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Raw Total Labor USD: $23,939.84 $74,150.00 $98,089.84 Parts USD: $196,307.51 $0.00 $196,307.51 Services USD: $1,547.68 $0.00 $1,547.68 Detail Subtotal USD: $221,795.03 $74,150.00 $295,945.03 Subtotal USD: $295.945.03 Funds on Deposit USD: 50.00 Total USD: Pre Test Flight Times /Cycles Airframe
p: 15.28.3 Completed Continue with removal of all requiered panels of CMP 553007; And Complied with steps B.(I) thru step B(22).All work done IAN' GIV AMM 53-30-00. Discrepancy: 15.29 CMP GIV 571011 Wing Front Beam Hi-Lite Collars (Left) - Inspection Resolution: COMPLIED WITH CMP GIV 571011 Wing Front
0 $14,342.00 $96,219.20 Pans USD: $49,601.41 $17,599.45 $67,200.86 Services USD: $0.00 $0.00 $0.00 Policy Prices USD $0.00 $0.00 $0.00 Detail Subtotal USD: $131,478.61 $31,941.45 $163,420.06 Tax USD: $0.00 Subtotal USD: $163,420.06 Funds on Deposit USD: $0.00 Invoice Number:90127788 Invoice D
TRUNNION L/H MOUNT PIN RETAINING BOLT AND REPOSITIONED PIN TO PROPERLY ALIGN GREASE FITTING. REINSTALLED RETAINING BOLT AND GREASED PIN. REFERENCED GIV AMM 32-24-01 FOR WORK PERFORMED. Billing Method Labor USD Time & Material ST Totals USD Hours Rate Total 1.700 $142.00 $241.40 $241.40 Item
.80 $105,278.80 Parts USD: $55,066.57 $21,766.39 $76,832.96 Services USD: $0.00 $7,781.00 $7,781.00 Policy Prices USD $0.00 $0.00 $0.00 Detail Subtotal USD: $140,408.57 $49,484.19 $189,892.76 Tax USD: $0.00 Subtotal USD: $189,892.76 Funds on Deposit USD: $0.00 Invoice Number:90129765 Invoice D
TRUNNION L/H MOUNT PIN RETAINING BOLT AND REPOSITIONED PIN TO PROPERLY ALIGN GREASE FITTING. REINSTALLED RETAINING BOLT AND GREASED PIN. REFERENCED GIV AMM 32-24-01 FOR WORK PERFORMED. For detailed description of the work complied with see the Work Order Detail report Unless otherwise indicated, all f
lat Rate Total Labor USD: 55,299.97 $204,738.00 $210,037.97 Pans USD: $0.00 $883,018.00 $883,018.00 Services USD: 5706.67 $0.00 $706.67 Detail Subtotal USD: $6,006.64 $1,087,756.00 $1,093,762.64 Subtotal USD: $1,093,762.64 Funds on Deposit USD: $761,252.00 Total USD: 361,252.00 4/26 400,000.00
hangar. All work done IAW Gulfstream GIV APU Retrofit Wiring Diagram 11595B49006. Rev L. sheet 3.001, for aircraft effectivity 1001, 1006.1182 and GIV AMM 49-60-00. Step: 12.1.10 Completed Complied with GIV-GER-9957 APU operational test after install of ASC 465. See item 6.9 for squawk. All other in
Entities connected to both Detail Subtotal USD and GIV AMM

Dallas
LOCATION
Savannah
LOCATIONJEGE, Inc.
ORGANIZATIONRIVET
ORGANIZATION
George W. Bush
PERSONDoug Band
PERSONGulfstream Aerospace Corporation
ORGANIZATION
Samantha Power
PERSONTime & Materials
ORGANIZATIONFAA CRS PB8R624N
ORGANIZATIONIAW GIV SRM
ORGANIZATIONSEMKIT
ORGANIZATIONSean Brown
PERSONAVIONICS
ORGANIZATION
Julie K. Brown
PERSONI.A.W.
ORGANIZATIONGIV CMP
ORGANIZATIONIlours
PERSONService Team
ORGANIZATIONLabor USD
ORGANIZATION