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FBI VOL00009

EFTA00811141

64 sivua
Sivut 1–20 / 64
Sivu 1 / 64
PRELIMINARY INVOICE 
IlfSfreani
t
DVNAMIC• COMININV 
500 Ciulfstream Rd. - Savannah, Georgia 31407 - 
Part/Model #: G550 
AC Serial No./Tail No.: 5173 / N415L111 
Mail Remittance To: 
Gulfstream Aerospace Corporation 
Overnight Remittance To: 
Gulfstream Aerospace Corporation (Box # 730349) 
do JP Morgan Chase Bank, NA 
ATTN: Dallas National Wholesale Lockbox TXI-0029 
14800 Frye Road 
Ft. Wash, TX 76155 
Wire Remittance To: 
Ciulfstream Aerospace Corporation 
JP Morgan Chase Bank. NA 
Chicago, IL 60670 
Account No. 10-15825 
Fedwirc Routing No. (ABA) 021 000 021 
S.W.I.F.T. CHASUS33 
ACH Credit Routing No. (ABA)071 000 013 
Bill To: Plan D, LLC. 
6100 Red Hook Quarters B3 
St. Thomas. 00802 
Virgin Islands US) 
Title: Plan D, LLC. 
Invoice Number: 
Invoice Date: 
Customer ID: 
P.O. Number: 
Repair Station: 
In Date: 
Out Date: 
Payment Type: 
Payment Temis: 
5517132452 
12/12/2017 
BP502 
Lindsay' 
FAA CRS CRC:1216M 
10/23/2017 
03/09/2018 
CIA- Wire 
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). 
GAC_RevenueSquawksInvoice.rpt v3 
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Bill To: Plan D, LLC. 
WO #: SC521661 
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 
Invoice Number: 5517132452 
*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: [email protected] 
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). 
GAC_RevenueSquawksInvoice.rpt v3 
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Bill To: Plan D, LLC. 
WO #: SC521661 
Invoice Number: 5517132452 
Item: 1 
Airframe Culfstream C550 
Team Manager: 
Customer Coordinator: 
Charles Thomas 
Julian Brown 
Pan/Model #: 6550 
AC Serial No/Tail No.: 5173 / N415LM 
TSN/TSO: 
CSN/CSO: 
Aircraft Time: 
Discrepancy: 1.17 
Consumables & Shop Supplies 
Resolution: For billing purposes only. 
Parts USD: 
Billing Method 
Hours 
Rate 
Total 
Flat Rate 
$5,000.00 
Total USD: 
$5,000.00 
Discrepancy: 1.27 
Resolution: 
Sales Concession 
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 
Resolution: 
Item written to invoice labor and materials not covered by Rolls Royce Corporate Care Contract 
Billing Method 
I lours 
Rate 
Total 
Labor USD: 
Flat Rate 
Pans USD: 
Flat Rate 
Total USD: 
$2,255.16 
$45.00 
52.300.16 
Item: 2 
ENGINE BR700-710C4-11 
Team Manager: 
Charles Thomas 
Customer Coordinator: 
Julian Brown 
Part/Model 11: BR700-710C4-II 
S/N: 15-149 
TSNffSO: 
CSN/CSO: 
Aircraft Time: 
Item: 3 
ENGINE BR700-710C4-11 
Team Manager: 
Customer Coordinator: 
Charles Thomas 
Julian Brown 
Part/Model #: BR700-710C4-11 
SIN: 15448 
TSN/TSO: 
CSNJCSO: 
Aircraft Time: 
Item: 5 
Technical Bulletins (ASC, CB, SB, AD, ACB) 
Team Manager: 
Charles Thomas 
Customer Coordinator: 
Julian Brown 
Part/Model #: 
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). 
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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: 
Customer Coordinator: 
Charles Thomas 
Julian Brown 
Part/Model /I: 
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). 
