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       Cessna A-37B Dragonfly
 In the first part of the 1950s Cessna 
      went in for military production, designing the first jet trainer for the 
      USAF, the T-37. From this machine (of which 1,268 models of three basic 
      versions were built between 1955 and 1977), an efficient attack plane was 
      derived in 1963, the A-37, which was also successfully exported. The 
      prototype flew on October 22 and the first 39 A-37As were produced by 
      direct conversion of other T-37Bs. The definitive version was the A-37B, 
      which first appeared in September 1967 and of which 577 were built with 
      the majority of these going to the USAF. One of the few aircraft designed from 
      the start for tactical support, the A-37 arrived in Vietnam toward the end 
      of the 1960s and was mainly used in support of helicopter operations. 
      Capable of mounting a wide range of weapons, it proved highly adaptable to 
      diverse operational needs. Particularly effective were its low-level 
      napalm bomb attacks. A fairly limited number of machines, under the 
      colours 
      of both the USAF and the VNAF (the illustration shows the VNAF insignia), 
      were used in action. US Army During the late 1950s the Army Aviation 
      Test Board and the Aviation Combat Developments Agency (ACDA) began to 
      jointly explore the feasibility of using Army-operated fixed-wing jet 
      aircraft in the artillery adjustment, tactical reconnaissance, and ground 
      attack roles. Operational necessity dictated that any such aircraft be 
      easy to maintain under field conditions and capable of operating from 
      unimproved forward air strips, and these prerequisites indicated that any 
      jet procured for Army use would have to be simple and relatively small, 
      yet at the same time be of robust construction and able to offer a 
      performance significantly better than that of the various piston-engined 
      machines then in Army service. Cessna's diminutive T-37 twin-engined 
      primary trainer admirably fulfilled all these requirements, and in early 
      1958 three examples borrowed from the Air Force were sent to Fort Rucker 
      to begin a one year Army evaluation programme dubbed Project LONG ARM. 
      
       US Army T-37
 The Cessna Model 318 had been adopted by 
      the Air Force as the T-37 after winning a 1953 USAF-sponsored design 
      competition for a new primary jet trainer. The first of two prototype 
      XT-37s had made its maiden flight in early 1954, and the first eleven 
      production T-37As had entered USAF service in 1955. The three aircraft 
      evaluated by the Army were all -A model machines of the fourth production 
      batch, and carried the serial numbers 56-3464 to -3466. The T-37, widely 
      if unofficially known as the 'Tweetybird', was characterized by low-set, 
      non-swept wings, side-by-side crew seats, and a broad forward fuselage. 
      The type was equipped with ejection seats for both crewmen, and its 
      cockpit instruments and controls were identical to those found in 
      frontline USAF aircraft. The T-37A was powered by two Continental J69 
      turbojets, one buried in each wing root, and was quite manoeuvrable and 
      relatively easy to fly. The Army's evaluation of the T-37 found 
      the aircraft to be ideally suited for Army use and both the Aviation Board 
      and the ACDA recommended quantity procurement of the type. However, 
      mounting Air Force opposition to Army ownership and operation of 
      fixed-wing jet aircraft eventually forced the Army to abandon the planned 
      T-37 acquisition and all three machines used in the Project LONG ARM tests 
      were returned to the Air Force in early 1959. 
       
      
         
      
         
      
       Technical Specifications Aircraft: 
      Cessna A-37BYear: 1967
 Type: attack
 Manufacturer: Cessna Aircraft Co.
 Engine: 2 x General Electric J85-CE-17A
 Power: 2,850 lb (1,293kg)
 Wingspan: 35ft 10½ in (10.93m)
 Length: 29ft 3in (8.92m)
 Height: 8ft 10½ in (2.70m)
 Wing area: 183.9sq ft (17.09m²)
 Max take-off weight: 15,000 lb (6,804kg)
 Empty weight: 5,873 lb (2,670kg)
 Max speed: 478mph at 15,000ft (769km/h at 4,572m)
 Service ceiling: 32,100ft (9,785m)
 Range: 450mi (724km)
 Crew: 2
 Load-armament: 1x7.62mm minigun; 5,4001b (2,450kg)
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