Overview
The Antonov An-140 was developed in the 1990s as a regional turboprop for domestic and export markets. Designed to replace older Soviet commuter aircraft, it emphasizes rugged performance. The aircraft entered service in the early 2000s.
Live Fleet Activity (A140)
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Specifications
Units
- Engine
- 2 × Pratt & Whitney PW127A or Klimov TV3-117WMA-SBM1
- Engine type
- Turboprop
- Power
- 2 × 2,465 shp · 1,838 kW
- Avionics
- Buran weather radar
- Wing tips
- No winglets
- Seats
- 52
- Crew
- —
- Cabin width
- 8 ft 6 in · 2.60 m
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 74 ft 2 in · 22.60 m
- Tail height
- 26 ft 11 in · 8.20 m
- Fuselage diameter
- 9 ft 2 in · 2.80 m
- Wing span
- 80 ft 5 in · 24.50 m
- Baggage volume
- 7 ft³ · 0.2 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 47,400 lb · 21,500 kg
- Max landing weight
- 46,300 lb · 21,000 kg
- Max payload
- 13,200 lb · 6,000 kg
- Fuel capacity
- 1,430 gal · 5,400 L · 4,300 kg (Jet A)
- Max cruise speed
- 310 kt · 357 mph · 574 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 2,000 nm · 2,300 mi · 3,700 km
- Fuel burn
- 2.47 nm/gal · 1.21 km/L
- Ceiling
- 24,900 ft · 7,600 m
- Rate of climb
- 1,344 ft/min · 7 m/s
- Takeoff distance
- 5,750 ft · 1,750 m
- Landing distance
- 4,450 ft · 1,360 m
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Live fleet activity details
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