EFTA00811141

Bill To: Plan D, LLC. 
Pans: 
Ref. No. 
Part number: 
WO #: SC521661 
Description 
Invoice Number: 5517132452 
Quantity 
13.1 #88 
M524694-C7 
SCREW. MACHINE, FLAT CTSK HD, 
7 
100 DEG, STRI, CROSS RECESSED 
13.1 #89 
MS21043-08 
NUT, SELF LOCKING, REDUCED H 
36 
13.1 #90 
M524694-C7 
SCREW, MACHINE, FLAT CTSK HD, 
24 
100 DEG, STRI, CROSS RECESSED 
13.1.1 #1 
NA51581K4R5 
BOLT 
22 
13.1.1 #2 
NA51580V3R6 
SCREW 
I50 
Services: 
Ref. No. 
Description 
Quantity 
13.1 #3 
Vendor Supplied Labor 
1.00 
13.1 #1 
IAS. Carders. 13.1.6.8 hrs. 2/5-2/11 
1.00 
13.1 #2 
1AS, Carders. 13.1.6.8 hrs, 2/12-2/18 
1.00 
13.1.2 #1 
1AS Graf, David 20.0 HRS item 13.1.2 
1.00 
13.13 #1 
1AS Biddle. Brett 40.0 IIRS and 4.0 HRS OT item 13.1.3 on 
1.00 
12/11/17-12/14/17 
13.13 #2 
1AS Graft. David 11.O IIRS item 13.13 on 12/13/17 
1.00 
13.1.5 #1 
1AS Blanton 40 hrs + 5Inrs ot 13.1.5 12/17 
1.00 
13.1.6 #1 
IASSIKES,12/25-12/31.13.1.6.„16 HOURS 
1.00 
13.1.6 #2 
1AS , Sikes ,13.1.6 , 46hrs. , 1/8 - 1/13 
1.00 
13.1.6 #3 
1AS, Johnson,I3.1.6, 2 hrs. 1/29-2/4 
1.00 
Step: 13.1.1 
Completed 
Mechanical Paint Traveler 
Step: 13.1.1.1 
Completed 
Temporarely install of panel 325AT. and panel 337CT for paint traveler per G550 AMM 
55-30-00 Rev.Nov 15/17. Ref.13.1.1 
Step: 13.1.1.2 
Completed 
Remove panel 325AT. and panel 337CT after completion of paint traveler per G550 
AMM 55-30-00 Rev.Nov 15/17. Ref.17.1 
Step: 13.1.1.3 
Completed 
Complied with landing gear cycling operational checks. No faults noted at this time. 
Work done per G550 MOM 3240-00. Nov 15117 
Step: 13.1.1.4 
Completed 
Panel 325AT installed. needs sealant, panel 337C1 waiting for ops checks prior to final 
installation 
Step: 13.1.1.5 
Completed 
Complied with Aircraft paint traveler RSQCT-330Rev.8. Ftetpaper copy for work 
performed. 
Step: 13.1.2 
Completed 
Strip Aircraft 
Step: 13.13 
Completed 
Prep Aircraft 
Step: 13.1.4 
Completed 
Layout Aircraft 
Step: 13.1.5 
Completed 
Paint Aircraft 
Step: 13.1.6 
Completed 
Detail Aircraft 
Step: 13.1.7 
Waiting 
approval 
Weight and balance 
(L/P/S) 
Step: 13.1.7.1 
Waiting 
lnsp 
Complied with the physical weighing of the aircraft as outlined in the steps of RSQCT 
15 Rev 17 and the 6550 Weight and Balance Manual. 
Step: 13.1.7.2 
Completed 
Competed the weight and balance report and insert into the customer's weight and 
balance manual. 
Step: 13.1.8 
Completed 
customer support 
Step: 13.1.9 
Completed 
engineering support 
Discrepancy: 133 
Radome to structure perimeter steps- detail inspection Rill side negative step of .053 out of limits, marked with 
masking tape with arrows per 6550 AMM 53-02-01 Rev. Nov 15/17. Ref.Piant traveler II A. 
Resolution: Complied with engineering disposition on item 133.1.1 see steps below for all work preformed 
Billing Method 
Hours 
Rate 
Total 
Labor USD: 
Time and Material 
ST 
0.45 
@ 
$146.00 
$65.70 
Labor USD: 
Time and Material 
ST 
0.25 
@ 
$222.00 
$55.50 
Total USD: 
$121.20 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawkslnvoice.rpt v3 
Page 21 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811161

Bill To: Plan D, LLC. 
WO #: SC521661 
Invoice Number: 5517132452 
Step: 133.1 
Step: 133.1.1 
Step: 133.2 
Step: 13.3.3 
Completed 
Request engineering disposition to correct R/Ii side negative step on radome that is out 
of limits. 
Completed 
Engineering Disposition: 
It is acceptable to repair the out-of-tolerance radome steps in accordance with 
Gulfstream Service Letter CR.005300001 Rev. - ."Aerodynamic Filler Sweep - Fair 
Procedure - Radome Steps". This Gulfstream Service Letter (GSL) is classified as a 
Manufacturer's Service Document and is governed by Advisory Circulars 20-176A and 
AC 120-77. Completing a repair per a Gulfstream Service Letter is similar to 
completing a repair per the Structural Repair Manual (SRM): No serial number specific 
FAA Form 8100-9 is required and will not be provided in support of a GM. repair. The 
Engineering (Source) Data for this Service Letter has been shown to comply with the 
applicable FAR's and is FAAApproved. Engineering source data is retained by 
Gulfstream as proprietary data. 
Completed 
Request paint to comply with engineering dispo during full strip and paint, ref item 13.1 
Completed 
Comply with post-paint radome to fixed structure perimeter steps and gap 
measurements. 
Discrepancy: 133 
Replace MED belicrank cover hardware where attaches at airstair riser rail with unpainted screws and washers 
per customer request. 
Resolution: Replaced MED hardware with correct hardware PN:AN525-832-7 per Drawing 159B140023 Revd]. 
Billing Method 
Hours 
Rate 
Total 
Parts USD: 
Time and Material 
$126.65 
Total USD: 
$126.65 
Pans: 
Ref. No. 
Pan number: 
Description 
Quantity 
Sell price USD 
Extended USD 
13.541 
AN525-832-1I 
SCREW 
I 
$7.27 
$7.27 
13.542 
NA51149DN816H 
WASHER, FLATALUMINUM 
10 
$0.23 
42.30 
13.543 
MS210421.08 
NUT, SELF LOCKING 
10 
$0.44 
$4.40 
13.514 
AN525-832R11 
SCREW 
I 
$0.22 
$0.22 
13.545 
AN525-8321211 
SCREW 
5 
$0.22 
$LI0 
13.546 
AN525-8321211 
SCREW 
I 
$0.22 
$0.22 
13.547 
AN525-8321211 
SCREW 
I 
50.22 
$0.22 
13.548 
WH832RIIDGI3WH 
SCREW 
14 
$7.87 
$110.18 
13.549 
AN525-8321211 
SCREW 
I 
$0.74 
$0.74 
Discrepancy: 13.7 
One drain dlverter missing just forward of tail compartment door. 
Resolution: Replaced drain diverter PN:1159B4147517-13 just forward of tall compartment door per G550 AMM 53-51-00 RevJan 
15/10. Time adhesive GAA100BD04 was applied 14:00 PM, set in 6 hours. 
Parts USD: 
Total USD: 
Billing Method 
Hours 
Rate 
Total 
Time and Material 
$11235 
$11235 
Pans: 
Ref. No. 
Pan number: 
Description 
Quantity 
Sell price USD 
Extended USD 
13.781 
115981O47517-B 
DIVERTER DRAIN, AFT LOWER 
1 
$11235 
4112.35 
PANEL 
Discrepancy: 13.8 
Customer Requests to polish and swap I.JH and FUR eventing E-light lenses. 
Resolution: •**Summan.*** 
Removed 6 et erwing emergency light lenses. Polished lenses. Reinstalled 6 °venting emergency light lenses. Sealed 6 
overwing emergency light lenses. 
See steps below for details of work performed. 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
riAC_RevenueSquawksInvoice.rpt v3 
Page 22 of 64 
Printed: 3/7/2018 3:15:05PM 
tit W. 
EFTA00811162

