Trisha Shetty (Editor)

Nash Petrel

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Wingspan
  
8.94 m

First flight
  
November 8, 1980

Length
  
6.22 m

Nash Petrel httpsuploadwikimediaorgwikipediacommonsthu

Manufacturers
  
Nash Aircraft, Procter Aircraft Associates

The Nash Petrel also known as the Procter Petrel is a two-seat aerobatic or glider tug aircraft. It was designed for amateur production by Procter Aircraft Associates of Camberley, Surrey, England. By the time the aircraft first flew, Procter had changed ownership and had been renamed Nash Aircraft Ltd.

Contents

Development

Based on the earlier Mitchell-Procter Kittiwake design, the Petrel is an all-metal low-wing cantilever monoplane of conventional design powered by a 130 hp Rolls-Royce Continental O-240-A piston engine. Only two aircraft were built, the prototype registered G-AXSF and one built by apprentices at the British Aircraft Corporation factory at Preston in 1973, registered G-BACA. G-BACA had a serious fault with the landing gear and only flew 15 hours before being grounded. The prototype still exists but without a current certificate of airworthiness. It is presently fitted with a Lycoming O-360-A3A engine.

Specifications

Data from Jane's All The World's Aircraft 1982–83

General characteristics

  • Crew: 2
  • Length: 6.22 m (20 ft 5 in)
  • Wingspan: 8.94 m (29 ft 4 in)
  • Height: 2.23 m (7 ft 4 in)
  • Wing area: 12.63 m2 (135.9 sq ft)
  • Aspect ratio: 6.6:1
  • Airfoil: NACA 3415
  • Empty weight: 540 kg (1,190 lb)
  • Max takeoff weight: 762 kg (1,680 lb)
  • Fuel capacity: 104.5 L (27.6 US gal; 23.0 imp gal)
  • Powerplant: 1 × Avco Lycoming O-320-D2A air-cooled flat-four engine, 89 kW (119 hp)
  • Performance

  • Maximum speed: 209 km/h; 113 kn (130 mph)
  • Cruise speed: 195 km/h; 105 kn (121 mph)
  • Stall speed: 74 km/h; 46 mph (40 kn) (flaps down)
  • Rate of climb: 5.6 m/s (1,100 ft/min)
  • References

    Nash Petrel Wikipedia