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         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  | 
           
          
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
         
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