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Fleet

Antonov AN-12

The AN-12 (Cub) was designed in the late 1950s and is essentially similar to the C-130 Hercules. Production started in 1957 and continued until 1973 after over 1,400 were built. Although lighter and smaller than the civil L100-30 Hercules, the AN-12 is just as versatile and capable, offering a 20 ton payload, 3,000 km range and an ability to operate from gravel strips. The aircraft has a rear loading ramp and on-board gantry crane to assist loading of oversize, bulk cargo.

Wing span 124 ft 727 in 38.015 m

Length 108 ft 634 in 33.11 m

Height 37 ft 535 in 11.44 m

Empty weight 81 571 lb 37 000 kg

Max take-off weight 134 482 lb 61 000 kg

Max landing weight 127 868 lb 58 000 kg

Powerplant Ivchenko AI-20M turboprops 4 x 4 250
ehp
4 x 3 169
kWatt

Structural payload 44 092 lb 20 000 kg

Structural volume 96,7 cub.m 96,7 cub.m

Min runway required 5 906 ft 1 800 m

Average cruise speed 297 knots 550 km/h

Fuel capacity (density 0.8) 27 500 L
48 502 lb
7265 usg
22 000 kg

Average fuel consumption 793 usg/h 2 400 kg/h
 

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