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Be-103 :
Specifications
Specifications
Aircraft cabin
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Specifications
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Civil aviation
Sukhoi Superjet 100
Be-103
Su-26, 29, 31
Su-80
Primary dimensions
Length
10.65 m
Height at parking
3.757 m
Span
12.72 m
Track
2.273 m
Base
4.06 m
Clearance
0.295 m
Wing area
25.1 m
2
Leading edge sweep angle
22°
Mean aerodynamic chord
2.139 m
Wing panel dihedral
5.05°
Aileron deflection angle
±25°
Vertical stabiliser:
Height
2.2 m
Sweep angle
33°
Area
4.4 m
2
Rudder deflection angle
±27°
Horizontal stabiliser:
Span
3.9 m
Sweep angle
14.65°
Area
3.68 m
2
Horizontal stabiliser settings
-14°/+16°
Fuselage maximum widt
1.35 m
Cabin length
3.2 m
Cabin width
1.25 m
Cabin height
1.23 m
Cabin volume
4.2 m
3
Maximum cargo length
2.5 m
Primary flight spe
Empty weight
1,680 kg
Operational empty weight
1,760 kg
Maximum takeoff weight
2,270kg
Maximum payload
385 kg
Useful load (cargo+fuel)
510 kg
Maximum landing weight
2,270 kg
Maximum fuel capacity
245 kg
Operating altitude
500-3,000 m
Service ceiling
5,000 m
Cruising speed:
economy (Vecon)
220 km/h
maximum (Vmax)
250 km/h
Stalling speed
109 km/h
Range (with 245 kg of fuel):
at altitude 500 m
1,180 km
at altitude 3,000 m
1,100 km
Range (with 149 kg of fuel)
590 êì
Mean fuel consumption per 1 hour:
economy speed (Vecon)
44 kg/h
maximum speed (Vmax)
58 kg/h
Run on land / water
440 m / 620 m
Roll on land / water
240 m / 320 m
Seagoing ability (wave height) sea state
2 (0.5 m)
© Sukhoi Company (JSC) 2004-2005
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