(Showcased structural values pertain to the base Avro 621 Tutor production variant)
1 x Armstrong Siddeley Lynx IVC air-cooled radial piston engine developing 240 horsepower driving two-bladed propeller at the nose.
(193 kph | 104 kts)
(4,877 m | 3 mi)
(402 km | 745 nm)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
(Showcased performance specifications pertain to the base Avro 621 Tutor production variant. Compare this aircraft entry against any other in our database)
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