Bill To: Plan D, LLC. 
WO #: SC521661 
Invoice Number: 5517132452 
Billing Method 
Hours 
Rate 
Total 
Labor USD: 
lime and Material 
ST 
18.00 
@ 
$146.00 
$2,628.00 
Total USD: 
$2,628.00 
Step: 13.8.1 
Completed 
Step: 13.8.2 
Completed 
Removed 6 overwing emergency light lease covers. 
Sealent required for 6 overwing emergency light loose coven 
Item: 
14 
Photographic Documentation - (Ref. Item D 2.1 of Proposal 104 7037536. ROO) 
Team Manager: 
Charles Thomas 
Customer Coordinator: 
Julian Brown 
Part/Model #: 
AC Serial No/Tail No.: 
TSN/TSO: 
CSN/CSO: 
Aircraft Time: 
Item: 
15 
Jet ConneX (Ka-band) High -Speed Data System Installation - (Ref. Item B 2.2 of Proposal ID# 7038248 R02) 
Team Manager: 
Charles Thomas 
Customer Coordinator: 
Julian Brown 
Part/islodel #: 
AC Serial No/Tail No.: 
TSWISO: 
CSN/CSO: 
Aircraft Time: 
Discrepancy: 15.1 
Jet ConneX (Ka-band) I firth-Speed Data System Installation 
Gulfstream will install this latest version of high-speed Broad-Band data system. 
One (1) Modem Manager (MODMAN) will be installed in the aft baggage compartment in a new cabinet. If Sat 
TV is 
installed, the existing cabinet will be modified and reused unless the cost exceeds the new cabinet installation. 
As the overall manager for the system, the MODMAN is responsible for providing the user interfaces to the 
aircraft/passengers. 
One (I) Aeronautical Personality Module (APN1) will be located in the baggage compartment equipment cabinet 
and 
holds the configuration data for the system. 
One (I) Ka-band Aircraft Network Data Unit (KANDU) will be installed in the boiler room. The KANDU receives 
commands front the MODMAN through an Ethernet Interface to configure the antenna/KRFU and reports status 
over 
this Ethernet interface 
One (I) Ka-band Frequency Unit (KRFU) will be installed in the proximity of the TMA assembly on top of the tail 
empennage. 
The KRFU contains a Block-Down Converter (BDC) to convert the received Ka-band frequencies to IF 
frequencies 
and also is made up of a Block-Up Convener (BUC) to convert the IF frequencies to Ka-band frequencies. A 
Iligh-
Potter Amplifier (IIPA) increases the signal strength for transmission by the antenna. 
One (I) Tail Mounted Antenna (TMA) will be mounted on top of the tail empennage underneath the radome. 
The antenna system is to acquire and establish communications with satellites in various orbits to enable beyond 
lineof-
sight communications between airborne, ground fixed, and ground transportable terminals. 
The Radome will be removed and replaced by a new Ka-band capable radome. 
Certification: The Jet ConneX (Ka-band) High-Speed Data System along with the Satcom Direct Router will be 
installed via Gulfstream STC; expected, availability of STC, 4th Quarter 2017. 
n* SEE APPENDIX *** 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoicc.rpt v3 
Page 23 of 64 
Printed: 3/7/2018 3:15:05PM 
tit W. 
EFTA00811163

Bill To: Plan D, LLC. 
WO #: SC521661 
Invoice Number: 5517132452 
Resolution: Complied with installation of Jet ConneX (Ka-band) High-Speed Data System per STC ST03238AT-D Index List 
GC413038007 Rev R. Configuration Lists 6C513038031 Rev A, GC513038034 Rev A, and GC513038035 Rev —. 
Reference Custom Electrical Drawing List CE51 496???? Rev ?? and Custom Mechanical Drawing List CE5200???? Rev 
?? for deviations. 
Complied with GC41 429G002 Rev — and GC51 303G007 Rev — Ground Test Plans with no defects noted. 
Instructions for Continued Airworthiness GC51 303A004 Rev F applicable to this installation and incorporated into 
maintenance program. 
Airplane Flight Manual Supplement GC51 303M005 Rev F incorporated into Flight Manual 
Reference GWBR000000160 Rev — for Weight and Balance Supplement. 
Reference GC51 4696768 Rev — for Electrical Load Analysis 
Ref 15.30 for Cockpit Storage Box upuolstered with Grospoint Poster P/N GPFR0242 (Ref work 15.20) 
Reference CE51 4696543 Rev -- for Electrical Load Supplement. 
One ( I ) SDR will be installed in the aft baggage and interfaced with the existing aircraft internet capable systems. 
New wiring for the 3C cellular antenna will be installed in the cabin in an engineering approved location. 
If the aircraft has an existing Gogo system installed, the SDR will be integrated with the Gogo utilizing existing 
Ethernet provisions for single MID, unless otherwise directed by Ow ner/Operator. If provisions are not present, 
Ethernet cabling will be quoted as a separate item. 
New Components: 
One (1) 90400012-0001 - Honeywell Modem Manager (MODMAN) 
One (I) 90401121 - Honeywell Aeronautical Personality Module (APM) 
One (I) 90401202 - Honeywell Ka-band Frequency Unit (KRFU Convection Cooled) 
One (1) 90400013-0001 - Honeywell Tail Mounted Antenna (TMA) 
One (I) 90401566 - Honeywell Ka-band Aircraft Network Data Uolt (KANDU) 
One (I) 1233-F-2191-10 - Satcom Direct Router (SDR) 
One (I) Radome 
Various Installation Kits 
Certification: The Jet ConneX (Ka-band) High-Speed Data System along with the Satcom Direct Router will be 
installed via Gulfstream STC: expected. availability of STC. 4th Quarter 2017. 
Notes: 
If an existing Sat TV system is removed to accommodate the Ka band system the CMS software may be modified 
to remove the Satellite Television. This modification is not included in the sell price of the Ka band system and will 
be provided after a detailed engineering review is completed. estimated charges approximately 518,000. 
Changes to the Aircraft's Completion Center Maintenance Handbook (COUR), or Cabin Operating Manual 
(COM) are not included as part of this Proposal. Should a modified CCMH or COM be requested by the 
Customer, it may be provided at additional charge. 
Gulfstream may require assistance front the Customer's Information Technologies (IT) department for the 
configuration of the high speed data system. 
Notes: (continued) 
This involvement will verify proper system configuration as well as provide system simplicity to the operator. 
This will be coordinated at the time of installation and will be completed prior to delivery of the aircraft. 
The Customer must establish and maintain a service subscription for the Ka-band system. 
Quote assumes sufficient space is available for the equipment above and does not include relocation of 
equipment to provide space. 
This installation is a managed program. Please contact your Regional Sales Manager to coordinate the availability 
of components and installation. 
Billing Method 
Hours 
Rate 
Total 
Labor USD: 
Flat Rate 
5192.054.00 
Pans USD: 
Flat Rate 
5492.946.00 
Semites USD: 
No Charge 
N/ C 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenuaquawksInvoice.rpt v3 
Page 24 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811164

Bill To: Plan D, LLC. 
Total USD: 
WO #: SC521661 
Invoice Number: 5517132452 
5685,000.00 
Parts: 
Ref. No. 
Part number: 
Description 
SATCOM DIRECT ROUTER 
ANTENNA 
ANTENNA 
ADAPTER, TNC TO SMA 
TERRETRIAL MODEM ANTENNA 
INSTALLATION OF SATCOM (HIGH 
SPEED DATA HD-I28) SYSTEM 
PEDESTAL SWITCH PANEL ASSY 
SLEEVE 
SPACER 
CONNECTOR 
PLUG, D-SUB, 25-PIN 
RCPT, SOCKET, D-SUB, 25-20 GA 
BACKSHELL 
SPACER 
KA PED OVERLAY 
SLEEVE 
SPACER 
CONNECTOR 
BACKSHELL 
CONNECTOR 
BACKSHELL 
CONNECTOR 
BACKSHELL 
SWITCH 
KIT, SDR COAX CABLE 
REMOTE WIFI ANTENNA 
RING 
RING 
CLIP 
CABLE, ONE CONTINUOUS LENGTH 
ON SPOOL 
BOLT, PROTRUDING SHEAR HEAD, 
TITANIUM 
BOLT 
BOLT 
BOLT, PROT SHEAR HEAD, TI 
BOLT 
BOLT, PROTRUDING SHEAR HEAD, 
TITANIUM 
COLLAR, SHEAR 
BOLT, PROTRUDING SHEAR HEAD. 
TITANIUM 
BOLT, PROTRUDING SHEAR HEAD. 
TITANIUM 
SOLDER SLEEVE (BRAID) 
SOLDER SLEEVE (PIG TAIL) 
LUG,TERMINAL,YELLOW,H8 
TERMINAL 
TERMINAL 
LUG, TERMINAL, RED, #8 
CAP END 
TERMINAL 
TERMINAL 
CLIP ASSEMBLY. 90 DEG. ANGLE 
HINGE BASE (BLUM LARGE) 
Quantity 
15.1 #1 
15.1 #2 
15.1 #3 
15.1 #4 
15.1 #5 
15.1 #6 
15.1 #7 
15.1 #8 
15.1 #9 
15.1 #10 
15.1 #11 
15.1 #12 
15.1 #13 
15.1 #14 
15.1 #15 
15.1 #16 
15.1 #17 
15.1 #18 
15.1 #19 
15.1 #20 
15.1 #2I 
15.1 #22 
15.1 #23 
15.1 #24 
15.1 #25 
15.1 /426 
15.1 #27 
15.1 #28 
15.1 #29 
15.1 #30 
15.1 #3I 
15.1 #32 
15.1 #33 
15.1 #34 
15.1 #35 
15.1 #36 
15.1 #37 
15.1 #38 
15.1 #39 
15.1 #40 
15.1 #4I 
15.1 #42 
15.1 #43 
15.1 #44 
15.1 #45 
15.1 /446 
15.1 #47 
15.1 #48 
15.1 #49 
15.1 #51 
I233-F-2191-I0 
100-1021-30 
100-1021-50 
PE9079 
PI8350-001 
ST03238AT-D 
GPM004001402-301 
27498-001 
27498-006 
GAC830T3 
M24308/4-3F 
M24308/2-3F 
DB115339-22 
27498-006 
GPM004001714-301 
27498-001 
27498-008 
hIS27473T12F3S 
M85049/49-2-12N 
N1S27473T16F55S 
M85049/49-2-161C 
N1S27473T18F35S 
M85049/49-2-181C 
27500-010 
500-35750-101 
PI6917-001 
GAR540BY16 
GAR540BY22 
D20419 
GAC861AH424S 
GAB511AB6B5 
GAB511AB6B6 
GAB511AB6B7 
GAB511AB6B8 
GABSIIAB6B4 
GAB5I [ABM 
GAN510AA6 
GAB511AB6B5 
GAB511AB6B5 
GAS830AJ2 
GAS830All I 
GA11051110-08 
GAT8051118-3B 
GA11051118-36 
GA11051118-08 
324484 
GAT805P8-08 
GAT8051110-3A 
5684-01 
173H7100 
2 
2 
6 
100 
100 
41 
30 
40 
20 
IS 
4 
70 
41 
41 
I00 
100 
50 
50 
50 
50 
100 
20 
75 
50 
12 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 25 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811165

