Search results
Results from the WOW.Com Content Network
The Rotax 912 was first sold in 1989 in non-certificated form for use in ultralights and motorgliders. [3] The original 60 kW (80 hp) 912 UL engine has a capacity of 1,211 cc (73.9 cu in) and a compression ratio of 9.1:1, and is designed to work with regular automotive gasoline, with up to 10% ethanol.
3Xtrim 3X55 showing its Rotax 912ULS engine installation 3Xtrim 3X55 showing its cockpit accommodation for two crew, side-by-side with vertically-hinged doors 3Xtrim 3X55 taxiing, showing front view of the aircraft 3Xtrim 3X55 with 30 degrees of flap deflection, showing the centre-section flap 3Xtrim 3X55 instrument panel
The Ikarus C42 is a single-engined high-wing monoplane with side-by-side seats for two in a 1.22 m (48 in) wide cabin. The C42 is manufactured with either an 80 hp (60 kW) Rotax 912 engine or a 100 hp (75 kW) Rotax 912s engine. The Rotax engine has a low fuel consumption and relatively low noise.
Initial version. Normally powered by a Rotax 914UL, but a 74 kW (99 hp) Rotax 912 ULS may be fitted. Introduced 2000. M-16-2006 Tandem Trainer Improved lubrication, cooling, centre of gravity position and avionics. Introduced 2006. M-19 Shark Enclosed cockpit version. [10] Only three prototypes built, no production. [11] M-22 Voyager
The Gemini's standard two-stroke 48 kW (64 hp) Rotax 582 engine was replaced in the Mirage by a 60 kW (80 hp) four-stroke Rotax 912UL. [2] The wings of the G3 Mirage have a constant chord centre section with straight tapered outer panels. The inboard sections carry electrically operated flaps. There is a single lift strut on each side, attached ...
The underwing cabin of the Sirius has a single piece windscreen, glazed side doors, rear side windows and an upper rear transparency. A choice of flat four engines offers either the 59.6 kW (80 hp) Rotax 912UL or the 73.5 kW (98.6 hp) Rotax 912 ULS.
EASA type-certified model in the CS-LSA category. Short wing version powered by a 100 hp (75 kW) Rotax 912 S3 engine. [11] Virus SW 600 D Based on the SW 121 but featuring a 100 hp (75 kW) Rotax 912 ULS engine, it is the first aircraft to be certified under the new German LTF-UL2019 rules for the 600 kg microlight category. [22]
Data from AVweb and Pipistrel General characteristics Crew: one Capacity: one passenger Length: 6.5 m (21 ft 4 in) Wingspan: 10.5 m (34 ft 5 in) Height: 2.05 m (6 ft 9 in) Wing area: 9.51 m 2 (102.4 sq ft) Empty weight: 279 kg (615 lb) Gross weight: 550 kg (1,213 lb) Fuel capacity: 50 litres (11 imp gal; 13 US gal) Powerplant: 1 × Rotax 912 UL four cylinder, horizontally opposed, four stroke ...