Twin-turboprop airliner/executive transport plane, developed in the late 1950's. 200 were built between 1959 and 1969, with civilian and military operators in Canada, Denmark, the Democratic Republic of Congo, France, Gabon, Greece, Israel, Kenya, Spain, Sweden, the UK, and the US.
https://en.wikipedia.org/wiki/Grumman_Gulfstream_I
GENERAL STATS
Crew: 2
Capacity: 24 passengers
Length: 63 feet 9 inches (19.43 meters)
Wingspan: 78 feet 6 inches (23.93 meters)
Height: 22 feet 9 inches (6.93 meters)
Wing area: 610.3 square feet (56.70 meters squared)
Max takeoff weight: 35,100 pounds (15,921 kilograms)
Max landing weight: 33,600 pounds (15,241 kilograms)
Fuel capacity: 1,550 US gallons (1,290.6 imperial gallons, 5,867.4 liters)
Powerplant: x2 Rolls Royce RB.53 Dart Mk.529 turboprop engines, 2,190 SHP per engine
Max speed: 362 MPH (583 KMH, 315 knots)
Approach speed: 128 MPH, 206 KMH, 111 knots)
Range: 2,540 miles (4,090 kilometers, 2,210 nautical miles)
Service ceiling: 33,600 feet (10,200 meters)
#Grumman G-159 Gulfstream I
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