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The kits originally sold for $2,000, and in 2011 the Weedhopper model 40 sold for US$8,495. [ 2 ] [ 1 ] [ 13 ] In its home country versions of the aircraft are eligible for the FAR 103 Ultralight Vehicles category, the experimental amateur-built category and the light-sport aircraft category.
The CB-40 was re-engineered to overcome problems of vibration and cooling in the original design. [2] Suited for ultralight use and single seat light sport aircraft, the engine weighs 86 lbs and produces 40 hp (30 kW). The engine uses a short aluminum crankcase with redesigned oil galleries for improved lubrication.
By May 2006, Limbach had produced more than 6000 engines. [2] The engines are certified according to CS-22 Subpart H [ 3 ] for use in motorgliders , CS-LSA [ 4 ] and CS-VLA [ 5 ] type of aircraft. Most Limbach engines are based on the Volkswagen flat-4 boxer unit with displacement of up to 2.4 liters, and up to 160 BHP in the turbocharged model.
The Rotax 447 is a development of the Rotax 377, increasing the power output from 26 kW (35 hp) to 29.5 kW (40 hp) by increasing the cylinder bore from 62 mm to 67.5 mm and the maximum rpm from 6500 to 6800. [2] The modern 447 has a single breakerless, magneto capacitor-discharge ignition (CDI) system.
Skyranger Original model, introduced 1990. [2]Skyranger Vfun Renamed original model for the Fédération Aéronautique Internationale microlight class. Standard engines available are the 64 hp (48 kW) Rotax 582 two-stroke, the 80 hp (60 kW) Rotax 912UL, the 100 hp (75 kW) Rotax 912ULS, 85 hp (63 kW) Jabiru 2200, the 60 to 80 hp (45 to 60 kW) VW and the 60 hp (45 kW) HKS 700E four-stroke ...
[1] [2] [3] The engine runs on a mixture of unleaded auto fuel and oil. [1] [2] Producing 45 hp (34 kW) at 5800 rpm, the G-50 competed in the early 1980s ultralight powerplant market against the similar Rotax 447. Production of the engine was completed in the late 1980s and today only used engines and parts are available. [1] [2]
It is equipped with a recoil starter system or optionally electric start and a 2.5 or 2.8:1 belt reduction drive. [1] [2] [3] The engine runs on a mixture of unleaded auto fuel and oil. [1] [2] Producing 22 hp (16 kW) at 6600 rpm, the G-25 competed in the early 1980s ultralight powerplant market against the similar Rotax 277. Production of the ...
The first models used a 26 hp 342 cc Normalair-Garrett two-cylinder two-stroke driving a pusher propeller. Performance was 35 to 185 knots (65 to 343 km/h; 40 to 213 mph) with an endurance from one to three hours. Flight control is by two elevons. Later models used Norton P73 wankel engines.
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