Bill To: Plan D, LLC. 
Pans: 
Ref. No. 
Pan number: 
WO #: SC521661 
Description 
Invoice Number: 5517132452 
Quantity 
15.1 #52 
GA436-5/3 
PANEL ASSY-CONSOLE BLANK 
2 
(COLOR GREY) 
15.1 #53 
NAS1581K4R6 
BOLT 
2 
15.1 #54 
110872 
TNC CONNECTOR, STRAIGHT PLUG 
3 
15.1 #55 
M24308/2-1F 
RCPT, D-SUB, 9-SOCKET 
I 
15.1 #56 
GAR835NK1 
RELAY 
I 
15.1 #57 
65009-001-513 
SOCKET 
I 
15.1 #58 
CTJ716E01D-513 
DEU COMPOSITE TERMINATION 
1 
SYSTEM 
15.1 #59 
1-480698-0 
PLUG 
1 
15.1 #60 
ABMM-A-C 
CABLE, TIE MOUNT 
20 
15.1 #61 
1032.119-24 B/R 
INSERT, THREADED 
50 
15.1 #62 
225791-3 
INSERT, SIZES FOR RG188 
2 
15.1 #63 
P18350-001 
TERRETR1AL MODEM ANTENNA 
I 
15.1 #64 
D38999/26FD19SN 
CONNECTOR, PLUG 
I 
15.1 #65 
D38999/26FC4PN 
CONNECTOR 
I 
15.1 #66 
AS21919WDG23 
CLAMP 
I 
15.1 #67 
M53367-1-9 
STRAP. TY WRAP 
1.000 
15.1 #68 
NAS1802-3-13P 
SCREW, HEX HD, CRUCIFORM REC. 
10 
FULL THD, A286 CRES 
15.1 #69 
NAS1802-3-8P 
SCREW 
10 
15.1 #70 
hIS210421.3 
NUT 
20 
15.1 #71 
NA51149F0332P 
WASHER. FLAT STEEL 
30 
15.1 #72 
NAS1802-3-10P 
SCREW. HEX HD, CRUCIFORM REC, 
10 
FULL THD. A286 CRES 
15.1 #73 
hIS27039C0807 
SCREW-MACHINE. CRES PAN HD, 
10 
STRI. 
15.1 #74 
NA51149FN832P 
WASHER. FLAT STEEL 
10 
15.1 #75 
M525083-7BB11 
JUMPER, BONDING CNT 
I 
15.1 #76 
310701 
CABLE, COAX 
50 
15.1 #77 
CTR002 
PLUG, TNC, 90 DEGREE 
I 
15.1#78 
BTS002 
RCPT,TNC BULKHEAD 
I 
15.1 #79 
2-139N602-70 
0 -RING 
2 
15.1 #80 
E1257-70/2-0I5 
0 RING RUBBER 
2 
15.1 #81 
NAS1580C3T12 
BOLT 
10 
15.1 #82 
BTS002 
RCPT,TNC BULKHEAD 
I 
15.1 #83 
CTR022 
CONNECTOR 
I 
15.1 #84 
27500-044 
SWITCH 
I 
15.1 #85 
C75-520/20 
CONTACT 
30 
15.1 #86 
XP-610 
PRINTER, EPSON 
I 
15.1 #87 
ABMM-A-C 
CABLE, TIE MOUNT 
15 
15.1 #88 
M24308/4-1F 
CONNECTOR 
I 
15.1 #89 
MS35207-269 
SCREW 
6 
15.1 #90 
D436-36 
SLEEVE 
200 
15.1 #91 
GAC860K-1 
END CAP, WHITE 
300 
15.1 #92 
324485 
WIRE END CAPS 
150 
15.1 #93 
GAC860K-3 
END CAP-BLUE 
100 
15.1 #94 
GAC860K-4 
END CAP (YELLOW) 
100 
15.1 #95 
CTS002 
PLUG, TNC, STRAIGHT 
I 
15.1 #96 
CTS022 
CONNECTOR 
I 
15.1 #97 
GARI00B2B0031 
RUBBER .031 SHEET 
9 
15.1 #98 
MS35207-260 
SCREW 
50 
15.1 #99 
MS35207-262 
SCREW 
50 
15.1 #100 
MS35207-264 
SCREW 
50 
15.1 #101 
MS35207-266 
SCREW, MACH, PAN HEAD, CROSS 
50 
REC, CARBON STL, CADMIUM PLD 
15.1 #102 
GANIOW1032 
NUT 
100 
15.1 #103 
NAS1149D0316H 
WASHER 
100 
15.1 #104 
NAS1149F0363P 
WASHER. FLAT STEEL 
100 
For detail description of the work complied with sec the Work Order Detail report. 
Unless otherwise indicated, all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 26 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811166

Bill To: Plan D, LLC. 
Pans: 
Ref. No. 
Pan number: 
WO #: SC521661 
Description 
Invoice Number: 5517132452 
Quantity 
15.1 4105 
NAS1149F0332P 
WASHER. FLAT STEEL 
100 
15.1 4106 
GAS805K3 
SPLICE 
30 
15.1 #107 
GAC860N08 
CAP D300-08 
30 
15.1 #108 
GAC860N12 
CAP 
30 
15.1 #109 
GAC860N18 
CAP, SPLICE 
30 
15.1 #110 
VS-08-RJ45-5-(//1P20 
CONNECTOR, RJ45 (GRAY) 
15 
15.14/111 
M81969-1-01 
INSERT/EXTRACT GREENAYHITE 
8 
METAL 
15.1 #112 
91066-4 
EXTRACTOR TOOL 
8 
15.1#113 
M81969-14-0I 
EXTRACTOR, GREENPNHITE 
12 
PLASTIC 
15.1 #114 
M81969/14-10 
TOOL, ORANGE/RED INSERTION 
15 
AND EXTRACTION 
15.1 #115 
M15570-22-I 
TOOL 
15 
15.1 #116 
hIS27039C1-12 
SCREW. PAN HEAD, X RECESSED 
4 
15.1#117 
294-541 
EXTRACTOR, AMOHENOL 
I 
15.1 WI III 
GARI00B2B0063 
RUBBER .063 SHEET 
5 
15.1 #119 
1159AV33022-5 
CIRCUIT BREAKERASSEMBLY 
1 
(ESDS MATERIAL) 
15.1 #120 
58T-101 
EATON EXTRACTION TOOL 
1 
15.1 #121 
43031-0009 
PIN 
15 
15.1 #122 
90401566 
KA-BAND AIRCRAFT NETWORK 
I 
DATA UNIT (KANDU) 
15.1.5#1 
GC524980001-121 
BRACKET ASSEMBLY 
2 
15.1.5 #2 
14524694555 
SCREW, 100 DEGREE CSK 
30 
STRUCTURAL 
15.1.5 43 
M527039-I-04 
SCREW, PAN HEAD MACHINE 
30 
15.1.5 44 
GSM805001267-10 I 
ANGLE 
2 
15.1.5 45 
GSM806002351-101 
BRACKET 
2 
15.1.5 46 
CB200-40 
ADHESIVE, ACRYLIC (DUAL PACK 
3 
CARTRIDGE) PLUNGER PLA050-10 
40 ML 
15.1.5 47 
021200-50009 
NOZZLE, STATIC MLXER, SHORT 
100 
GOLD NOZZLE FOR 1.5OZ 
15.1.5 48 
CCS1005-09-48.00 
ANGLE 
1 
15.1.5 49 
CCS1005-33-48.00 
ANGLE 
1 
15.1.5 410 
NAS1836-06-10 
INSERT 
20 
15.1.5 411 
MS35206-226 
SCREW 
20 
15.1.5 412 
TC141 
BRACKET, TIE
-DOWN 
20 
15.1.5 413 
MS21266-7T 
GROMMET, PLASTIC, EDGING 
2 
15.1.5 414 
M53339-4-9 
PLATE MOUNTING 
5 
15.1.5 415 
NIS20470A4-5N RED 
RIVET 
25 
15.1.5 416 
NASI149DN832J 
WASHER 
25 
15.1.5 417 
GAB51IGA3-4 
BOLT 
100 
15.1.5 418 
GAB51IGA3-6 
BOLT 
100 
15.1.5 419 
GAB51IGA3-7 
HI-BOLT 
100 
Services: 
Ref. No. 
Description 
Quantity 
15.1.1 41 
REF.. M. Eddy, 15.1.1, 3.0 hrs, 11/27 -12103/2017 
1.00 
15.1.1 42 
REF.. Eddy. 15.1.1, 3 HRS, 11/27 - 12/03 
1.00 
15.1.2 41 
AETS. Molnar. .15.1.2, 1.0 hrs, 1)22 -112812018 
1.00 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 27 of 64 
Printed: 3/712018 3:15:05PM 
tit W. 
EFTA00811167

