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Grumman Gulfstream II
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| Gulfstream II | |
|---|---|
| A USCG Gulfstream II, 1969 | |
| Type | Business jet |
| Manufacturer | Grumman/Gulfstream Aerospace |
| Developed from | Grumman Gulfstream I |
| Variants | Gulfstream III |
The Gulfstream II is a large twin engine business jet built by Gulfstream Aerospace, and its US military designation is C-11 Gulfstream II. It has been succeeded by the C-20 Gulfstream III.
Military Operators
Specifications
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.- Length: 79.11 ft (24.1 m)
- Height: 24.6 ft (7.5 m)
- Wing span: 77.1 ft (23.5 m)
- Crew: 2
- Passenger: 19 maximum, 12 normal
- Speed: 459 mph
- Ceiling: 45,000 ft
- Cruise altitude: 39,000 ft
- Rate of climb: 4,350 ft/min
- Max weight: 65,000 lb (29,545 kg)
- Max payload: 5,456 lb (2,480 kg)
- Engine: Two Rolls-Royce Spey 511-8 @ 11,400 lb (5181 kg) each
Related content
Related development
Designation sequence
Related lists
Template:Active military aircraft of the United States
Gulfstream aircraft
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