Epstein Secrets

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 Remit

ded 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 Ceili

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

Ref. No. Pan number: Description Quantity Sell price USD Extended USD 8.19 81 8.19 #4 Step: 8.19.1 Step: 8.19.2 Step: 8.19.3 WE3883738-1 VALVE, SOLENOID 1 35,572.61 M25981U2-904 PACKING 2 50.82 Completed Gained access to 181A1PI ( on APU Ceiling). Disconnected plug. inspected and cle

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, GA31402 For detail description of the work compiled with see the Work Order Detail report. Unless otherwise indicated, all financial values listed

DRAINED L/H PLENUM AND NOTED ABOUT 1/2 GAL OF FUEL DRAINED OUT. GAINED ACCESS TO L/H WING OUTBD VENT FLOAT VALVES AT RBS 428 AND VENT FLOAT RELIEF VALVE AT BL 12.5. UPON INSPECTION OF VALVES NOTED FWRD OUTBD VENT FLOAT VALVE AT ABS 428 TO NOT BE OPERATING SMOOTHLY. REMOVED VALVE P/N: L49700-3 S/N: 75

structions of ASC 143, except as provided for on the above listed Wiring Diagrams. All parts were purchased from Gulfstream Aerospace Corporation — Savannah, GA and were new at the time of installation. Successfully performed — ASC 143 Operational Test in accordance with Paragraph E. of the ASC's instru

nual operated the Auxiliary Power Unit and started both main engines and verified that the APU AIR. LOAD, ENGINE START or CRANK, and the ISOLATION. VALVE cockpit switches performed their intended &actions. Recorded compliance with this FAA form 337 in the aircraft's maintenance records and returned