by date← Dec 12, 2017·Dec 12, 2017 →

EFTA00811141

Dataset 9

December 12, 201764 pages23,904 words

https://www.justice.gov/epstein/files/DataSet%209/EFTA00811141.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: Wire Remittance To: Gulfstream 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 CRC:1216M In Date: 10/23/2017 Out Date: 03/09/2018 Payment Type: CIA- Wire Payment Temis: Title: Plan D, LLC. INVOICE SUMMARY FOR WORK ORDER NUMBER: SC521661 Time & Materials Flat Rate Total Labor USD: $42,049.78 $693,548.16 $735,597.94 Parts USD: $66,949.00 $674,209.00 $741,158.00 Services USD: $2,384.17 $497,215.90 $499,600.07 Misc Charges USD: 425,000.00 425,000.00 Detail Subtotal USD: $86,382.95 51,864,973.06 S1,951,356.01 Subtotal USD: $1,951,356.01 Funds on Deposit USD: $392,500.00 Total USD: S1,558,856.01 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page I of 64 tit W. EFTA00811141 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 ancVor 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 2 of 64 tat W. EFTA00811142 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Item: 1 Airframe Culfstream C550 Team Manager: Charles Thomas Pan/Model #: 6550 Customer Coordinator: Julian Brown AC Serial No/Tail No.: 5173 / N415LM TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 1.17 Consumables & Shop Supplies Resolution: For billing purposes only. Billing Method Hours Rate Total Parts USD: Flat Rate $5,000.00 Total USD: $5,000.00 Discrepancy: 1.27 Sales Concession Resolution: Billing Method flours 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 -$25,000.00 Discrepancy: 1.28 Item written to invoice labor and materials not covered by Rolls Royce Corporate Care Contract Resolution: Billing Method I lours Rate Total Labor USD: Flat Rate $2,255.16 Pans USD: Flat Rate $45.00 Total USD: 52.300.16 Item: 2 ENGINE BR700-710C4-11 Team Manager: Charles Thomas Part/Model 11: BR700-710C4-II Customer Coordinator: Julian Brown S/N: 15-149 TSNffSO: CSN/CSO: Aircraft Time: Item: 3 ENGINE BR700-710C4-11 Team Manager: Charles Thomas Part/Model #: BR700-710C4-11 Customer Coordinator: Julian Brown SIN: 15448 TSN/TSO: CSNJCSO: Aircraft Time: 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 / HANGARA 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: 3/7/2018 3:15:05PM Page 3 of 64 tat W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811143 Bill To: Plan D, LLC. WO #: SC52166I Invoice Number: 5517132452 Discrepancy: 5.2 CMP G550 970531 ASC 53A Communications Management Function ARINC Direct - Datalink Service Provider Resolution: COMPLIED WITH CMP 6550 970531 ASC 53A Communications Management Function ARINC Direct - Datalink Service Provider. Gray Disk: PN OFF: N212JE OxAICIBD 28NOV2017 SN OFF: ASC065-123 PN ON: N212JE OxAICIBD 02MAR2018 SN ON: ASC053-065-123 Orange Disk: PN OFF: 69001791-505 SN OFF: CDC 04JUL2017 PN ON: 69003236-502 SN ON: ARINC DIRECT 25JAN2018 Billing Method flours Rate Total Parts USD: Time and Material 51,500.00 Total USD: 51,500.00 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 5.281 ASC053A-1 G5SP KIT, COMMUNICATIONS 1 51,500.00 51,500.00 MANAGEMENT FUNCTION ARINC DIRECT, DATA LINK SERVICE PROVIDER, 5001-9999 6 As Ionics Team Manager: Charles Thomas Part/Model /I: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNffSO: CSN/CSO: Aircraft Time: 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 flight guidance panel (pn: 7021852-901 sn: 08080720) and performed Autopilot operational check with no defects noted. All work done ref CHIP G550 221002 item 11.10 and 6550 CMP 22100 item 11.8. See steps below for work performed. Billing Method flours Rate Total Labor USD: Time and Material ST 4.00 (a $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 63 #1 7021852-901 CONTROLLER, GUIDANCE PANEL 1 $0.00 $0.00 Step: 63.1 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 6550 CMP 221001. Ref item 11.8 for CMP R&I. Step: 63.2 Completed Performed Autopilot operational check n ith no defects noted. All work done ref CMP 6550 221002 item 11.10. 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: 3/7/2018 3:15:05PM Page 4 of 64 tit W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811144 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Discrepancy: 6.4 DU #4 loop. 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 G550 CMP 316024 and CMP 316030. Ref items 11.7 and 11.9. Billing Method Hours Rate Total Labor USD: Time and Material ST 3.51 @ $146.00 $512.46 Pans USD: No Charge N/C Total USD: $512.46 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 6.4 NI 7028140-905 DISPLAY UNIT, FLAT PANEL 1 $0.00 50.00 (DU-I3I0) Discrepancy: 6.5 Customer request to update RAAS settings. Resolution: Updated RAAS settings IANV CMP G550 319025 Gulfstream, Setting / Rigging 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 Services USD: 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 new blue paint scheme and to add the company logo. as requested by customer. Ref. Item 20.1.16 Billing Method Hours Rate foul Parts USD: Time and Material $3,894.00 Total USD: $3,894.00 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 6.6#I 925940-4794-4V2 AIRSHOW SOFTWARE I $3,894.00 $3,894.00 Discrepancy: 6.7 Ft/II wing static wicks MEGG out of tolerance. Resolution: Replaced all 3 Rai wing static wicks po: 2-16SC-I. Performed functional check with no defects. All maintenance performed using G550 AMM 23-61-01 Oct 30/ 08. Megger CN: 557026 Date Due: 02/18 DLRO CN: 560572 Date Due: 02/18 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: 3/7/2018 3:15:05PM riAC_RevenueSquawksInvoiccrpt v3 Page 5 of 64 tit kW EFTA00811145 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 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 #1 2-16SC-I DISCHARGER. STATIC WICK 3 556.25 $168.75 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 WDM 6550 27-60-00 June 20113. Performed LH Spoiler RVDT functional check with no defects noted. All maintenance performed using 6550 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 $861.40 Pans USD: Time and Material 5329.22 Total USD: $1,190.62 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 6.8#1 447HW151XNI0902 BACKSHELL I $323.22 $323.22 6.8 #2 N181969/14-01 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 6550 27-60-00 June 20113. Step: 6.8.2 Completed Performed LH Spoiler RVDT functional check with no defects noted. All maintenance performed using 6550 AMM 2745-00 Dated November 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 6C515050250 Rev -. Billing Method Hours Rate Total Labor USD: Time and Material ST 1.00 ® $146.00 $146.00 Total USD: $146.00 Discrepancy: 6.11 Cabin Upwash will not dim from AFT VIP seat or AFT galley switch panels Resolution: Billing Method Hours Rate Total Labor USD: Flat Rate $2,336.00 Pans USD: Time and Material $90532 Total USD: $3,24132 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 6.11 #1 AL-2024 MODULE, DIMMER I $90532 $90532 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: 3/7/2018 3:15:05PM Page 6 of 64 Pit kW GAC_RevenueSquawksInvoice.rpt v3 EFTA00811146 Bill To: Plan D, LLC. WO #: SC52166I Invoice Number: 5517132452 Step: 6.11.1 Completed Removed entry way carpet and padding. Gained access to AFT upper dim module 581PS3 and disconnected connector 581PS3P1. Disconnected FWD Upper DIM Module connector 581PS1PI and swapped dim modules connectors. Performed operational check and FM 1) and AFT Upper Lights would not dim. Returned dim modules connectors to original configuration. Performed operational check and only AFT upper lights would not dim. Disconnected connector 581PS3P1 and Checked for 28VDC on connector 581PS3P1 pin I with no defects noted. Checked pin 2 for ground with no defects noted. Reconnected connector 581PS3P1. All work done per (350 DWG (;C515810316 Rev -. Step: 6.11.2 Wailing Reinstall entry way carpet and padding (Interior Vest/Crewrest 108-101)) approval (LIP) Step: 6.11.3 Completed Connected DIAG 3000 to aircraft connector port in REER and checked switching function of LM AFT VIP switch panel and galley switch panel with no defects noted. Removed 3 connectors from CMMI and 031312 and swapped ( :M NI's and performed operational check with AFT Upper cabin wash still unable to dim. Returned aircraft to original configuration. Performed operational check and AFT Upper cabin wash was still unable to dim. Checked power at AFT Upper Dim Module and Output voltage was either at 27VDC when up wash light on or OVDC with up wash lights off. Output voltage will not adjust when trying to dim lighting. All work done per 6550 DWG GC515810316 Rev -. Item: 7 Interior Team Manager: Charles Thomas Pan/Model 11: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 7.9 Galley Microwave retainer block cracked. Resolution: Replaced, cracked galley Microwave retainer block, with new CSN1344001014-101 STOP, per GPM308001581-301 Rev A. Billing Method Hours Rate Total Parts USD: Time and Material $35.63 Total USD: $35.63 Parts: Ref. No. Part number: Description Quantity Sell price USD Extended USD 7.9 NI GSNI344001014-101 STOP 1 535.63 535.63 Discrepancy: 7.13 Grosspoint material behind LH #1 and RH kl 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 @ S146.00 5474.50 Total USD: 5474.50 Discrepancy: 7.14 Acoustic door bearing are 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 S-OPN-DD. Work done per CP521400001 REV. C. Billing Method Hours Rate Taal Labor USD: Time and Material ST 2.00 ® 5146.00 5292.00 Pans USD: Time and Material $216.52 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: 3/7/2018 3:15:05PM Page 7 of 64 tat W. liAC_RevenueSquawksInvoice.rpt v3 EFTA00811147 Bill To: Plan D, LLC. WO #: SC52166I Invoice Number: 5517132452 Total USD: $508.52 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 7.14 #1 SUPER 8-OPN-DD BEARING, LINEAR, BALL, 4 $UM S216.52 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-T5038CTYPE-IV webbing. MI 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: Fiat Rate 32,920.00 Pans USD: Time and Material $298.56 Total USD: 33,218.56 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 7.17 #2 40044-10 HOOK ASSY, LOOP& KEEPER 6 $2.12 $12.72 7.17 #3 FDA5352 HOOK AND BUCKLE 6 $42.61 $255.66 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. PIN SRS9XMSS+400LM. All work done PER. GP5210000I Rev.C. Billing Method I lours Rate 'Foul Pans USD: Time and Material 5596.36 Total USD: 5596.36 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 7.1881 SRS9XMSS+400LM RAIL ASSY 2 S298.18 S596.36 Discrepancy: 7.20 Fwd Lav fwd 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 lival Labor USD: Time and Material ST 6.62 Qa 5146.00 S966.52 Total USD: $966.52 Item: g Mechanical Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Discrepancy: 8.3 Customer request full cleaning and operational checks of the Lavatory tank and system. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 8 of 64 tit W. EFTA00811148 Bill To: Plan D. LLC. WO #: 5C521661 Invoice Number: 5517132452 Resolution: Complied with cleaning of la% systems and toilets/waste tank per G550 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 Re111A7. No discrepacies noted with logic module. Toilet operation check performed per CMP 380001 Ref.7.15. Operated okay and no leaks noted al 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 Pans USD: Time and Material $18,672.83 Total USD: $21,008.83 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.3 NI NAS1611-150A ORING 2 $2.25 $4.50 8.3#2 MS295I3-226 PACKING, PREFORMED. 2 50.64 $1.28 HYDROCARBON FUEL RESISTANT. O RING 8.3 #3 7700248 SENSOR, TANK WASTE I 516.56330 $16,56330 8.3 #4 7600123 GASKET, WASTE TANK SENSOR I 52.103.75 $2,103.75 Step: 8.3.1 Completed Removed. ckaned. inspected, and reinstalled ultrasonic sensors PN:7700395-00I lift SN:07-G-170. and R/11 SN:07-G-167 per CMP 3800151383024. 