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Aircraft cabin |  Specifications | 

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 m2
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 m2
Rudder deflection angle ±27°
Horizontal stabiliser:
Span 3.9 m
Sweep angle 14.65°
Area 3.68 m2
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 m3
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)


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