Antonov An-12
1957
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Antonov An-12

Prototype (7900101), built at Irkutsk, flew 16 December 1957, with Kuznetsov NK-4 turboprops, as rear-loading development of An-10 airliner; more than 900 built with AI-20K engines for military and civil use, ending in USSR in 1973; An-12BP ("Cub") was standard medium-range paratroop and cargo transport of Soviet Military Transport Aviation (VTA) from 1959; replacement with Il-76 began 1974, but about 170 remain in air force service, plus at least 25 An-12BK/PP/PPS "Cub-A/B/C/D" electronic warfare conversions in air forces and Naval Aviation. More than 100 (of 183 originally exported) are used by nine other air forces; further 190 flown by some 70 freight airlines. Shaanxi Aircraft Company, China, manufactures redesigned Yunshuji-8 (Y-8) transport version and derivatives.

Antonov An-12


Specification 
 CREW6
 PASSENGERS130
 ENGINE4 x turbo-prop AI-20, 3125 kW
 WEIGHTS
    Take-off weight54000-61000 kg119050 - 134483 lb
    Empty weight30500 kg67241 lb
 DIMENSIONS
    Wingspan38.0 m124 ft 8 in
    Length37.0 m121 ft 5 in
    Height9.8 m32 ft 2 in
    Wing area121.7 m21309.97 sq ft
 PERFORMANCE
    Max. speed640 km/h398 mph
    Cruise speed600 km/h373 mph
    Ceiling10000 m32800 ft
    Range5500 km3418 miles
 ARMAMENT2 x 23mm machine-guns

Antonov An-12

Comments 
hernowo, hernowo_st(@)yahoo.com, 27.11.2008

i need to know about :
1. runway length requirement in ARFL condition?
2. main landing gear dimension?
I need it to design the airside.
thank you

vic sulit, vic(@)saharaaviation.com, 11.10.2008

Please provide me the basic operating cost of AN12, like how much do we need to allot for maintenance (schedule and unchedule)per flying hour. also kindly include the estimated cost for pilot and crew training (transition and recurrency)

Nabil Alaeddin, alaeddin_nabil(@)msn.com, 14.06.2007

I need to know about the specification or requirements of ( Tie-downs or they call it Mooring points)
Tank you

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