billing Method Hours Rate Fowl Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.7 CMP G550 251007 Crew Seats Inertia Reel (Copilot) - Operational Test Resolution: COMPLIED WITH CMP G550 251007 Crew Seats Inertia Reel (Copilot) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.8 CMP G550 251008 Crew Scats Inertia Reel (Observer) - Operational Test Resolution: COMPLIED WITH CMP G550 251008 Crew Seats Inertia Reel (Observer) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.9 CMP G550 251016 Crew Seat Restraints (Pilot) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 251016 Crew Seat Restraints (Pilot) - Detailed Inspection Billing Method Hours Rate Iota' Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.10 CMP G550 251017 Crew Seat Restraints (Copilot) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 251017 Crew Seat Restraints (Copilot) - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.11 CMP G550 251018 Crew Seat Restraints (Observer) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 251018 Crew Seat Restraints (Observer) - Detailed Inspection 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 50 of 63 Set 01 EFTA00811254 Bill To: Plan D, LLC. WO it: SC521661 Invoice Number: 5517132452 Labor USD: Flat Rate 5152.00 Total USD: $152.00 Discrepancy: 40.12 CMP G550 252102 Passenger Seats Restraints - Detailed Inspection Resolution: COMPLIED WITH CMP G550 252102 Passenger Seats Restraints - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: 5152.00 Discrepancy: 40.13 CMP €550 252104 Passenger Seats Inertia Reels - Operational Test Resolution: COMPLIED WITH CMP G550 252104 Passenger Seats Inertia Reels - Operational Test Billing Method Hours Rate Fowl Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.14 CMP €550 256019 EVAS System (Leh)- Periodic Inspection Resolution: COMPLIED WITH CMP G550 256019 EVAS System (Left) - Periodic Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.15 CMP G550 256020 EVAS System (Right) - Periodic Inspection Resolution: COMPLIED WITH CMP G550 256020 EVAS System (Right) - Periodic Inspection Billing Method Hours Rate Total .:11,or t Flat Rate 5152.00 total USD: 5152.00 Discrepancy: 40.16 CMP 6550 256205 life Vest - Restore Resolution: The Squawk for this specific task shall be signed off as " Verified compliance of CMP 256205 under vender stork order number SAP017-08768 dated Feburaury 20 2018. This documentation is for CMP data base update only - no maintenance accomplished by CAC." COMPLIED WITH CMP G550 256205 Life Vest - Restore Life Vests Restored P/N: 63600-105 S/N :L784996 PIN: 63600-105 FSN :L784997 P/N: 63600-105 FSN :L784998 P/N: 63600-105 FSN :L784999 P/N: 63600-105 S/N :L785000 P/N: 63600-105 S/N :L785001 P/N: 63600-105 SfN :L785002 P/N: 63600-105 SIN :L785003 P/N: 63600-105 SIN :L785004 P/N: 63600-105 SIN :L785006 P/N: 63600-105 SIN :L785007 P/N: 63600-105 S/N :L785009 P/N: 63600-105 S/N :L785010 P/N: 63600-105 S/N :L785011 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). Printed: 3/9/2018 4:29:22PM Page 51 of 63 Set 01 riAC_RevenueSquawksInvoice.rpt v3 EFTA00811255 Bill To: Plan D, LLC. WO ft: SC52166I Invoice Number: 5517132452 Billing Method Hours Rate Total Labor USD: Flat Rate $304.00 Total USD: $304.00 Discrepancy: 40.17 CMP 6550 256404 Defibrillator Battery - Inspect / Check Resolution: COMPLIED WITH CMP 6550 256404 Defibrillator Battery - Inspect / Check Billing Method Hours Rate Total Labor USD Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.18 CMP G550 256407 Defibrillator Electrode Pads - Inspection Resolution: COMPLIED WITH CMP G550 256407 Defibrillator Electrode Pads - Inspection Billing Method Hours Rate Toed Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.19 •"*DELETE** CMP G550 256438 - LIFE KIT Resolution: Equipment not installed in aircraft, customer email approving deletion is on file Billing Method Hours Rate Taal Fiat Rate 5152.00 total t SD 5152.00 Discrepancy. 