GAC_RevenueSquawksInvoice.rpt v3 
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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 
Labor USD: 
Time and Material 
Pans USD: 
No Charge 
Total USD: 
Pans: 
ST 
Hours 
Rate 
Total 
3.51 
@ 
$146.00 
$512.46 
N/C 
$512.46 
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 
Labor USD: 
Services USD: 
Total USD: 
Step: 6.5.1 
Billing Method 
Hours 
Rate 
Total 
Flat Rate 
Flat Rate 
Completed 
Created one Settings and Riggings per GER 5767 
$438.00 
$762.00 
$1,200.00 
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). 
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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. 
6.8#1 
6.8 #2 
Step: 6.8.1 
Step: 6.8.2 
Pan number: 
Description 
Quantity 
Sell price USD 
Extended USD 
447HW151XNI0902 
BACKSHELL 
I 
$323.22 
$323.22 
N181969/14-01 
INSERTION/EXTRACTION TOOL, 
GREEN 
5 
$1.20 
$6.00 
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. 
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 -. 
Labor USD: 
Billing Method 
Hours 
Rate 
Total 
Time and Material 
ST 
1.00 
® 
$146.00 
$146.00 
Total USD: 
$146.00 
Discrepancy: 6.11 
Resolution: 
Cabin Upwash will not dim from AFT VIP seat or AFT galley switch panels 
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). 
GAC_RevenueSquawksInvoice.rpt v3 
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Bill To: Plan D, LLC. 
WO #: SC52166I 
Invoice Number: 5517132452 
Step: 6.11.1 
Step: 6.11.2 
Step: 6.11.3 
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 581PS1 PI 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 -. 
Wailing 
Reinstall entry way carpet and padding (Interior 
Vest/Crewrest 108-101)) 
approval 
(LIP) 
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 
Customer Coordinator: 
Julian Brown 
Pan/Model 11: 
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. 
Labor USD: 
Billing Method 
Hours 
Rate 
Total 
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. 
Labor USD: 
Pans USD: 
Billing Method 
Hours 
Rate 
Taal 
Time and Material 
Time and Material 
ST 
2.00 
® 
5146.00 
5292.00 
$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). 
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Bill To: Plan D, LLC. 
Total USD: 
WO #: SC52166I 
Invoice Number: 5517132452 
$508.52 
Pans: 
Ref. No. 
 Pan number: 
Description 
Quantity  
Sell price USD 
Extended USD 
7.14 #1 
SUPER 8-OPN-DD 
BEARING, LINEAR, BALL, 
ACOUSTIC DOOR 
4 
$UM 
S216.52 
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 
Pans USD: 
Time and Material 
Total USD: 
Pans: 
32,920.00 
$298.56 
33,218.56 
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 - 
Labor USD: 
Billing Method 
Hours 
Rate 
lival 
Time and Material 
ST 
6.62 
Qa 
5146.00 
S966.52 
Total USD: 
$966.52 
Item: g 
Mechanical 
Team Manager: 
Charles Thomas 
Customer Coordinator: 
Julian Brown 
Part/Model #: 
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). 
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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. 
Labor USD: 
Pans USD: 
Total USD: 
Pans: 
Billing Method 
Hours 
Flat Rate 
Time and Material 
Rate 
Total 
$2,336.00 
$18,672.83 
$21,008.83 
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 
approval 
Waste tank "full" light does not go off. 
(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) 
Labor USD: 
Parts USD: 
Total USD: 
Pans: 
Billing Method 
Hours 
Time and Material 
Time and Material 
Rate 
Total 
ST 
2.40 
(a 
5146.00 
$350.40 
$268.82 
$619.22 
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). 
GAC_RevenueSquawksInvoice.rpt v3 
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EFTA00811149
Sivu 10 / 64
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. 
Labor USD: 
Billing Method 
Hours 
Rate 
Total 
Time and Material 
ST 
0.90 (-0, 
$146.00 
$131.40 
Total USD: 
$131.40 
Step: 8.5.1 
Step: 8.5.2 
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. 
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). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 10 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811150
Sivu 11 / 64
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 
8.19 #2 
8.19 #4 
WE3883738-I 
WE3883842-2 
M25988/2-904 
Step: 8.19.1 
Completed 
Step: 8.19.2 
Completed 
Step: 8.19.3 
Completed 
VALVE, SOLENOID 
VALVE, FLOW DIVIDER 
PACKING 
I 
$5,572.61 
$5,572.61 
I 
$7,078.11 
S7,078.11 
2 
50.82 
41.64 
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. 
