enow.com Web Search

Search results

  1. Results from the WOW.Com Content Network
  2. Cessna 210 Centurion - Wikipedia

    en.wikipedia.org/wiki/Cessna_210_Centurion

    Data from Janes' All The World's Aircraft 1982-83 General characteristics Crew: One Capacity: Five passengers Length: 28 ft 2 in (8.59 m) Wingspan: 36 ft 9 in (11.20 m) Height: 9 ft 8 in (2.95 m) Wing area: 175 sq ft (16.3 m 2) Empty weight: 2,303 lb (1,045 kg) Gross weight: 4,000 lb (1,814 kg) Fuel capacity: 87 US gal (72 imp gal; 330 L) (usable capacity) Powerplant: 1 × Continental Motors ...

  3. Continental IO-520 - Wikipedia

    en.wikipedia.org/wiki/Continental_IO-520

    The IO-520 series engines normally produce 285 to 310 horsepower (210 to 230 kW) and are used in numerous aircraft such as certain models of the Bellanca Viking 300 and Super Viking, the Beech Bonanza and Baron, and Cessna 185- 206-, 210-, 310-, and 400-series aircraft. The IO-520 remained in production in 2019. [1]

  4. List of Cessna models - Wikipedia

    en.wikipedia.org/wiki/List_of_Cessna_models

    Single piston engine utility helicopter Cessna CH-4: Single piston engine utility helicopter Cessna CR-1: 1 Single piston engine monoplane racer Cessna CR-2: 1930 1 Single piston engine monoplane racer Cessna CR-3: 1933 1 Single piston engine monoplane racer Cessna CW-6: 1928 Single piston engine monoplane utility airplane Cessna C-34 Airmaster ...

  5. SMA SR305-230 - Wikipedia

    en.wikipedia.org/wiki/SMA_SR305-230

    The SMA SR305-230 is an air/oil-cooled, horizontally opposed, four-cylinder, four-stroke, diesel piston aircraft engine producing 170 kW (227 hp). The engine is manufactured by SMA Engines, and is currently the only product of this French company. The engine is offered as a conversion package for the Cessna 182.

  6. Cessna X210 - Wikipedia

    en.wikipedia.org/wiki/Cessna_X210

    Work on a potential replacement for the Cessna 195 began in 1949. The resulting in the Model X210 was similar to the 195, sharing the latter's basic design and conventional landing gear configuration, but was powered by a 240 hp (179 kW) Continental O-470 flat-six engine mounted on a redesigned forward fuselage. [2]

  7. Honeywell HTF7000 - Wikipedia

    en.wikipedia.org/wiki/Honeywell_HTF7000

    Average fuel consumption is about 950 lb. per hour for a 7,765 lbf engine on a G280, to be compared to 875 lb. per hour for a 4,420 lbf TFE731 on a G150. [3] More than 3.5 million flight hours have been logged till October 2017, and the 2,000th engine should be delivered in 2018. [2] Honeywell maintenance program is $447 for two engines per ...

  8. List of aircraft engines - Wikipedia

    en.wikipedia.org/wiki/List_of_aircraft_engines

    3W-210; 3W-220; A. Abadal (Francisco Serramalera Abadal) 1] Abadal Y-12 350/400 hp ... Rocket engines [14] Armstrong Siddeley Alpha; Armstrong Siddeley Beta;

  9. Rolls-Royce AE 3007 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_AE_3007

    In September 1990, it was selected for the Cessna Citation X. [1] The engine was first ground tested in mid-1991. [3] On August 21, 1992, the engine had its first test flight on a Cessna Citation VII testbed aircraft. [4] In 1995, Rolls-Royce bought Allison Engine Company and the engine had its first flight on the EMB-145.