1989 Gulfstream IV used
Description
The Gulfstream IV (G-IV) is a twin-engine long-range business jet, produced by General Dynamics’ Gulfstream Aerospace division. It is an improved version of the Gulfstream III (G-III) and features an all-new wing design and more powerful engines. It made its first flight in 1985 and was certified in 1987. The G-IV was popular among business executives and celebrities, with over 500 aircraft produced.
The G-IV was powered by two Rolls-Royce Tay engines, with a maximum takeoff weight of 61,500 lb (27,876 kg). It had a range of 4,350 nmi (8,062 km), could reach speeds of Mach 0.88, and had a maximum altitude of 45,000 ft (13,716 m). The cabin was designed to be comfortable, with seats for up to 16 passengers and a galley, lavatory, and private stateroom.
The G-IV was eventually superseded by the Gulfstream V (G-V) in 1995, which featured more powerful engines and a longer range. The G-IV was retired in 2005, and all remaining G-IVs were eventually sold off or retired.
Features
- Total Time: 13572
- Avionics Package: Honeywell SPZ-8000 IFCS/Pro Line 4
- AFIS: 6 Tube EFIS
- Autopilot: Honeywell SPZ-8000
- Flight Directors: Dual Honeywell FZ 820
- Comms: Triple Collins VHF-422B with 8.33 spacing
- Navs: Dual Collins VIR-432 with FM immunity
- FMS: Dual Honeywell NZ 2000 5.2 Software
- Single Universal UNS-1M with GPS
- GPS: Universal UNS-1M with GPS
- IRS: Dual Honeywell Laseref II, Single Laseref III
- HF: Dual MTRLA 190 with SELCAL
- SATCOM: Collins 906 6 channel
- Airborne Phone: Dual Magnastor C2000
- DME: Dual Collins DME-442
- ADF: Dual Collins ADF-462B
- Transponder: Dual Collins TDR-94D w/ Mode S
- Color Radar: Honeywell Primus 880
- Stormscope: LP 850
- Radio Altimeter: Dual Honeywell RT-300
- EGPWS: Honeywell
- TCAS: Honeywell TCAS II
- CVR: Loral
- FDR: Wiring Provisions
- ELT: Artex C406-2 ELT with GPS nav interface
- ADS-B: Compliant
- RVSM
Location