Ran API: and still had constant APU mains. required message for CMC fault code 
4922222APU (APU Flow Divider Sol Short) 
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: 
Pans: 
Ref. No. 
Part number: 
Description 
$1,145.84 
Quantity 
Sell price USD 
Extended USD 
8.22 NI 
8.22 82 
1159CSNI50558-001 
PLUG, HORIZONTAL STABILIZER 
HOISTING STOP 
1159CSNI50558-001 
PLUG, HORIZONTAL STABILIZER 
HOISTING STOP 
5389.48 
S389.48 
2 
$378.18 
S756.36 
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). 
GAC_RevenueSquawksInvoice.rpt v3 
Page II of 64 
Printed: 3/7/2018 3:15:05PM 
tit kW 
EFTA00811151
Sivu 12 / 64
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 
Labor USD: 
Pans USD: 
Total USD: 
Pans: 
Billing Method 
Flat Rate 
Time and Material 
I
Rate 
Total 
31,168.00 
$999.18 
32,167.18 
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. 
Labor USD: 
Parts USD: 
Total USD: 
Pans: 
Ref. No. 
Billing Method 
Time and Material 
Time and Material 
Pan number: 
Hours 
Rate 
Total 
ST 
8.92 
@ 
5146.00 
$1,302.32 
$1,056.60 
Description 
32,358.92 
Quantity 
Sell price USD 
Extended USD 
8.2181 
8.2182 
8.24 83 
Step: 8.24.1 
Step: 8.24.2 
Step: 8.24.3 
KRP233012FT 
NAS67041.II 
NAS67041.II 
Completed 
Completed 
Completed 
ROLLER, FLAPTRACK 
BOLT 
BOLT 
I 
$703.50 
$703.50 
I 
$117.70 
$117.70 
2 
$117.70 
$235.40 
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 
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. 
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 
Labor USD: 
Parts USD: 
Billing Method 
Time and Material 
Time and Material 
Hours 
Rate 
Total 
ST 
3.47 
(a 
5146.00 
$506.62 
$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). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 12 of 64 
Printed: 3/7/2018 3:15:05PM 
tit f6I 
EFTA00811152
Sivu 13 / 64
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). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 13 of 64 
Printed: 3/7/2018 3:15:05PM 
tit kW 
EFTA00811153
Sivu 14 / 64
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: 
831 #1 
GAS830CV100-0 
831 #2 
GAS830CV150-0 
Description 
Quantity 
Sell price USD 
Extended USD 
SLEEVE 
4 
$0.69 
42.76 
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). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 14 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811154
Sivu 15 / 64
Bill To: Plan D, LLC. 
Pans: 
WO #: SC521661 
Invoice Number: 5517132452 
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, 
GVFS490 
1 
$250.00 
$250.00 
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). 
(iAC_RevenueSquawksInvoice.rpt v3 
Page 15 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811155
Sivu 16 / 64
Bill To: Plan D, LLC. 
Pans: 
WO #: SC521661 
Invoice Number: 5517132452 
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 
Customer Coordinator: 
Julian Brown 
Part/Model #: 
AC Serial No/Tail No.: 
TSNffSO: 
CSN/CSO: 
Aircraft Time: 
Item: 
10 
Outstanding Parts. Materials, and / or Services 
Team Manager: 
Charles Thomas 
Customer Coordinator: 
Julian Brown 
Part/Model #: 
AC Serial No/Tail No.: 
TSNffSO: 
CSN/CSO: 
Aircraft Time: 
Item: 11 
Follow on CMP Codes / Maintenance Tasks 
Team Manager: 
Customer Coordinator: 
Charles Thomas 
Julian Brown 
Part/Model #: 
AC Serial No/Tail No.: 
TSNffSO: 
CSN/CSO: 
Aircraft Time: 
Item: 
12 
WCR's - Work Change Requests 
Team Manager: 
Charles Thomas 
Customer Coordinator 
Julian Brown 
Pan/Model #: 
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 
Pans USD: 
Flat Rate 
Total USD: 
510.840.00 
5207.00 
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). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 16 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811156
Sivu 17 / 64
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 
Pans USD: 
Flat Rate 
Total USD: 
Parts: 
$7,884.00 
$1,338.00 
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 
$9,222.00 
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). 
