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Rotax 912ULS 100 hp (75 kW) installation in a Blue Yonder Merlin EZ Pusher engine installation of two Rotax 912ULSs in a Lockwood Aircam Rotax 912ULS with tuned exhaust in a Dyn'Aéro MCR01 with 3-blade hydraulic CSU propeller. The Rotax 912 is a horizontally-opposed four-cylinder, naturally-aspirated, four-stroke aircraft engine with a ...
Data from Jane's All the World's Aircraft 2010/11 General characteristics Capacity: two Length: 5.69 m (18 ft 8 in) Wingspan: 9.04 m (29 ft 8 in) Height: 2.00 m (6 ft 7 in) Wing area: 9.40 m 2 (101.2 sq ft) Empty weight: 284 kg (626 lb) including parachute Max takeoff weight: 472.5 kg (1,042 lb) Fuel capacity: 65 L (15.8 imp gal, 19.0 US gal) standard Powerplant: 1 × Rotax 912ULS 4- cylinder ...
Standard engine is the 100 hp (75 kW) Rotax 912ULS and cruise speed is 120 mph (193 km/h) with that engine. Acceptable power range is 52 to 120 hp (39 to 89 kW) and alternate engines include the 52 hp (39 kW) Rotax 503, 64 hp (48 kW) Rotax 582, 80 hp (60 kW) Rotax 912UL, 85 hp (63 kW) Jabiru 2200, or the 120 hp (89 kW) Jabiru 3300. Still in ...
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.
This can be installed on new-build aircraft and also retro-fitted to aircraft already in service with a single screen. [15] A new variant, the RV-12iS, was introduced in 2017. The RV-12iS is an incremental improvement over the RV-12 which allows the installation of the Rotax 912ULS (carbureted) or the Rotax 912iS (fuel-injected) engines.
Data from Jane's All The World's Aircraft 2003–2004 General characteristics Crew: 2 Length: 6.40 m (21 ft 0 in) Wingspan: 8.41 m (27 ft 7 in) Height: 2.29 m (7 ft 6 in) Wing area: 12.20 m 2 (131.3 sq ft) Empty weight: 281 kg (619 lb) Gross weight: 450 kg (992 lb) Fuel capacity: 70 L (15 imp gal; 18 US gal) Powerplant: 1 × Rotax 912 ULS flat-four engine, 73.5 kW (98.6 hp) Propellers: 2 ...
The cockpit width is 1.15 m (45 in). Standard engines available are the 100 hp (75 kW) Rotax 912ULS, the Rotax 912iS [5] and the 115 hp (86 kW) Rotax 914 four-stroke powerplants. A glider towhook is optional equipment. [2] [3] [6] The design has been developed into a three to four seat aircraft, the Aerospool WT10 Advantic. [2]
Standard engine is the 100 hp (75 kW) Rotax 912ULS and the 2010 base price is US$99,000. [16] S-6S Super Six Improved version with dope and fabric covering, introduced in 1993. Standard engine is the 100 hp (75 kW) Rotax 912ULS. Available with standard wing, "116" wing and "light sport wing". In production in 2010. [3] [5] [6] [13]