Search results
Results From The WOW.Com Content Network
Ultralight aircraft plans: Beaujon Aircraft, also known as Beaujon Ultralights, ... three axis control Enduro available for free download as 25 JPEGs. [3] Aircraft
The aircraft was designed long before the adoption of the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg), but nonetheless complies with them. The aircraft has a standard empty weight of 150 lb (68 kg) and is billed as the "World's Tiniest Homebuilt Helicopter" by the plans supplier.
Beaujon Aircraft publishes the plans along with six other designs in book form under the name How to Build Ultralights. [1] The Mach .07 was specifically designed to comply with the United States ultralight category and its FAR 103 Ultralight Vehicles rules, including the category's maximum 254 lb (115 kg) empty weight. [1] [2]
The aircraft is a monoplane derivation of the biplane H-2 Honey Bee and was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). The aircraft has a standard empty weight of 252 lb (114 kg), when equipped with the now-out of production Rotax 277 single cylinder engine.
The A/W 95 was designed to comply with the US Experimental - Amateur-built aircraft rules, but if built lightly enough may qualify as an ultralight aircraft, under the US FAR 103 Ultralight Vehicles rules, with that category's maximum empty weight restriction of 254 lb (115 kg). The aircraft has a standard empty weight of 272 lb (123 kg). [1]
Free Bird Innovations, Inc. is an American aircraft manufacturer based in Detroit Lakes, Minnesota and formed in about 2003. The company specializes in the design and manufacture of ultralight aircraft in the form of plans and kits for amateur construction and ready-to-fly aircraft in the US FAR 103 Ultralight Vehicles category.
Like many pusher ultralight aircraft the Enduro sits on its tail skid when unoccupied and on its nose skid when a pilot is sitting in the seat. No brakes are specified in the design. [3] The controls are three-axis, with an overhead-mounted control column. The rudder and ailerons are designed to be interconnected and controlled via the control ...
A horizontal tailplane maintains the aircraft pitch angle in flight and a large fin and rudder is provided. The main rotor system is of low-inertia and requires pilot skill to manage energy on landing. [2] [4] The aircraft plans cost US$160 in 2001. Construction time is estimated as 400 hours, much of which is consumed fabricating the composite ...