Yak-42 Clobber (YAKOVLEV)
Version | Yak-42D |
Takeoff weight | 57 500 kg |
Engine | D-36 |
Takeoff thrust, kg | 3 õ 6 500 |
Passenger capacity, persons | 90 — 126 |
Cruising speed | 750 km/h |
Flight altitude | 9 600 m |
Payload: | |
— maximum | 13 500 kg |
— normal | 10 500 kg |
Range of flight: | |
—maximum payload | 1 960 km |
— normal payload | 2 790 km |
Airfield runway length | 2 200 m |
Version | Yak-42 1980 | Yak-42D 1987 | Yak-42D 2001 | Yak-42M 1987, project |
Take-off mass | 54 000 kg | 56 500 kg | 57 500 kg | 63 500 kg |
Engine | D-36 | D-36 | D-36 | D-436Ì |
Take-off thrust, êãñ | 3 x 6 500 | 3 x 6 500 | 3 x 6 500 | 3 x 7 500 |
Passenger number | 120 | 120 | 120 | 168 |
Cruise speed | 750 km/h | 750 km/h | 750 km/h | 830 km/h |
Height of flight | 9 100 ì | 9 100 ì | 9 600 ì | 11 400 m |
Payload: | ||||
— maximum | 14 500 kg | 13 500 kg | 13 500 kg | 16 500 kg |
— normal | 10 500 kg | 10 500 kg | 10 500 kg | 14 000 kg |
Range: | ||||
— with maximum payload | 450 km | 1 480 km | 1 960 km | 1 950 km |
— with normal payload | 1 530 km | 2 150 km | 2 790 km | 2 900 km |
Runway lenght | 1 800 m | 2 000 m | 2 200 m | 2 200 m |
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