The AVRO 621 Tutor 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 Lynx IVc | |
| Engine Power | 179 kW | 240hp |
| max. Cruise Speed | 169 km/h | 91kts |
| Speed | 196 km/h | 106kts |
| Service Ceiling | 4.938 m | 16.200 ft |
| Range | 402 km | 217 NM |
| Empty Weight | 839 kg | 1.850lbs |
| max. Takeoff Weight | 1.115 kg | 2.458lbs |
| Wing Span | 10,36 m | 34,0ft |
| Wing Area | 28,0 m² | 301ft² |
| Length | 8,08 m | 26,5ft |
| Height | 2,92 m | 9,6ft |
| First Flight | 26.06.1926 | |
| Production Status | out of production | |
| Total Production | 795 | |
| ICAO Code | TUTR | |
| Data for (Version) | AVRO 621 Tutor | |
| Variants | AVRO Sea Tutor, 621 Tutor II, P.W.S.18 |
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