General Aircraft Cagnet

The General Aircraft GAL.33 Cagnet was a British light trainer aircraft designed by General Aircraft Ltd which flew from 1939 to 1941. Only one example was constructed.

GAL.33 Cagnet
Role Trainer
Manufacturer General Aircraft Ltd
First flight 1939
Number built 1

Design

The Cagnet was a two-seat pusher propeller aircraft. The side-by-side seating was in an open cockpit just ahead of the strut-mounted inline engine. The low cantilever wings featured a gull shape, with twin booms mounted, one at each wing's bend point. A horizontal stabilizer and elevator ran between twin fins with rudders, one at the end of each boom.

The fixed landing gear used a nosewheel. First flight was in 1939; the aircraft bore the serial number T46.

General Aircraft proposed the Cagnet as a basic trainer. It was tested as a Flying Observation post trainer by the Royal School of Army Co-operation from February through June 1940 (with military serial number W7646). After that testing, it underwent various other tests. Its final flight was in 1941.

The engine was a 90 hp (67 kW) Blackburn Cirrus Minor, which gave a cruising speed of 100 mph (160 km/h).

Specifications (Cagnet)

General characteristics

  • Crew: 2
  • Length: 22 ft 9 in (6.93 m)
  • Wingspan: 33 ft 0 in (10.06 m)
  • Gross weight: 2,976 lb (1,350 kg)
  • Powerplant: 1 × Blackburn Cirrus Minor 4-cyl. inverted air-cooled in-line piston engine, 90 hp (67 kW)

Performance

  • Maximum speed: 100 mph (160 km/h, 87 kn)
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References
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