Ellison-Mahon Gweduck

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Gweduck
Gweduck.jpg
Gweduck on display at EAA Airshow
Role 4-passenger amphibious aircraft
National origin USA
Manufacturer Ellison-Mahon Aircraft
Designer Ben Ellison, Brian Mahon
First flight 2 May 2009
Number built 1

The Ellison-Mahon Gweduck is a modern, twin engine amphibious aircraft, built from composites and closely resembling the Grumman Widgeon. It was designed and is built in the United States and was first flown in 2009.

Gweduck instrument panel

Design and development[edit]

The Gweduck is a re-engined "re-creation" in modern composite materials of the early 1940s Grumman Widgeon. The name can also be written Geoduck and is not named for a bird, but a large clam. Though it is broadly similar to the Widgeon and follows its cantilever high-wing monoplane, twin engined, cruciform tail and tailwheel undercarriage layout, it has more powerful engines, retractable floats, more cabin windows and larger dimensions.[1][2]

The Gweduck's structure is formed from glass and carbon fibre. Its high wings are trapezoidal in plan, fitted with externally balanced ailerons and Fowler flaps. Each wing has a float mounted below it on a single, wide chord strut which rotates through 90° after take-off to place the float at the wing tip. A pair of 300 hp (224 kW) Lycoming IO-540 six cylinder horizontally opposed engines are mounted forward of the wing leading edge with their thrust lines above the upper surface. The Gweduck has a single step hull, with the pilots' cabin just forward of the wing leading edge; behind them, the passenger cabin has four windows on each side. Tail surfaces are straight edged, the tailplane trapezoidal and the fin leading edge swept, with a horn balanced rudder and externally mass balanced elevators. On land the Gweduck uses a conventional undercarriage, with mainwheels that retract but remain exposed in the fuselage sides and a tailwheel that retracts behind doors in the extreme rear fuselage.[1]

The first flight was on 2 May 2009 from Lake Washington. By June 2010, 200 flying hours had been logged.[3]

Specifications[edit]

Data from Jane's All the World's Aircraft 2010/12[1]

General characteristics

  • Crew: 2 pilots
  • Capacity: 4 passengers
  • Length: 34 ft 5 in (10.49 m)
  • Wingspan: 48 ft 0 in (14.63 m) floats down
  • Height: 10 ft 6 in (3.20 m) propellers "Y"
  • Wing area: 295.0 sq ft (27.41 m2)
  • Aspect ratio: 7.8
  • Airfoil: GA35U-A315
  • Empty weight: 4,200 lb (1,905 kg) prototype
  • Max takeoff weight: 5,999 lb (2,721 kg)
  • Fuel capacity: 167 Imp gal (200 US gal; 758 L)
  • Powerplant: 2 × Lycoming IO-540-M1B5 flat-six piston, 300 hp (220 kW) each
  • Propellers: 3-bladed MT-propeller MTV-9-B-C-F-R(M)/CFR213-59

Performance

  • Cruising speed: 155 mph; 135 kn (250 km/h) at 65% power at 915 m (3000 ft)
  • Wing loading: 20.3 lb/sq ft (99.3 kg/m2) maximum
  • Power/mass: 164 W/kg (0.10 hp/lb)

References[edit]

  1. ^ a b c Jackson, Paul (2011). Jane's All the World's Aircraft 2011-12. Coulsdon, Surrey: IHS Jane's. pp. 735–6. ISBN 978-0-7106-2955-5. 
  2. ^ Simpson, Rod (2001). Airlife's World Aircraft. Shrewsbury: Airlife Publishing Ltd. p. 262. ISBN 1 84037 115 3. 
  3. ^ "Project news". Retrieved 19 May 2012. 

External links[edit]