Grumman / Gulfstream Gulfstream I (Grumman G-159)
Corporate Aircraft
The Grumman G-159 Gulfstream I is a twin-engined turboprop corporate aircraft produced by the US-American manufacturer Grumman Aircraft Engineering Corporation.
The version G-159C Gulfstream I-C was a stretched regional airliner variant.
Crew | 2 | |
Passengers | 24 (I-C= 37) |
Propulsion | 2 Turboprop Engines | |
Engine Model | Rolls-Royce Dart Mk.529-8X | |
Engine Power (each) | 1491 kW | 2000 shp |
Speed | 537 km/h | 290 kts 334 mph |
Service Ceiling | 9.144 m | 30.000 ft |
Range | 806 km | 435 NM 501 mi. |
Empty Weight | 10.747 kg | 23.693 lbs |
max. Takeoff Weight | 16.329 kg | 36.000 lbs |
Wing Span | 23,88 m | 78 ft 4 in |
Wing Area | 56,7 m² | 610 ft² |
Length | 22,96 m | 75 ft 4 in |
Height | 7,01 m | 22 ft 12 in |
First Flight | 14.08.1958 | |
Production Status | out of production | |
Production Range | 1959-1969 | |
Total Production | 211 |
ICAO Code | G159 | |
IATA Code | GRS | |
Data for (Version) | Gulfstream I-C |
[Photo-ID: 11385] © Karsten Palt 2015-06-01 | |
Grumman TC-4C Academe (G-159) United States Navy Reg.: 155724 c/n: 180 retired 1992, Celebrity Row | |
AMARG - Boneyard [Tucson, AZ] |