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 toiktstwaste tank per G550 AMM 38-31-01 Rev.03/31/17. Waste tank full light does not go off. Step: 8.33 Waiting Waste tank "full" light does not go off. approval (L/P) 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 (a 5146.00 $350.40 Parts USD: Time and Material $268.82 Total USD: $619.22 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.4 NI H5000-2-102-142 LATCH, SERVICE DOOR $258.12 $258.12 8.4 N2 hIS20426AD3-4 RIVET 10 $0.22 42.20 8.4 #3 hIS20426AD3-3 RIVET to 50.22 $2.20 8.4 #4 hIS20426AD3-4.5 RIVET 10 $0.41 $4.10 8.4 #5 hIS20426AD3-5 RIVET- SOLID, CSK 100 DEG 10 $0.22 $2.20 Step: 8.4.1 Completed Removed discrepant latch on the external MED switch service door per BP 1159851110 Rev G. Step: 8.4.2 Completed Installed New latch P/N H5000-2-102-142 per BP 1159851110 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 MM 52-40-00 October 30/06 finding no further discrepancies. Step: 8.4.3 Completed Request paint on external MED snitch service door due to new latch installation. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 317/2018 3:15:05PM Page 9 of 64 tat W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811149 Bill To: Plan D, LLC. WO SC521661 Invoice Number: 5517132452 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 (-0, $146.00 $131.40 Total USD: $131.40 Step: 8.5.1 Completed Complied with potable water tank senice per (350 ANN 38-14-01 March 31/17. No indication on external panel noted throughout entire senice. 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 31105. Discrepancy: 8.6 CMP G550 275019 Flap Actuator Travel Nut (Left) - Lubrication Resolution: COMPLIED WITH CMP G550 275019 Flap Actuator Travel Nut (Lea)- Lubrication Billing Method Hours Rate fowl Labor USD: Flat Rate 5146.00 Total USD: 5146.00 Discrepancy: 8.7 CMP 6550 275020 Flap Actuator Travel Nut (Right) - Lubrication Resolution: COMPLIED WITH CMP 6550 275020 Flap Actuator Travel Nut (Right) - Lubrication Billing Method Hours Rate -foal Labor USD: Flat Rate 5146.00 'total USD: $146.00 thscrenancy: 8.9 CMP G550 491005 APU Enclosure FS 767 - FS 797 - Zonal Inspection Resolution: COMPLIED WITH CMP G550 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 Parts USD: Time and Material 5162.00 Total USD: $162.00 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.1001 KEYS KEYS 12 $13.50 $162.00 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 10 of 64 tat W. EFTA00811150 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 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 C550 AMM 28-16-00 dated August 30, 2009. Decade resistor box 113/4 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 Mahn Required" Cas message on APU start. CMC fault code 4922222APU (APU Flow Divider Sol Short) Resolution: Summary: Removed and replaced fuel Bow 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 CN1P 493011. See steps below for detailed work performed. Billing Method Hours Rate Total Labor USD: Time and Material ST 10.61 ® SI46.00 $1,549.06 Labor USD: Time and Material OT 0.18 ® SI46.00 S26.28 Pans USD: Time and Material 412,652.36 Total USD: $14,227.70 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.19N1 WE3883738-I VALVE, SOLENOID I $5,572.61 $5,572.61 8.19 #2 WE3883842-2 VALVE, FLOW DIVIDER I $7,078.11 S7,078.11 8.19 #4 M25988/2-904 PACKING 2 50.82 41.64 Step: 8.19.1 Completed Gained access to 18IA I PI ( on APU Ceiling). Disconnected plug, inspected and cleaned cannon plug with no defects noted. Returned aircraft to original configuration. All maintenance performed using WDNI 49-60-00 June 15/16. Step: 8.19.2 Completed Ran API: and still had constant APU mains. 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 Rill hoist plug stripped. Ref. 13.1 Resolution: Replaced horizontal stabilizer FUll and Lill hoist plugs PN: 1159CSM50558-00I with new horizontal stabilizer R/II and Lai hoist plugs PN: 1159CSM50558-001 per drawing 1159CSM50558 Rev.B. and C550 AMM 20-42-00 Rev. Mar.31/17. Billing Method Hours Rate Total Pans USD: Time and Material $1,145.84 Total USD: $1,145.84 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.22 NI 1159CSNI50558-001 PLUG, HORIZONTAL STABILIZER 5389.48 S389.48 HOISTING STOP 8.22 82 1159CSNI50558-001 PLUG, HORIZONTAL STABILIZER 2 $378.18 S756.36 HOISTING STOP 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page II of 64 tit kW EFTA00811151 Bill To: Plan D, LLC. WO At: SC521661 Invoice Number: 5517132452 Discrepancy: 8.23 L/II Flap "B" Track Aft I/B Roller is worn beyond limits per 6550 AMM 27-50-00 Rev. March 31/17 Ref. 13.2 Resolution: Replaced Lill Flap "B" hack Aft I/B Roller n it It new roller, P/N KRP233012FT, IAW CMP 6550 275037 and Drawing 1159C554220 Rev C Billing Method I Rate Total Labor USD: Flat Rate 31,168.00 Pans USD: Time and Material $999.18 Total USD: 32,167.18 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.23 #1 KRP233012FT ROLLER, FLAPTRACK $703.50 $703.50 8.23 #5 1159CSNI54233-19 WASHER 2 591.20 $182.40 8.2386 MS17826-8 NUT 2 $2.42 $4.84 8.2387 hIS24665-370 COTTER PIN 2 50.22 50.44 8.23 W8 NAS6704L13 BOLT $108.00 5108.00 Discrepancy: 8.24 IUD Flap "B" hack Aft UB Roller is worn beyond limits per 6550 ANIN1 27-50-00 Rev. March 31/17 Ref. 13.2 Resolution: Summary: Removed R/II Flap "B" Track Aft outboard bracket. Replaced Rai Flap "B" Track Aft I1B roller with new roller, P/N KRP233012FT. Installed Rill Flap "B" Track Aft outboard bracket. Work performed per CMP 6550 275038 and Drawing 1159CS54220 Rev C. See steps below for detailed work performed. Billing Method Hours Rate Total Labor USD: Time and Material ST 8.92 @ 5146.00 $1,302.32 Parts USD: Time and Material $1,056.60 Total USD: 32,358.92 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.2181 KRP233012FT ROLLER, FLAPTRACK I $703.50 $703.50 8.2182 NAS67041.II BOLT I $117.70 $117.70 8.24 83 NAS67041.II BOLT 2 $117.70 $235.40 Step: 8.24.1 Completed Removed Rdi Flap "B" Track Aft outboard bracket. Replaced Rai Flap "B" Track Aft I/B roller with new roller. P/N KRP233012FT. per CMP G550 275038 and Drawing 1159O354220 Rev C Step: 8.24.2 Completed Recieved ok to install and installed R/H Flap Track "B" AFT O/B roller fitting. Bolts still require torque and fitting requires sealant per 1159CS54220 Rev G. Step: 8.24.3 Completed Bolts require torque and fitting requires sealant per 1159CS54220 Rev G. Discrepancy: 8.27 Rill Pylon leading edge seal torn Resolution: Replaced R/H Pylon leading edge seal per DWG 1159P57911 rev. C Billing Method Hours Rate Total Labor USD: Time and Material ST 3.47 (a 5146.00 $506.62 Parts USD: Time and Material $2,044.87 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM Page 12 of 64 tit f6I GAC_RevenueSquawksInvoice.rpt v3 EFTA00811152 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Total USD: $2,551.49 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 8.27 #1 1159SCP510-18E SEAL, LEADING EDGE, Rai I 52,02736 $2,027.56 8.27#2 NAS8802-3 BOLT 3 52.72 $8.16 8.2783 MS21043-04 NUT-SELF LKG,CRES,RING BASE 3 52.06 $6.18 8.2784 NASI149DN816K WASHER 3 50.22 50.66 8.27 #5 hIS21043-08 NUT, SELF LOCKING. REDUCED H 3 $0.77 $231 Discrepancy: 8.29 NLG wire harness is contacting hydraulic lines in aft NLG wheel well when gear is retracted. Found while accomplishing clearance check. REF 13.1.1 paint traveler 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 ANINI G55032-26-03 Dated MArch 31/17 Billing Method Hours Rate Total Labor USD: Flat Rate $876.00 Total USD: $876.00 Discrepancy: 830 UH 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 MLG brake harness insulation tear repair IAN' SR1052 Rev-B. No defects noted. See steps below for details of work performed. Billing Method Hours Rate Total Labor USD: Flat Rate $584.00 Pans USD: Time and Material $35.44 Total USD: $619.44 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.3081 GAC501K400H1 BANDCLAMP I $32.99 $32.99 8.3083 GAS830CV150-0 SLEEVING I $1.76 41.76 8.30#4 GAS830CV100-0 SLEEVE I $0.69 S0.69 Step: 830.1 Completed Replaced upper broken clamp on Left MIA: strut. All maintenance performed using DWG 11591.50300 REV K. Torque Wrench CN: 562086 Date Due: 09118 Step: 830.2 Completed Complied with LH N11.6 brake harness insulation tear repair 1AW SRI052 Rev-B. No defects noted. Discrepancy: 831 UH MLG 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: Summary : Added heat shrink to harness to move the bending point of the harness. Placed material 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 8.311 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 13 of 64 tit kW EFTA00811153 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Billing Method Hours Rate Total Labor USD: Flat Rate 51.168.00 Pans USD: Time and Material $6.28 Total USD: $1,174.28 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 831 #1 GAS830CV100-0 SLEEVE 4 $0.69 42.76 831 #2 GAS830CV150-0 SLEEVING 2 $1.76 $3.52 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 aprox. 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 %bring 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 Lill #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 till #5 pillow block assembly PN-1159SCC504-15 SN-3924 and installed new block PN-1159SCC504-15 SN-7992 per C550 AMM 27-53-05 Aug 30/09. Complied with flap system operational with no defects noted per O550 AMM 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: Ref. No. Part number: Description Quantity Sell price USD Extended USD 83281 1159SCC504-15 PILLOW BLOCK, FLAP CONTROL 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 NASII49D0163K WASHER 2 50.23 $0.46 832#5 202-16126-41 NUT, SELF LOCKING 2 $23.62 $47.24 832 #6 MS24665-153 PIN, COTTER 2 $0.22 $0.44 832 #7 MS24665-86 COTTER PIN 6 $0.23 $138 Discrepancy: 833 FUI I #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/II #5 pillow block assembly PN-I159SCC504-15 SN-3945 and installed new block PN-1159SCC504-15 SN-7995 per C550 AMM 27-53-05 Aug 30/09. Complied with flap system operational with no defects noted per 0550 AMM 27-50-00 Nov 15/17. Billing Method Hours Rate Total Labor USD: Time and Material ST 14.05 @ $146.00 $2,05130 Labor USD: Time and Material OT 035 @ $146.00 S51.10 Pans USD: Time and Material 31,810.51 Total USD: 33,912.91 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 14 of 64 tat W. EFTA00811154 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.33 #1 1159SCC504-15 PILLOW BLOCK, FLAP CONTROL 1 $1.758.99 $1,758.99 DRIVE 8.33 #2 NAS6404U6D BOLT 2 $0.00 $0.00 8.33 #3 NAS1587-4C WASHER 2 $1.69 $3.38 8.33 #4 NAS1149D0463K WASHER 2 $0.23 $0.46 8.33 #5 202-16126-4L NUT, SELF LOCKING 2 523.62 $47.24 8.33 #6 14524665-153 PIN, COTTER 2 50.22 $0.44 Discrepancy: 8.36 Rill NLG door step is out of limits .060. (0.035 Max)) Ref. 13.1.1 Paint Travel Section D Line NI Resolution: Removed cotter pins (2ea.), loosened jam nuts and adjusted R/II and L/H NLG door control rod P/N: 159L10085-9. 1/2 turn out to achieve proper door fit stated per GV-GER-313 Rev. P Adjusted R/H NLG 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 Q $146.00 $876.00 Total USD: $876.00 Discrepancy: 838 RAI #2 E-window upper heat contactor showing signs of arcing. Ref item 19.1.12 Resolution: Removed contactor P/N 1159F50236-22 from Rill #2 E-window frame and installed new contactor P/N 1159F50236-22 as per CAC Drawing 1159F50236 Rev B. Ref item 19.1.12 for heat check following window installation Billing Method Hours Rate Total Labor USD: Flat Rate $146.00 Pans USD: Time and Material $250.00 Total USD: $396.00 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 838 #1 1159F50236-22 CONNECTOR ASSY. WDO-RH, 1 $250.00 $250.00 GVFS490 Discrepancy: 8.40 Lill engine has Fire-loop B fault, during and atter fireloop test in cockpit. Resolution: Removed 1/H Fire control box PN: 51653-154 SN: 3305 and installed repaired Fire control box PN: 51653-154 SN: 2763. Performed operational check alth no defects noted. All work done per C550 CMP 261201 (Ref 11.151) and CMP G550 261211 (Ref 11.154) Billing Method Hours Rate Labor USD: Time and Material ST 0.50 Q $146.00 $73.00 Labor USD: Time and Material OT 1.50 @, $146.00 $219.00 Pans USD: Time and Material $7,922.87 Total USD: $8,214.87 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.40 #1 51653-154 CONTROLLER, FIREWIRE 1 $7,921.03 $7,921.03 8.40 #2 14835207-264 SCREW 4 50.23 $0.92 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: 3/7/2018 3:15:05PM (iAC_RevenueSquawksInvoice.rpt v3 Page 15 of 64 tat W. EFTA00811155 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.40 03 NA51149D0316H WASHER 4 $0.23 50.92 Item: 9 Paint Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNffSO: CSN/CSO: Aircraft Time: Item: 10 Outstanding Parts. Materials, and / or Services Team Manager: Charles Thomas Part/Model #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNffSO: CSN/CSO: Aircraft Time: Item: 11 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 Pan/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 LH #2 and Ril #2 console tables and lids from the cabin side ledges Per CE522280107 Rev - Res eneered 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 [lours Rate Total Labor USD: Flat Rate 510.840.00 Pans USD: Flat Rate 5207.00 Total USD: 511.047.00 Step: 123.1 Completed Wood Labor Only Step: 123.2 Completed INT Support (R&R) Labor Only Step: 1233 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 CE522280I07-01 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. 