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Miles M.28


The Miles M28 was designed to fulfill two major functions, a two seater ab-initio/intermediate trainer and a three seat communications aircraft.

It was designed to be powered by either a Cirrus Major 150 HP engine or a Gypsy Major IIA with fixed pitch propeller or a Gypsy Major III with a constant speed propeller. With Miles low drag flaps and drooping ailerons as well as a fuselage air brake, landing speeds were as low as 40 miles per hour. The prototype had an R.A.F. Service Number of U-0232

Engine: Gypsy Major III
Top speed: 176 mph
Span: 30 ft 6 in
Length: 22 ft 1.5 in
Height: 8 ft 6 in
Wing area: 160 sq. ft

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