Grumman / Gulfstream Gulfstream II (Grumman G-1159)
Corporate Jet
The Gulfstream Aerospace Gulfstream II is a twin-engined corporate jet aircraft produced by the US-American manufacturer Grumman Aerospace Corporation, as of 1978 Gulfstream Aerospace Corporation.
The Gulfstream II is a development of the Grumman G-159 Gulfstream I.
Crew | 2 | |
Passengers | 10-12, max. 19 |
Propulsion | 2 Turbofan Engines | |
Engine Model | Rolls-Royce RB.163 Spey Mk.511-8 | |
Engine Power (each) | 50,7 kN | 11400 lbf |
max. Cruise Speed | 850 km/h | 459 kts 528 mph |
Mmo (max. Mach) | Mach 0.85 | |
Service Ceiling | 13.716 m | 45.000 ft |
Range | 6.578 km | 3.552 NM 4.088 mi. |
Empty Weight | 16.576 kg | 36.544 lbs |
max. Takeoff Weight | 29.363 kg | 64.734 lbs |
Wing Span | 21,00 m | 68 ft 11 in |
Wing Area | 86,8 m² | 934 ft² |
Length | 24,36 m | 79 ft 11 in |
Height | 7,47 m | 24 ft 6 in |
First Flight | 02.10.1966 | |
Production Status | out of production | |
Production Range | 1967-1979 | |
Total Production | 258 | |
Developed from | Grumman Gulfstream I |
ICAO Code | GLF2 | |
IATA Code | GRJ | |
FAA TCDS | A12EA | |
EASA TCDS | A.070 | |
Data for (Version) | Gulfstream II | |
Variants | Gulfstream IIB |
[Photo-ID: 11060] © Karsten Palt 2015-06-03 | |
Gulfstream Aerospace Gulfstream II NASA Reg.: N948NA c/n: 222 | |
Pima Air and Space Museum [Tucson, AZ] |