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Air-Copter D JP Max

Air-Copter designed the blade from extruded dural, with a biconvex NACA 23112 profile.
Engine: Hirth F30 , 80 hp
Rotor span: 7 m
Blade area: 0.215 sq.m
MAUW: 350 kg
Empty weight: 145 kg
Fuel capacity: 35 lt
Max speed: 170 kph
Cruise speed: 120 kph
Minimum speed: 15 kph
Climb rate: 10 m/s
Seats: 2
Fuel consumption: 17 lt/hr
Plan price (1998): 500 Fttc
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