Bill To: Plan D, LLC. 
WO #: SC521661 
Invoice Number: 5517132452 
Step: 15.1.1 
Waiting 
approval 
Avionics Engineering Labor Avionics 
(L/P/S) 
Step: 15.1.2 
Waiting 
approval 
Mech Engr Labor Avionics 
(L/P/S) 
Step: 15.13 
Waiting 
approval 
AVI Systems Test Labor Only 
(L/P/S) 
Step: 15.1.4 
Waiting 
approval 
AVI /Electrical Labor Only 
(L/P/S) 
Step: 15.1.5 
Waiting 
approval 
AVI Sheet Metal Labor Only 
(L/P/S) 
Step: 15.1.5.1 
Completed 
Lightly scuff sanded 5" area around routed area. then cleaned area with cheese cloth 
and isopropyl alcohol. 
Cut and impregnated 3 plies of 120 style fiberglass cloth with 828 resin. Applied 
impregnated fiberglass on routed area and vacuum bagged and 24 inches of mercury. 
Let dwell for 1 hour and heat cured at 140 for 4 hours. 
After cure sanded excess resin smooth to blend new plies into original contour. 
Reference engineers dispo ## 15.8.1.1 
Step: 15.1.6 
Completed 
INT Support (R&R) Labor Only 
Step: 15.1.7 
Waiting 
approval 
SC Ntaintenancefflangar / Primary Codes /Touch Labor Only 
(L/P/S) 
Step: 15.1.8 
Waiting 
approval 
SC Paint Labor Only 
(L/P/S) 
Step: 15.1.9 
Waiting 
approval 
Inspection Labor Only 
(L/P/S) 
Step: 15.1.10 
Waiting 
approval 
Weight and Balance Labor Only 
(L/P/S) 
Item: 
16 
KA BAND HARNESS FABRICATION 
Team Manager: 
Customer Coordinator: 
Charles Thomas 
Julian Brown 
Part/Model 8: 
AC Serial No/Tail No.: 
TSN/TSO: 
CSN/CSO: 
Aircraft Time: 
Item: 
17 
ASC 085A X61 Weather Installation - (Ref. Item B 2.3 of Proposal ID# 7038248 R02) 
Team Manager: 
Charles Thomas 
Customer Coordinator: 
Julian Brown 
Pan/Model ft: 
AC Serial No/Tail No.: 
TSN/TSO: 
CSNJCSO: 
Aircraft Time: 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksinvoice.rpt v3 
Page 28 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811168

Bill To: Plan D, LLC. 
WO #: SC52166I 
Invoice Number: 5517132452 
Discrepancy: 17.1 
ASC 085A XN1 Weather Installation 
This Service Change installs an antenna, receiver, two (2) data ports and associated wiring for the XM satellite 
weather system. 
Either a fore or an aft installation may be selected based on aircraft configuration. 
Aircraft that are provisioned for XM installation may require an engineering review to complete the installation. 
Provisions may include wiring, antenna, receiver, data ports or any combination of these components and are 
typically 
installed during completion. 
Prerequisites: 
ASC 908 - PlaneView Master Operating Software System Software Update (Cert Fox) 
Prior to. or at the time this ASC is ordered, operators will be required to supply a configuration report of the 
Central Maintenance Computer (CMC). 
The CMC report can be stored on the aircraft PC laptop then electronically submitted to Culfstream at 
asc.softwareCrgulfstream.com. 
Allow three (3) to five (5) days for the CMC report review and up to twenty-one (21) days for the creation of a 
new 
Options Data disk. 
Effectivity: This Service Change is applicable to aircraft Serial Numbers 5001 - subsequent. 
Notes: 
Interior access to perform this installation is not included in the kit price. 
Aircraft configuration. installation location of the system and availability 
of spare wiring may impact labor 
hours, 
amount of access required and could necessitate additional engineering. 
This ASC is a managed program. Incorporation must be coordinated through Culfstream Aircraft Scheduling 
at 
800-810-GULF (4853) or 912-965-4178. 
If not scheduled, aircraft downtime could increase significantly. 
This Service Change may only be installed at a Culfstream Aerospace facility. 
Resolution: Complied with ASC 085A XM Weather Installation 
Ref Item 17.2 CN1P 970851 
Billing Method 
Hours 
Rate 
Total 
Labor USD: 
Flat Rate 
$16,060.00 
Pans USD: 
Flat Rate 
563,940.00 
Total USD: 
480,000.00 
Parts: 
Ref. No. 
Pan number: 
Description 
Quantity 
17.1 #1 
A.SC0S5A-1 GSSP 
KIT, XM SATELLITE WEATHER 
I 
INSTALLATION, 5001-SUB(KIT 
ONLY) 
17.182 
RGI42Bill 
COAX 
35 
17.1#3 
HET-A-02C 
FERRULE, SHIELD 
6 
17.1 #4 
PLC1.51-58 
TYRAP 
10 
17.1 #5 
BTS722 
RCPT, RFTNC 
I 
17.1 #6 
CTS722 
CONNECTOR 
1 
17.1 #8 
M24308/4-IF 
CONNECTOR 
I 
17.189 
GAC835MR20S 
CONTACT 
10 
17.1#10 
CSS722 
PLUG, ShIA, STRAIGHT 
1 
17.1 #11 
CSR722 
PLUG, SMA,90° 
I 
17.1 #12 
CTS722 
CONNECTOR 
I 
17.1 #13 
NIS21919WDG2 
CLAMP 
4 
17.1 #14 
NIS21919WDG4 
CLAMP PTYPE-CUSHIONED,IM IN 
4 
17.1#15 
NIS21919WDG3 
CLAMP PTYPE-CUSHIONED,3116 
4 
INCH 
17.1 #16 
DCR-IA-05 
RAIL 
I 
17.1 #18 
GAN IOW 1032 
NUT 
10 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 29 of 64 
Printed: 3/7/2018 3:15:05PM 
tit kW 
EFTA00811169

Bill To: Plan D, LW. 
Pans: 
Ref. No. 
Part number: 
WO #: SC521661 
Description 
Invoice Number: 5517132452 
Quantity 
17.1 819 
GATIIF-BR3-I0A 
TERMINAL INSTALL, ELEC 
2 
GROUNDING AND BONDING 
17.1821 
ABI4-SA 
LUG,TERMINAL-ELEC 
5 
17.1822 
GATIIF-BR3-I0A 
TERMINAL INSTALL, ELEC 
4 
GROUNDING AND BONDING 
17.1 823 
A10086 
TIE-DEX BAND 
10 
17.1824 
AS21919WDG08 
CLAMP. LOOP 
8 
17.1 825 
NASI802-3-14P 
SCREW (AP) 
2 
17.1826 
NASI802-3-8P 
SCREW 
3 
17.1 #27 
58T-101 
EATON EXTRACTION T(Xli. 
1 
Item: 18 
ASC 912 and ASC 123 Planeview MOS Upgrade - (Ref. Item B 2.4 of Proposal ID# 7038248 R02) 
Team Manager: 
Customer Coordinator: 
Charles Thomas 
Julian Brown 
ParttModcl #: 
AC Serial No/Tail No.: 
TSWISO: 
CSN/CSO: 
Aircraft Time: 
Discrepancy: 18.1 
ASC 912 and ASC 123 Planeview MOS Upgrade 
ASC 912: 
This Service Change (ASC 912) installs the Planeview Master Operating System (MOS) software Media Part 
Number 
(PN) MM7031235-024. 
ASC 123: 
This Service Change (ASC 123) loads a combination of new and existing software based on current aircraft 
configuration. 
Prerequisites: 
Submit an APN1 Settings & Riggings form 
ASC 910 - Planeview MOS Software Update or later; or production equivalent is the minimum cert level 
required. 
Prior to. or at the time this ASC is ordered, operators will be required to supply a configuration report of the 
Central Maintenance Computer (CMC). 
The CMC report can be stored on the aircraft PC laptop then electronically submitted to C airstream at 
asc.software(it gulfstream.com. 
Operators utilizing Custom Electronic Checklist (ECL) must order new software. Prior to. or at the time this 
ASC is 
ordered, software may be ordered from the Custom ECL page on NlyCulfstream.com 
Concurrent Requirements: ASC 912 and ASC 123 are complied with in conjunction. 
Effectivity: This Service Change is applicable to aircraft Serial Numbers 5001 - 5549. This, or a similar change. 
will be 
installed during initial phase manufacturing on aircraft Serial Numbers 5550 and subsequent. 
Notes: 
Aircraft that do not meet the prerequisite minimum level for modification may utilize drawing 11595857083 to 
meet the requirements of ASC 107 and ASC 910. This drawing may only be used concurrently with ASC 123 and 
ASC 912. 
Aircraft utilizing drawing 1159SB57083 to meet the prerequisite minimum requirements of ASC 107 and AM' 
910 
are part of a managed program conducted by Product Support Program Management (PSPM). 
Resolution: COMPLIED WITH ASC 912 and ASC 123 Planeview MOS Upgrade 
Billing Method 
Flours 
Rate 
Total 
Labor USD: 
Flat Rate 
53,306.00 
Parts USD: 
No Charge 
N/ C 
Total USD: 
53,306.00 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 30 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811170

