Overview
The Sukhoi Su-80 is a twin-engine turboprop utility aircraft developed for passenger and cargo roles. Designed to serve remote regions, it emphasizes rugged construction and short-field performance. The aircraft entered limited production in the 2000s.
Live Fleet Activity (SU80)
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Specifications
Units
- Engine
- 2 × General Electric GE CT7-9B Turboprop
- Engine type
- Turboprop
- Power
- 2 × 1,750 shp · 1,305 kW
- Avionics
- SBKV-P strapdown heading and altitude system, VIM-95C (VOR/ILS/SP/MRK) navigation and landing systems, SO-94R (UVD) radar responder,
- Wing tips
- Blended tips
- Seats
- 30
- Crew
- —
- Cabin width
- 7 ft 1 in · 2.17 m
- Cabin height
- 6 ft 0 in · 1.82 m
- Cabin length
- 25 ft 5 in · 7.75 m
- Exterior length
- 59 ft 11 in · 18.26 m
- Tail height
- 18 ft 10 in · 5.74 m
- Fuselage diameter
- 7 ft 10 in · 2.40 m
- Wing span
- 76 ft 1 in · 23.18 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 29,800 lb · 13,500 kg
- Max landing weight
- 29,900 lb · 13,600 kg
- Max payload
- 6,000 lb · 2,750 kg
- Fuel capacity
- 660 gal · 2,500 L · 2,000 kg (Jet A)
- Max cruise speed
- 250 kt · 288 mph · 463 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 760 nm · 870 mi · 1,410 km
- Fuel burn
- 1.22 nm/gal · 0.60 km/L
- Ceiling
- 24,900 ft · 7,600 m
- Rate of climb
- —
- Takeoff distance
- 2,750 ft · 840 m
- Landing distance
- 1,510 ft · 460 m
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Live fleet activity details
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