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Inside of the tailcone of a Murphy Moose under construction, showing the semi-monocoque design. The Murphy Moose is a Canadian high-wing utility light aircraft produced in kit form by Murphy Aircraft of Chilliwack, British Columbia for amateur construction. The Moose can be purchased as a "quick-build" kit which comes partly pre-assembled. [1 ...
Producing 360 hp (268 kW), its design dates from the 1940s (Kotelnikov 2005), and is itself a development of the Ivchenko AI-14 engine. The engine has been used extensively by the Yakovlev and Sukhoi Design Bureaus. The M14P is also used in some experimental aircraft and kit designs such as the Murphy Moose, Radial Rocket, Pitts Model 12, and ...
The engine's propeller drive is via a Rotax type C or E style gearbox. The standard engine includes a muffler exhaust system and an intake silencer and filter, with an after muffler also available to further reduce engine noise. The standard starter is an electric starter. An integral alternating current generator produces 12 volts and 200 ...
The Murphy Yukon is a Canadian amateur-built aircraft, produced by Murphy Aircraft of Chilliwack, British Columbia, introduced at the AirVenture show in 2007. The aircraft is supplied as a kit for amateur construction. [1] [2] [3] The design is derived from the Murphy SR2500 Super Rebel and Murphy Moose. [1] [2] [3]
The JDM-8 has a conventional landing gear with a tailwheel and can be powered by a Rotax engine from 20-80HP. [2] An unusual feature is the upwards folding wing for storage and transportation. [1] [2] The fuselage of the JDM-8 is of semi-monocoque aluminum construction. The 5 US gal (19 L) fuel tank is located in front of the instrument panel.
The Lycoming O-540 is a family of air-cooled six-cylinder, horizontally opposed fixed-wing aircraft and helicopter engines of 541.5 cubic inches (8.9 L) displacement, manufactured by Lycoming Engines.
The primary difference between them is the engine. [9] RAF 2000 GTX SE Equipped with a 130 hp (97 kW) Subaru flat four carburetted engine RAF 2000 GTX SE FI Equipped with the same engine but it is fuel injected thus making it a little more economical RAF 2000 GTX SE FI 2.5 Equipped with a more powerful 165 hp (123 kW) Subaru fuel injected engine.
First run 1987. Flown in twin-engine MBB BO105 for demonstration only. [2] PW206A Maximum continuous power 550 shp (410 kW) [3] for use on the MD Explorer PW206B Maximum continuous power 431 shp (321 kW), [3] for use on the Eurocopter EC135 PW206B2 Maximum continuous power 431 shp (321 kW). [3] PW206C