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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
01 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 finan
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:
01 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 finan
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
I-ICE SYSTEM TEMPERATURE 18 AUXILIARY POWER UNIT (APU) 19 AIR TURBINE STARTER & BLEED CONTROL VALVE 20 VALVE. DOOR SEAL PRESSURE REGULATOR 21 FILTER, SERVO AIR PRESSURE 22 VALVE. DUAL PORT SOLENOID SHUTOFF 23 VALVE, SOLENOID SHUTOFF. TOTAL TEMP PROBE 24 SWITCH. BLEED AIR OVERPRESSURE (65 PSI
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