Following the success of the civil Miles Hawk Trainer, the Air Ministry
drew up Specification T.40/36 for a development of the Hawk as an
elementary trainer for the RAF. Design changes included the provision
of larger cockpits and blind-flying equipment, production of the Miles
M.14 Magister starting in early 1937 to the revised Specification
T.37/37. Initial deliveries to the RAF were made in May 1937, these
being the first low-wing monoplane trainers used in the history of the
Royal Air Force. Also, it was also a radical departure from the
declared policy of the Air Ministry that all future Service aircraft
were to be of metal construction.
The Magister was, in addition, the first R.A.F. aeroplane in which
magnesium alloy castings were used for stressed parts, and the first
low-wing cantilever monoplane with full Air Ministry approval for
acrobatic flying, including protracted spins. The Magister's spinning
problem was soon rectified and modified aircraft and subsequent
production aircraft had the designation M.14A.
At the time of the Magister's introduction, the first deliveries of
Hurricanes and Spitfires were being made, and the new trainer, with its
low-wing monoplane characteristics and split trailing-edge flaps,
reproduced the handlings qualities of these types in a safe manner.
Built from 1937 to 1941, the total construction by Miles amounted to
1,293, and an additional 100 were built under licence in Turkey
following the evaluation of four received from Miles. RAF contracts
covered 1,229 aircraft, and other countries acquiring Magisters for
military use included Eire (15), Egypt (42) and New Zealand (2). In
addition, a number were supplied to civil customers, and after the end
of World War 2 many ex RAF Magisters came on to the civil market under
the designation Hawk Trainer III. At the peak of
RAF use Magisters equipped 16 Elementary Flying Training Schools and
the Central Flying School, and were in use with the RAF commands, the
last being retired in 1948; in addition, they saw service with the
British army and the Fleet Air Arm.
Design Company: |
Phillips & Powis Aircraft
Ltd |
First Flight: |
Early 1937 |
M.14 Magister: |
1293 - Phillips & Powis,
Woodley
100 - Turkey |
Type
Specification |
Applies to: |
Miles M.14A Magister I |
Type: |
Elementary trainer for RAF
to specification T.40/36 developed from Hawk Trainer |
Wing: |
Low wing cantilever
monoplane of spruce structure covered in plywood. Centre section has
no dihedral and is of constant section, outer sections have dihedral
and taper towards the tip. Split flaps fitted as standard
|
Fuselage: |
Fuselage of spruce
structure with plywood covering |
Tail Unit: |
Cantilever tailplane with
elevator at top of fuselage with single fin and rudder |
Landing Gear: |
Fixed main wheels beneath
wing. Tail wheel |
Power Plant: |
One 130 hp de Havilland
Gipsy Major in nose |
Accommodation: |
Seats for two in tandem
open cockpits above the wing |
Dimensions |
Span: |
33 ft 10 in |
Length: |
24 ft 7 in |
Height: |
6 ft 8 in |
Wing Area: |
176 sq ft |
Weights |
Empty: |
1,286 lb |
All-up: |
1,900 lb |
Performance |
Max Speed: |
140 mph at sea level |
Initial Rate of Climb: |
750 ft/min |
Service Ceiling: |
16,500 ft |
Range: |
367 miles |
|