40.20 CMP G550 261302 APU (Fire) Shutdown Circuit - Operational Test Resolution: COMPLIED WITH CMP 6550 261302 APU (Fire) Shutdown Circuit - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate $304.00 Total USD: $304.00 Discrepancy: 40.21 CMP G550 262122 Engine and APU Fire Extinguishing Firing Circuitry (Left Engine) - Integrity Test Resolution: COMPLIED WITH CMP G550 262122 Engine and APU Fire Extinguishing Firing Circuitry (Left Engine) - Integrity Test multlmeter 556315 due date:9/18 Billing Method Hours Rate Total Labor USD: Flat Rate $228.00 Total USD: $228.00 Discrepancy: 40.22 CMP G550 262123 Engine and APU Fire Extinguishing Firing Circuitry (Right Engine) - Integrity Test Resolution: COMPLIED WITH CMP G550 262123 Engine and APU Fire Extinguishing Firing Circuitry (Right Engine) - Integrity Test multimeter 556315 due date:9/18 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 52 of 63 Set 01 EFTA00811256 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.23 CMP 6550 262124 Engine Fire Bottle Pressure Switch (Left) - Operational Test Resolution: COMPLIED WITH CMP G550 262124 Engine Fire Bottle Pressure Switch (Leib- Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 40.24 CMP 6550 262125 Engine Fire Bottle Pressure Switch (Right) - Operational Test Resolution: COMPLIED WITH CMP G550 262125 Engine Fire Bottle Pressure Switch (Right) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 40.25 CMP 6550 262126 Engine and APU Fire Extinguishing Firing Circuitry (APU) - Integrity Test Resolution: COMPLIED WITH CMP G550 262126 Engine and APU Fire Extinguishing Firing Circuitry (APU) - Integrity Test multlmeter 556315 due date:9/18 Billing Method Hours Rate Taal Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.26 CMP G550 262605 Portable I laion Fire Extinguisher (Cockpit) - Visual Inspection Resolution: COMPLIED WITH CMP G550 262605 Portable Halon Fire Extinguisher (Cockpit) - Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.27 CMP G550 262626 Portable Halon Fire Extinguisher (Aft Cabin) - Visual Inspection Resolution: COMPLIED WITH CMP G550 262626 Portable Helen Fire Extinguisher (Aft Cabin) - Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.28 CMP G550 262646 Portable !talon Fire Extinguisher (Aft Lavatory) - Visual Inspection Resolution: COMPLIED WITH CMP G550 262646 Portable Helen Fire Extinguisher (Aft Lavatory) - Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 53 of 63 Set 01 EFTA00811257 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Discrepancy: 40.29 CMP 6550 271011 Aileron Control and Trim Cables in Main Wheel Wells / Wing Trailing Edge - Detailed Inspection Resolution: COMPLIED WITH CMP G550 271011 Aileron Control and Trim Cables in Main Wheel Wells / Wing Trailing Edge - Detailed Inspection Tensiometer 66853 Due Date 5/18 Billing Method Hours Rate Total Labor USD: Flat Rate $304.00 Total USD: $304.00 Discrepancy: 4030 CMP 6550 272108 Rudder Control and Trim Cables in Main Wheel Well / Tail Compartment - Detailed Inspection Resolution: COMPLIED WITH CMP G550 272108 Rudder Control and Mini Cables in Slain Wheel Well / Tail Compartment - Detailed Inspection Billing Method Hours Ratc Total Labor USD: Flat Rate $304.00 Total USD: $304.00 Discrepancy: 4031 CMP 6550 273100 ELEV/TRIM CABLE(MTVW/TAIL)-INSP Resolution: COMPLIED WITH CMP G550 273100 ELEVITRIM CABLE(MWW/TAIL)-INSP Billing Method Hours Rate Total Labor USD: Flat Rate $912.00 Total USD: $912.00 Discrepancy: 4032 CMP 6550 276105 SPEEDBRAKE CABLE(MWW/WING)INSP Resolution: COMPLIED WITH CMP G550 276105 SPEEDBRAKE CABLE(MINW/WING)INSP Tensiometer 66853 Due Date 05/I8 Billing Method Hours Rate Total Labor USD: Flat Rate 5912.00 Total USD: 5912.00 Discrepancy: 4033 CMP G550 282606 Engine Feed Dual Wall Fuel Line (Left) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 282606 Engine Feed Dual Wall Fuel Line (Left) - Detailed Inspection Billing Method Mors Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 4034 CMP G550 282607 Engine Feed Dual Wall Fuel Line (Right) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 282607 Engine Feed Dual Wall