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AN-140-100 Specifications

Maximum takeoff weight 36500 kg
Maximum payload 10000 kg
Maximum speed 700 km/h
Operating ceiling 10100 m
Crew 2 pilots
Wingspan 31.890
Length 28.068 m
Height 8.650 m
Wing area 98.620 . m
Fuselage diameter 3.100 m
Wheel track 4.094 m
Wheel base 8.670 m
Takeoff power (H=0, M=0):
      - Thrust, kgf (kN)6,500 (63,7)
      - Specific fuel consumption, kg/kgf*h 0,358
- Maximum continuous power (H=0, M=0):
      - Thrust, kgf (kN) 5,000 (49)
- Maximum cruising power (H=8,000 m, M=0.75):
      - Thrust, kgf (kN) 1,600 (16,0)
      - Specific fuel consumption, kg/kgf*h0,602
Critical altitude 11,000 m
Engine starting critical altitude::
      on the ground up to 3,600 m
      in the flight up to 8,000 m
An-74TK-100 is equipped with two turbojet bypass engines D-36 of 3A series produced by Motor Sich (Zaporozhye), which correspond to ICAO requirements to low noise and emission. D-36 engines and their modifications are highly reliable and economic. Among their main advantages are low specific fuel consumption, ability to take off in the extreme weather conditions, "hot and high" characteristics. These engines are simple to service and repair because of their modular construction.
The exhaust section of the bypass duct is arranged to make it possible to equip the engine with a thrust reverser.

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Page last modified: 09-07-2011 13:33:31 ZULU