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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