Gulfstream GIISP
Download The Specification SheetGulfstream - GIISP
Aircraft Specification G-IISP/ SERIAL No. 092 STATUS AS OF Jan 2010 AIRCRAFT TT: 14,644 TC: 8,710 LH (#1) ENGINE RH (#2) ENGINE Rolls-Royce Spey 511-8 Rolls-Royce Spey 511-8 TT: 9,221 TT: 9,221 TC: 5,626 TC: 5,626 TSM: 780 TMS: 780 Overhaul in September 2015 or 3,219 Hours Overhaul in June 2015 or 3,219 Hours APU Honeywell GTCP36-6 / PN 380514-1-43 TT: 7,268.3 HSI due in 635.7 APU-Hours AVIONICS
Autopilot Sperry SP-50G autopilot system Transponders Dual Collins TDR-94D VHF Comm Dual Collins VHF-22C (8.33 KHz) VHF Nav Dual Collins VIR-30A (FM Immune) ADF Dual Collins ADF-60 DME Dual Collins DME-40 Flight Director Dual Collins FD-109 FMS Dual Universal UNS-1D HF Dual King KHF-950 with SELCAL LRN Dual Litton LTN-92 ELT: 406 MHz L3 Communications WX-1000 Stormscope AirShow 400 Fairchild Cockpit Voice Recorder Bendix RDR-1150HP color radar system Honeywell TCAS-2000 (change 7) Universal TAWS (Class A) RVSM compliant – ASC 498 (STC ST01833AT-D)
Interior New 2006. 13 passenger executive interior featuring 4 forward berthable single seats, mid cabin has a 4-place conference group with opposing credenza with kibitzer seat, the aft cabin has a single berthable single seat opposite a 3-place divan. New Carpet and Padding and Divan installed February 2009. All seating is covered in Tan leather with the exception of the divan which is covered in fabric. A privacy door separates the forward cabin from the cockpit. Cabin is complete with sound proofing, high gloss dark cabinetry and dark wood trim, medium beige carpeting, fully equipped Aft galley and Aft Lavatory. In-flight entertainment – two DVD/CD/MP3 players 2 forward bulkhead mounted monitors 7 individual monitors ICG NxtLink-100 Iridium Phone System with 2x Sigma 7 Backlit in the cabin and 1 handset in the Cockpit (Installed Feb 2009) Exterior New 2006. Blue bottom with 3 blue stripes. ASC Status ASC 81 for 62,500 pound increased gross weight modification ASC 216 to permit simultaneous use of speed brakes and wing flaps up to a max of 20-degrees wing flaps ASC 226 to preclude the penetration of the nose gear drag brace into the cabin environment ASC 299 for increased operating altitude to 45,000 feet AiResearch Aviation Company long range oxygen system (STC SA1654WE) DeVore Aviation Corporation Tel-Tail Floodlights (STC SA4749SW) Aviation Partners Inc winglets (STC ST00080SE) Concorde Battery Corporation lead acid main batteries (STC ST00773LA) Maintenance Status: Fresh 12 and 24 Month Inspection – February 2009. Specifications are subject to verification upon inspection and should not provide a basis for reliance or create any other binding obligation. |
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