Bill To: Plan D, LLC. 
Pans: 
WO #: SC521661 
Invoice Number: 5517132452 
Ref. No. 
Pan number: 
Description 
Quantity 
Sell price USD 
Extended USD 
18.1 81 
ASC912-I GSSP 
18.1 82 
ASC123-I GSSP 
KIT, INDICATING/ RECORDING 
1 
$0.00 
$0.00 
PLANEVIEW MOS UPDATE, 
5001-5549 
KIT, INDICATING/RECORDING 
1 
$0.00 
$0.00 
PLANEV1EW AVIONICS 
ENHANCEMENTS. 5001-5549 
Item: 19 
Reveneer Woodwork - (Ref. Item A 1.1 of Proposal ID# 7039407 ROO) 
Team Manager: 
Charles Thomas 
Part/Model 8: 
Customer Coordinator: 
Julian Brown 
AC Serial No/Tail No.: 
TSNffSO: 
CSN/CSO: 
Aircraft Time: 
Discrepancy: 19.1 
Reveneer Woodwork 
The existing veneer covered components will be removed from the aircraft and stripped of all veneer surfaces, 
hardwood caps. and nosing. 
All substrate will be cleaned and prepped for application of new selected veneer with corresponding hardwood 
caps and nosing. 
Modifications or repairs to any substrate material or structural hardware will be evaluated and addressed on a 
time and material basis. 
All the existing latches will be cleaned and retained. New hardware. if requested. will be addressed on a time and 
materials basis. 
New Customer Selected Veneer will be applied to the existing substrates. 
The new veneer will be finished with Gulfstreant standard III-BIL clear coat finish and polished to a 
predetermined luster. 
All applicable internal surfaces will be cleaned and retained in existing condition. Painting or recovering of the 
internal surfaces will he addressed on a time and materials basis. 
Inlays of any type such as wood. metal. or stone inlays are not included in this proposal. Existing inlays will be 
evaluated on a case-by-case basis and addressed on a time and materials basis. 
Burn certification is predicated upon the existing substrates meeting all the FAA flammability requirements. 
Gu[(stream is not responsible for any existing materials meeting burn requirements. 
The recovered doors, panels, and cabinetry will be reassembled and installed in aircraft. All adjustments will be 
made to ensure correct fit and function. 
Equipment relocation is not part of this proposal and will be addressed on a time and materials basis. 
***SEE APPENDIX FOR ADDITIONAL INFO*" 
Resolution: Ref steps 19.2 thru 19.23, For details of veneer covered components that were removed from the aircraft and stripped of 
all veneer surfaces, hardwood caps, and nosing. Reveneered and new hardwood caps and nosings were completed with 
customer approved materials. Ref R&I for details of reinstallation 
REF 19.24 and 19.30 for Veneer & Hardwood Flammability 
Notes: 
Staining or Tinting Finish to achieve a specific color or grain pattern is not included in this proposal. Any finish other 
than natural will be evaluated and addressed on a time and materials basis. 
This proposal includes Natural Wood Veneer. Composite Veneer (due to ordering limitations) may require Gulfstream 
to purchase additional sheets of that product. Should additional sheets will be required: the Customer will be advised of 
the additional charges. 
Sharp radiuses on ledges and other cabinetry that are covered with veneer will require additional labor charges and 
will be accomplished on a time and materials basis. 
Proposal is based on reusing all applicable substrate and componentry. 
All plating will be accomplished on a time and materials basis. 
Billing Method 
Hours 
Rate 
Total 
Labor USD: 
Flat Rate 
Parts USD: 
Flat Rate 
5169.036.00 
$68.984.00 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 31 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811171

Bill To: Plan D, LLC. 
WO #: SC521661 
Invoice Number: 5517132452 
&niers USD: 
Total USD: 
Pans: 
Ref. No. 
Flat Rate 
Part number: 
Description 
5470,155.00 
5706,175.00 
Quantity 
19.1 #1 
M520-01437 
STAIN, RAW UMBER PENETRATING 
2 
19.1 #2 
M520-2247 
MOHAWK BLACK ULTRA 
2 
PENETRATING STAIN 
19.1 #3 
M520-00017 
REDUCER, ULTRA PENETRATING 
2 
STAIN, GALLON 
19.1 #4 
P63563A 
LEX EDGE OUTDOR SOYD. 
1 
19.1 45 
P77709A 
INTENSE RED (FOIL) 
1 
19.1 #6 
P77685A 
91M FX BLACK SPOT FOIL GERBER 
1 
EDGE GSP 
19.1 #7 
P77753A 
PLACARD, RUBY RED GERBER 
I 
FOIL 
19.1 kt1 
T1310-14 
TRANSFER RITE 1310 UTRACLEAR 
1 
TAPE 14" x 100 VD 
19.1 #9 
GSE150717-1LP 
QTR FIG DARK EUCALYPTUS 
1,139 
19.1 #10 
P65580A 
GERBER 1MAGECAST, CLEAR, IS 
50 
IN/38CM-P 
19.1 #11 
1357 NEUTRAL 5GAL 
ADHESIVE CEMENT, 5GAL, 
I 
GAA100AU1 
19.1 #12 
923450GL 
CLEARCOAT, MULTI-TEMP BAKING 
26 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
19.1 #13 
929-91-3.5L 
HARDENER,GLASURIT FINISH 
15 
19.1 #14 
352-91 GAL 
REDUCER 
15 
19.1 #15 
8-4QTR-SAWN-MOZAMBK HARD WOOD QTR SAWN 
150 
MOZAMBIQUE 
19.1 #20 
MS2469456 
SCREW 
3 
19.1 #21 
NIS24694S6 
SCREW 
15 
19.1 #22 
hIS35206-226 
SCREW 
50 
19.1423 
222S 
PAINT-MID-COAT ADHESION 
2 
PROMOTER 
19.1 #24 
NAS1149FN832P 
WASHER, FLAT STEEL 
100 
19.1425 
GSE150717-1LP 
QTR FIG DARK EUCALYPTUS 
126 
19.1 #26 
DMA50 
DISPENSING GUN KIT FOR 50hIL 
1 
EPDXY CARTRIDGES 
19.1427 
hIEGM10001 
PRO SPEED COMPOUND 
5 
19.1 #28 
P65580A 
GERBER IMAGECAST, CLEAR, IS 
50 
IN/38CM-P 
19.1 #29 
1357 NEUTRAL 5GAL 
ADHESIVE CEMENT, SGAL, 
1 
GAA100AU1 
19.1 430 
923450GL 
CLEARCOAT, MULTI-TEMP BAKING 
6 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
19.1432 
923450GL 
CLEARCOAT, MULTI-TEMP BAKING 
4 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
19.1 #33 
923450GL 
CLEARCOAT, MULTI-TEMP BAKING 
6 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
19.1 #34 
929-93 
GLASURIT HARDNER (35 LITER) 
3 
19.1#35 
929-91-3.5L 
HARDENER,GLASURIT FINISH 
2 
19.1 #36 
P77788A 
WHITE (FOIL! 
I 
19.1 #37 
DPIOOFR 
EPDXY ADHESIVE, 1.7 OZ 
2 
19.1 #38 
CA40 
ADHESIVE I OZ 
2 
19.1#39 
PRONTO SURFACE 
ACTIVATOR 
3 
19.1 #45 
923460GL 
CLEARCOAT, MULTI-TEMP BAKING 
I 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 32 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811172

Bill To: Plan D, LLC. 
Pans: 
Ref. No. 
Pan number: 
WO #: SC521661 
Invoice Number: 5517132452 
Description 
Quantity 
19.1 #47 
437-2263 
PRIMER, IN WC EXTUFF (5 GAL 
PAIL) 
19.1 #46 
923-4S0GL 
CLEARCOAT, MULTI-TEMP BAKING 
6 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
19.1 #48 
923-45061 
CLEARCOAT, MULTI-TEMP BAKING 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
19.1 #49 
923-450GL 
CLEARCOAT, MULTI-TEMP BAKING 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
19.1 #50 
923-450GL 
CLEARCOAT, MULTI-TEMP BAKING 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
19.1#51 
923-450GL 
CLEARCOAT, MULTI-TEMP BAKING 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
19.1 #52 
923-450 ;L 
CLEARCOAT, MULTI-TEMP BAKING 
4 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
19.1#53 
929-91-3.51 
HARDENER,GLASURIT FINISH 
1 
19.1 #54 
929-91-3.51 
HARDENER, GLASURIT FINISH 
1 
19.1 #55 
929-91-3.51 
HARDENER,GLASURIT FINISH 
2 
19.1 #56 
832J16-2IBR 
INSERT 
12 
19.1 #57 
400 EVERCOAT 
EVERCOAT FILLER 
1 
19.1 #58 
GMS5005-I QT 
EPDXY PRIMER COATING (TYPE I) 
3012 QUART KIT (44GN011 QK) 
19.1 #59 
282.01.701 
SUPPORT, SHELF 
20 
19.1#611 
PRONTO SURFACE 
ACTIVATOR 
2 
19.1 #63 
923450GL 
CLEARCOAT, MULTI-TEMP BAKING 
10 
URETHANE ACRYLIC, GLASURIT 
(35 LITER) 
19.1 #64 
DMD1684/GL 
PAINT, DELTRON BASECOAT 
WHITE 
19.1 #65 
DMD1683IGL 
PAINT, DELTRON BASECOAT 
BLACK 
19.1 #66 
CA8000KICKER QT 
PAINT KICKER 
2 
19.1 #67 
929-91-3.51 
HARDENER, GLASURIT FINISH 
1 
19.1 #68 
929-91-3.51 
HARDENER, GLASURIT FINISH 
1 
19.1 #69 
929-91-3.51 
HARDENER, GLASURIT FINISH 
6 
19.1 #70 
522-10 
ACCELERATOR, DRYING ADDITIVE 
19.1 #71 
522-10 
ACCELERATOR, DRYING ADDITIVE 
4 
19.1 #72 
352-91 GAL 
REDUCER 
6 
19.1 #73 
GMS5005-I QT 
EPDXY PRIMER COATING (TYPE I) 
2 
3012 QUART KIT (44GN011 QK) 
19.1 #74 
hIEGNI10001 
PRO SPEED COMPOUND 
4 
19.1 #75 
M524693-C26 
SCREW, MACHINE, FLAT 
12 
COUNTERSUNK HD. 100 DEG. 
CROSS RECESS 
19.1 #76 
MS24694-53 
SCREW, MACHINE, FLAT CTSK HD, 
8 
100 DEG, STRL, CROSS RECESSED 
19.1 #77 
22001-15 
ISOLATOR 
2 
19.1 #78 
MS27039-1-6 
SCREW 
143 
19.1 #79 
MS27039-1-09 
SCREW, MACHINE PAN HEAD 
150 
STRUCTURAL 
19.1 #80 
NAS1149F0332P 
WASHER. FLAT STEEL 
100 
19.1 #81 
NAS6603-7 
BOLT-HEX HEAD, CLOSE 
25 
TOLERANCE 
19.1 #82 
AN970-3 
WASHER. FLAT 
50 
19.1 #83 
M527039-1-06 
SCREW-MACHINE,PAN HEAD 
7 
19.1 #84 
1032J19-24 B/R 
INSERT. THREADED 
20 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawkslnvoice.rpt v3 
Page 33 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811173

