Overview
The Antonov An-32 is a twin-engine turboprop transport developed as an enhanced version of the An-26. Designed to operate in extreme climates and at high-altitude airfields, it became widely used by military and civil operators. The aircraft entered service in the late 1970s.
Live Fleet Activity (AN32)
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Specifications
Units
- Engine
- 2 × ZMKB AI-20DM turboprop
- Engine type
- Turboprop
- Power
- 2 × 5,112 shp · 3,812 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 50 economy · 42 business · 24 first
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 78 ft 0 in · 23.78 m
- Tail height
- 28 ft 8 in · 8.75 m
- Fuselage diameter
- —
- Wing span
- 95 ft 10 in · 29.20 m
- Baggage volume
- 1,059 ft³ · 30.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 131,000 lb · 59,500 kg
- Max landing weight
- —
- Max payload
- 14,800 lb · 6,700 kg
- Fuel capacity
- 790 gal · 3,000 L · 2,400 kg (Jet A)
- Max cruise speed
- 250 kt · 288 mph · 463 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 1,300 nm · 1,500 mi · 2,410 km
- Fuel burn
- 1.95 nm/gal · 0.95 km/L
- Ceiling
- 31,200 ft · 9,500 m
- Rate of climb
- 1,260 ft/min · 6 m/s
- Takeoff distance
- 4,050 ft · 1,240 m
- Landing distance
- 5,600 ft · 1,700 m
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Live fleet activity details
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