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: 3/7/2018 3:15:05PM Page 16 of 64 tat W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811156 Bill To: Plan D, LLC. WO tr. SC521661 Invoice Number: 5517132452 Resolution: Removed all cabin dual cupholders and replaced with single cupholders.RH #1, 2 and LI1#1, 2, and 3 Ledges.Removed cupholders at the divan area and Rev ennered with Dark Eucalyptus Veneer part# GSE150717-1LP Lt 17-366384 All work done per CE522280108 Rev - Reference RSQCT-400 Rev.-, Index #9 for details of work done. Billing Method Hours Rate Total Labor USD: Flat Rate 413,322.00 Pans USD: Flat Rate 51,105.00 Total USD: 514,427.00 Parts: Ref. No. Pan number: Description Quantity 12.4 HI 2123X2.43NEC CUPHOLDER 12 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 CE522280108-01 Discrepancy: 12.6 WCR 6- APPROVED: Customer requests to replace the galley and galley 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 # LTI7-365416 LAI Galley Veneer P/N GSE 150717-ILP LOT# LT17-366384 Bonded per CCS 1136 TYPE 1 REV K. & CCSII09 Rev A Ref. Ref 19.24 for flammability & Ref 12.6.7 for work performed) Billing Method Hours Rate Total Labor USD: Flat Rate $7,884.00 Pans USD: Flat Rate $1,338.00 Total USD: $9,222.00 Parts: Ref. No. Pan number: Description Quantity 12.6 #1 GSNI344001007-101 STOP 2 12.6#2 AN525-10R10 SCREW 10 12.6#3 AN525-101211 SCREW 10 12.6#4 AN525-10R12 SCREW 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 17 of 64 tat W. EFTA00811157 Bill To: Plan D, LLC. WO H: SC52166I Invoice Number: 5517132452 Step: 12.6.1 Completed Wood Labor Only Step: 12.6.2 Completed INT Finish and Paint Labor Only Step: 12.63 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 WM Galley annex,and Lai Galley Veneer P/N GSE 150717-1LP LOTH LT17-366384. Hardwood P/N 8-JQTR-SAWN-MOZAMBIQUE ILOT H 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 Of LT17-365416. Bonded hardwood nosing on LTH Galley Assy per CCS 1136 TYPE 1 REV K. Ref. CP31308001581-301 rev nc. Step: 12.6.8 Completed Finish- Lai Galley hardwood nosing Step: 12.6.9 Completed Finish - Rill Galley annex Item: 13 Option 1- Full Paint - (Ref. Item D 1.1 of Proposal ID// 7037536. ROO) Team Manager: Charles Thomas Part/Model Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: 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 he 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 the same base color as the outside surface. The landing gear will be cleaned. O 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. O Previously polished metal surfaces will be buffed. O The inside surfaces of the airbrakes will be painted. - 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 Gulfstream facilities Paint Operations Manager, including labor and materials on a Work Change Request (WCR). ***SEE APPENDIX FOR ADDITIONAL INFO*" Resolution: For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM liAC_RevenueSquawksInvoice.rpt v3 Page IS of 64 tit kW EFTA00811158 Bill To: Plan IX LLC. WO It: SC521661 invoice Number: 5517132452 In addition to the paint specifications listed above, the following standard Cu[(stream 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 doorjamb. 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 be 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 Gulfstream facility's Paint Operations Manager. including labor and materials on a Work Change Request (WCR). Billing Method Hours Rate Total Labor USD: Flat Rate 4223,060.00 Pans USD: Flat Rate 4'25,294.00 Services USD: Flat Rate $21,108.00 Total USD: 5269,462.00 Pans: Ref. No. Part number: Description Quantity 13.181 PAINT KIT GV 6550 PAINT KIT FOR GV, G550 I 13.182 CA1805CX GAL SOLVENT REDUCER 6 13.183 P10010-155 LACQUER, ACRYLIC -FLAT BLACK 4 13.184 J328 DEGREASER, ZONE DEFENSE (I EA- 1 5 GL PAIL) 13.185 PRI440B1-2-654 SEALANT, 6 OUNCE A1654 SENIKIT 24 12 HOUR WORK LIFE 13.186 CM3905HP CLEAR COAT KIT GL 1 13.1 #7 AN525-832-8 SCREW 5 13.1 #8 NASI149DN816K WASHER :. 13.1 #9 MS210421,08 NUT, SELF LOCKING ' 13.1810 738651E5-01 PAINT, ELITE BLUE IMRON AF700 40 13.1811 137755-0IGL THINNER 10 13.1 #12 AF740 PAINT, CLEAR COAT 40 13.1813 131105 CATALYST 1 13.1814 137655 REDUCER 1 13.1815 131105 CATALYST 1 13.1816 131105 CATALYST 1 13.1817 131105 CATALYST 1 13.181% 131105 CATALYST 1 13.1819 131105 CATALYST 1 13.1 #20 131105 CATALYST 1 13.1821 131105 CATALYST 1 13.1 #22 131105 CATALYST 1 13.1 #23 131105 CATALYST 1 13.1 #24 131105 CATALYST 1 13.1 #25 131105 CATALYST 1 13.1826 131105 CATALYST 1 13.1 #27 131105 CATALYST 1 13.1 #28 131105 CATALYST 1 13.1 #29 131105 CATALYST 1 13.1 #30 131105 CATALYST 1 13.1831 131105 CATALYST 1 13.1 #32 131105 CATALYST 1 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 19 of 64 tit kW EFTA00811159 Bill To: Plan D, LLC. WO ti: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity 13.1 #33 I3110S CATALYST 13.1 #34 I3765S REDUCER 13.1 #35 13765.5 REDUCER 13.1 #36 13765.5 REDUCER 13.1 #37 13765.5 REDUCER 13.1 #38 13765.5 REDUCER 13.1 #39 13765.5 REDUCER 13.1 #40 13765.5 REDUCER 13.1 #41 13765.5 REDUCER 13.1 #42 13765.5 REDUCER 13.1 #43 13765.5 REDUCER 13.1 #44 13765.5 REDUCER 13.1 #45 13765.5 REDUCER 13.1 #46 13765.5 REDUCER 13.1 #47 13765.5 REDUCER 13.1 #48 13765.5 REDUCER 13.1 #49 13765.5 REDUCER 13.1 #50 13765.5 REDUCER 13.1 #51 13765.5 REDUCER 13.1 #52 137655 REDUCER 13.1 #54 CA1805CX GAL SOLVENT REDUCER 8 13.1 #55 PR1440B1-2-654 SEALANT, 6 OUNCE #654 SEMKIT 24 1/2 HOUR WORK LIFE 13.1 #56 CA8905HP CLEAR COAT KIT GL 13.1 #57 D9001 CONVERTER 2 13.1 #58 D8003 SURFACER, SANDING 2 13.1 #59 400 EVERCOAT EVERCOAT FILLER 3 13.1 #60 140N2022S1 FUSELAGE DRAIN VALVE 13.1 #6I GAS13AN-1-41 SEAL, BUTTONED STRIP, WHEEL 9 WELL DOOR (5' SECTION) 13.1 #62 NIS27039C0807 SCREW-MACHINE, CRES PAN HD, 34 STRL 13.1 #63 NAS1149DN816K WASHER 46 13.1 #64 MS27039C0808 SCREW, PAN HEAD, X RECESSED 8 13.1 #65 MS24693526 SCREW, MACHINE, FLAT I8 COUNTERSUNK HD, 100 DEG, CROSS RECESS 13.1 #66 MS24693-528 SCREW 13.1 #67 AN525832R7 BOLT 12 13.1 #68 AN525-832R11 SCREW 10 13.1 #69 NASI149DN816H WASHER, FLAT ALUMINUM 10 13.1 #70 NIS21042L08 NUT, SELF LOCKING 10 13.1 #71 AN525-832R5 SCREW 21 13.1 #72 MS27039-0809 SCREW, MACHINE 9 13.1 #73 NAS1149CN816R WASHER-FLAT CRES 13.1 k74 140N2022S1 FUSELAGE DRAIN VALVE 13.1 k75 MS24665-155 COTTER PIN 2 13.1 #78 MS27039C0807 SCREW-MACHINE, CRES PAN HD, 10 STRL 13.1 #79 NAS43DD3-36FC SPACER SLEEVE 2 13.1 #80 SJ8665FP021-1 RADOME BOOT 13.1 #81 MS24665-302 COTTER PIN 24 13.1 #82 GAS18N1-1-1440 SEAL 3 13.1 #84 GASI8h1-I-I440 SEAL 12 13.1 #85 MS24694-C7 SCREW, MACHINE, FLAT CTSK HD, 30 100 DEG, STRL, CROSS RECESSED 13.1 #86 NIS24694C7 SCREW, CSK -100 DEGREE - 5 STRUCTURAL - ST 13.1 #87 NA51149CN816R WASHER-FLAT CRES 36 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM Page 20 of 64 tat W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811160 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Part number: Description Quantity 13.1 #88 M524694-C7 SCREW. MACHINE, FLAT CTSK HD, 7 100 DEG, STRI, CROSS RECESSED 13.1 #89 MS21043-08 NUT, SELF LOCKING, REDUCED H 36 13.1 #90 M524694-C7 SCREW, MACHINE, FLAT CTSK HD, 24 100 DEG, STRI, CROSS RECESSED 13.1.1 #1 NA51581K4R5 BOLT 22 13.1.1 #2 NA51580V3R6 SCREW I50 Services: Ref. No. Description Quantity 13.1 #3 Vendor Supplied Labor 1.00 13.1 #1 IAS. Carders. 13.1.6.8 hrs. 2/5-2/11 1.00 13.1 #2 1AS, Carders. 13.1.6.8 hrs, 2/12-2/18 1.00 13.1.2 #1 1AS Graf, David 20.0 HRS item 13.1.2 1.00 13.13 #1 1AS Biddle. Brett 40.0 IIRS and 4.0 HRS OT item 13.1.3 on 1.00 12/11/17-12/14/17 13.13 #2 1AS Graft. David 11.O IIRS item 13.13 on 12/13/17 1.00 13.1.5 #1 1AS Blanton 40 hrs + 5Inrs ot 13.1.5 12/17 1.00 13.1.6 #1 IASSIKES,12/25-12/31.13.1.6.„16 HOURS 1.00 13.1.6 #2 1AS , Sikes ,13.1.6 , 46hrs. , 1/8 - 1/13 1.00 13.1.6 #3 1AS, Johnson,I3.1.6, 2 hrs. 1/29-2/4 1.00 Step: 13.1.1 Completed Mechanical Paint Traveler Step: 13.1.1.1 Completed Temporarely install of panel 325AT. and panel 337CT for paint traveler per G550 AMM 55-30-00 Rev.Nov 15/17. Ref.13.1.1 Step: 13.1.1.2 Completed Remove panel 325AT. and panel 337CT after completion of paint traveler per G550 AMM 55-30-00 Rev.Nov 15/17. Ref.17.1 Step: 13.1.1.3 Completed Complied with landing gear cycling operational checks. No faults noted at this time. Work done per G550 MOM 3240-00. Nov 15117 Step: 13.1.1.4 Completed Panel 325AT installed. needs sealant, panel 337C1waiting for ops checks prior to final installation Step: 13.1.1.5 Completed Complied with Aircraft paint traveler RSQCT-330Rev.8. Ftetpaper copy for work performed. Step: 13.1.2 Completed Strip Aircraft Step: 13.13 Completed Prep Aircraft Step: 13.1.4 Completed Layout Aircraft Step: 13.1.5 Completed Paint Aircraft Step: 13.1.6 Completed Detail Aircraft Step: 13.1.7 Waiting Weight and balance approval (L/P/S) Step: 13.1.7.1 Waiting Complied with the physical weighing of the aircraft as outlined in the steps of RSQCT lnsp 15 Rev 17 and the 6550 Weight and Balance Manual. Step: 13.1.7.2 Completed Competed the weight and balance report and insert into the customer's weight and balance manual. Step: 13.1.8 Completed customer support Step: 13.1.9 Completed engineering support Discrepancy: 133 Radome to structure perimeter steps- detail inspection Rill side negative step of .053 out of limits, marked with masking tape with arrows per 6550 AMM 53-02-01 Rev. Nov 15/17. Ref.Piant traveler II A. Resolution: Complied with engineering disposition on item 133.1.1 see steps below for all work preformed Billing Method Hours Rate Total Labor USD: Time and Material ST 0.45 @ $146.00 $65.70 Labor USD: Time and Material ST 0.25 @ $222.00 $55.50 Total USD: $121.20 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM Page 21 of 64 tat W. GAC_RevenueSquawkslnvoice.rpt v3 EFTA00811161 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Step: 133.1 Completed Request engineering disposition to correct R/Ii 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 CR.005300001 Rev. - ."Aerodynamic Filler Sweep - Fair Procedure - Radome Steps". This Gulfstream Service Letter (GSL) is classified as a Manufacturer's Service Document and is governed by Advisory Circulars 20-176A and AC 120-77. Completing a repair per a Gulfstream Service Letter is similar to completing a repair per the Structural Repair Manual (SRM): No serial number specific FAA Form 8100-9 is required and will not be provided in support of a GM. repair. The Engineering (Source) Data for this Service Letter has been shown to comply with the applicable FAR's and is FAAApproved. Engineering source data is retained by Gulfstream as proprietary data. Step: 133.2 Completed Request paint to comply with engineering dispo during full strip and paint, ref item 13.1 Step: 13.3.3 Completed Comply with post-paint radome to fixed structure perimeter steps and gap measurements. Discrepancy: 133 Replace MED belicrank cover hardware where attaches at airstair riser rail with unpainted screws and washers per customer request. Resolution: Replaced MED hardware with correct hardware PN:AN525-832-7 per Drawing 159B140023 Revd]. Billing Method Hours Rate Total Parts USD: Time and Material $126.65 Total USD: $126.65 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 13.541 AN525-832-1I SCREW I $7.27 $7.27 13.542 NA51149DN816H WASHER, FLATALUMINUM 10 $0.23 42.30 13.543 MS210421.08 NUT, SELF LOCKING 10 $0.44 $4.40 13.514 AN525-832R11 SCREW I $0.22 $0.22 13.545 AN525-8321211 SCREW 5 $0.22 $LI0 13.546 AN525-8321211 SCREW I $0.22 $0.22 13.547 AN525-8321211 SCREW I 50.22 $0.22 13.548 WH832RIIDGI3WH SCREW 14 $7.87 $110.18 13.549 AN525-8321211 SCREW I $0.74 $0.74 Discrepancy: 13.7 One drain dlverter missing just forward of tail compartment door. Resolution: Replaced drain diverter PN:1159B4147517-13 just forward of tall compartment door per G550 AMM 53-51-00 RevJan 15/10. Time adhesive GAA100BD04 was applied 14:00 PM, set in 6 hours. Billing Method Hours Rate Total Parts USD: Time and Material $11235 Total USD: $11235 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 13.781 115981O47517-B DIVERTER DRAIN, AFT LOWER 1 $11235 4112.35 PANEL Discrepancy: 13.8 Customer Requests to polish and swap I.JH and FUR eventing E-light lenses. Resolution: •**Summan.