Epstein Secrets

other instrument tendered as full satisfaction of a debt, must be forwarded to: Gulfstream Aerospace Attn: Credit Manager M/S B•05 PO BOX 2206, Savannah, GA 31402 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial values liste

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

on P.O. Box 730349 Dallas, Texas 75373-0349 Courier Remittance To: Gulfstream Aerospace Corporation ATTN: Treasury Manager 30 Innovation Drive Savannah, GA 31407 Preliminary Invoice Part/Model# GIV AC Serial Norfail No: 1085/N1201E Wire Remittance To: Gulfstream Aerospace Corporation JP Morgan

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

on P.O. Box 730349 Dallas, Texas 75373-0349 Courier Remittance To: Gulfstream Aerospace Corporation ATTN: Treasury Manager 30 Innovation Drive Savannah, GA 31407 Preliminary Invoice Part/Model# GIV AC Serial No/Tail No: 1085/N1201E Wire Remittance To: Gulfstream Aerospace Corporation JP Morgan

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

Software P/N Verification still required IAW Method 3 of ASC; Awaiting verification fixture P/N: T326948.901 and adapter cable PIN: 200F-00084 from Savannah; New labels for TCAS II required after software P/N verification; All work accomplished lAVi" GIV AMM 34-00-00 Item: 16 ADSB-B Out GAC0313-223-GI

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