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"All wood" construction with additional
styrofoam
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Overall length
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4.90 m / 16 ft
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Overall wing span
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6.30 m / 20.66 ft
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Vertical stabilizer height
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1.76 m / 5.6 ft
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Fuselage width
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0.64 m / 26 in
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Cabin height
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1.04 m / 3.15 ft
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Cabin width at pilot elbow
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0.64 m / 26 in.
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Swep wing rectangular without dihedral
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Canard wing rectangular and rectilinear
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Main wing equipped with "flaperons"
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Dual controls (push-pull tubes)
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Nose wheel steering coupled to the rudder
pedals
(fixed landing gear)
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Cabin heated, brakes on rear-weels
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Main landing gear of laminated wood
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12 V alternator powered electrical system
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VHF, VOR (or GPS NAV) - transponder
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Fuel tanks in wing leading edge
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60 liters / 16.2 US.G
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Electrical contents indication
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Internal luggage stowage behind passenger
head
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One-piece canopy, opens laterally (special
"IBIS" canopy)
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Max. take-off weight
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470 kg (VZ
3.5 m/s) - 1034 lbs
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Empty weight with starter equipment
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260 kg - 572 lbs
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Payload (full fuel)
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170 kg - 374 lbs
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Front pilot weight limits
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65/95 kg - 143/209 lbs
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G-loading
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+4.5 and -3.0
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Max. speed (VMO)
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260 km/h
(140kts) - 161 mph
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Approach speed
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120 km/h (65 kts) - 74
mph
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Stall speed
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95 km/h (52 kts) - 59
mph
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Normal cruise
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65% 200 km/h (108 kts) - 124
mph
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Long range cruise
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180 km/h (97 kts) - 112
mph
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Max. range
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900 km (485 Nms) + VFR reserves - 559 SM
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Takeoff distance
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1000 ft
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Landing distance
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1050 ft
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Climb rate (VW 1835 CC)
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700 fpm at M.T.O. weight.
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Service ceiling
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depends on the engine power
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