| General Data | |||
| First Flown: | 1965 | Length: | |
| Lift Capability: | Height: | ||
| Range: | Rotor Span: | ||
| Top Speed: | Empty Weight: | ||
| Service Ceiling: | Max Gross Weight: | ||
| Engines: | 2 General electric T700-GE-700 turboshafts rated at 1,500 shp | ||
| Armament: | |||
| Accommodations: | 14 seats | Cargo: | |
| Operators: | |||
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| Similar Aircraft: | |||
| Other Features: | 4 blades on tail and main rotors | ||
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| Notes | |||
| This helicopter was never built but was a prototype submitted by Bell for the Utility Tactical Transport Aircraft System (UTTAS) competition in 1965. It was designed as a replacement to the UH-1. Boeing and Sikorsky won this competition. | |||