Passenger Turbo Props
Vultee V-1
ICAO: V1
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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Operational Context
Sukhoi Su-80 — twin-engine regional utility turboprop
The Su-80 first flew in 2001 as part of Sukhoi’s effort to expand into the regional transport market. The aircraft features a high wing and rear loading ramp for cargo flexibility. It was designed to operate in challenging environments across Russia and neighboring regions.
Powered by two General Electric CT7 turboprop engines producing approximately 1,750 shaft horsepower each, the Su-80 cruises at around 250 knots (460 km/h). Maximum takeoff weight is roughly 30,000 pounds (13,600 kg). The cabin can accommodate around 30 passengers depending on configuration.
Production numbers have remained limited, but the design reflects efforts to modernize regional aviation in Russia. The Su-80 combines transport and utility capability in a single platform. It represents a niche entrant in the regional turboprop segment.
Sources and references used for research and fact-checking.