The AVRO 631 / 643 Cadet is a single-engine two-seat trainer biplane aircraft produced by the British manufacturer AVRO, A.V. Roe and Company.
Crew | 2 | |
Propulsion | 1 Radial Engine | |
Engine Model | Armstrong Siddeley Gent Major 1A | |
Engine Power | 112 kW | 150hp |
max. Cruise Speed | 161 km/h | 87kts |
max. Speed (vne) | 187 km/h | 101kts |
Service Ceiling | 3.658 m | 12.000 ft |
Range | 522 km | 282 NM |
Empty Weight | 583 kg | 1.285lbs |
max. Takeoff Weight | 907 kg | 2.000lbs |
Wing Span | 9,19 m | 30,2ft |
Wing Area | 24,3 m² | 262ft² |
Length | 7,54 m | 24,7ft |
Height | 2,69 m | 8,8ft |
First Flight | 10/1931 | |
Production Status | out of production | |
Total Production | 105 | |
Developed from | AVRO 621 Tutor | |
Data for (Version) | AVRO 643 Cadet | |
Variants | AVRO 631 Cadet, 643 Cadet |
Remarks
The AVRO 631 is a development of the AVRO 621 Tutor.
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