Overview
The Yakovlev Yak-142 was a proposed short takeoff and landing airliner derived from the Yak-42. Developed during the late Soviet period, it aimed to improve efficiency and performance. The project did not enter production.
Live Fleet Activity (YK42)
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Specifications
Units
- Engine
- 3 × Lotarev D-36
- Engine type
- Turbofan
- Thrust
- 3 × 14,330 lbf · 64 kN
- Avionics
- AlliedSignal avionics
- Wing tips
- No winglets
- Seats
- 120
- Crew
- —
- Cabin width
- 12 ft 6 in · 3.80 m
- Cabin height
- 6 ft 10 in · 2.08 m
- Cabin length
- 65 ft 3 in · 19.90 m
- Exterior length
- 119 ft 4 in · 36.38 m
- Tail height
- 32 ft 3 in · 9.83 m
- Fuselage diameter
- 12 ft 10 in · 3.90 m
- Wing span
- 114 ft 5 in · 34.88 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 127,000 lb · 57,500 kg
- Max landing weight
- 112,500 lb · 51,000 kg
- Max payload
- 39,700 lb · 18,000 kg
- Fuel capacity
- 4,900 gal · 18,500 L · 14,800 kg (Jet A)
- Max cruise speed
- 440 kt · 506 mph · 815 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 130 kt · 150 mph · 241 km/h
- Range
- 2,200 nm · 2,530 mi · 4,070 km
- Fuel burn
- —
- Ceiling
- 32,000 ft · 9,800 m
- Rate of climb
- 2,500 ft/min · 13 m/s
- Takeoff distance
- 5,900 ft · 1,800 m
- Landing distance
- 3,600 ft · 1,100 m
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Live fleet activity details
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