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Cranfield A1


General information


ManufacturerCranfield
ModelA1
ModificationA1
CountryUnited Kingdom
Years1976
TypeLight aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan10.00 m
Length8.05 m
Height-
Wing area15.00 m2
Zero fuel weight-
Empty weight-
Maximum takeoff weight850 kg
Normal takeoff weight-
Flight duration-
Engine1 Avco Lycoming IO-540-D
Power1 x 250 HP
Thrust-
Maximum speed-
Cruising speed240 km/h
Rate of climb-
Practical range-
Service ceiling8858 m
Hovering ceiling-
Crew1
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