| 
       Antonov An-72A Coaler
 
       
       The An-72 (NATO came 
      'Coaler') was designed as a replacement for the An-26 tactical transport 
      in Soviet service. The first of two An-72 
      prototypes flew for the first time on December 22 1977, although it was 
      not until 1985 that the first of eight extensively revised pre production 
      An-72s flew. Included in this pre production batch were two An-74s, 
      differing from the An-72s in their ability to operate in harsh weather 
      conditions in polar regions because of an improved avionics suite. Transport versions of the 
      An-72 family include the An-72A base model with extended wings and 
      fuselage compared to the prototypes, the An-72AT which can carry 
      international standard containers, and the An-72S VlP transport. Versions 
      of the An-74 include the base An-74A with enlarged nose radome, the An-74T 
      freighter, the An-74TK convertible passenger/freighter model, and the 
      An-74P Salon VIP transport. A prototype AEW An-71 ('Madcap') has also 
      flown. The An-72P maritime patrol 
      aircraft meanwhile is based on the basic An-72 fuselage with a 23mm gun, 
      rocket pods, four light bombs carried internally, day and night downward 
      looking and oblique optical cameras and an optical TV sight. ln service 
      with Ukraine, the An-72P is designed for close-in coastal surveillance. 
      Antonov is now offering an improved development of the An-72P in 
      conjunction with Israel Aircraft Industries. Changes include a glass 
      cockpit, Elta EUM 2022A radar, Electro Optical day and night long range 
      observation system and Elisra electronic warfare suite. The most significant 
      design feature of the An-72 and An-74 is the use of engine exhaust gases 
      blown over the wing's upper surface to improve STOL performance and lift." 
        
          | Origin: | Ukraine |  
          | Type: | STOL transport |  
          | Max Speed: | 705 km/h / 438 
          mph |  
          | Max Range | 800 km / 497 
          miles |  
          | Dimensions: | span 31.89 m 
          (104ft 7.5 in) length 28.07 m (92 ft 1.1 in)
 height 8.65 m (28ft 4.5in)
 |  
          | Weight: | empty 19050 kg 
          (41,997 Ib); maximum take-off 34500 kg (76,059 Ib) |  
          | Powerplant: | two 6500-kg 
          (14,330-lb) dry thrust Zaporozhye/Lota rev D-36 turbofans |  
          | Armament: | none |  |