*** Removed 6 et erwing emergency light lenses. Polished lenses. Reinstalled 6 °venting emergency light lenses. Sealed 6 overwing emergency light lenses. See steps below for details of work performed. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM Page 22 of 64 tit W. riAC_RevenueSquawksInvoice.rpt v3 EFTA00811162 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Billing Method Hours Rate Total Labor USD: lime and Material ST 18.00 @ $146.00 $2,628.00 Total USD: $2,628.00 Step: 13.8.1 Completed Removed 6 overwing emergency light lease covers. Step: 13.8.2 Completed Sealent required for 6 overwing emergency light loose coven Item: 14 Photographic Documentation - (Ref. Item D 2.1 of Proposal 104 7037536. ROO) Team Manager: Charles Thomas Part/Model #: 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 Part/islodel #: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSWISO: CSN/CSO: Aircraft Time: Discrepancy: 15.1 Jet ConneX (Ka-band) I firth-Speed Data System Installation Gulfstream will install this latest version of high-speed Broad-Band data system. One (1) Modem Manager (MODMAN) will be installed in the aft baggage compartment in a new cabinet. If Sat TV is installed, the existing cabinet will be modified and reused unless the cost exceeds the new cabinet installation. As the overall manager for the system, the MODMAN is responsible for providing the user interfaces to the aircraft/passengers. One (I) Aeronautical Personality Module (APN1) will be located in the baggage compartment equipment cabinet and holds the configuration data for the system. One (I) Ka-band Aircraft Network Data Unit (KANDU) will be installed in the boiler room. The KANDU receives commands front the MODMAN through an Ethernet Interface to configure the antenna/KRFU and reports status over this Ethernet interface One (I) Ka-band Frequency Unit (KRFU) will be installed in the proximity of the TMA assembly on top of the tail empennage. The KRFU contains a Block-Down Converter (BDC) to convert the received Ka-band frequencies to IF frequencies and also is made up of a Block-Up Convener (BUC) to convert the IF frequencies to Ka-band frequencies. A Iligh- Potter Amplifier (IIPA) increases the signal strength for transmission by the antenna. One (I) Tail Mounted Antenna (TMA) will be mounted on top of the tail empennage underneath the radome. The antenna system is to acquire and establish communications with satellites in various orbits to enable beyond lineof- sight communications between airborne, ground fixed, and ground transportable terminals. The Radome will be removed and replaced by a new Ka-band capable radome. Certification: The Jet ConneX (Ka-band) High-Speed Data System along with the Satcom Direct Router will be installed via Gulfstream STC; expected, availability of STC, 4th Quarter 2017. n* SEE APPENDIX *** For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoicc.rpt v3 Page 23 of 64 tit W. EFTA00811163 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: Complied with installation of Jet ConneX (Ka-band) High-Speed Data System per STC ST03238AT-D Index List GC413038007 Rev R. Configuration Lists 6C513038031 Rev A, GC513038034 Rev A, and GC513038035 Rev —. Reference Custom Electrical Drawing List CE51 496???? Rev ?? and Custom Mechanical Drawing List CE5200???? Rev ?? for deviations. Complied with GC41 429G002 Rev — and GC51 303G007 Rev — Ground Test Plans with no defects noted. Instructions for Continued Airworthiness GC51 303A004 Rev F applicable to this installation and incorporated into maintenance program. Airplane Flight Manual Supplement GC51 303M005 Rev F incorporated into Flight Manual Reference GWBR000000160 Rev — for Weight and Balance Supplement. Reference GC51 4696768 Rev — for Electrical Load Analysis Ref 15.30 for Cockpit Storage Box upuolstered with Grospoint Poster P/N GPFR0242 (Ref work 15.20) Reference CE51 4696543 Rev -- for Electrical Load Supplement. One ( I ) SDR will be installed in the aft baggage and interfaced with the existing aircraft internet capable systems. New wiring for the 3C cellular antenna will be installed in the cabin in an engineering approved location. If the aircraft has an existing Gogo system installed, the SDR will be integrated with the Gogo utilizing existing Ethernet provisions for single MID, unless otherwise directed by Ow ner/Operator. If provisions are not present, Ethernet cabling will be quoted as a separate item. New Components: One (1) 90400012-0001 - Honeywell Modem Manager (MODMAN) One (I) 90401121 - Honeywell Aeronautical Personality Module (APM) One (I) 90401202 - Honeywell Ka-band Frequency Unit (KRFU Convection Cooled) One (1) 90400013-0001 - Honeywell Tail Mounted Antenna (TMA) One (I) 90401566 - Honeywell Ka-band Aircraft Network Data Uolt (KANDU) One (I) 1233-F-2191-10 - Satcom Direct Router (SDR) One (I) Radome Various Installation Kits Certification: The Jet ConneX (Ka-band) High-Speed Data System along with the Satcom Direct Router will be installed via Gulfstream STC: expected. availability of STC. 4th Quarter 2017. Notes: If an existing Sat TV system is removed to accommodate the Ka band system the CMS software may be modified to remove the Satellite Television. This modification is not included in the sell price of the Ka band system and will be provided after a detailed engineering review is completed. estimated charges approximately 518,000. Changes to the Aircraft's Completion Center Maintenance Handbook (COUR), or Cabin Operating Manual (COM) are not included as part of this Proposal. Should a modified CCMH or COM be requested by the Customer, it may be provided at additional charge. Gulfstream may require assistance front the Customer's Information Technologies (IT) department for the configuration of the high speed data system. Notes: (continued) This involvement will verify proper system configuration as well as provide system simplicity to the operator. This will be coordinated at the time of installation and will be completed prior to delivery of the aircraft. The Customer must establish and maintain a service subscription for the Ka-band system. Quote assumes sufficient space is available for the equipment above and does not include relocation of equipment to provide space. This installation is a managed program. Please contact your Regional Sales Manager to coordinate the availability of components and installation. Billing Method Hours Rate Total Labor USD: Flat Rate 5192.054.00 Pans USD: Flat Rate 5492.946.00 Semites USD: No Charge N/ C For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM GAC_RevenuaquawksInvoice.rpt v3 Page 24 of 64 tat W. EFTA00811164 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Total USD: 5685,000.00 Parts: Ref. No. Part number: Description Quantity 15.1 #1 I233-F-2191-I0 SATCOM DIRECT ROUTER 15.1 #2 100-1021-30 ANTENNA 15.1 #3 100-1021-50 ANTENNA 15.1 #4 PE9079 ADAPTER, TNC TO SMA 2 15.1 #5 PI8350-001 TERRETRIAL MODEM ANTENNA 15.1 #6 ST03238AT-D INSTALLATION OF SATCOM (HIGH SPEED DATA HD-I28) SYSTEM 15.1 #7 GPM004001402-301 PEDESTAL SWITCH PANEL ASSY 15.1 #8 27498-001 SLEEVE 2 15.1 #9 27498-006 SPACER 15.1 #10 GAC830T3 CONNECTOR 15.1 #11 M24308/4-3F PLUG, D-SUB, 25-PIN 15.1 #12 M24308/2-3F RCPT, SOCKET, D-SUB, 25-20 GA 15.1 #13 DB115339-22 BACKSHELL 15.1 #14 27498-006 SPACER 15.1 #15 GPM004001714-301 KA PED OVERLAY 15.1 #16 27498-001 SLEEVE 15.1 #17 27498-008 SPACER 15.1 #18 hIS27473T12F3S CONNECTOR 15.1 #19 M85049/49-2-12N BACKSHELL 15.1 #20 N1S27473T16F55S CONNECTOR 15.1 #2I M85049/49-2-161C BACKSHELL 15.1 #22 N1S27473T18F35S CONNECTOR 15.1 #23 M85049/49-2-181C BACKSHELL 15.1 #24 27500-010 SWITCH 15.1 #25 500-35750-101 KIT, SDR COAX CABLE 15.1 /426 PI6917-001 REMOTE WIFI ANTENNA 15.1 #27 GAR540BY16 RING 15.1 #28 GAR540BY22 RING 6 15.1 #29 D20419 CLIP 100 15.1 #30 GAC861AH424S CABLE, ONE CONTINUOUS LENGTH 100 ON SPOOL 15.1 #3I GAB511AB6B5 BOLT, PROTRUDING SHEAR HEAD, 41 TITANIUM 15.1 #32 GAB511AB6B6 BOLT 30 15.1 #33 GAB511AB6B7 BOLT 40 15.1 #34 GAB511AB6B8 BOLT, PROT SHEAR HEAD, TI 20 15.1 #35 GABSIIAB6B4 BOLT IS 15.1 #36 GAB5I [ABM BOLT, PROTRUDING SHEAR HEAD, 4 TITANIUM 15.1 #37 GAN510AA6 COLLAR, SHEAR 70 15.1 #38 GAB511AB6B5 BOLT, PROTRUDING SHEAR HEAD. 41 TITANIUM 15.1 #39 GAB511AB6B5 BOLT, PROTRUDING SHEAR HEAD. 41 TITANIUM 15.1 #40 GAS830AJ2 SOLDER SLEEVE (BRAID) I00 15.1 #4I GAS830All I SOLDER SLEEVE (PIG TAIL) 100 15.1 #42 GA11051110-08 LUG,TERMINAL,YELLOW,H8 50 15.1 #43 GAT8051118-3B TERMINAL 50 15.1 #44 GA11051118-36 TERMINAL 50 15.1 #45 GA11051118-08 LUG, TERMINAL, RED, #8 50 15.1 /446 324484 CAP END 100 15.1 #47 GAT805P8-08 TERMINAL 20 15.1 #48 GAT8051110-3A TERMINAL 75 15.1 #49 5684-01 CLIP ASSEMBLY. 90 DEG. ANGLE 50 15.1 #51 173H7100 HINGE BASE (BLUM LARGE) 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: 3/7/2018 3:15:05PM Page 25 of 64 tat W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811165 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity 15.1 #52 GA436-5/3 PANEL ASSY-CONSOLE BLANK 2 (COLOR GREY) 15.1 #53 NAS1581K4R6 BOLT 2 15.1 #54 110872 TNC CONNECTOR, STRAIGHT PLUG 3 15.1 #55 M24308/2-1F RCPT, D-SUB, 9-SOCKET I 15.1 #56 GAR835NK1 RELAY I 15.1 #57 65009-001-513 SOCKET I 15.1 #58 CTJ716E01D-513 DEU COMPOSITE TERMINATION 1 SYSTEM 15.1 #59 1-480698-0 PLUG 1 15.1 #60 ABMM-A-C CABLE, TIE MOUNT 20 15.1 #61 1032.119-24 B/R INSERT, THREADED 50 15.1 #62 225791-3 INSERT, SIZES FOR RG188 2 15.1 #63 P18350-001 TERRETR1AL MODEM ANTENNA I 15.1 #64 D38999/26FD19SN CONNECTOR, PLUG I 15.1 #65 D38999/26FC4PN CONNECTOR I 15.1 #66 AS21919WDG23 CLAMP I 15.1 #67 M53367-1-9 STRAP. TY WRAP 1.000 15.1 #68 NAS1802-3-13P SCREW, HEX HD, CRUCIFORM REC. 10 FULL THD, A286 CRES 15.1 #69 NAS1802-3-8P SCREW 10 15.1 #70 hIS210421.3 NUT 20 15.1 #71 NA51149F0332P WASHER. FLAT STEEL 30 15.1 #72 NAS1802-3-10P SCREW. HEX HD, CRUCIFORM REC, 10 FULL THD. A286 CRES 15.1 #73 hIS27039C0807 SCREW-MACHINE. CRES PAN HD, 10 STRI. 15.1 #74 NA51149FN832P WASHER. FLAT STEEL 10 15.1 #75 M525083-7BB11 JUMPER, BONDING CNT I 15.1 #76 310701 CABLE, COAX 50 15.1 #77 CTR002 PLUG, TNC, 90 DEGREE I 15.1#78 BTS002 RCPT,TNC BULKHEAD I 15.1 #79 2-139N602-70 0 -RING 2 15.1 #80 E1257-70/2-0I5 0 RING RUBBER 2 15.1 #81 NAS1580C3T12 BOLT 10 15.1 #82 BTS002 RCPT,TNC BULKHEAD I 15.1 #83 CTR022 CONNECTOR I 15.1 #84 27500-044 SWITCH I 15.1 #85 C75-520/20 CONTACT 30 15.1 #86 XP-610 PRINTER, EPSON I 15.1 #87 ABMM-A-C CABLE, TIE MOUNT 15 15.1 #88 M24308/4-1F CONNECTOR I 15.1 #89 MS35207-269 SCREW 6 15.1 #90 D436-36 SLEEVE 200 15.1 #91 GAC860K-1 END CAP, WHITE 300 15.1 #92 324485 WIRE END CAPS 150 15.1 #93 GAC860K-3 END CAP-BLUE 100 15.1 #94 GAC860K-4 END CAP (YELLOW) 100 15.1 #95 CTS002 PLUG, TNC, STRAIGHT I 15.1 #96 CTS022 CONNECTOR I 15.1 #97 GARI00B2B0031 RUBBER .031 SHEET 9 15.1 #98 MS35207-260 SCREW 50 15.1 #99 MS35207-262 SCREW 50 15.1 #100 MS35207-264 SCREW 50 15.1 #101 MS35207-266 SCREW, MACH, PAN HEAD, CROSS 50 REC, CARBON STL, CADMIUM PLD 15.1 #102 GANIOW1032 NUT 100 15.1 #103 NAS1149D0316H WASHER 100 15.1 #104 NAS1149F0363P WASHER. FLAT STEEL 100 For detail description of the work complied with sec the Work Order Detail report. Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM Page 26 of 64 tat W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811166 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Pans: Ref. No. Pan number: Description Quantity 15.1 4105 NAS1149F0332P WASHER. FLAT STEEL 100 15.1 4106 GAS805K3 SPLICE 30 15.1 #107 GAC860N08 CAP D300-08 30 15.1 #108 GAC860N12 CAP 30 15.1 #109 GAC860N18 CAP, SPLICE 30 15.1 #110 VS-08-RJ45-5-(//1P20 CONNECTOR, RJ45 (GRAY) 15 15.14/111 M81969-1-01 INSERT/EXTRACT GREENAYHITE 8 METAL 15.1 #112 91066-4 EXTRACTOR TOOL 8 15.1#113 M81969-14-0I EXTRACTOR, GREENPNHITE 12 PLASTIC 15.1 #114 M81969/14-10 TOOL, ORANGE/RED INSERTION 15 AND EXTRACTION 15.1 #115 M15570-22-I TOOL 15 15.1 #116 hIS27039C1-12 SCREW. PAN HEAD, X RECESSED 4 15.1#117 294-541 EXTRACTOR, AMOHENOL I 15.1 WI III GARI00B2B0063 RUBBER .063 SHEET 5 15.1 #119 1159AV33022-5 CIRCUIT BREAKERASSEMBLY 1 (ESDS MATERIAL) 15.1 #120 58T-101 EATON EXTRACTION TOOL 1 15.1 #121 43031-0009 PIN 15 15.1 #122 90401566 KA-BAND AIRCRAFT NETWORK I DATA UNIT (KANDU) 15.1.5#1 GC524980001-121 BRACKET ASSEMBLY 2 15.1.5 #2 14524694555 SCREW, 100 DEGREE CSK 30 STRUCTURAL 15.1.5 43 M527039-I-04 SCREW, PAN HEAD MACHINE 30 15.1.5 44 GSM805001267-10 I ANGLE 2 15.1.5 45 GSM806002351-101 BRACKET 2 15.1.5 46 CB200-40 ADHESIVE, ACRYLIC (DUAL PACK 3 CARTRIDGE) PLUNGER PLA050-10 40 ML 15.1.5 47 021200-50009 NOZZLE, STATIC MLXER, SHORT 100 GOLD NOZZLE FOR 1.5OZ 15.1.5 48 CCS1005-09-48.00 ANGLE 1 15.1.5 49 CCS1005-33-48.00 ANGLE 1 15.1.5 410 NAS1836-06-10 INSERT 20 15.1.5 411 MS35206-226 SCREW 20 15.1.5 412 TC141 BRACKET, TIE -DOWN 20 15.1.5 413 MS21266-7T GROMMET, PLASTIC, EDGING 2 15.1.5 414 M53339-4-9 PLATE MOUNTING 5 15.1.5 415 NIS20470A4-5N RED RIVET 25 15.1.5 416 NASI149DN832J WASHER 25 15.1.5 417 GAB51IGA3-4 BOLT 100 15.1.5 418 GAB51IGA3-6 BOLT 100 15.1.5 419 GAB51IGA3-7 HI-BOLT 100 Services: Ref. No. Description Quantity 15.1.1 41 REF.. M. Eddy, 15.1.1, 3.0 hrs, 11/27 -12103/2017 1.00 15.1.1 42 REF.. Eddy. 15.1.1, 3 HRS, 11/27 - 12/03 1.00 15.1.2 41 AETS. Molnar..15.1.2, 1.0 hrs, 1)22 -112812018 1.00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/712018 3:15:05PM Page 27 of 64 tit W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811167 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Step: 15.1.1 Waiting Avionics Engineering Labor Avionics approval (L/P/S) Step: 15.1.2 Waiting Mech Engr Labor Avionics approval (L/P/S) Step: 15.13 Waiting AVI Systems Test Labor Only approval (L/P/S) Step: 15.1.4 Waiting AVI /Electrical Labor Only approval (L/P/S) Step: 15.1.5 Waiting AVI Sheet Metal Labor Only approval (L/P/S) Step: 15.1.5.1 Completed Lightly scuff sanded 5" area around routed area. then cleaned area with cheese cloth and isopropyl alcohol. Cut and impregnated 3 plies of 120 style fiberglass cloth with 828 resin. Applied impregnated fiberglass on routed area and vacuum bagged and 24 inches of mercury. Let dwell for 1 hour and heat cured at 140 for 4 hours. After cure sanded excess resin smooth to blend new plies into original contour. Reference engineers dispo ## 15.8.1.1 Step: 15.1.6 Completed INT Support (R&R) Labor Only Step: 15.1.7 Waiting SC Ntaintenancefflangar / Primary Codes /Touch Labor Only approval (L/P/S) Step: 15.1.8 Waiting SC Paint Labor Only approval (L/P/S) Step: 15.1.9 Waiting Inspection Labor Only approval (L/P/S) Step: 15.1.10 Waiting Weight and Balance Labor Only approval (L/P/S) Item: 16 KA BAND HARNESS FABRICATION Team Manager: Charles Thomas Part/Model 8: Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSN/TSO: CSN/CSO: Aircraft Time: Item: 17 ASC 085A X61 Weather Installation - (Ref. Item B 2.3 of Proposal ID# 7038248 R02) Team Manager: Charles Thomas Pan/Model ft: 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: 3/7/2018 3:15:05PM Page 28 of 64 tat W. GAC_RevenueSquawksinvoice.rpt v3 EFTA00811168 Bill To: Plan D, LLC. WO #: SC52166I Invoice Number: 5517132452 Discrepancy: 17.1 ASC 085A XN1 Weather Installation This Service Change installs an antenna, receiver, two (2) data ports and associated wiring for the XM satellite weather system. Either a fore or an aft installation may be selected based on aircraft configuration. Aircraft that are provisioned for XM installation may require an engineering review to complete the installation. Provisions may include wiring, antenna, receiver, data ports or any combination of these components and are typically installed during completion. Prerequisites: ASC 908 - PlaneView Master Operating Software System Software Update (Cert Fox) Prior to. or at the time this ASC is ordered, operators will be required to supply a configuration report of the Central Maintenance Computer (CMC). The CMC report can be stored on the aircraft PC laptop then electronically submitted to Culfstream at asc.softwareCrgulfstream.com. Allow three (3) to five (5) days for the CMC report review and up to twenty-one (21) days for the creation of a new Options Data disk. Effectivity: This Service Change is applicable to aircraft Serial Numbers 5001 - subsequent. Notes: Interior access to perform this installation is not included in the kit price. Aircraft configuration. installation location of the system and availability of spare wiring may impact labor hours, amount of access required and could necessitate additional engineering. This ASC is a managed program. Incorporation must be coordinated through Culfstream Aircraft Scheduling at 800-810-GULF (4853) or 912-965-4178. If not scheduled, aircraft downtime could increase significantly. This Service Change may only be installed at a Culfstream Aerospace facility. Resolution: Complied with ASC 085A XM Weather Installation Ref Item 17.2 CN1P 970851 Billing Method Hours Rate Total Labor USD: Flat Rate $16,060.00 Pans USD: Flat Rate 563,940.00 Total USD: 480,000.00 Parts: Ref. No. Pan number: Description Quantity 17.1 #1 A.SC0S5A-1 GSSP KIT, XM SATELLITE WEATHER I INSTALLATION, 5001-SUB(KIT ONLY) 17.182 RGI42Bill COAX 35 17.1#3 HET-A-02C FERRULE, SHIELD 6 17.1 #4 PLC1.51-58 TYRAP 10 17.1 #5 BTS722 RCPT, RFTNC I 17.1 #6 CTS722 CONNECTOR 1 17.1 #8 M24308/4-IF CONNECTOR I 17.189 GAC835MR20S CONTACT 10 17.1#10 CSS722 PLUG, ShIA, STRAIGHT 1 17.1 #11 CSR722 PLUG, SMA,90° I 17.1 #12 CTS722 CONNECTOR I 17.1 #13 NIS21919WDG2 CLAMP 4 17.1 #14 NIS21919WDG4 CLAMP PTYPE-CUSHIONED,IM IN 4 17.1#15 NIS21919WDG3 CLAMP PTYPE-CUSHIONED,3116 4 INCH 17.1 #16 DCR-IA-05 RAIL I 17.1 #18 GANIOW 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 29 of 64 tit kW EFTA00811169 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 T(Xli. 1 Item: 18 ASC 912 and ASC 123 Planeview MOS Upgrade - (Ref. Item B 2.4 of Proposal ID# 7038248 R02) Team Manager: Charles Thomas ParttModcl #: 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 30 of 64 tat W. EFTA00811170 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 Gulfstreant standard III-BIL clear coat finish and polished to a predetermined luster. All applicable internal surfaces will be cleaned and retained in existing condition. Painting or recovering of the internal surfaces will he addressed on a time and materials basis. Inlays of any type such as wood. metal. or stone inlays are not included in this proposal. Existing inlays will be evaluated on a case-by-case basis and addressed on a time and materials basis. Burn certification is predicated upon the existing substrates meeting all the FAA flammability requirements. Gu[(stream is not responsible for any existing materials meeting burn requirements. The recovered doors, panels, and cabinetry will be reassembled and installed in aircraft. All adjustments will be made to ensure correct fit and function. Equipment relocation is not part of this proposal and will be addressed on a time and materials basis. ***SEE APPENDIX FOR ADDITIONAL INFO*" Resolution: Ref steps 19.2 thru 19.23, For details of veneer covered components that were removed from the aircraft and stripped of all veneer surfaces, hardwood caps, and nosing. Reveneered and new hardwood caps and nosings were completed with customer approved materials. Ref R&I for details of reinstallation REF 19.24 and 19.30 for Veneer & Hardwood Flammability Notes: Staining or Tinting Finish to achieve a specific color or grain pattern is not included in this proposal. Any finish other than natural will be evaluated and addressed on a time and materials basis. This proposal includes Natural Wood Veneer. Composite Veneer (due to ordering limitations) may require Gulfstream to purchase additional sheets of that product. Should additional sheets will be required: the Customer will be advised of the additional charges. Sharp radiuses on ledges and other cabinetry that are covered with veneer will require additional labor charges and will be accomplished on a time and materials basis. Proposal is based on reusing all applicable substrate and componentry. All plating will be accomplished on a time and materials basis. Billing Method Hours Rate Total Labor USD: Flat Rate 5169.036.00 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 31 of 64 tat W. EFTA00811171 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 &niers USD: Flat Rate 5470,155.00 Total USD: 5706,175.00 Pans: Ref. No. Part number: Description Quantity 19.1 #1 M520-01437 STAIN, RAW UMBER PENETRATING 2 19.1 #2 M520-2247 MOHAWK BLACK ULTRA 2 PENETRATING STAIN 19.1 #3 M520-00017 REDUCER, ULTRA PENETRATING 2 STAIN, GALLON 19.1 #4 P63563A LEX EDGE OUTDOR SOYD. 1 19.1 45 P77709A INTENSE RED (FOIL) 1 19.1 #6 P77685A 91M FX BLACK SPOT FOIL GERBER 1 EDGE GSP 19.1 #7 P77753A PLACARD, RUBY RED GERBER I FOIL 19.1 kt1 T1310-14 TRANSFER RITE 1310 UTRACLEAR 1 TAPE 14" x 100 VD 19.1 #9 GSE150717-1LP QTR FIG DARK EUCALYPTUS 1,139 19.1 #10 P65580A GERBER 1MAGECAST, CLEAR, IS 50 IN/38CM-P 19.1 #11 1357 NEUTRAL 5GAL ADHESIVE CEMENT, 5GAL, I GAA100AU1 19.1 #12 923450GL CLEARCOAT, MULTI-TEMP BAKING 26 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #13 929-91-3.5L HARDENER,GLASURIT FINISH 15 19.1 #14 352-91 GAL REDUCER 15 19.1 #15 8-4QTR-SAWN-MOZAMBK HARD WOOD QTR SAWN 150 MOZAMBIQUE 19.1 #20 MS2469456 SCREW 3 19.1 #21 NIS24694S6 SCREW 15 19.1 #22 hIS35206-226 SCREW 50 19.1423 222S PAINT -MID-COAT ADHESION 2 PROMOTER 19.1 #24 NAS1149FN832P WASHER, FLAT STEEL 100 19.1425 GSE150717-1LP QTR FIG DARK EUCALYPTUS 126 19.1 #26 DMA50 DISPENSING GUN KIT FOR 50hIL 1 EPDXY CARTRIDGES 19.1427 hIEGM10001 PRO SPEED COMPOUND 5 19.1 #28 P65580A GERBER IMAGECAST, CLEAR, IS 50 IN/38CM-P 19.1 #29 1357 NEUTRAL 5GAL ADHESIVE CEMENT, SGAL, 1 GAA100AU1 19.1 430 923450GL CLEARCOAT, MULTI-TEMP BAKING 6 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1432 923450GL CLEARCOAT, MULTI-TEMP BAKING 4 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #33 923450GL CLEARCOAT, MULTI-TEMP BAKING 6 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #34 929-93 GLASURIT HARDNER (35 LITER) 3 19.1#35 929-91-3.5L HARDENER,GLASURIT FINISH 2 19.1 #36 P77788A WHITE (FOIL! I 19.1 #37 DPIOOFR EPDXY ADHESIVE, 1.7 OZ 2 19.1 #38 CA40 ADHESIVE I OZ 2 19.1#39 PRONTO SURFACE ACTIVATOR 3 19.1 #45 923460GL CLEARCOAT, MULTI-TEMP BAKING I URETHANE ACRYLIC, GLASURIT (35 LITER) For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM Page 32 of 64 tat W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811172 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#53 929-91-3.51 HARDENER,GLASURIT FINISH 1 19.1 #54 929-91-3.51 HARDENER, GLASURIT FINISH 1 19.1 #55 929-91-3.51 HARDENER,GLASURIT FINISH 2 19.1 #56 832J16-2IBR INSERT 12 19.1 #57 400 EVERCOAT EVERCOAT FILLER 1 19.1 #58 GMS5005-I QT EPDXY PRIMER COATING (TYPE I) 3012 QUART KIT (44GN011 QK) 19.1 #59 282.01.701 SUPPORT, SHELF 20 19.1#611 PRONTO SURFACE ACTIVATOR 2 19.1 #63 923450GL CLEARCOAT, MULTI-TEMP BAKING 10 URETHANE ACRYLIC, GLASURIT (35 LITER) 19.1 #64 DMD1684/GL PAINT, DELTRON BASECOAT WHITE 19.1 #65 DMD1683IGL PAINT, DELTRON BASECOAT BLACK 19.1 #66 CA8000KICKER QT PAINT KICKER 2 19.1 #67 929-91-3.51 HARDENER, GLASURIT FINISH 1 19.1 #68 929-91-3.51 HARDENER, GLASURIT FINISH 1 19.1 #69 929-91-3.51 HARDENER, GLASURIT FINISH 6 19.1 #70 522-10 ACCELERATOR, DRYING ADDITIVE 19.1 #71 522-10 ACCELERATOR, DRYING ADDITIVE 4 19.1 #72 352-91 GAL REDUCER 6 19.1 #73 GMS5005-I QT EPDXY PRIMER COATING (TYPE I) 2 3012 QUART KIT (44GN011 QK) 19.1 #74 hIEGNI10001 PRO SPEED COMPOUND 4 19.1 #75 M524693-C26 SCREW, MACHINE, FLAT 12 COUNTERSUNK HD. 100 DEG. CROSS RECESS 19.1 #76 MS24694-53 SCREW, MACHINE, FLAT CTSK HD, 8 100 DEG, STRL, CROSS RECESSED 19.1 #77 22001-15 ISOLATOR 2 19.1 #78 MS27039-1-6 SCREW 143 19.1 #79 MS27039-1-09 SCREW, MACHINE PAN HEAD 150 STRUCTURAL 19.1 #80 NAS1149F0332P WASHER. FLAT STEEL 100 19.1 #81 NAS6603-7 BOLT-HEX HEAD, CLOSE 25 TOLERANCE 19.1 #82 AN970-3 WASHER. FLAT 50 19.1 #83 M527039-1-06 SCREW-MACHINE,PAN HEAD 7 19.1 #84 1032J19-24 B/R INSERT. THREADED 20 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM Page 33 of 64 tat W. GAC_RevenueSquawkslnvoice.rpt v3 EFTA00811173 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: 3/7/2018 3:15:05PM Page 34 of 64 tat W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811174 Bill To: Plan D, LLC. WO it: SC521661 Invoice Number: 5517132452 Step: 19.1.1 Completed AV1 /Electrical Labor Only Step: 19.1.2 Completed INT Sheet Metal Labor Only Step: 19.13 Completed Wood Labor Only (270 ) Deducted 270 hours from the original 1897 hours for vendor supplied labor (SAPS) Step: 19.1.4 Completed INT Finish and Paint Labor Only Total Hours 1186 Outside Labor for 11/27 to 12/6 197 hrs Outside Labor for 12/4 to 12/10 208 hrs Outside Labor for 12/11 to 12/17 58 hrs Outside Labor for 12118 to 12124 40 hrs Outside Labor for 1/2 to 1/7 90 hrs Outside Labor for 1/8 to 1/14 180 hrs Outside Labor for 1/15 to 1/21 120hrs Outside Labor for 1122 to 1/28 180hrs Outside Labor for1/29 to 214 60 hrs Outside Labor for2/5 to VII 50 hrs Step: 19.1.5 Completed NT Support (R&R) Labor Only Step: 19.1.5.1 Completed ****VOID**** Entere din wrong section Removed all old sealant from the outboard edges of the MED entn way fwd and aft bulkhead veneer pieces per .A3134 G550 20-4240 March 31/17. The edges are taped and are ready to be scaled. Step: 19.1.5.2 Completed *****VOID*** ENT in wrong section ref Applied PR 1440 BI/2 sealant to M.E.D. aft bulkhead veneer closeout at 01:00 on 3/1/2018 per 6550 AMM 20-42-00 March 31/17. Step: 19.1.6 Completed Inspection Labor Only Step: 19.1.7 Completed Flammability t Placards Labor Only Step: 19.1.8 Completed Wood Shop Labor to Strip Existing Veneer. Step: 19.1.8.1 Completed Strip Veneer - RH and LH 680 Bulkheads and Door. Step: 19.1.8.2 Completed Strip Veneer -AFT LAN' Niche and Shroud. Step: 19.1.8.3 Completed Strip Veneer -AFT Lay Vanity Step: 19.1.8.4 Completed Strip Veneer -AFT LH Closet. Step: 19.1.8.5 Completed Strip Veneer -AFT RH Closet. Step: 19.1.8.6 Completed Strip Veneer -AFT LH Galley. Step: 19.1.8.7 Completed Strip Veneer -AFT RH Galley Annex. Step: 19.1.8.8 Completed Strip Veneer - 4 Divan End Cabinets. Step: 19.1.8.9 Completed Strip Veneer -Cabin Ledges. Step: 19.1.8.10 Completed Strip Veneer - Console Tables. Step: 19.1.8.11 Completed Strip Veneer- FWD Pocket Door. Step: 19.1.8.12 Completed Strip Veneer - FWD RH and 1.11 Cabin Bulkheads. Step: 19.1.8.13 Completed Strip Veneer - PSU Handrails. Step: 19.1.8.14 Completed Strip Veneer - FWD Crew Refresh Cabinet. Step: 19.1.8.15 Completed Strip Veneer - FWD RH Lay. Step: 19.1.8.16 Completed Strip Veneer - REER and LEER panels. Step: 19.1.8.17 Completed Strip Veneer -Acoustic Door. Step: 19.1.8.18 Completed Strip Veneer - Entry Panels (2) Step: 19.1.8.19 Completed Strip Veneer - AFT LAV Door. Step: 19.1.8.20 Completed Strip Veneer - FWD Lav Door. Step: 19.1.8.21 Completed Strip Veneer - Magazine Racks. Step: 19.1.9 Completed Wood Shop Labor to Reveneer Cabinets. Step: 19.1.9.1 Completed Labor to Veneer -1.11 and RH 680 Bulkheads and Door. Step: 19.1.9.2 Completed Labor to Veneer - AFT LAV Niche and Shroud. Step: 19.1.9.3 Completed Labor to Veneer -AFT Lay Vanity. Step: 19.1.9.4 Completed Labor to Veneer -AFT LH Closet. Step: 19.1.9.5 Completed Labor to Veneer -AFT RH Closet. Step: 19.1.9.6 Completed Labor to Veneer -AFT LH Galley. Step: 19.1.9.7 Completed Labor to Veneer -AFT RH GalleyAnnex. Step: 19.1.9.8 Completed Labor to Veneer - 4 Divan End Cabinets. Step: 19.1.9.9 Completed Labor to Veneer -Cabin Ledges. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM Page 35 of 64 tit W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811175 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: 3/7/2018 3:15:05PM Page 36 of 64 tit W. GAC_RevenueSquawksinvoicc.rpt v3 EFTA00811176 Bill To: Plan D, LLC. WO SC521661 Invoice Number: 5517132452 Step: 19.1.13.1 Completed Applied PR 1440 8112 sealant to M.E.D. aft bulkhead 'veneer closeout at 01:00 on 3/1/2018 per 6550 AMM 20-42-00 March 31/17. Step: 19.1.13.2 Completed Applied PR 1440 B1/2 sealant to M.E.D. fwd bulkhead veneer closeout at 4:30pm on 3/1/2018 per 6550 AMM 20-42-00 March 31/17. Step: 19.1.14 Completed Permanently install MED airstair upper handrail bolts where handrails attach to bulkheads (NA and aft). Item: 20 Registration Change Team Manager: Charles Thomas Part/Model Customer Coordinator: Julian Brown AC Serial No/Tail No.: TSNITSO: CSN/CSO: Aircraft Time: Discrepancy: 20.1 Comply with registration change as outlined in RSQCT-115 Rev. 12. Registration change to N2I2JE. Resolution: Complied with registration change as outlined in RSQCT-115 Rev. 12. Reference steps below and traveler paper copy index 013A for details of work performed. Billing Method Hours Rate Total Labor USD: Time and Material ST 37.64 @ $146.00 $5,495.44 Labor USD: Time and Material OT 4.46 ® $146.00 $651.16 Labor USD: Time and Material ST 4.63 @ $222.00 $1,027.86 Parts USD: Time and Material $31.80 Total USD: $7,206.26 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 20.181 CTS-S22/22 CONTACT 30 $0.51 $15.30 20.182 GAS805IC2 SPLICE 30 50.22 $6.60 20.1 83 GAC860K-2 END CAP-RED 30 $033 49.90 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM Page 37 of 64 tat W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811177 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: 3/7/2018 3:15:05PM Page 38 of 64 tit kW liAC_RevenueSquawksInvoice.rpt v3 EFTA00811178 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 39 of 64 tat W. EFTA00811179 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 CUP Tasks (Exhibit 3) - (Ref. Item C 1.3 of Proposal ID# 7039702 ROO) Team Manager: Charles Thomas Pan/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: O Correction of discrepancies is not included in the quoted price. O Materials / Outside Services will be billed as required. Resolution: Billing Method flours Rate Total Labor USD: Flat Rate $8,953.00 Total USD: $8,953.00 Discrepancy: 23.12 CMP G550 282651 Main Fuel Boost Pump (Left) - Fuel Leak Check Resolution: COMPLIED WITH CMP G550 282651 Main Fuel Boost Pump (Left) - Fuel Leak Check TW 558064 Date Due 08/18 Billing Method Hours Rate Total Labor USD: No Charge N/ C Pans USD: Time and Material 51.88 Total USD: $1.88 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 23.12#1 NAS1612-3A 0 -RING. 0.188 INCH OD TUBING 4 50.47 41.88 Discrepancy: 23.17 CMP G550 323012 Landing Gear Emergency Extension Nitrogen Blow-down Bottle (Right) - (Hydrostatic) Functional Test Resolution: COMPLIED WITH CMP G550 323012 Landing Gear Emergency Extension Nitrogen Blow-down Bottle (Right) - (Hydrostatic) Functional Test Billing Method Hours Rate Total Labor USD: No ('barge N/ C Pans USD: Time and Material $2.86 Total USD: $2.86 Parts: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 23.17#1 NAS1612-4A SEAL, 0.250 INCH OD TUBING 2 5030 50.60 23.17 #2 2-212 E0540-80 SEAL -0 RING 2 $1.13 52.26 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoicc.rpt v3 Page 40 of 64 tat W. EFTA00811180 Bill To: Plan D, LLC. WO #: SC52166I Invoice Number: 5517132452 Discrepancy: 23.34 CMP G550 262620 Portable Halon Fire Extinguisher (Aft Cabin) - Removal / Installation Resolution: EOMPLIED WITH CMP G550 262620 Portable Halon Fire Extinguisher (Aft Cabin) - Removal / Installation Billing Method Hours Rate Total Pans USD: Time and Material S3.15 Total USD: S3.15 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 2334 MI 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 G550 351222 Passenger Oxygen Cylinder (No.2)- Removal / Installation Billing Method Hours Rate Total Labor USD: No Charge NI C Pans USD: Time and Material S5.31 Total USD: S5.31 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 23.43 in hIS21044C08 NUT SELF LKG-CRES.PASS1VATED 1 $0.41 $0.41 23.43 62 hIS21044C3 NUT 1 $4.90 $4.90 Item: 24 Discrepancies related to Miscellaneous CMPTasks (Exhibit 3) - (Ref. Item C 13 of Proposal ID# 7039702 ROO) Team Manager: Charles Thomas ParttModcl 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 #1 2013-BR BATTERY. EMERGENCY LIGHTS 2 51,40532 $2,810.64 Discrepancy: 24.4 (1) passanger 02 mask has a broken valve and (1) 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 Atom 35-25-01 dated June 15,2016 Billing Method Hours Rate Total Labor USD: Time and Material ST 6.50 (t! 5146.00 S949.00 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: 3/7/2018 3:15:05PM riAC_RevenueSquawksInvoicc.rpt v3 Page 41 of 64 tit W. EFTA00811181 Bill To: Plan D, LLC. WO #: SC52166I Invoice Number: 5517132452 Pans USD: Time and Material $159.46 Total USD: $1,108.46 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 24.4 #1 289-601-224-I MASK 2 579.73 S159.46 Discrepancy: 24.5 One light bulb from "No smoking" light on cabin PSU #5 LI1 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 RH. Ops ck good. PN on/off GE387 Billing Method Hours Rate Total Parts 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 BULBS/A GE387 10 5035 $3.50 Item: 25 Replace all Main and Nose tires - (Ref. Item C 1.5 of Proposal ID# 7039702 ROO) Team Manager: Charles Thomas Pan/Model Customer Coordinator Julian Brown AC Serial NoJTail No.: TSN/TSO: CSNJCSO: Aircraft Time: Discrepancy: 25.1 Remove and Replace all main and nose landing gear tires. Resolution: Summary: Removed all MLC wheel assemblies (4ea.) and NI.0 (2ea.) and routed to back shop for lire changes and NUT. reference items 34,35,36,37,38 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 NILC wheel assembly WI CMPs and 11.93 and 11.94 for NLG w heel ass). R/I CMPs See steps below Billing Method Hours Rate fowl Labor USD: Flat Rate 52.686.00 Pans USD: Flat Rate 515.350.00 Total USD: 518,036.00 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 CNIP 324001 and G550 CMP 324002 and routed to back shop for tire replacement. Step: 25.1.3 Completed Installed red wheels on NLG per AMM 6550 32-41-01 rev 3131/17 TW: 560296 Cal Due: 04/18 Step: 25.1.4 Completed Removed IJH and R/H NLG red wheels. Received ok to install and Installed L/H NLG Wheel Assy P/N 1159150400-37 SiN 508117 per CMP 6550 324002. Received ok to install and installed R/H NLG Wheel Assy P/N 1159/50400-37 S/N 508217 per ChIP 6550 324003. Serviced 14/H and R/H NIG Wheels to 120PS1 per 6550 AMM 12-33-01 Rev. June 20/13. Step: 25.1.5 Completed Installed main wheels (4) IAW 6550 CMPs 324003.324004.324005. and 324006. Ref items 11.58 thru 11.61 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: 3/7/2018 3:15:05PM Page 42 of 64 tit W. GAC_RevenueSquawksInvoiceept v3 EFTA00811182 Bill To: Plan D, LLC. WO 1r: SC521661 Invoice Number: 5517132452 Rem: 26 CUSTOMER PROPERTY OUT TO VENDOR Team Manager: Charles Thomas Customer Coordinator. Julian Brown S/N: N/A TSWISO: 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 - N415LM REQUESTED RETURN DATE - 11/9 Resolution: Recleved Blow Down Bottle Billing Method Hours Rate Total Services USD: Flat Rate 5270.60 Total USD: 5270.60 Services: Ref. No. Description Quantity 26.1 41 HYDROSTATIC TEST 1.00 Part Ref: 1159SCH233-II 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 - N415LM REQUESTED RETURN DATE - 11/11 Resolution: Recleved O2 Bottle. Billing Method Hours Rate Total Services USD: Flat Rate 52,527.80 Total USD: 52,527.80 Services: Ref. No. Description Quantity 26.2 41 HYDROSTATIC TEST 1.00 Pan Ref: 805983-IS BOTTLE, OXYGEN Discrepancy: 26.3 SEND 02 MASK TO SUPPLIER FOR RESTORE/RECERTIFY AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N415LM REQUESTED RETURN DATE 11124 Resolution: Recleved O2 Mask Billing Method Hours Rate Total Services USD: Flat Rate 52392.50 Total USD: $2.392.50 Services: Ref. No. Descripiion Quantity 26381 REPAIR 1.00 Part Ref: A1O0-15-158 MASK, OXYGEN, CREW 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: 3/7/2018 3:15:05PM Page 43 of 64 tit kW GAC_RevenueSquawksInvoice.rpt v3 EFTA00811183 Bill To: Plan D, LLC. WON: SC521661 Invoice Number: 5517132452 Discrepancy: 26.5 SEND 18 EA LIFE VEST TO THE SUPPLIER FOR RESTORE AND RETURN TO AIRCRAFT CUSTOMER PROPERTY AC 5173 TN - N415LSI 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: 5884.17 Services: Ref. No. Description Quantity Sell Price USD Extended USD 26.5 NI 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 QCP588 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. 