The AVRO 626 is a single-engine two-or three-seat trainer biplane aircraft produced by the British manufacturer AVRO, A.V. Roe and Company.
| Crew | 2 / 3 | |
| Propulsion | 1 Radial Engine | |
| Engine Model | Armstrong Siddeley Lynx IVC | |
| Engine Power | 179 kW | 240hp |
| Speed | 180 km/h | 97kts |
| Service Ceiling | 4.511 m | 14.800ft |
| Range | 385 km | 208 NM |
| Empty Weight | 801 kg | 1.766lbs |
| max. Takeoff Weight | 1.247 kg | 2.749lbs |
| Wing Span | 10,36 m | 34,0ft |
| Wing Area | 27,9 m² | 300 ft² |
| Length | 8,08 m | 26,5ft |
| Height | 2,92 m | 9,6ft |
| First Flight | 1930 | |
| Production Status | out of production | |
| Total Production | ca. 200 | |
| Developed from | AVRO 621 Tutor | |
| Data for (Version) | AVRO 626 | |
| Variants | AVRO 637, Tatra T-126 |
Remarks
The AVRO 626 is a development of the AVRO 621 Tutor
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