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Model 40

Model 40 - Weedhopper
VS (stall speed): 17 kts | 20 mph | 32 kph
VC (cruise speed): 48 kts | 55 mph | 89 kph
VNE (never exceed speed) : 56 kts | 65 mph | 105 kph
Climb ratio: 1000 ft/min | 5 m/s

Takeoff distance over 50ft (15m) obstacle: 100 ft | 30 m
Landing distance over 50ft (15m) obstacle: 100 ft | 30 m

MEW (manufacturers empty weight): 113 kg | 250 lbs
MTOW (maximum takeoff weight): 249 kg | 550 lbs

Engine: Rotax 447 or Rotax 277

The Weedhopper is an American 2-axis controlled ultralight aircraft. It was developed by John Chotia during the 70s ultralight boom. The Weedhopper was introduced in 1977, at a time where most ultralights were of the weight shift type.

The Weedhopper has a stick that controls the rudder and elevator. The dihedral angle in combination with the backward swept leading edge of the wing gives this aircraft stable characteristics.

The Weedhopper is powered by a Rotax 277 (28hp) or a Rotax 447 (40hp).

As of today more than 13 000 Weedhoppers have been sold!

Photo from http://www.weedhopperusa.net/


Price: 7995 USD

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