Fuel Line (Right) - Detailed Inspection Billing Method Hours Ratc Total Labor USD: Flat Rate $152.00 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). Printed: 3/9/2018 4:29:22PM liAC_RevenueSquawksInvoice.rpt v3 Page 54 of 63 urw EFTA00811258 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Total USD: $152.00 Discrepancy: 40.35 CMP G550 282608 APU Feed Dual Wall Fuel Line - Detailed Inspection Resolution: COMPLIED WITH CMP G550 282608 APU Feed Dual Wall Fuel Line - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 40.36 CMP G550 282609 Engine Heated Return Feed Dual Wall Fuel Line (Left) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 282609 Engine Heated Return Feed Dual Wall Fuel Line (Left) - Detailed Inspection Billing Method Hours Rate Total Labor USD: fl at Rale $152.00 Total USD: $152.00 Discrepancy: 40.37 CMP G550 282610 Engine Heated Return Feed Dual Wall Fuel Line (Right) - Detailed Inspection Resolution: COMPLIED WITH CMP G550 282610 Engine Heated Return Feed Dual Wall Fuel Line (Right) - Detailed Inspection Billing Method Hours Rate Foul Labor USD: fl at Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.38 CMP G550 282629 Engine Fuel Shut-off Valve (Left) - Operational Check Resolution: COMPLIED WITH CMP G550 282629 Engine Fuel Shut-off Valve (Left) - Operational Check Billing Method Hours Rate Total Labor USD: Flat Rale 5152.00 Total USD: 5152.00 Discrepancy: 40.39 CMP G550 282630 Engine Fuel Shut-off Valve (Right) - Operational Check Resolution: COMPLIED WITH CMP G550 282630 Engine Fuel Shut-off Valve (Right) - Operational Check Billing Method Hours Rate Total Labor USD: Flat Rale 5152.00 Total USD: 5152.00 Discrepancy: 40.40 CMP 6550 291501 Hydraulic System Shut-off Valve (Left) - Operational Test Resolution: COMPLIED WITH CMP G550 291501 Hydraulic System Shut-off Valve (Left) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.41 CMP 6550 291502 Hydraulic System Shut-off Valve (Right) - Operational Test Resolution: COMPLIED WITH CMP G550 291502 Hydraulic System Shut-off Valve (Right) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 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). Printed: 3/9/2018 4:29:22PM riAC_RevenueSquawksInvoice.rpt v3 Page 55 of 63 Set 01 EFTA00811259 Bill To: Plan D, LLC. WO Ii: SC521661 Invoice Number: 5517132452 Total USD: $304.00 Discrepancy: 40.42 CMP G550 313002 DFDR - Functional Test Resolution: COMPLIED WITH CMP 6550 313002 DFDR - Functional Test See step below for details of work performed. Billing Method Hours Rate 'fowl Labor USD: Flat Rate 5608.00 Total USD: 5608.00 Step: 40.42.1 Completed Comply.. ith FDR data report from dottnload at. placid on thumhdrite Discrepancy: 40.43 CMP G550 316205 FDR FAIL MESSAGE-OPS TEST Resolution: COMPLIED WITH CHIP 6550 316205 FDR FAIL MESSAGE-OPS TEST Billing Method Hours Rate -fond Labor USD: Flat Rate $76.00 Total USD: $76.00 Discrepancy: 40.44 CMP 6550 319013 Red Disk Honeywell /Jeppesen - Aerospace, Communication, Navigation Data. (28 Day Interval) Resolution: COMPLIED WITH CMP 6550 319013 Red Disk Honeywell / Jeppesen - Aerospace, Communication, Navigation Data. (28 Day Interval) Expires: 28Mar2018 Billing Method Hours Rate Total Labor USD: Flat Rate S152.00 Total USD: S152.00 Discrepancy: 40.45 CMP 6550 319014 Blue Disk Honeywell! Jeppesen - Electronic Terminal Charts, Geopolitical Boundaries. Airport Information Obstacle Data (14 Day Interval) Resolution: COMPLIED WITH CMP 6550 319014 Blue Disk Honeywell / Jeppesen - Electronic Terminal Charts, Geopolitical Boundaries, Airport Information Obstacle Data (14 Day Interval) Expires: 14Mar2018 Billing Method Hours Rate Total ' Flat Rate 5152.00 total t SH: S152.00 Discrepancy: 40.46 CMP G550 319016 Green Disk Honeywell / Jeppesen - Terrain Data (On condition or Six Month Interval) Resolution: COMPLIED WITH CHIP 6550 319016 Green Disk Honeywell! Jeppesen - Terrain Data (On condition or Six Month Interval) Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.47 CMP G550 321005 Main Landing