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      Percival Provost T1 performance and specifications 
            
            
                                    
                                      
            
                                    
                                    Designed by 
                                    Percival Aircraft before it became part of 
                                    the Hunting Group in 1954. A cantilever 
                                    low-wing monoplane with fixed tailwheel 
                                    landing gear and powered by an Alvis 
                                    Leonides 126 engine, it provided 
                                    side-by-side seating for instructor and 
                                    pupil. Three prototypes were built, two 
                                    powered initially by the Armstrong Siddeley 
                                    Cheetah I8, the other Cheetah-engined 
                                    prototype flying on the 24th by an Alvis 
                                    Leonides, the first February  
                                    
                                    
                                    Adopted as the 
                                    RAF's basic trainer in 1953 superseding the 
                                    Percival Prentice in Flying Training 
                                    Command, the Provost remained in service in 
                                    that role until replaced by a development of 
                                    the design, the Jet Provost, in 1961. 
                                     
                                    The Provost was selected for production 
                                    following competitive trials with the 
                                    Handley Page HPR2. The first flight took 
                                    place on 24 February 1950. 
                                    Of the 15 
                                    companies involved in the fierce competition 
                                    for design approval, Percival led the pack 
                                    because it had privately developed a mockup 
                                    trainer that anticipated many of the RAF's 
                                    requirements. Called the P.56, 
                                    the Percival entry also had the edge because 
                                    their early start made them the only firm 
                                    able to meet the time limits specified by 
                                    the RAF for delivery of a prototype. Thus, 
                                    an initial order for 200 of the aircraft was 
                                    placed with Percival in May, 1951. 
                                     
                                    First production deliveries were made to the 
                                    Central Flying School. The first Flying 
                                    Training School (FTS) to be so equipped was 
                                    No.6 FTS at Ternhill in October 1953. Other 
                                    FTSs equipped were at Syerston, Hullavington, 
                                    Feltwell and Worksop. 
                                     
                                    The Provost proved to be a popular machine 
                                    with good aerobatic qualities and 397 
                                    aircraft were delivered to the RAF. 
                                     
                                    The Provost was the last piston engined 
                                    basic trainer to be used by the RAF. The 
                                    last training unit re-equipped with a 
                                    jet-powered version of the design, called 
                                    the Jet Provost, in August 1961 but a few 
                                    Provosts lingered on until the last one was 
                                    retired in November 1969. 
                                    
                                    Specifications: 
                                    
                                            
                                    Engine: One 550-hp Alvis Leonides 126 radial 
                                    piston engine 
                                            
                                    Weight: Empty 3,350 lbs., Max Takeoff 4,400 
                                    lbs. 
                                            
                                    Wing Span: 35ft. 2in. 
                                            
                                    Length: 28ft. 8in. 
                                            
                                    Height: 12ft. 2.5in. 
                                            
                                    Performance: 
                                                
                                    Maximum Speed: 200 mph 
                                                
                                    Ceiling: 22,500 ft. 
                                                
                                    Range: 648 miles 
                                            
                                    Armament: None 
                                    
                                    Number Built: 
                                    461 
                                    
                                    Number Still Airworthy: 
                                    Approximately 5 
        
                                    
            
            
                                     
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