SU80

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 (metric)
23.18 m
Length (metric)
18.26 m
Height (metric)
5.74 m
Powerplant

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

Engine Model(s)
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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