|
Plans for the Falconar F-9A through F-12 series of
homebuilt aircraft were prepared by Mr. C. Falconar who founded the
first Canadian EAA chapter in Edmonton in the 1950’s. The F-10A is a
stronger version of the F-9A with a maximum take-off weight of
875lb(397kg) These aircraft are modified versions of the Jodel D.9 and
D.11.
Unregistered
Canada
Single seat ultralight first flown in 1965
Engine: 60hp(44kW) VW
Length: 17’11"(5.45m)
Height: 5’6"(1.67m)Wingspan: 23’6"(7.15m)
No.built: 20+ Range: 420miles(674km)
Cruising speed: 80mph(128kmh) Empty weight: 360lb(163kg)
Maximum take-off weight: 600lb(272kg)
|
AircraftWorldDirectory.com