2/22/18- 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 $1,500.00 Total USD: $1,500.00 Services: Ref. No. Description Quantity Sell Price USD Extended USD 26.6 #1 PLATING 1.00 50.00 S0.00 Part Ref: AC5173PLATINGKIT KIT 26.682 EXPEDITE FEE 1.00 $1,500.00 $1,500.00 26.683 PLATING 1.00 50.00 S0.00 Part Ref: AC5173PLATINGKIT KIT Item: 27 AIRCRAFT BATTERY (FCS EBIIA BATTERY & MAIN SHIP BATTERY) Team Manager: Charles Thomas PartModcl N: 1159SCAV519-1 Customer Coordinator: Julian Brown S/N: 0905200069DDF TSN/TS0: N/A CSN/CS0: N/A Aircraft Time: Na 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 44 of 64 tat W. EFTA00811184 Bill To: Plan D, LW. WO #: SC521661 Invoice Number: 5517132452 Item: 28 AVIATION BATTERY TYPE - CORE (FCS EBIIA BATTERY & MAIN SIIIP BATTERY) Team Manager: Charles Thomas Pan/Model #: 5317C1I-1 Customer Coordinator: Julian Brown S/N: 09052001067B3 TSN/TS0: N/A CSN/CS0: N/A Aircraft Time: N/A Item: 29 FAIRING ASSY, BULLET, FWD Team Manager: Charles Thomas Part/Model #: 1159C51152024-405 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 - N415LM 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# ->1159CS1152024-405 Seel ->NFA Final finish will apply at service center. Billing Method Hours Rate Total Labor USD: Time and Material ST 68.78 (a $146.00 $10,041.88 Labor USD: Time and Material ST 1.02 (-a $222.00 $226.44 Pans USD: Time and Material $2,318.91 Total USD: $12,587.23 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 29.1 #1 LSSQW00-0460 LIGHTNING DIVERTER I $772.97 $772.97 29.1#2 LSSQW00-0460 LIGHTNING DIVERTER I $772.97 $772.97 29.1#3 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: 3/7/2018 3:15:05PM GAC_RevenueSquawkslnvoice.rpt v3 Page 45 of 64 tit kW EFTA00811185 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Step: 29.1.1 Completed Incoming Inspection Step: 29.1.2 Completed Teardown Step: 29.13 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.1/17/06. Billing Method Hours Rate Total Labor USD: Time 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 are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 46 of 64 tit kW EFTA00811186 Bill To: Plan D, LLC. WO Si: 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 I/17/06. Discrepancy: 29.3 Puncture on LAI 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 $3,996.00 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: 3/7/2018 3:15:05PM Page 47 of 64 tat kW GAC_RevenueSquawksInvoice.rpt v3 EFTA00811187 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 F7G. 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: 3/7/2018 3:15:05PM Page 48 of 64 tit W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811188 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/6. 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.: TSWISO: CSN/CSO: Aircraft Time: Discrepancy: 30.2 CMP G550 330934 SWITCH PANEL #34 (Ref. 30.1) Resolution: COMPLIED WITH CUP G550 330934 SWITCH PANEL #34 PN OFF: 2501-2-110Q588A SN OFF: 31B3J PN ON: 2501-2-714Q588A SN ON: 48NOHIC Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Item 31 BATTERY, EMERGENCY LIGHTS Team Manager: Charles Thomas Pan/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 #: 2013-BR Customer Coordinator: Julian Brown S/N: B8663 TSNffSO: N/A CSN/CSO: N/A Aircraft Time: N/A Item: 33 BATTERY, EMERGENCY LIGHTS Team Manager: Charles Thomas Part/Modcl #: 2013-BR Customer Coordinator Julian Brown S/N: B8660 TSN/TSO: N/A CSN/CSO: N/A Aircraft Time: N/A Item: 34 MAIN WHEEL Team Manager: Charles Thomas PartfIsiodcl #: 1159SCL503-9 Customer Coordinator: Julian Brown S/N: 5159FX TSNEISO: N/A CSN/CSO: N/A Aircraft Time: 54022 11725 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: 3/7/2018 3:15:05PM Page 49 of 64 tit W. GAC_RevenueSquawksInvoice.rpt v3 EFTA00811189 Bill To: Plan D, LLC. WO #: SC521681 Invoice Number: 5517132452 Item: 35 MAIN WHEEL ASSEMBLY Team Manager: Charles Thomas Pan/Model #: 1159SCL503-7 Customer Coordinator. Julian Brown S/N: 5167FP TSN/TS0: N/A CSN/CS0: N/A Aircrafaime: 5402.8 11225 Item: 36 MAIN WHEEL Team Manager: Charles Thomas Part/Modcl #: 1159SCL503-9 Customer Coordinator Julian Brown S/N: 5I75GC TSNEIS0: N/A CSN/CS0: N/A Aircraft Time: 5402.8 / 1225 Item: 37 MAIN WHEEL ASSEMBLY Team Manager: Charles Thomas Pan/Model #: 1159SCL503-7 Customer Coordinator: Julian Brown S/N: 5188FP TSNEIS0: 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/Modcl #: 1159SCL505-7111TD Customer Coordinator Julian Brown S/N: 5082FZ TSN/TS0: N/A CSN/CS0: N/A Aircraft Time: 5402.8 Item: 39 NOSE WHEEL/TIRE ASSEMBLY-MOUNTED 1159L50400-37 Team Manager: Charles Thomas Part/Model #: 1159SCL505-7MTD Customer Coordinator: Julian Brown S/N: 5081EZ TSNfIS0: N/A CSN/CS0: N/A Aircraft Time: 5402.8 Item: 40 Customer Requested Due List Items as of 02/15/18 Team Manager: Charles Thomas Part/Modcl #: Customer Coordinator Julian Brown AC Serial No/Tail No.: N/A / N/A TSWIS0: N/A CSN/CS0: Aircraft Time: N/A Discrepancy: 40.1 CMP G550 231108 Airshow 4000 Sys Components - GVI Resolution: COMPLIED WITH CMP G550 231108 Airshow 4000 Sys Components - GVI Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.2 CMP G550 231113 Securaplane 500 Components - GVI Resolution: COMPLIED WITH CMP G550 231113 Securaplane 500 Components - Billing Method I lours Rate Total Labor USD: Flat Rate $152.00 Total USD: 5152.00 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: 3/7/2018 3:15:05PM DAC_RevenueSquawksInvoicc.rpt v3 Page 50 of 64 tit kW EFTA00811190 Bill To: Plan D, LLC. WO SC521661 Invoice Number: 5517132452 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 O550 240108 Fwd Emergency Battery - BITE / Battery Level Test Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.5 CMP G550 240109 Aft Emergency Battery - BITEJBattery Level Test Resolution: COMPLIED WITH ChIP G550 240109 Aft Emergency Battery - BITE! Battery Level Test Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: 5152.00 Discrepancy: 40.6 CMP G550 251006 Crew Scats Inertia Reel (Pilot) - Operational Test Resolution: cOMPLIED WITH CMP O550 251006 Crew Seats Inertia Reel (Pilot) - Operational Test Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.7 CMP G550 251007 Crew Scats 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 O550 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 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 51 of 64 tat W. EFTA00811191 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 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 SI 52.00 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 Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.12 CMP G550 252102 Passenger Seats Restraints - Detailed Inspection Resolution: COMPLIED WITH CMP 6550 252102 Passenger Seats Restraints - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.13 CMP G550 252104 Passenger Seats Inertia Reels - Operational Test Resolution: COMPLIED WITH CMP G550 252104 Passenger Seats Inertia Reels - Operational Test Billing Method Hours Rate Taal Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.14 CMP G550 256019 EVAS System (Left) - Periodic Inspection Resolution: COMPLIED WITH CMP G550 256019 EVAS System (Left) - Periodic Inspection Billing Method Hours Rate Taal 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 owl Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.16 CMP 6550 256205 Life Vest - Restore 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 52 of 64 tat W. EFTA00811192 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: The Squawk for this specific task shall be signed off as " Verified compliance of CMP 256205 under vender work order number SAPO17-08768 dated Feburaury 20 2018. This documentation is for CMP data base update only - no maintenance accomplished by GAC." COMPLIED WITH ChIP G550 256205 Life Vest - Restore Life Vests Restored P/N: 63600-105 S/N :L784996 P/N: 63600-105 S/N :L784997 P/N: 63600-105 S/N :L784998 P/N: 63600-105 S/N :L784999 P/N: 63600-105 S/N :L785000 P/N: 63600-105 S/N :L785001 P/N: 63600-105 S/N :L785002 P/N: 63600-105 S/N :L785003 P/N: 63600-105 S/N :1.785004 P/N: 63600-105 SIN A.785006 P/N: 63600-105 SIN :L785007 P/N: 63600-105 SIN :L785009 P/N: 63600-105 SIN :L785010 P/N: 63600-105 S/N :L785011 Billing Method Hours Rate Ioial Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.17 CMP G550 256404 Defibrillator Battery - Inspect / Check Resolution: COMPLIED WITH CMP G550 256404 Defibrillator Battery - Inspect I Check Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.18 CUP 6550 256407 Defibrillator Electrode Pads - Inspection Resolution: COMPLIED WITH CMP G550 256107 Defibrillator Electrode Pads - Inspection Billing Method Hours Rate Total Labor USD. Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.19 •""DELETE*** ChIP G550 256438 - LIFE KIT Resolution: Equipment not installed in aircraft, customer email approving deletion is on file Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.20 ChIP G550 261302 APU (Fire) Shutdown Circuit - Operational Test Resolution: COMPLIED WITH CMP G550 261302 APU (Fire) Shutdown Circuit - Operational Test Billing Method Hours Rate Total Labor USD Flat Rate $304.00 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 53 of 64 tit W. EFTA00811193 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Total USD: 5304.00 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 5228.00 Total USD: 5228.00 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 multlmeter 556315 due date:9/18 Billing Method Hours Rate Total Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.23 CMP G550 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 5152.00 Total USD: 5152.00 Discrepancy: 40.24 CMP G550 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 5152.00 Total USD: 5152.00 Discrepancy: 40.25 CMP G550 262126 Engine and APU Fire Extinguishing Firing Circuitry (API) - Integrity Test Resolution: COMPLIED WITH CMP G550 262126 Engine and APU Fire Extinguishing Firing Circuitry (APU) - Integrity Test multimeter 556315 due date:9/18 Billing Method Hours Rate -lotal Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.26 CMP 6550 262605 Portable I lalon Fire Extinguisher (Cockpit) - Visual Inspection Resolution: COMPLIED WITH CMP G550 262605 Portable Halon Fire Extinguisher (Cockpit) - Visual Inspection For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM riAC_RevenueSquawksInvoice.rpt v3 Page 54 of 64 rut ma EFTA00811194 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Billing Method Hours Rate Total Labor USD: Flat Rate 5152.00 Total USD: $152.00 Discrepancy: 40.27 CMP 6550 262626 Portable union Fire Extinguisher (Aft Cabin) - Visual Inspection Resolution: COMPLIED WITH CMP 6550 262626 Portable Haien Fire Extinguisher (Aft Cabin) - Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 40.28 CMP 6550 262646 Portable I lalon Fire Extinguisher (Aft Lavatory) - Visual Inspection Resolution: COMPLIED WITH Cup G550 262646 Portable Halton Fire Extinguisher (Aft Lavatory) - Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 