Design and Development
The Magister was designed to meet Air Ministry Specification T.40/36P and first flew in March 1937. The design was based on an open-cockpit, low wing cantilever monoplane of spruce structure covered in plywood. The wing centre section has no dihedral and is of constant section with outer sections having dihedral and tapering towards the tip. Split flaps were fitted as standard. The initial M.14 was followed by the definitive Miles M.14A Magister I with a taller rudder and, eventually, anti-spin strakes on rear fuselage.
Notwithstanding the relatively large number built, contemporary glues used to assemble the wooden aircraft have not stood the test of time and seemingly only one remains airworthy on the British register in 2007 with a few others designated Hawk Trainers.
Read more about this topic: Miles Magister
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