Sukhoi Su-80

· Sukhoi Civil Aircraft
Airplanes
Length
18.26 m
Flat Wing Span
23.17 m
Height
5.52 m
Flat Wing Area
44 m²
Flat Wing Aspect Ratio
12.2
Max Seating
30
Cruise Speed
470 km/h
Max Ceiling
7600 m
Number of Engines
2
First Flight
2001-09-04
Number Built
8
Maximum Take-Off Weight
13.5 t (paragliders: kg)
Total Fuel Capacity
2350
Maximum Range
1400 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity Maximum Range (km)
Sukhoi Su-80 13.5 2350 1400

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All data (25 fields)
Name
Sukhoi Su-80
Manufacturer
Sukhoi Civil Aircraft
Description
The Sukhoi Su-80 (formerly known as the Sukhoi S-80) is a Russian twin-turboprop, twin-boom STOL transport aircraft.
ICAO Code
SU80
First Flight
2001-09-04
Designer
Sukhoi Civil Aircraft
Type
STOL transport aircraft
Length (m)
18.26
Height (m)
5.52
Cockpit Crew
1
Max Seating
30
Cruise Speed (km/h)
470
Max Ceiling (m)
7600
Armament
Wing and fuselage hardpoints for bombs, rockets, machine guns and light autocannon.
Capacity Description
30 pax / 3300 kg max payload
Number Built
8
Powerplant Description
2 × General Electric CT7-9B turboprop engines, 1305 kW (1750 hp) each
Primary Users
Border Service of the National Security Committee of the Republic of Kazakhstan (discontinued sale)
Status
Retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/Sukhoi_Su-80
Flat Wing Span (m)
23.17
Flat Wing Area (m²)
44
Flat Wing Aspect Ratio
12.2
Wake Category
M
Number of Engines
2