Bill To: Plan D, LLC. 
Pans: 
Ref. No. 
Part number: 
WO #: SC521661 
Description 
Invoice Number: 5517132452 
Quantity 
19.1 #ss 
NAS6603-6 
BOLT, HEX HEAD, CLOSE 
24 
TOLERANCE 
19.1 #86 
CA40 
ADHESIVE I OZ 
2 
19.1 #87 
PRONTO SURFACE 
ACTIVATOR 
2 
19.1 #88 
GAPIO5A15C 
KYDEX 100(#62015) IVORY-.060 
I 
19.1 #89 
151.01.710 
FLUSH HANDLE 
I 
19.1 #90 
NAS1149D0332K 
WASHER. FLAT ANODIZED 
8 
ALUMINUM 
19.1 #91 
NAS1149D0363H 
WASHER 
8 
19.1 #92 
1159F57355-3 
BRACKET AS.SY 
1 
19.1 #94 
GAG8106H3 
GASKET, U.S. 100% INSPECTED 
10 
19.1 #95 
GAG8106H3 
GASKET, U.S. 100% INSPECTED 
10 
19.1 #96 
MS24693-530 
SCREW, MACHINE, FLAT 
10 
COUNTERSUNK HD, 100 DEG, 
CROSS RECESS 
19.1 #97 
MS24693-532 
SCREW, COUNTERSINK-I00 
10 
DEGREE 
19.1 #98 
MS24665-300 
COTTER PIN 
4 
19.1 #99 
NAS1580C3T17 
BOLT 
2 
19.1.5 #2 
NAS1611-015A 
0 -RING 
8 
19.1.5 #3 
NASM24665-I53 
COTTER PIN 
4 
19.1.5#4 
NAS1611-013A 
0 -RING 
' 
19.1.5 #8 
DPIOOFR 
EPDXY ADHESIVE, 1.7 OZ 
1 
19.1.5#9 
DPIOOFR 
EPDXY ADHESIVE, 1.7 DZ 
1 
19.1.5 #10 
DPIOOFR 
EPDXY ADHESIVE, 1.7 OZ 
1 
19.1.5 #11 
DPIOOFR 
EPDXY ADHESIVE, 1.7 OZ 
1 
19.1.5 #12 
DPIOOFR 
EPDXY ADHESIVE, 1.7 OZ 
1 
19.1.5 #13 
DPIOOFR 
EPDXY ADHESIVE, 1.7 OZ 
1 
19.1.5 #14 
DPIOOFR 
EPDXY ADHESIVE, 1.7 OZ 
1 
19.1.5 #15 
DPIOOFR 
EPDXY ADHESIVE, 1.7 OZ 
1 
19.1.5 #16 
DPIOOFR 
EPDXY ADHESIVE, 1.7 OZ 
1 
19.1.5 #17 
DPIOOFR 
EPDXY ADHESIVE, 1.7 OZ 
I 
19.1.8.6 #1 
M52469456 
SCREW 
2 
19.1.8.6 #2 
M52469456 
SCREW 
IS 
Services: 
Ref. No. 
Description 
Quantity 
19.1 #1 
Vendor Supplied Labor 
1.00 
19.13 #1 
Vendor Supplied Labor SAPS 
1.00 
19.1.4 #1 
Vendor Supplied Labor 
1.00 
19.1.4 #2 
Vendor Supplied Labor 
1.00 
19.1.4 #3 
Vendor Supplied Labor 
1.00 
19.1.4 #4 
Vendor Supplied Labor 
1.00 
19.1.4 #5 
Vendor Supplied Labor 
1.00 
19.1.4 #6 
Vendor Supplied Labor 
1.00 
19.1.4 #7 
Vendor Supplied Labor 
1.00 
19.1.4 #8 
Vendor Supplied Labor 
1.00 
19.1.4 #9 
Vendor Supplied Labor 
1.00 
19.1.4 #11 
Vendor Supplied Labor 
1.00 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 34 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811174

Bill To: Plan D, LLC. 
WO it: SC521661 
Invoice Number: 5517132452 
Step: 19.1.1 
Completed 
AV1 /Electrical Labor Only 
Step: 19.1.2 
Completed 
INT Sheet Metal Labor Only 
Step: 19.13 
Completed 
Wood Labor Only (270 ) 
Deducted 270 hours from the original 1897 hours for vendor supplied labor (SAPS) 
Step: 19.1.4 
Completed 
INT Finish and Paint Labor Only 
Total Hours 1186 
Outside Labor for 11/27 to 12/6 
197 hrs 
Outside Labor for 12/4 to 12/10 208 hrs 
Outside Labor for 12/11 to 12/17 58 hrs 
Outside Labor for 12118 to 12124 40 hrs 
Outside Labor for 1/2 to 1/7 90 hrs 
Outside Labor for 1/8 to 1/14 180 hrs 
Outside Labor for 1/15 to 1/21 120hrs 
Outside Labor for 1122 to 1/28 180hrs 
Outside Labor for1/29 to 214 60 hrs 
Outside Labor for2/5 to VII 50 hrs 
Step: 19.1.5 
Completed 
NT Support (R&R) Labor Only 
Step: 19.1.5.1 
Completed 
****VOID**** Entere din wrong section 
Removed all old sealant from the outboard edges of the MED entn way fwd and aft 
bulkhead veneer pieces per .A3134 G550 20-4240 March 31/17. The edges are taped and 
are ready to be scaled. 
Step: 19.1.5.2 
Completed 
*****VOID*** ENT in wrong section ref 
Applied PR 1440 BI/2 sealant to M.E.D. aft bulkhead veneer closeout at 01:00 on 
3/1/2018 per 6550 AMM 20-42-00 March 31/17. 
Step: 19.1.6 
Completed 
Inspection Labor Only 
Step: 19.1.7 
Completed 
Flammability t Placards Labor Only 
Step: 19.1.8 
Completed 
Wood Shop Labor to Strip Existing Veneer. 
Step: 19.1.8.1 
Completed 
Strip Veneer - RH and LH 680 Bulkheads and Door. 
Step: 19.1.8.2 
Completed 
Strip Veneer -AFT LAN' Niche and Shroud. 
Step: 19.1.8.3 
Completed 
Strip Veneer -AFT Lay Vanity 
Step: 19.1.8.4 
Completed 
Strip Veneer -AFT LH Closet. 
Step: 19.1.8.5 
Completed 
Strip Veneer -AFT RH Closet. 
Step: 19.1.8.6 
Completed 
Strip Veneer -AFT LH Galley. 
Step: 19.1.8.7 
Completed 
Strip Veneer -AFT RH Galley Annex. 
Step: 19.1.8.8 
Completed 
Strip Veneer - 4 Divan End Cabinets. 
Step: 19.1.8.9 
Completed 
Strip Veneer -Cabin Ledges. 
Step: 19.1.8.10 
Completed 
Strip Veneer - Console Tables. 
Step: 19.1.8.11 
Completed 
Strip Veneer- FWD Pocket Door. 
Step: 19.1.8.12 
Completed 
Strip Veneer - FWD RH and 1.11 Cabin Bulkheads. 
Step: 19.1.8.13 
Completed 
Strip Veneer - PSU Handrails. 
Step: 19.1.8.14 
Completed 
Strip Veneer - FWD Crew Refresh Cabinet. 
Step: 19.1.8.15 
Completed 
Strip Veneer - FWD RH Lay. 
Step: 19.1.8.16 
Completed 
Strip Veneer - REER and LEER panels. 
Step: 19.1.8.17 
Completed 
Strip Veneer -Acoustic Door. 
Step: 19.1.8.18 
Completed 
Strip Veneer - Entry Panels (2) 
Step: 19.1.8.19 
Completed 
Strip Veneer - AFT LAV Door. 
Step: 19.1.8.20 
Completed 
Strip Veneer - FWD Lav Door. 
Step: 19.1.8.21 
Completed 
Strip Veneer - Magazine Racks. 
Step: 19.1.9 
Completed 
Wood Shop Labor to Reveneer Cabinets. 
Step: 19.1.9.1 
Completed 
Labor to Veneer -1.11 and RH 680 Bulkheads and Door. 
Step: 19.1.9.2 
Completed 
Labor to Veneer - AFT LAV Niche and Shroud. 
Step: 19.1.9.3 
Completed 
Labor to Veneer -AFT Lay Vanity. 
Step: 19.1.9.4 
Completed 
Labor to Veneer -AFT LH Closet. 
Step: 19.1.9.5 
Completed 
Labor to Veneer -AFT RH Closet. 
Step: 19.1.9.6 
Completed 
Labor to Veneer -AFT LH Galley. 
Step: 19.1.9.7 
Completed 
Labor to Veneer -AFT RH GalleyAnnex. 
Step: 19.1.9.8 
Completed 
Labor to Veneer - 4 Divan End Cabinets. 
Step: 19.1.9.9 
Completed 
Labor to Veneer -Cabin Ledges. 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 35 of 64 
Printed: 3/7/2018 3:15:05PM 
tit W. 
EFTA00811175

