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The aircraft has a standard empty weight of 70 kg (154 lb). It features two contra-rotating main rotors, a single-seat open cockpit without a windshield, four-wheeled landing gear and four twin-cylinder, air-cooled, two-stroke , 10 hp (7 kW) GEN 125-F engines to provide operational redundancy since the aircraft cannot autorotate in the event of ...
Agricultural coaxial heli China [21] Red Coaxial Helicopter China Coaxial Single Seater [22] White Coaxial Chopper China Coaxial Single Seater [23] Homebuilt Coaxial Heli China Coaxial Single Seater [24] Yellow tail coaxial heli China [25] Famà Kiss 209: Italy Sk-1 Twinpower Italy [26] G-250 Eagle: Italy Engine Turbine LCA LH 212 Delta: Italy ...
The CoAX 2D/2R was originally known as the FLIP 2 (Fly In Perfection) and is a derivative of the FLIP 1, a conventional helicopter with a main and tail rotor.[1]The CoAX 2D/2R was designed to comply with the European Class 6 microlight helicopter rules, including the category's maximum takeoff weight of 450 kg (992 lb).
The aircraft has conventional landing gear, with wheel pants as an option. The company claims that a builder can complete the aircraft in 350–400 hours from the kit. [5] [9] The aircraft was originally intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight.
The FP-202 was designed by Fisher Aircraft in the United States in 1981 and was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight. It is also a 51% approved kit for the US homebuilt aircraft category.
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.
The Livella Uno was designed to comply with the US FAR 103 Ultralight Vehicles and the European 120 kg class ultralight aircraft rules. It features a dual coaxial main rotors, with an inverted V-tail, a single open-air pilot's seat without a windshield, tricycle landing gear and a 40 hp (30 kW) Wankel Aixro XH40 engine.
Founded by Herbert Beaujon in the 1970s, Beaujon Aircraft has published the designs for eight ultralight aircraft and marketed seven of them in book form under the name How to Build Ultralights. The book and its plans have received praise from reviewers. Andre Cliche wrote: [1] “How to build ultralights".