SUKHOI Su-80

Aircraft
Name: 
Su-80
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
High wing
Type Code: 
L2T
Engine: 
Turboprop
Engine Count: 
Multi
Position: 
(Front) Wing leading mounted
Landing gear: 
Tricycle retractable
Manufacturered as
SUKHOI Su-80

SU80

The Sukhoi Su-80 is a Russian twin-turboprop, twin-boom Short Take-Off and Landing (STOL) transport aircraft.

Technical Data
Wing span: 
23.18 m
Length: 
18.26 m
Height: 
5.74 m
Powerplant: 

2 x General Electric CT7-9B turboprop, 1,305 kW (1,750 hp) each.

Engine Model: 
General Electric CT7
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
1400 m
MTOW: 
12500 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
250 kts
MACH: 
n/a
Ceiling: 
290
Range: 
1600 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
640 m

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