Sud-Ouest SO.1310 Farfadet ![]()
In the forepart there is a Turbomeca Artouste II turbo-prop engine with a take-off power of 360 hp, operating a variable-pitch airscrew. During forward flight, the rotor originally used for take-off continues to auto-rotate, but with low lift, and the greater part of the lift is transferred to the fixed wing. Mounted over the fixed wing is the pilot's cabin, fitted with dual control, and in this cabin there is room for either three passengers, a freight load or two stretchers stacked on top of each other.
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SO.1310 Farfadet
Engine: 1 x 360 hp Turbomeca Artouste II gas turbine & 1 x 360 hp Turbomeca Arrius II gas turbine
Rotors: 3-blade tip-powered main rotor; 2-blade propeller
Rotor diameter: 11.2m / 36 ft 6 in
Wingspan: 6.3m / 19 ft
Fuselage length: 10.08m
Height: 3.3m
Weight fully loaded: 1510kg
Empty weight: 995kg
Cruising speed as a helicopter: 155km/h
Cruising speed as an autogyro: 250km/h
Range: 400km / 250 miles at 149 mph
Seats: 3
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