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WMD-10 CLASSIC is a side-by-side, two-seat, braced high-wing plane of composite structure with a load-bearing cage in the central part of the fuselage and a fixed tricycle landing gear, meant for sport and recreational flying under VFR conditions in SLZ category. The power plant is a four stroke, four cylinder engine ROTAX 912 ULS with a ground adjustable, three blade propeller Woodcomp SR 200. The plane can be fitted with a ballistic rescue system.
Technical Specifications
Wing span .....................................................................10,0 m
Wing area.......................................................................10,5 m2
Aspect ratio......................................................................9,52
Length...............................................................................6,3 m
Height................................................................................2,2 m
Mean camber line.........................................................1,05 m
Ailerons, Flaps and Tail Assembly
Aileron length.................................................................1,45 m
Aileron area....................................................................0,36 m2
Flap length......................................................................2,50 m
Flap area.........................................................................0,81 m2
Tailplane span ................................................................2,4 m
Tailplane area ...............................................................1,68 m2
Fin/rudder height............................................................1,19 m
Fin/rudder area...............................................................1,02 m2
Undercarriage
Main undercarriage wheel spacing............................1,75 m
Wheel base ....................................................................1,52 m
Main undercarriage wheel dimension.......................0,35 m
Nose undercarriage wheel dimension......................0,32 m
Weights
Empty weight with fixed undercarriage.......................280 kg
Empty weight with ballistic rescue system ...............305 kg
Maximum take-off weight...............................................450 kg
Live load...........................................................................170 kg
Fuel tanks capacity……...................................................90 litres
Power plant.......ROTAX 912 ULS ( 73,6 kW ) at 5800 rpm
1.68 m, three-blade, ground adjustable propeller SR 200
Propeller ground clearance..........................................250 mm.
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