Gear (Left) - Lubrication Resolution: COMPLIED WITH CMP G550 321005 Main Landing Gear (Left) - Lubrication Billing Method Hours Rate -foal Labor USD: Flat Rate S304.00 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). Printed: 3/9/2018 4:29:22PM riAC_RevenueSquawksInvoice.rpt v3 Page 56 of 63 Set 01 EFTA00811260 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Total USD: $304.00 Discrepancy: 40.48 CMP G550 321006 Main Landing Gear (Right) - Lubrication Resolution: COMPLIED WITH CMP 6550 321006 Main Landing Gear (Right) - Lubrication Billing Method Hours Rate Taal Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.49 CMP G550 322004 Nose Landing Gear - Lubrication Resolution: COMPLIED WITH CMP G550 322004 Nose Landing Gear - Lubrication Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.50 CMP G550 322306 Nose Landing Gear Bungee - Lubrication Resolution: COMPLIED WITH CMP 6550 322306 Nose Landing Gear Bungee - Lubrication Billing Method Hours Rate Total Labor USD: Flat Rate 5456.00 Total USD: 5456.00 Discrepancy: 40.51 CMP G550 323037 Main Landing Gear Bungee (LeR) - Lubrication Resolution: COMPLIED WITH CMP G550 323037 Main Landing Gear Bungee (Left) - Lubrication TW 568539 Due 2/19 TW 567919 Due 01/19 Billing Method Hours Rate Total Labor USD: Flat Rate $456.00 Total USD: 5456.00 Discrepancy: 40.52 CMP G550 323038 Main Landing Gear Bungee (Right) - Lubrication Resolution: COMPLIED WITH CMP 6550 323038 Main Landing Gear Bungee (Right) - Lubrication TW 568539 Due 2/19 TW 567919 Due 01/19 Billing Method Hours Rate Total Labor USD: Flat Rate $608.00 Total USD: $608.00 Discrepancy: 40.53 CMP G550 325202 Nose Wheel Steering Collar Assembly! Slave Gear - Lubrication Resolution: COMPLIED WITH CMP G550 325202 Nose Wheel Steering Collar Assembly / Slave Gear - Lubrication 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 57 of 63 Set 01 EFTA00811261 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Labor USD: Flat Rate $76.00 Total USD: $76.00 Discrepancy: 40.54 CMP G550 491007 APU Enclosure Thermal Blanket / Coating - General Visual Inspection Resolution: COMPLIED WITH CMP 6550 491007 APU Enclosure Thermal Blanket / Coating - General Visual Inspection Reference items 8.14 and 8.17 Billing Method Hours Rate Total Labor USD: Flat Rate $760.00 Pans USD: Time and Material S10.45 Total USD: $770.45 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 40.54 MI NAS1580C3T12 BOLT 5 52.09 S10.45 Discrepancy: 40.55 CMP G550 491300 APU Compartment Drain Collectors - General Visual Inspection Resolution: COMPLIED WITH CMP 6550 491300 APU Compartment Drain Collectors - General Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.56 CMP G550 491301 Auxiliary Power Unit Turbine Plenum Drains - Operational Test Resolution: COMPLIED WITH CMP G550 491301 Auxiliary Power Unit Turbine Plenum Drains - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5456.00 Total USD: 5456.00 Discrepancy: 40.57 CMP G550 523003 Baggage Compartment Door Seal - Detailed Inspection Resolution: COMPLIED WITH CMP G550 523003 Baggage Compartment Door Seal - Detailed inspection Air Regulator: 556959 Cal Due:06/18. Billing Method Hours Rate Total Labor USD: Flat Rate $608.00 Total USD: $608.00 Discrepancy: 40.58 CMP G550 523004 Baggage Compartment Door Seal Air Supply Moisture Drain Orifice - Detailed Inspection Resolution: COMPLIED WITH CMP 6550 523004 Baggage Compartment Door Seal Air Supply Moisture Drain Orifice - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.59 CMP 6550 523008 Baggage Door Seal Check Valve - Operational Test For detail description of the work complied with sec the York Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 58 of 63 Set 01 EFTA00811262 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: COMPLIED WITH CMP G550 523008 Baggage Door Seal Check Valve - Operational Test Ale Regulator: 556959 Cal Due: 06/18. Billing Method Hours Rate Total Labor USD: Flat Rate $456.00 Total USD: $456.00 Discrepancy: 40.60 CMP 6550 527001 Main Entrance Door Secondary