WING Wing span 9.96 m Mean Aerodynamic Chord 1.33 m Wing surface area 12.47 m2 Wing loading 72.2 kgm-2 Aspect ratio 7.91 Taper ratio 1.375 Dihedral 5°
FUSELAGE Fuselage length 6.17 m Overall length 7.10 m Overall width 1.15 m Overall height 2 50m
EMPENNAGE Horizontal stabilizer span 2.83 m Horizontal stabilizer surface area 0.96 m2 Elevator surface area 1.02 m2 Horizontal stabilizer angle of incidence ‐2.5° Vertical stabilizer span 1.47 m Vertical stabilizer surface area 0.53 m2 Rudder surface area 0.59 m2
LANDINGGEAR Wheel track 1.95m Wheel base 1.67m Wheel hubs and brakes Main gear tyres 15 X 6.00 ‐ 6, 6 ply Nose gear tyres 5.00–5, 6 ply
CONTROL SURFACE TRAVEL LIMITS Ailerons 22° up and down Elevator 28° up and 20° down Trim tab 20° up and 25° down Rudder 25° left and right Flaps 0° to 40° down
ENGINE Manufacturer Bombardier‐Rotax GmbH Model 914 UL Type 4 cylinder horizontally opposed with overall displacement 1211cc, mixed cooling (water‐cooled heads and air‐cooled cylinders), turbo charged, twin carburetors, integrated reduction gearbox with torque damper Maximum power 84.5 kW (115hp) @ 5 800 rpm (max 5 mins) 73.5 kW (100hp) @ 5 500 rpm (continuous) Power loading 7.8 kghp‐1 PROPELLER Manufacturer Airmaster, electric constant speed Model 72.5 inch 3 blade composite No of blades 3 Diameter 1.78m Type composite
FUEL Fuel grade High octane gasoline DIN 51600, O‐NORM 1103 (red) Unleaded gasoline DIN 51603, O‐NORM 1101 AVGAS 100LL Fuel tanks 2 wing tanks integrated within wing’s leading edge, equipped with finger strainers outlet and drain fittings Capacity of each tank 92.5 liters Total capacity 185 liters Total usable fuel 183 liters
OIL SYSTEM Oil system type forced, with external oil reservoir Oil Automotive grade API “SF” or “SG” type oil preferably synthetic or semi‐synthetic Oil capacity 3.5 liters
COOLING Cooling system Mixed air and liquid pressurized closed circuit system Coolant Antifreeze liquid (type BASF Glysanthin Anticorrosion or equivalent) and water mixture 75/25 Capacity 3 liters
MAXIMUM WEIGHTS Maximum take‐off weight 900kg Maximum landing weight 900kg Maximum baggage weight 40kg Maximum rear seat/baggage weight 140kg
STANDARD WEIGHTS Standard empty weight 475 kg Maximum useful load 425 kg
SPECIFIC LOADINGS Wing loading 59.10 kgm‐2 Power loading 7.11 kghp‐1
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WING Wing span 9.165 m Mean Aerodynamic Chord 1.339 m Wing surface area 11.845 m2 Wing loading 59.10 kgm-2 Aspectratio 7.04 Taperratio 1.375 Dihedral 5°
FUSELAGE Fuselage length 5.77 m Overall length 6.675 m Overall width 1.15 m Overall height 2 500m EMPENNAGE Horizontal stabilizer span 2.825 m Horizontal stabilizer surface area 0.96 m2 Elevator surface area 1.02 m2 Horizontal stabilizer angle of incidence ‐4° Vertical stabilizer span 1.47 m Vertical stabilizer surface area 0.53 m2 Rudder surface area 0.59 m2
LANDINGGEAR Wheel track 1.95m Wheel base 1.41m Wheel hubs and brakes Main gear tyres 15 X 6.00 ‐ 6, 4 ply Nose gear tyres 5.00–5, 4 ply
CONTROL SURFACE TRAVEL LIMITS Ailerons 22° up and down Elevator 28° up and 20° down Trim tab 20° up and 25° down Rudder 25° left and right Flaps 0° to 32° down
ENGINE Manufacturer Bombardier‐Rotax GmbH Model 912 ULS Type 4 cylinder horizontally opposed with overall displacement 1352cc, mixed cooling (water‐cooled heads and air‐cooled cylinders), twin carburetors, integrated reduction gearbox with torque damper Maximum power 73.5 kW (98.5hp) @ 5 800 rpm (max 5 mins) 69 kW (92.5hp) @ 5 500 rpm (continuous)
PROPELLER Manufacturer Warp drive Model 70 inch 3 blade composite No of blades 3 Diameter 1.78m Type composite
FUEL Fuel grade High octane gasoline DIN 51600, O‐NORM 1103 (red) Unleaded gasoline DIN 51603, O‐NORM 1101 AVGAS 100LL Fuel tanks 2 wing tanks integrated within wing’s leading edge, equipped with finger strainers outlet and drain fittings Capacity of each tank 75 liters Total capacity 150 liters Total usable fuel 146 liters
OIL SYSTEM Oil system type forced, with external oil reservoir Oil Automotive grade API “SF” or “SG” type oil preferably synthetic or semi‐synthetic Oil capacity 2.5 liters
COOLING Cooling system Mixed air and liquid pressurized closed circuit system Coolant Antifreeze liquid (type BASF Glysanthin Anticorrosion or equivalent) and water mixture Capacity 3 liters
MAXIMUM WEIGHTS Maximum take‐off weight 700kg Maximum landing weight 700kg Maximum baggage weight 35kg
STANDARD WEIGHTS Standard empty weight 360kg Maximum useful load 340 kg
SPECIFIC LOADINGS Wing loading 59.10 kgm‐2 Power loading 7.11 kghp‐1
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