Two-seat training biplane powered by an Armstrong Siddeley Mongoose III radial engine. Small number built for the RAF, for civil registration and for export to Canada and New Zealand.
|A three-view drawing (1280 x 1046)|
| ENGINE||1 x Armtrong Siddeley Mongoose IIIC, 112kW|
| Take-off weight||794 kg||1750 lb|
| Empty weight||499 kg||1100 lb|
| Wingspan||8.71 m||29 ft 7 in|
| Length||7.21 m||24 ft 8 in|
| Height||2.54 m||8 ft 4 in|
| Wing area||22.09 m2||237.77 sq ft|
| Max. speed||200 km/h||124 mph|
| Ceiling||5945 m||19500 ft|
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