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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.
These new rules are expected to allow four seat LSAs up to a gross weight of 3,000 lb (1,361 kg), with a maximum 61 kn (113 km/h; 70 mph) stall speed to be allowed in the US. Since Brazil has already approved the new regulations, the company expects to have the aircraft approved under the new rules in Brazil by mid-2024 and then in the US later.
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.
The single seat Javelin I was designed to comply with the American FAR 103 ultralight regulations, including that category's maximum 254 lb (115 kg) empty weight. [ 1 ] [ 2 ] [ 3 ] Capella Aircraft went out of business in late 2007, and the type is no longer in production.
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.
D-FAAA to D-FZZZ for single-engine aircraft with 2–5.7 t MTOW; D-GAAA to D-GZZZ for multi-engine aircraft up to 2 t MTOW; D-HAAA to D-HZZZ for rotorcraft; D-IAAA to D-IZZZ for multi-engine aircraft with 2–5.7 t MTOW; D-KAAA to D-KZZZ for powered gliders; D-LAAA to D-LZZZ for airships; D-MAAA to D-MZZZ for powered ultralight aircraft
Single seat, wired-braced Part 103 ultralight flying boat. Engines available were the 28 hp (21 kW) Rotax 277 and the 35 hp (26 kW) Rotax 377. [1] Buccaneer SX Single seat, strut-braced flying boat. Engines available were the 40 hp (30 kW) Rotax 447 and the 50 hp (37 kW) Rotax 503. [1] Buccaneer II Two seat, strut-braced flying boat.
Single engine piston aircraft with tricycle landing gear [1]; Model Engine Power hp Seats Wing Sq. Ft. MTOW lb Empty lb Cruise knots Range nmi AS 202 Bravo NG: L. AEIO-360: 180: 3: 149: 2,202: 1,389