Bill To: Plan D, LLC. 
WO #: SC521661 
Invoice Number: 5517132452 
Completed 
Labor to Veneer - FWD Pocket Door. 
Completed 
Labor to Veneer - FWD LH and RH Bulkheads. 
Completed 
Labor to Veneer - PSU Hand Rails. 
Completed 
Labor to Veneer - FWD Crew Refresh Cabinet. 
Completed 
Labor to Veneer - FWD RH Lay. 
Completed 
Labor to Veneer - LEER and Reer Panels. 
Completed 
Labor to Veneer - Acoustic Doors. 
Completed 
Labor to Veneer - Entry Bulkheads (2) 
Completed 
Labor to Veneer -AFT Lav Door. 
Completed 
Labor to Veneer - FWD Lay Door. 
Completed 
Labor to Veneer - Console Tables. 
Completed 
1.abor to Veneer - Magazine Racks. 
Completed 
Wood Shop Labor to Assemble Cabinets. 
Completed 
Labor to Assemble - LH and RH 680 Bulkheads and Door. 
Completed 
1.abor to Assemble -AFT Lay Niche and Shroud. 
Completed 
Labor to Assemble - AFT Lay Vanity. 
Completed 
Labor to Assemble -AFT LH Closet. 
Completed 
1.abor to Assemble - AFT RH Closet. 
Completed 
Labor to Assemble - AFT LH Galley. 
Completed 
Labor to Assemble - AFT RH Galley Annex. 
Completed 
1.abor to Assemble - 4 Divan End Cabinets. 
Completed 
Labor to Assemble - Cabin Ledges. 
Completed 
1.abor to Assemble - Console tables. 
Completed 
1.abor to Assemble - FWD Pocket Door. 
Completed 
1.abor to Assemble - FWD LH and RH Cabin Bulkheads. 
Completed 
Labor to Assemble - FWD Crew Refresh Cabinet. 
Completed 
Labor to Assemble - FWD RH Lim 
Completed 
Labor to Assemble - Leer and Reer Panels. 
Completed 
Labor to Assemble - Acoustic Doors. 
Completed 
Labor to Assemble - AFT Lay Door. 
Completed 
Labor to Assemble - FWD Lay Door. 
Completed 
***Entered in Error******* 
Flammability Data. 
Completed 
Removal/Install of R/H #1 and R/H #2 E-windows required for access for interior 
installation. As per 6550 AMM 52-22-00 Rev Nov 15/17. 
Step: 19.1.9.10 
Step: 19.1.9.11 
Step: 19.1.9.12 
Step: 19.1.9.13 
Step: 19.1.9.14 
Step: 19.1.9.15 
Step: 19.1.9.16 
Step: 19.1.9.17 
Step: 19.1.9.18 
Step: 19.1.9.19 
Step: 19.1.9.20 
Step: 19.1.9.21 
Step: 19.1.10 
Step: 19.1.10.1 
Step: 19.1.10.2 
Step: 19.1.10.3 
Step: 19.1.10.4 
Step: 19.1.10.5 
Step: 19.1.10.6 
Step: 19.1.10.7 
Step: 19.1.10.8 
Step: 19.1.10.9 
Step: 19.1.10.10 
Step: 19.1.10.11 
Step: 19.1.10.12 
Step: 19.1.10.13 
Step: 19.1.10.14 
Step: 19.1.10.15 
Step: 19.1.10.16 
Step: 19.1.10.17 
Step: 19.1.10.18 
Step: 19.1.11 
Step: 19.1.12 
Step: 19.1.12.1 
Step: 19.1.12.2 
Step: 19.1.12.3 
Step: 19.1.12.4 
Step: 19.1.12.5 
Step: 19.1.12.6 
Step: 19.1.13 
R/H #1 P/N 1159SCCE500-23 S/N 0702030 
R/H #2 P/N 1159SCCE500-23 S/N 0701885 
Completed 
Removed FUH #1 and R/H #2 E-windows for access for interior installation. As per 
6550 .AMM 52-22-00 Rev Noy 15/17. 
FUN #1 P/N II 59SCCE500-23 S/N 0702030 
FUN #2 P/N 1159SCCE500-23 S/N 0701885 
Completed 
Install of R/H #1 and Rill #2 E-windows for access for interior installation. As per G550 
AMM 52-22-00 Rev Nov 15/17. 
Ref.11.141. 11.142 
Rill #1 P/N 1159SCCE500-23 S/N 0702030 
RAF #2 P/N 1159SCCE500-23 SIN 0701885 
Completed 
CMP G550 562115 Cabin Windows- Leak Check 
Ref.11.143 
Completed 
CMP G550 560001 Emergency Window Release Mechanism - Functional Test 
Ref.11.144 
Completed 
CMP 6550 304110 CABIN WINDOW HEAT - 0PS TEST 
Ref.11.145 
Completed 
E-window #2 is out of limits on emergency window release mechanism - fuctional test. 
inside pull is at 42. and outside pull is at 65. 
Completed 
Summary: 
Removed all old sealant from the outboard edges of the MED entry way fwd and aft 
bulkhead veneer pieces per AMM G550 20-42-00 March 31/17. The edges are taped and 
are ready to be scaled. 
see sub-steps below 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksinvoicc.rpt v3 
Page 36 of 64 
Printed: 3/7/2018 3:15:05PM 
tit W. 
EFTA00811176

Bill To: Plan D, LLC. 
WO 
SC521661 
Invoice Number: 5517132452 
Step: 19.1.13.1 
Completed 
Applied PR 1440 8112 sealant to M.E.D. aft bulkhead 'veneer closeout at 01:00 on 
3/1/2018 per 6550 AMM 20-42-00 March 31/17. 
Step: 19.1.13.2 
Completed 
Applied PR 1440 B1/2 sealant to M.E.D. fwd bulkhead veneer closeout at 4:30pm on 
3/1/2018 per 6550 AMM 20-42-00 March 31/17. 
Step: 19.1.14 
Completed 
Permanently install MED airstair upper handrail bolts where handrails attach to 
bulkheads (NA and aft). 
Item: 
20 
Registration Change 
Team Manager: 
Charles Thomas 
Customer Coordinator: 
Julian Brown 
Part/Model 
AC Serial No/Tail No.: 
TSNITSO: 
CSN/CSO: 
Aircraft Time: 
Discrepancy: 20.1 
Comply with registration change as outlined in RSQCT-115 Rev. 12. Registration change to N2I2JE. 
Resolution: Complied with registration change as outlined in RSQCT-115 Rev. 12. 
Reference steps below and traveler paper copy index 013A for details of work performed. 
Billing Method 
Hours 
Rate 
Total 
Labor USD: 
Time and Material 
ST 
37.64 
@ 
$146.00 
$5,495.44 
Labor USD: 
Time and Material 
OT 
4.46 
® 
$146.00 
$651.16 
Labor USD: 
Time and Material 
ST 
4.63 
@ 
$222.00 
$1,027.86 
Parts USD: 
Time and Material 
$31.80 
Total USD: 
$7,206.26 
Pans: 
Ref. No. 
Pan number: 
Description 
Quantity 
Sell price USD 
Extended USD 
20.181 
CTS-S22/22 
CONTACT 
30 
$0.51 
$15.30 
20.182 
GAS805IC2 
SPLICE 
30 
50.22 
$6.60 
20.1 83 
GAC860K-2 
END CAP-RED 
30 
$033 
49.90 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 37 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811177

