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2. Rotax 912 - Wikipedia

   en.wikipedia.org/wiki/Rotax_912

   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.

3. Aeromot AMT-200 Super Ximango - Wikipedia

   en.wikipedia.org/wiki/Aeromot_AMT-200_Super_Ximango

   Built from glassfibre, the Super Ximango is a low-wing cantilever monoplane with conventional landing gear and a T-tail. Powered by front-mounted 80 hp Rotax 912A, it has an enclosed side-by-side cockpit for two.

4. Tecnam P96 Golf - Wikipedia

   en.wikipedia.org/wiki/Tecnam_P96_Golf

   Print/export Download as PDF; ... (98.6 hp) Rotax 912 ULS engine. [3] Specifications (P96 Golf 80) ... Service ceiling: 4,000 m (13,000 ft)

5. Ikarus C42 - Wikipedia

   en.wikipedia.org/wiki/Ikarus_C42

   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.

6. Rotax 912U - Wikipedia

   en.wikipedia.org/?title=Rotax_912U&redirect=no

   Print/export Download as PDF; Printable version; From Wikipedia, the free encyclopedia. Redirect page. Redirect to: Rotax 912; Retrieved from " ...

7. 3Xtrim 3X55 Trener - Wikipedia

   en.wikipedia.org/wiki/3Xtrim_3X55_Trener

   Download as PDF; Printable version; In other projects ... 1 × Rotax 912 4-cylinder air-cooled horizontally-opposed piston engine, ... Service ceiling: 4,000 m ...

8. Rans S-6 Coyote II - Wikipedia

   en.wikipedia.org/wiki/Rans_S-6_Coyote_II

   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]

9. Tecnam P2004 Bravo - Wikipedia

   en.wikipedia.org/wiki/Tecnam_P2004_Bravo

   Data from Jane's All the World's Aircraft 2010-11 General characteristics Crew: 1 Capacity: 3 pax Length: 6.61 m (21 ft 8 in) Wingspan: 8.6 m (28 ft 3 in) Height: 2.6 m (8 ft 6 in) Wing area: 11 m 2 (120 sq ft) Empty weight: 336 kg (741 lb) Max takeoff weight: 600 kg (1,323 lb) Max useful weight: 269 kg (593 lb) Powerplant: 1 × Rotax 912 ULS 4-cylinder air-cooled horizontally-opposed piston ...