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  2. GEN H-4 - Wikipedia

    en.wikipedia.org/wiki/GEN_H-4

    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 ...

  3. List of ultralight helicopters - Wikipedia

    en.wikipedia.org/wiki/List_of_ultralight_helicopters

    Coaxial Single Seater [17] Shandong coax heli China Coaxial Single Seater [18] Guo Leiting's Coax China Yuncheng Farmer's Chopper Shantou Copters China Homebuilt Helis by Farmer Chen Ruihua Jiangsu China Coaxial Single Seater [19] Coaxial heli Zhuzhou China Coaxial Single Seater [20] Agricultural coaxial heli China [21] Red Coaxial Helicopter China

  4. Arrow Coax Livella Uno - Wikipedia

    en.wikipedia.org/wiki/Arrow_Coax_Livella_Uno

    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.

  5. Free Bird Innovations - Wikipedia

    en.wikipedia.org/wiki/Free_Bird_Innovations

    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.

  6. Rotorfly R-30 - Wikipedia

    en.wikipedia.org/wiki/Rotorfly_R-30

    The Rotorfly R-30 helicopter is a coaxial helicopter with two two-blade fiberglass rotors. The control rods of the upper main rotor are located inside the shaft which reduces turbulence, It has been described as a hingeless teetering blade mount. [2] The aircraft claimed to be very quiet in general. [5]

  7. Howland H-3 Pegasus - Wikipedia

    en.wikipedia.org/wiki/Howland_H-3_Pegasus

    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.

  8. Team Mini-Max Hi-MAX - Wikipedia

    en.wikipedia.org/wiki/Team_Mini-Max_Hi-MAX

    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.

  9. Capella Aircraft - Wikipedia

    en.wikipedia.org/wiki/Capella_Aircraft

    Capella Aircraft Corporation was an American aircraft manufacturer based in Austin, Texas. Formed about 1988, the company specialized in the design and manufacture of light aircraft in the form of kits for amateur construction , including for the US FAR 103 Ultralight Vehicles rules.

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