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Description
| Notes: Af version of UH-1E with modified tail boom and skid landing gear. Logistics support to sac icbm units (1 CREW, 10 PASSENGERS) . | ||
| Manufacturer: | Bell | |
| Base model: | H-1 | |
| Designation: | UH-1 | |
| Version: | F | |
| Nickname: | Iroquois | |
| Designation System: | U.S. Tri-Service | |
| Designation Period: | 1962-Present | |
| Basic role: | Helicopter | |
| Modified Mission: | Utility | |
| First Flew: | 1964/02/20 | |
| Serial/Bureau Number: | 66-1215 | |
| Location: | Minot AFB, Minot AFB North Dakota | |
Specifications
| Length: | 41' 5" | 12.6 m | |
| Height: | 12' 6" | 3.8 m | |
| Wingspan: | 48' | 14.6 m | |
| Empty Weight: | 4,430 lb | 2,009 kg | |
| Gross Weight: | 9,000 lb | 4,081 kg | |
| Max Weight: | 9,500 lb | 4,308 kg | |
Propulsion
| No. of Engines: | 1 | ||
| Powerplant: | General Electric T58-GE-3 | ||
| Horsepower (each): | 1272 | ||
Performance
| Range: | 347 miles | 558 km | |
| Cruise Speed: | 123 mph | 198 km/h | 107 kt |
| Max Speed: | 138 mph | 222 km/h | 120 kt |
| Climb: | 2,123 ft/min | 647 m/min | |
| Ceiling: | 22,000 ft | 6,705 m | |