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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: 
Customer Coordinator: 
Charles Thomas 
Julian Brown 
Part/Model 
AC Serial No/Tail No.: 
TSN/TSO: 
CSN/CSO: 
Aircraft Time: 
Discrepancy: 13.1 
Resolution: 
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. 
K A new radome boot will be applied. 
K 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*" 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
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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). 
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Bill To: Plan D, LLC. 
Pans: 
Ref. No. 
Pan number: 
Description 
CATALYST 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
REDUCER 
SOLVENT REDUCER 
SEALANT, 6 OUNCE #654 SEMKIT 
1/2 HOUR WORK LIFE 
CLEAR COAT KIT GL 
CONVERTER 
SURFACER, SANDING 
EVERCOAT FILLER 
FUSELAGE DRAIN VALVE 
SEAL, BUTTONED STRIP, WHEEL 
WELL DOOR (5' SECTION) 
SCREW-MACHINE, CRES PAN HD, 
STRL 
WASHER 
SCREW, PAN HEAD, X RECESSED 
SCREW, MACHINE, FLAT 
COUNTERSUNK HD, 100 DEG, 
CROSS RECESS 
SCREW 
BOLT 
SCREW 
WASHER, FLAT ALUMINUM 
NUT, SELF LOCKING 
SCREW 
SCREW, MACHINE 
WASHER-FLAT CRES 
FUSELAGE DRAIN VALVE 
COTTER PIN 
SCREW-MACHINE, CRES PAN HD, 
STRL 
SPACER SLEEVE 
RADOME BOOT 
COTTER PIN 
SEAL 
SEAL 
SCREW, MACHINE, FLAT CTSK HD, 
100 DEG, STRL, CROSS RECESSED 
SCREW, CSK -100 DEGREE - 
STRUCTURAL - ST 
WASHER-FLAT CRES 
WO ti: SC521661 
Invoice Number: 5517132452 
Quantity 
13.1 #33 
13.1 #34 
13.1 #35 
13.1 #36 
13.1 #37 
13.1 #38 
13.1 #39 
13.1 #40 
13.1 #41 
13.1 #42 
13.1 #43 
13.1 #44 
13.1 #45 
13.1 #46 
13.1 #47 
13.1 #48 
13.1 #49 
13.1 #50 
13.1 #51 
13.1 #52 
13.1 #54 
13.1 #55 
13.1 #56 
13.1 #57 
13.1 #58 
13.1 #59 
13.1 #60 
13.1 #6I 
13.1 #62 
13.1 #63 
13.1 #64 
13.1 #65 
13.1 #66 
13.1 #67 
13.1 #68 
13.1 #69 
13.1 #70 
13.1 #71 
13.1 #72 
13.1 #73 
13.1 k74 
13.1 k75 
13.1 #78 
13.1 #79 
13.1 #80 
13.1 #81 
13.1 #82 
13.1 #84 
13.1 #85 
13.1 #86 
13.1 #87 
I3110S 
I3765S 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
13765.5 
137655 
CA1805CX GAL 
PR1440B1-2-654 
CA8905HP 
D9001 
D8003 
400 EVERCOAT 
140N2022S1 
GAS13AN-1-41 
NIS27039C0807 
NAS1149DN816K 
MS27039C0808 
MS24693526 
MS24693-528 
AN525832R7 
AN525-832R11 
NASI149DN816H 
NIS21042L08 
AN525-832R5 
MS27039-0809 
NAS1149CN816R 
140N2022S1 
MS24665-155 
MS27039C0807 
NAS43DD3-36FC 
SJ8665FP021-1 
MS24665-302 
GAS18N1-1-1440 
GASI8h1-I-I440 
MS24694-C7 
NIS24694C7 
NA51149CN816R 
8 
24 
2 
2 
3 
9 
34 
46 
8 
I8
12 
10 
10 
10 
21 
9 
2 
10 
2 
24 
3 
12 
30 
5 
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). 
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