Bill To: Plan D, LLC. 
WO St: SC521661 
Invoice Number: 5517132452 
Step: 20.1.1 
Completed 
Customer requests that the Gulfstream (WA issue a replacement standard airworthiness 
certificate due to registration change. Provide to the ODA the following items: 
A. A copy of the workorder cover sheet with current hours and landings. 
B. Standard Airworthiness Certificate. FAA Form 8100-2. 
C. Certificate of Aircraft Registration. AC Form 8050-3. 
Step: 20.1.2 
Completed 
Require a written original statement signed by the registered owner or certificate 
opreator to request a replacement airworthiness certificate. The request shall include the 
registration number. serial number. make and model of the aircraft as well as the reason 
for the request. 
Step: 20.1.3 
Completed 
Review the aircraft records and inspect the aircraft to ensure the request is justified and 
the aircraft is eligible for the certification requested. Records review consists of 
verification that there are no open maintenance due actions or airworthiness directives. 
Aircraft inspection consists of a data plate and registration marking examination. with a 
visual review of the aircraft for obvious conditions impacting aircraft safety. 
Step: 20.1.4 
Completed 
Verify current aircraft registration. reference 14 CFR 47: Hard copy Registration AC: 
form 8050-3 for new registration number or Assignment of Special Registration Number 
AC form 81)50-64 alnd hard copy of old Registration AC Form 8050-3 8050-3 or Dealer 
Registration AC Form K050-6. 
Step: 20.1.5 
Completed 
Verify new registration number is installed on the aircraft. Ref: I4CFR 45.23, 45.25. 
45.29 & 4533. 
Step: 20.1.6 
Completed 
Verify aircraft ID plate installation. Ref: 14 CFR Part 45. 
Step: 20.1.7 
Completed 
FAA form 8100-2 issued for new registration number by Gulfstream ODA. 
Step: 20.1.8 
Completed 
If the customer defers Gulfstream ()DA issuance of a replacement airworthiness 
certificate. a Corridor squawk will be signed as deferred by the customer. Rref : 14 
CFR 91.203 (a) (1) 1
Step: 20.1.9 
Completed 
Re-strap/ Re-program transponders to new registration. (Transponders with Mode S) 
Step: 20.1.10 
Completed 
Re-Strap/Re- program SEI.CAl. to new code if ownership changes. 
Step: 20.1.11 
Completed 
Commission SATCOM for new ownership / or Re-Strap SDU for new registration 
number change. 
Step: 20.1.12 
Completed 
Reconfigure Magnastar. Aircell. & Iridium systems. 
Step: 20.1.13 
Completed 
Configure AFIS. New installation or registration number change. Re-strap via Laptop. 
Step: 20.1.14 
Completed 
Install new registration number placards in cockpit. 
Step: 20.1.15 
Completed 
Install(if new) SELCAL number in cockpit. 
Step: 20.1.16 
Completed 
Change logo on Airshow / Cabinview. if ownership changes. 
Step: 20.1.17 
Completed 
Re-strap or re-program ELT's (406MHZ) in aircraft ( As required to new registration 
and / or country code). 
Step: 20.1.18 
Completed 
Reconfigure High Speed Data Units or BBML. 
Step: 20.1.19 
Completed 
Reconfigure Display Controllers Tail number ISELCAL. 
Step: 20.1.20 
Completed 
Verify proper registration of ELT's (406MHZ) ( if installed in life rafts). 
Step: 20.1.21 
Completed 
Reconfigure the Enhanced Flight Identification Code to the current registration 
Step: 20.1.22 
Completed 
()plain a copy of the Export Certificate of Airworthiness. Foreign Airworthiness 
Certificates. all Foreign Registration Documents and archive with the workorder. 
Item: 
21 
12 Month CNIP Tasks (Exhibit 1)-(Ref. Item C 1.1 of Proposal ID4 7039702 ROO) 
Team Manager: 
Customer Coordinator: 
Charles Thomas 
Julian Brown 
Pan/Model 8: 
AC Serial No/Tail No.: 
TSN/TSO: 
CSNJCSO: 
Aircraft Time: 
Discrepancy: 21.1 
Accomplish 12 Month CNIP Tasks (Exhibit 1) 
Notes: 
Correction of discrepancies is not included in the quoted price. 
Materials / Outside Services will be billed as required. 
Resolution: Complied with 12 Month CMP Tasks. 
See squawks below for details of all work accomplished. 
(Complied with all required tasks for a 12 months/1C check) 
Billing Method 
Hours 
Rate 
Total 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
liAC_RevenueSquawksInvoice.rpt v3 
Page 38 of 64 
Printed: 3/7/2018 3:15:05PM 
tit kW 
EFTA00811178

Bill To: Plan D, LLC. 
WO #: SC521661 
Invoice Number: 5517132452 
Labor USD: 
Flat Rate 
$9,298.00 
Total USD: 
$9,298.00 
Discrepancy: 21.32 
CMP G550 312003 BATTERY, PILOT CLOCK 
Resolution: COMPLIED WITH CMP G550 312003 BATTERY, PILOT CLOCK 
Billing Method 
Hours 
Rate 
Total 
Pans USD: 
Time and Material 
$2.63 
Total USD: 
$2.63 
Pans: 
Ref. No. 
 Part number: 
Description 
Quantity 
Sell price USD 
Extended USD 
21.32 #1 
MN9I00 
BATTERY, LW SIZE N, DURACELL 
1 
$2.63 
52.63 
Discrepancy: 21.33 
CMP G550 312004 BATTERY, COPILOT CLOCK 
Resolution: COMPLIED WITH CMP G550 312004 BATTERY, COPILOT CLOCK 
Billing Method 
Hours 
Rate 
Total 
Pans USD: 
Time and Material 
$2.63 
Total USD: 
$2.63 
Pans: 
Ref. No. 
 Pan number: 
Description 
 
Quantity 
Sell price USD 
Extended USD 
2133 #1 
MN9100 
BATTERY, I.5V SIZE N. DURACELL 
1 
$2.63 
52.63 
Discrepancy: 21.65 
CMP G550 381039 WATER STERILIZER 
Resolution: COMPLIED WITH CMP G550 381039 WATER STERILIZER 
Billing Method 
Hours 
Rate 
Total 
Labor USD: 
No Charge 
N/C 
Pans USD: 
Tittic and Material 
$40.50 
Total USD: 
$40.50 
Pans: 
Ref. No. 
 Part number: 
 Description 
 
Quantity  
Scll price USD 
I:mended l'til) 
21.65 #1 
02-190002-012 
WATER FILTER 0 -RIM; 
3 
513.50 
$40.50 
Discrepancy: 21.67 
CAW G550 382002 Water Sterilizer Filter - Removal I Installation 
Resolution: COMPLIED WITH CMP G550 382002 Water Sterilizer Filter - Removal / Installation 
Billing Method 
Hours 
Rate 
Total 
Labor USD: 
No Charge 
N/ C 
Parts USD: 
Time and Material 
$119.25 
Total USD: 
$119.25 
Pans: 
Ref. No. 
Pan number: 
Description 
Quantity 
Sell price USD 
Extended USD 
21.67 #1 
06-133802-001 
FILTER, WATER 
1 
$92.25 
$92.25 
21.67#2 
02-190002-018 
WATER FILTER 0 -RING 
1 
$13.50 
$13.50 
21.67 #3 
02-190002-019 
WATER SYSTEM 0 -RING, FILTER 
1 
$13.50 
$13.50 
SPACER 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoice.rpt v3 
Page 39 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811179

Bill To: Plan D, LLC. 
WO #: SC521661 
Invoice Number: 5517132452 
Item: 22 
Discrepancies related to 12 Month CMP Tasks (Exhibit 1) - (Ref. Item C 1.1 of Proposal ID# 7039702 ROO) 
Team Manager: 
Customer Coordinator: 
Charles Thomas 
Julian Brown 
ParUModel #: 
AC Serial No/Tail No.: 
TSN/TSO: 
CSN/CSO: 
Aircraft Time: 
Item: 23 
Miscellaneous CUP Tasks (Exhibit 3) - (Ref. Item C 1.3 of Proposal ID# 7039702 ROO) 
Team Manager: 
Customer Coordinator: 
Charles Thomas 
Julian Brown 
Pan/Model #: 
AC Serial No/Tail No.: 
TSN/TSO: 
CSN/CSO: 
Aircraft Time: 
Discrepancy: 23.1 
Accomplish Miscellaneous CMP Tasks (Exhibit 3) 
Notes: 
O Correction of discrepancies is not included in the quoted price. 
O Materials / Outside Services will be billed as required. 
Resolution: 
Billing Method 
flours 
Rate 
Total 
Labor USD: 
Flat Rate 
$8,953.00 
Total USD: 
$8,953.00 
Discrepancy: 23.12 
CMP G550 282651 Main Fuel Boost Pump (Left) - Fuel Leak Check 
Resolution: COMPLIED WITH CMP G550 282651 Main Fuel Boost Pump (Left) - Fuel Leak Check 
TW 558064 
Date Due 08/18 
Billing Method 
Hours 
Rate 
Total 
Labor USD: 
No Charge 
N/ C 
Pans USD: 
Time and Material 
51.88 
Total USD: 
$1.88 
Pans: 
Ref. No. 
 Pan number: 
 Description 
 
Quantity 
Sell price USD 
Extended USD 
23.12#1 
NAS1612-3A 
0 -RING. 0.188 INCH OD TUBING 
4 
50.47 
41.88 
Discrepancy: 23.17 
CMP G550 323012 Landing Gear Emergency Extension Nitrogen Blow-down Bottle (Right) - (Hydrostatic) 
Functional Test 
Resolution: COMPLIED WITH CMP G550 323012 Landing Gear Emergency Extension Nitrogen Blow-down Bottle (Right) -
(Hydrostatic) Functional Test 
Billing Method 
Hours 
Rate 
Total 
Labor USD: 
No ('barge 
N/ C 
Pans USD: 
Time and Material 
$2.86 
Total USD: 
$2.86 
Parts: 
Ref. No. 
Pan number: 
Description 
Quantity 
Sell price USD 
Extended USD 
23.17#1 
NAS1612-4A 
SEAL, 0.250 INCH OD TUBING 
2 
5030 
50.60 
23.17 #2 
2-212 E0540-80 
SEAL-0 RING 
2 
$1.13 
52.26 
For detail description of the work complied with see the Work Order Detail report. 
Unless otherwise indicated. all financial values listed in this document are in US Dollars (USD). 
GAC_RevenueSquawksInvoicc.rpt v3 
Page 40 of 64 
Printed: 3/7/2018 3:15:05PM 
tat W. 
EFTA00811180