De Havilland Fox Moth:
Specifications:
General characteristicsCrew: 1
Capacity: 3-4
Length: 25 ft 9 in (7.85 m)
Wingspan: 30 ft 10+5⁄8 in (9.41 m)
Height: 8 ft 9+1⁄2 in (2.68 m)
Wing area: 261.5 sq ft (24.29 m2)
Airfoil: RAF 15[9]
Empty weight: 1,071 lb (486 kg)
Max takeoff weight: 2,000 lb (907 kg)
Powerplant: 1 × de Havilland Gipsy III 4-cylinder air-cooled inveted in-line piston engine, 120 hp (89 kW)
Propellers: 2-bladed fixed-pitch propeller
Performance:Maximum speed: 106 mph (171 km/h, 92 kn)
Cruise speed: 91 mph (146 km/h, 79 kn)
Range: 425 mi (684 km, 369 nmi)
Service ceiling: 12,700 ft (3,900 m)
Rate of climb: 450 ft/min (2.3 m/s)
Variants:
DH.83 Fox Moth: Light transport biplane; 98 built in the United Kingdom, plus two more in each of Australia and Canada.
DH.83C Fox Moth: 53 aircraft were built in Canada after World War II.
Gasuden KR-1: This was an unlicensed Japanese-built copy of the Fox Moth powered by a 150 hp (112 kW) Gasuden Jimpu 3 radial engine. The first prototype, J-BBJI named Chidorigo (Plover) flew on 23 December 1933. Seven KR-1s were built.[4]
Gasuden KR-2: The KR-1 design with modified wings and other tweaks