GRUMMAN AMERICAN GULFSTREAM II/ III / IV/V
1967’ Present
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| STANDARD DATA: (II) Seats 19. Gross wt. 62,000. Empty wt. 29,000. Fuel capacity 3,478. Engines two 11,440-lb. s.t. Rolls-Royce Spey turbofans. PERFORMANCE: Top mph 588. Cruise mph 526. Stall mph 116. Initial climb rate 4,350. Range 3,886. Ceiling 43,000. Takeoff run 5,000. Landing roll 3,190. |
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| STANDARD DATA: (III) Seats 19. Gross wt. 68,200. Empty wt. 38,300. Fuel capacity 4,400. Engines two 11,400-lb. s.t. Rolls-Royce Spey turbofans. PERFORMANCE: Top speed Mach 0.85. Cruise speed Mach 0.77. Stall mph 121. Ceiling 45,000. Range 4,330. Takeoff run 5,850. Landing roll 3,400. |
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| STANDARD DATA: (IV) Seats 14-24. Gross wt. 70,200. Empty wt. 33,400. Fuel capacity 4,340. Engines two 12,420-lb. s.t. Rolls-Royce Tay turbofans. PERFORMANCE: Top mph 564. Economy cruise mph 528. Stall mph 121. Ceiling 45,000. Range 4,952. Takeoff run 5,100. Landing roll 3,200. STANDARD DATA: (V) Seats 14-24. Gross wt. 70,200. Empty wt. 33,400. Fuel capacity 4,340. Engines two 12,420-lb. s.t. Rolls-Royce Tay turbofans. |
The Grumman Gulfstream II was originally designed as a business jet, but an enlarged version would eventually serve in feeder airline use. This aircraft evolved from the Gulfstream I turboprop, which was introduced in 1958. Production of the swept-wing Model II version with turbofan engines started in 1965, and the first delivery was in 1967. It is one of the larger business jets, with a gross weight of 58,000 pounds. It is also one of the fastest, with a top speed of 589 mph, and it has a long-range capability of up to 3,600 miles.
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