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==Specifications (Moose M-14P)==
==Specifications (Moose M-14P)==
===General Characteristics===
===General characteristics===
* '''Crew:''' one pilot
* '''Crew:''' one pilot
* '''Capacity:''' 3-5 passengers
* '''Capacity:''' 3-5 passengers
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[[Category:Canadian civil utility aircraft 2000-2009]]
[[Category:Canadian civil utility aircraft 2000-2009]]
[[Category:Homebuilt aircraft]]
[[Category:Homebuilt aircraft]]


{{aero-2000s-stub}}
{{aero-2000s-stub}}

Revision as of 11:13, 6 March 2006

A radial-equipped Murphy Moose.

The Murphy Moose is a large high-wing utility monoplane designed to handle nearly any airport under any conditions. A homebuilt kit aircraft, the Moose can be purchased as a "quick-build" kit which comes partly pre-assembled. Similar in many respects to the de Havilland Canada DHC-2 Beaver, the Moose is cheaper both to buy and to operate.

Builders can choose whether to equip their aircraft with the 269 kW (360 hp) Russian M14P 9-cylinder radial, or the horizontally-opposed 187 kW (250 hp) Lycoming O-540. Both engines allow the Moose to take off in roughly 180 m (600 ft), although the radial is lighter, more powerful, and allows for higher endurance.

Specifications (Moose M-14P)

General characteristics

  • Crew: one pilot
  • Capacity: 3-5 passengers
  • Length: 8.43 m (25 ft 8 in)
  • Wingspan: 11.05 m (36 ft 3 in)
  • Height: m (ft in)
  • Wing area: 16.9 m² (182 ft²)
  • Empty: 816 kg (1,800 lb)
  • Loaded: 1,586 kg (3,500 lb)
  • Maximum takeoff: kg ( lb)
  • Powerplant: 1x supercharged Russian M14P 9-cylinder radial, 269 kW (360 hp)

Performance

  • Maximum speed: 109 km/h (175 mph)
  • Range: 1,840 km (1,150 miles)
  • Service ceiling: ft ( m)
  • Rate of climb: 458 m/min (1,500 ft/min)
  • Wing loading: 94 kg/m² (19 lb/ft²)
  • Power/Mass: 0.17 kW/kg (0.10 hp/lb)

Related development: Murphy Rebel

Comparable aircraft: De Havilland Canada DHC-2 Beaver - Max Holste M.H. 1521 Broussard