Type 3-seat sportplane and trainer
Engine 1 De Havilland Gipsy Six I
Dimensions Length 7,62 m , height 1,98 m ,  span 10,67 m , wing area   ,
Weights Empty 590 kg, loaded 998 kg  
Performance Max.233 km/h. speed  , cruising speed 200 km/h , range 990 km, endurance  , service ceiling 4600 m  , climb
Type Werk.Nr Registration History
M.3B 256 D-EGYV, G-AFBF, AV973 Registered in Germany November 1935 to K.T. Rochling at Aachen. Sold to UK in october 1937
The M.3 Falcon was a clean, single engined low-wing monoplane with trousered main undercarriage and fixed tail-wheel, designed in 1934. It was structurally similar to the earlier Miles M.2F Hawk Major family, but had side-by-side seating for two behind the pilot in a glazed cockpit. It was powered by a 130 hp (97 kW) de Havilland Gipsy Major piston engine. The prototype, G-ACTM, built by Philips and Powis first flew at Woodley Aerodrome on 12 October 1934.

The first production aircraft (designated M.3A Falcon Major) was flown in January 1935. It had a wider fuselage than the prototype to improve passenger comfort and revised glazing with a forward sloping windscreen. The M.3A was somewhat underpowered, so the (M.3B Falcon Six) and later versions were fitted with a 200 hp (150 kW) de Havilland Gipsy Six engine.