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Fleet

Antonov AN-26

Derived from the AN-24 passenger transport, the AN-26 (Curl) was developed in the late 1960s. The type entered civilian service with Aeroflot in 1970. Approximately 1,410 were built, many for military use. The type was also a major export success and remains in service around the world. The AN-26 has a unique feature, a rear loading ramp which can be rolled forward under the fuselage to allow for vehicles to reserve up to the cargo bay. The AN-26 has an Auxiliary Power Unit (APU) fixed to the starboard engine nacelle that serves as a turbojet booster on take-off.

Wing span 95 ft 805 in 29.2 m

Length 78 ft 0,87 in 23.8 m

Height 28 ft 216 in 8.6 m

Empty weight 35 935 lb 16 300 kg

Max take-off weight 52 911 lb 24 000 kg

Max landing weight 52 911 lb 24 000 kg

Powerplant Ivchenko AI-24WT turboprops 2 x 2 780
ehp
2 x 2 073
kWatt

Structural payload 12 125 lb 5 500 kg

Structural volume 30 cub.m 30 cub.m

Min runway required 4 265 ft 1 300 m

Average cruise speed 227 knots 420 km/h

Fuel capacity (density 0.8) 6 875 L
12 125 lb
1 816 usg
5 500 kg

Average fuel consumption 297 usg/h 900 kg/h

 

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