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  2. Sabelt - Wikipedia

    en.wikipedia.org/wiki/Sabelt

    Sabelt sells ultralight racing suits, carbon fiber seats that adapt to the driver and seat belts for cars of all types of racing. From the world of motorsport, it has developed a range of sports seats for car manufacturers. Each seat is designed and created exclusively by Sabelt in collaboration with its customers, the car manufacturers.

  3. Houde Speedmax - Wikipedia

    en.wikipedia.org/wiki/Houde_Speedmax

    The Speedmax features a cantilever low-wing, a single seat enclosed cockpit under a bubble canopy, fixed conventional landing gear and a single engine in tractor configuration. [1] [2] The aircraft is made from wood, with some parts fabricated from carbon fibre. The standard engine available is the 64 hp (48 kW) Rotax 582 two-stroke powerplant ...

  4. Fisher Flying Products - Wikipedia

    en.wikipedia.org/wiki/Fisher_Flying_Products

    Single seat high wing ultralight Fisher Culex: Tandem 2-seat twin-engined mid-wing monoplane Fisher Mariah: Tandem 2-seat low-wing monoplane Fisher FP-101: 1982 Single seat high wing ultralight Piper J-3 Cub: Fisher FP-202 Koala: 1981 325 (2004) Single seat high wing ultralight Piper J-3 Cub: Fisher FP-303: 1982 200 (2004) Low wing, single seat ...

  5. Flying K Sky Raider - Wikipedia

    en.wikipedia.org/wiki/Flying_K_Sky_Raider

    Stretched version with two seats in tandem, a gross weight of 950 lb (431 kg), an acceptable power range of 60 to 80 hp (45 to 60 kW). Engines used include the two-stroke 50 hp (37 kW) Rotax 503 and the four-stroke 60 hp (45 kW) HKS 700E engine. Described as an "intimate tandem two seater" due to the small rear seat space. Production completed.

  6. Robertson B1-RD - Wikipedia

    en.wikipedia.org/wiki/Robertson_B1-RD

    The aircraft 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 B1-RD has a standard empty weight of 220 lb (100 kg).

  7. Phantom X1 - Wikipedia

    en.wikipedia.org/wiki/Phantom_X1

    Two seat side-by-side configuration ultralight trainer, first flown in 1995, with first deliveries in February 1998. Folding wings were a factory option. Standard engine is the 50 hp (37 kW) Rotax 503 or 64 hp (48 kW) Rotax 582 as an option. [1] [2] [3] Phantom I Single seat ultralight aircraft with struts in place of cable-bracing.

  8. Milholland Legal Eagle - Wikipedia

    en.wikipedia.org/wiki/Milholland_Legal_Eagle

    Model for larger pilots with a wider and taller seat, greater wing area and longer tail. 246 lb (112 kg) empty weight [6] [7] [11] Double Eagle Model with two seats in side-by-side configuration with a 385 lb (175 kg) empty weight and a 900 lb (408 kg) gross weight. Designed as an ultralight trainer and Light Sport Aircraft.

  9. Advanced Aeromarine Carrera - Wikipedia

    en.wikipedia.org/wiki/Advanced_Aeromarine_Carrera

    The Carrera is a two-seat ultralight aircraft marketed for home building. Designed by Advanced Aeromarine, it has also been marketed by Advanced Aviation and Arnet Pereyra Inc. It is a high-wing taildragger aircraft of pusher configuration with side-by-side seating. It is of fabric-covered tubular construction.