Epstein Secrets

essed 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 existin

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)

iguration 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 n

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

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)

tion 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 Culfstream facility's Paint Operations Manager. including labor and materials on a Work Change Request (WCR). Billing NIethod flours Rate Total Labor USD:

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

ous other engine components. For the airplane, fan air is routed 2A-36-00 PRODUCTION AIRCRAFT SYSTEMS Revision 6 EFTA_R1_02095980 EFTA02705528 Culfstream IV OPERATING MANUAL through the precoolers to reduce the temperature of 7th and/or 12th stage bleed air. The precooler fan air modulating valve (ins

ck Diagram: SN 1285 and Subsequent; SN 1000- 1284 Having ASC 364 Figure 2 2A-36-00 Page 13 / 14 January 31102 EFTA_R1_02095988 EFTA02705536 GuIfstream IV OPERATING MANUAL ITEM NO. DESCRIPTION 1 VALVE. H P BLEED AIR PRESSURE REG & S/O 2 VALVE. L.P. BLEED AIR CHECK 3 SENSOR. BLEED AIR TEMPERATUR

H SERVO CONTROL SYSTEM 1 S TO OVERT EWA YARNING LIGHT 28 VOC TO BLEED AIR PRESSURE WARNING LIGHT TO BLEED AIR PRESSURE INDICATOR TO VALVE OPEN / CLOSE /WATCH LIGHT ON (OPEN) 20 TO DOOR SEAL SYSTEM 21 TO TOTAL TEMP PROBE LN SERVO CONTROL SYSTEM TO YANG ANTI - ICE SYSTEM P

Gulfstreamx A DYNAMIC• COPAP"IdiV PRELIMINARY INVOICE Part/Model #: GIV AC Serial NoJTail No.: 1085 / N212JE 7 Char Drive- Westfield, Massachusetts 01085-1

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

7-9-96 Michael natty PURPOSE OF DATA TO SHCE4 OCMPLIAI4CE WITH FEDERAL AIRWORTHINESS REGULATIONS, ON AIRCRAFT MODIFICATION WIRING DIAGRAM CN ANY GULFSTREAM G-IV HAVING ASC-143 APPUCABLE REQUIREMENTS (List spades sections) 25.1301(a,b,c,d); 25.1309(bl); 25.1353(a,b); 25.1357(a,c); 25.1431(c) CERTIFICATION

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