Handle Lock Switch and Circuitry - Operational Test Resolution: COMPLIED WITH CMP 6550 527001 Main Entrance Door Secondary Handle Lock Switch and Circuitry - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate $912.00 Total USD: $912.00 Discrepancy: 40.61 CMP G550 531005 External Lower Fuselage FS -4 thru FS 758 View Front Ground - Zonal Inspection Resolution: COMPLIED WITH ChIP 6550 531005 External Lower Fuselage FS -4 thru FS 758 View Front Ground - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $304.00 Total USD: $304.00 Discrepancy: 40.62 CMP 6550 531055 Aft Cabin Below Floor FS 612 - FS 684 - Zonal Inspection Resolution: COMPLIED WITH CMP G550 531055 Aft Cabin Below Floor FS 632 - FS 684 - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $912.00 Total USD: $912.00 Discrepancy: 40.63 CMP G550 531060 Baggage Compartment Below Floor FS 684 - FS 758 - Zonal Inspection Resolution: COMPLIED WITH CMP G550 531060 Baggage Compartment Below Floor FS 684 - Fs 758 - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $608.00 Total USD: $608.00 Discrepancy: 40.64 CMP G550 531065 External Upper Fuselage FS 63 - FS 758 View From Ground - Zonal Inspection Resolution: COMPLIED WITH CMP 6550 531065 External Upper Fuselage FS 63 - ES 758 View From Ground - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 Total USD: $304.00 Discrepancy: 40.65 CMP G550 531082 Electronic Equipment Rack FS 147 - FS 181 - (Enhanced) Zonal Inspection Resolution: COMPLIED WITH CMP 6550 531082 Electronic Equipment Rack FS 147 - Fs 181 - (Enhanced) Zonal Inspection 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). Printed: 3/9/2018 4:29:22PM riAC_RevenueSquawksInvoice.rpt v3 Page 59 of 63 ucw EFTA00811263 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Labor USD: Flat Rate $456.00 Total USD: $456.00 Discrepancy: 40.66 CMP 6550 531085 Ext Aft Fuselage/Empennage (from Ground) - Zonal Inspection Resolution: COMPLIED WITH CMP G550 531085 Ext Aft Fuselage/Empennage (from Ground) - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $304.00 Total USD: $304.00 Discrepancy: 40.67 CMP 6550 575021 Wing Rear Beam (Left Enhanced) - Zonal Inspection Resolution: COMPLIED WITH CMP 6550 575021 Wing Rear Beam (Left Enhanced) - Zonal Inspection Ref 41.2 for discrepancy found Billing Method Hours Rate Total Labor USD: Flat Rate $532.00 Total USD: $532.00 Discrepancy: 40.68 CMP G550 575022 Wing Rear Beam (Right Enhanced) - Zonal Inspection Resolution: COMPLIED WITH CMP G550 575022 Wing Rear Beam (Right Enhanced) - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $532.00 Total USD: $532.00 Discrepancy: 40.69 CMP 6550 711301 External - Powerplants, Cowl Doors. Inlet Areas, Thrust Reverser and Nose Cowls (as viewed from ground) - Zonal Inspection Resolution: COMPLIED WITH CMP 6550 711301 External - Powerplants, Cowl Doors, Inlet Areas, Thrust Reverser and Nose Cowls (as viewed from ground) - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $228.00 Total USD: $228.00 Discrepancy: 40.70 CMP 6550 711302 External - Powerplants, Cowl Doors, Inlet Areas, Thrust Reverser and Nose Cowls (as viewed from ground) - Zonal Inspection Resolution: COMPLIED WITH CMP 6550 711302 External - Powerplants, Cowl Doors, Inlet Areas, Thrust Reverser and Nose Cowls (as viewed from ground) - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $228.00 Total USD: $228.00 Discrepancy: 40.73 CMP 6550 994042 AD 2017-18-12 B/E Aerospace Resolution: Complied with paragraph (g) of this AD by inspection and found to be N/A by pan number of PBE units Installed. No further action required. Billing Method I lours 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). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 60 of 63 Set 01 EFTA00811264 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 40.74 CMP G5540 994045 AD 2017-20-08 - Gu[(stream Aerospace - Gu[(stream AFM Supplement Incorporation Resolution: Complied with paragraph (g) and (h) (4) of this AD by inserting AFM Supplement G550-2016-01, dated July 27. 