40.29 CMP 6550 271011 Aileron Control and Trim Cables in Main Wheel Wells! Wing hailing 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: Ma Rate $304.00 Total USD: $304.00 Discrepancy: 40.30 CMP G550 272108 Rudder Control and Trim Cables in Main Wheel Well / Tail Compartment - Detailed Inspection Resolution: COMPLIED WITH CUP G550 272108 Rudder Control and Trim Cables in Main Wheel Well / Tail Compartment - Detailed Inspection Billing Method I lours Rate Total Labor USD: Flat Rate $304.00 Total USD: 5304.00 Discrepancy: 40.31 CMP G550 273100 ELEVITRIM CABLE(6IVVW/TAIL)-INSP Resolution: COMPLIED WITH CMP G550 273100 ELEV/TRIM CABLE(MWW/TAIL)-INSP Billing Method Hours Rate Total Labor USD: Flat Rate $912.00 Total USD: $912.00 Discrepancy: 40.32 CMP G550 276105 SPEEDBRAKE CABLE(111WW/WING)INSP 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 55 of 64 tat W. EFTA00811195 Bill To: Plan D, LLC. WO /I: SC521661 Invoice Number: 5517132452 Resolution: COMPLIED WITH CMP G550 276105 SPEEDBRAICECABLE(MWW/WING)INSP Tensiometer 66853 Due Date 05/18 Billing Method Flours Rate Total Labor USD Flat Rate $912.00 Total USD: $912.00 Discrepancy: 4033 CMP 6550 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 Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 4034 CMP 6550 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 Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 4035 CMP O550 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: 4036 CMP G550 282609 Engine heated Return Feed Dual Wall Fuel Line (Left) - Detailed Inspection Resolution: COMPLIED WITH CMP 6550 282609 Engine Heated Return Feed Dual Wall Fuel Line (Left) - Detailed Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 4037 CMP G550 282610 Engine Heated Return Feed Dual Wall Fuel Line (Right) - Detailed Inspection Resolution: COMPLIED WITH CMP 6550 282610 Engine I kated Return Feed Dual Wall Fuel Line (Right) - Detailed Inspection Billing Method I lours Rate Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 4038 CMP G550 282629 Engine Fuel Shut-off Valve (Left) - Operational Check Resolution: COMPLIED WITH ChIP G550 282629 Engine Fuel Shut-off Valve (Left) - Operational Check Billing Method Hours Rate Total Labor USD Flat Rate 5152.00 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 56 of 64 tat W. EFTA00811196 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Total USD: $152.00 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 Ratc Total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 Discrepancy: 40.40 CMP G550 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 G550 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 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 Ratc Total Labor USD: Flat Rate $608.00 Total USD: $608.00 Step: 40.42.1 Completed Comply with FDR data report from download a% placed on thumbdrne Discrepancy: 40.43 CMP G550 316205 FDR FAIL MESSAGE-OPS TEST Resolution: COMPLIED WITH CMP G550 316205 FDR FAIL MESSAGE-OPS TEST Billing Method Hours Rate Total 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 I Jeppesen - Aerospace, Communication, Navigation Data. (28 Day Interval) Expires: 28Nlar2018 Billing Method Hours Rate -total Labor USD: Flat Rate 5152.00 Total USD: 5152.00 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 57 of 64 tit W. EFTA00811197 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 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 ChIP G550 319014 Blue Disk Honeywell / Jeppesen - Electronic Terminal Charts, Geopolitical Boundaries, Airport Information Obstacle Data (14 Day Interval) Expires: 14Mar2018 Billing Method flours Rate Total Labor USD Fiat Rate $152.00 Total USD: $152.00 Discrepancy: 40.46 CMP G550 319016 Green Disk Honeywell! Jeppesen - Terrain Data (On condition or Six Month Interval) Resolution: COMPLIED WITH CMP G550 319016 Green Disk Honeywell / Jeppesen - Terrain Data (On condition or Six Month Interval) Billing Method Hours Rate Taal 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 Taal Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.48 CMP G550 321006 Main Landing Gear (Right) - Lubrication Resolution: COMPLIED WITH CMP G550 321006 Main Landing Gear (Right) - Lubrication Billing Method Hours Rate Total 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 $304.00 Total USD: $304.00 Discrepancy: 40.50 CMP 6550 322306 Nose Landing Gear Bungee - Lubrication Resolution: COMPLIED WITH CMP G550 322306 Nose Landing Gear Bungee - Lubrication Billing Method Hours Rate Total Labor USD: FM Rate $456.00 Total USD: $456.00 Discrepancy: 40.51 CMP G550 323037 Main Landing Gear Bungee (Left) - Lubrication 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 58 of 64 tut Me EFTA00811198 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: COMPLIED WITH CMP 6550 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 5456.00 Total USD: 5456.00 Discrepancy: 40.52 CMP 6550 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 Labor USD: Flat Rate $76.00 Total USD: $76.00 Discrepancy: 40.54 CMP G550 491007 APU Enclosure Thermal Blanket I Coating - General Visual Inspection Resolution: COMPLIED WITH ChIP G550 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 Parts USD: Time and Material 510.45 Total USD: $770.45 Pans: Ref. No. Pan number: Quantity Sell price USD Extended USD 40.54 MI NAS1580C3T12 BOLT 52.09 $10.45 Discrepancy: 40.55 CMP 6550 491300 APU Compartment Drain Collectors - General Visual Inspection Resolution: COMPLIED WITH CMP G550 491300 APU Compartment Drain Collectors - General Visual Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $304.00 Total USD: $304.00 Discrepancy: 40.56 CMP 6550 491301 Auxiliary Power Unit Turbine Plenum Drains - Operational Test 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: 3/7/2018 3:15:05PM riAC_RevenueSquawksInvoice.rpt v3 Page 59 of 64 tat W. EFTA00811199 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: COMPLIED WITH CMP G550 491301 Auxiliary Power Unit Tbrbine 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 ChIP G550 523003 Baggage Compartment Door Seal - Detailed Inspection Air Regulator: 556959 Cal Due:06/I8. 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 G550 523008 Baggage Door Seal Check Valve - Operational Test 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 G550 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 5912.00 Total USD: 5912.00 Discrepancy: 40.61 CMP G550 531005 External Lower Fuselage FS -4 thru FS 758 View From Ground - Zonal Inspection Resolution: COMPLIED WITH CMP G550 531005 External Lower Fuselage FS -4 thru FS 758 View From Ground - Zonal Inspection Billing Method Hours Rate total Labor USD: Flat Rate 5304.00 Total USD: 5304.00 Discrepancy: 40.62 CMP 6550 531055 Aft Cabin Below Floor FS 632 - FS 684 - Zonal Inspection For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM GAC_RevenuaquawksInvoice.rpt v3 Page 60 of 64 tat W. EFTA00811200 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: COMPLIED WITH CMP 6550 531055 Aft Cabin Below Floor FS 632 - FS 684 - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate 5912.00 Total USD: 5912.00 Discrepancy: 40.63 CMP G550 531060 Baggage Compartment Below Floor FS 684 - FS 758 - Zonal Inspection Resolution: COMPLIED WITH CMP 6550 531060 Baggage Compartment Below Floor FS 684 - ES 758 - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $608.00 Total USD: $608.00 Discrepancy: 40.64 CMP 6550 531065 External Upper Fuselage FS 63 - Fs 758 View From Ground - Zonal Inspection Resolution: COMPLIED WITH CMP 6550 531065 External Upper Fuselage Fs 63 - FS 758 View From Ground - Zonal Inspection Billing Method Hours Rate Total Labor USD: Flat Rate $304.00 Total USD: $304.00 Discrepancy: 40.65 CMP 6550 531082 Electronic Equipment Rack FS 147 - FS 181 - (Enhanced) Zonal Inspection Resolution: COMPLIED WITH CMP G550 531082 Electronic Equipment Rack Fs 147 - Fs 181 - (Enhanced) Zonal Inspection Billing Method Hours Rate Total 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 CNIP G550 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 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: 3/7/2018 3:15:05PM riAC_RevenueSquawksInvoice.rpt v3 Page 61 of 64 tat W. EFTA00811201 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 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 G550 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: Billing Method Hours Rate Total Labor USD: Flat Rate $152.00 Total USD: $152.00 Discrepancy: 40.74 CMP 6550 994045 AD 2017-20-08 - Gulfstrcam Aerospace - Gulfstream AFM Supplement Incorporation Resolution: Billing Method Hours Rate Total Labor USD: Flat Rate S152.00 Total USD: $152.00 Discrepancy: 40.75 CMP 6550 282641 APU Fuel Shut-off Valve - Operational Check Ref Item 40.20 Resolution: COMPLIED WITH CMP 6550 282641 APU Fuel Shut-off Valve - Operational Check Billing Method Hours Rate Total Labor USD Flat Rate $304.00 Total USD: $304.00 Item: 41 Discrepancies - Customer Requested Due List Items as of 02/15/18 Team Manager: Charles Thomas Part/Modcl #: 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 R/II MLC Bungee upper housing is seized on lower housing. ref. item 40.52 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 62 of 64 tit W. EFTA00811202 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Resolution: Removed kill MLG Bungee P/N 1159150903.1. Ordered and recieved new Rill MLG Bungee P/N 1159L57903-1. Reference Item 11.130 for installation of new Bungee. Billing Method Hours Rate Total Parts USD: Time and Material $4,371.44 Total USD: 54,371.44 Pans: Ref. No. Pan number: Description Quantity Sell price USD Extended USD 41.1 #1 11591.57903-I BUNGEE. MAIN LANDING GEAR 1 $4371.44 $4,371.44 Discrepancy: 41.2 Found broken grounding strap on L11 wing rear beam just outboard of flight spoiler while complying with rear beam inspection, ref item 40.67 Resolution: Summary: Removed discrepant bonding jumper and Installed new bonding jumper on L/11 wing out board of flight spoiler. Ref. ANIN1 27-63-11 Aug. 31/03. See steps below for full details of work accomplished and regulatory sign offs. Billing Method Hours Rate Total Pans USD: Time and Material $41.74 Total USD: $41.74 Pans: Ref. No. Part number: Description Quantity Sell price USD Extended USD 41.2 #1 NIS25083-7BB11 JUMPER, BONDING CNT 1 $41.20 $41.20 41.2 #2 NIS21042-3 NUT, SLF-LKG, 450 DEG. RDC HEX. 2 50.27 50.54 RDC HGT, RING BASE, NON-ORES Step: 41.2.1 Completed Removed broken grounding strap on 1111 wing rear beam outboard of flight spoiler board. Ref. AMM 27-63-11 Aug. 31/03 Step: 41.2.2 Completed Installed new grounding strap on Lilt sting out board of Right spoiler. Ref. ANINI 27-63-11 Aug. 31/03 Item: 42 Customer Eval flight Team Manager: Charles Thomas Pan/N(Ode' #: 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: 42.1 Comply with customer eval flight. Resolution: Billing Method Hours Rate Total Labor USD: Time and Material ST 22.73 ® 5146.00 $3,318.58 Labor USD: Time and Material OT 0.07 @' 5146.00 $10.22 Total USD: $3,328.80 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). Printed: 3/7/2018 3:15:05PM Page 63 of 64 tit W. riAC_RevenueSquawksInvoice.rpt v3 EFTA00811203 Bill To: Plan D, LLC. WO #: SC521661 Invoice Number: 5517132452 Step: 42.1.1 Waiting Perform Preflight Inspection. approval (L) Step: 42.1.2 Waiting Perform Tool Clearance procedure as outlined in SOP 3.028. approval (L) Step: 42.1.3 Waiting "Comply stab evaluation flight technical support to observe or correct interior articles approval (L) fitment or operation. All in flight actions are to be coordinated and approved by the pilot in command. Record entry to be made in work order upon return." Step: 42.1.4 Waiting Perform Inbound Inspection as outlined in RSQCT 0056 approval (L) Step: 42.1.5 Waiting Update aircraft hours and landing, engine hours and cycles and APU hours for the approval (L) appropriate Items as applicable. 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: 3/7/2018 3:15:05PM GAC_RevenueSquawksInvoice.rpt v3 Page 64 of 64 tat W. EFTA00811204

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