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Bell D292 ACAP

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General Data
Notes
First Flown
1985

This was a demonstration aircraft for the the Advanced composite Airframe Programme. the goal of which was the development of an al composite helicopter fuselage that would be lighter and cheaper to produce.
Length
Height
Rotor Span
Lift Capability
Range
Top Speed
Empty Weight
Max Gross Weight
Service Ceiling
Armament
Engines
2 Avco Lycoming LTS 101-750C-1 turboshafts rated at 510 shp
Accommodations
Cargo
Operators
Similar Aircraft
Bell 222
Other Features
none

Bell D292 ACAP

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