2016 into the Limitations Section of the AFM. Billing Method Hours Rate Total Labor UM) Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.75 CMP G550 282641 APU Fuel Shut-off Valve - Operational Check Ref Item 40.20 Resolution: COMPLIED WITH CMP G550 282641 APU Fuel Shut-off Valve - Operational Check Billing Method Hours Rate Taal Labor UM) Flat Rate 5304.00 Total [SD: 5304.00 Item: 41 Discrepancies - Customer Requested Due List Items as of 02/15/18 Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: N/A / N/A TSN/TSO: N/A CSN/CSO: N/A Aircraft Time: N/A Discrepancy: 41.1 RAI MU: Bungee upper housing is seized on lower housing. ref. item 40.52 Resolution: Removed R/II MLG Bungee P/N 1159L50903-1. Ordered and recieved new R/H MLG Bungee P/N 1159L57903-1. Reference Item 11.130 for installation of new Bungee. Billing Method hours Rate Total Labor USD: Time and Material ST 2.00 Y/ 5146.00 5292.00 Labor USD: Time and Material OT 0.05 (a 5146.00 57.30 Parts USD: Time and Material $4,371.44 Total USD: $4,670.74 Pans: Ref. No. Pan number: Description Quantity Sell pike USD Extended USD 41.1 #1 1159L57903-I BUNGEE, MAIN LANDING GEAR 1 $4,371.44 $4,371.44 Discrepancy: 41.2 Found broken grounding strap on LH wing rear beam Just outboard of flight spoiler while complying with rear beam inspection, ref item 40.67 Resolution: Summary: Removed discrepant bonding juniper and installed new bonding jumper on Lill wing out board of flight spoiler. Ref. AMM 27-63-11 Aug. 31/03. See steps below for full details of work accomplished and regulatory sign offs. 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). Printed: 3/9/2018 4:29:22PM riAC_RevenueSquawksInvoice.rpt v3 Page 61 of 63 Set 01 EFTA00811265 Bill To: Plan D, LLC. WO U: SC521661 Invoice Number: 5517132452 Labor USD: Time and Material ST 2.00 @ $146.00 $292.00 Labor USD: Time and Material OT 0.20 @ S146.00 $29.20 Pans USD: Tinie and Material $41.74 Total USD: $362.94 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 41.2 #1 hIS25083-7BB11 JUMPER, BONDING CNT 541.20 $41.20 41.2 #2 MS21042-3 NUT, SLF-LKG, 450 DEG. RDC HEX, 2 $0.27 $0.54 RDC HGT, RING BASE, NON-ORES Step: 41.2.1 Completed Removed broken grounding strap on LJH wing rear beam outboard of flight spoiler board. Ref. ATOM 27-63-11 Aug. 31/03 Step: 41.2.2 Completed Installed new grounding strap on I./H wing out board of flight spoiler. Ref. A3131 27-63-11 Aug. 31/03 Item: 42 Customer Eval flight Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: N/A / N/A TSN/TSO: N/A CSN/CSO: N/A Aircraft Time: N/A Item: 43 Customer Eval flight discrepancies Team Manager: Charles Thomas Pan/Model K: Customer Coordinator: Julian Brown AC Serial No/Tail No.: N/A / N/A TSN/TSO: N/A CSN/CSO: N/A Aircraft Time: N/A Discrepancy: 43.14 HUD and EVS is totally Mop Resolution: Billing Method Hours Rate Total Labor USD: Flat Rate $1,460.00 Pans USD: No Charge N/ C Total USD: $1,460.00 Parts: Ref. No. Pan number: Description Quantity 43.14 #1 7023171-901 DISPLAY UNIT, HEADS-UP (HUD) E0-201 VGS Step: 43.14.1 Waiting Evaluated the VGS Parameters page in the CMC for the HUD and EVS system. Most Insp parameters would X out intermittently and combiner unit stayed failed. HUD 310N reason for blanking code is 2048. This code calls for replacement of the Overhead Unit. Placed Unit on order. Ref 6550 WDM 34-29-02 Dated June 20'13 Ref G550 WDM 3445-00 Dated November 30/10 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). Printed: 3/9/2018 4:29:22PM Page 62 of 63 Set 01 GAC_RevenueSquawksInvoice.rpt v3 EFTA00811266 Bill To: Plan D, LLC. WO SC521661 Invoice Number: 5517132452 Communications concerning disputed debts, including a check or other instrument tendered as full satisfaction of a debt, must be forwarded to: Gulfstream Aerospace Aun. Credit Manager PO Box 2206 MIS B-05 Savannah, GA 31402 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/9/2018 4:29:22PM GAC_RevenueSquawksInvoice.rpt v3 Page 63 of 63 Set 01 EFTA00811267

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