(Pilatus) PC-6 Porter @·AIRCRAFTUBE

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    Pilatus PC-6 Porter
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  • PC-6 B2-H4 Turbo Porter PC-6 B2-H4 Turbo Porter
    PC-6 B2-H4 Turbo Porter
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  • Turbo Porter Turbo Porter
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  • PC-6 - V-618 Swiss Air_Force PC-6 - V-618 Swiss Air_Force
    PC-6 - V-618 Swiss Air_Force
  • PC-6 B1-H2 PC-6 B1-H2
    PC-6 B1-H2
  • PC-6 B2-H4 Turbo Porter PC-6 B2-H4 Turbo Porter
    PC-6 B2-H4 Turbo Porter
  • Pilatus PC-6 Porter Pilatus PC-6 Porter
    Pilatus PC-6 Porter
  • Pilatus PC-6 Porter Pilatus PC-6 Porter
    Pilatus PC-6 Porter
  • Fairchild AU-23A Peacemaker Fairchild AU-23A Peacemaker
    Fairchild AU-23A Peacemaker

Pilatus PC-6 Porter & Turbo Porter

The Pilatus PC-6 Porter is a single-engined Short Take-Off and Landing (STOL) utility aircraft designed by Pilatus Aircraft of Switzerland. First flown in 1959, the PC-6 has been built in both piston engine and turboprop powered versions, and has been built both by Pilatus and by Fairchild Hiller in the United States. It remains in production as of August 2011.

Design and development

The first prototype made its maiden flight on 4 May 1959 powered by a 254 kW piston engine. The first Turbo Porter, powered by a turboprop, flew in 1961. The Turbo Porter received an engine upgrade in 1963, which increased its power to its present value of 410 kW.

In the United States, the Porter was manufactured under license by Fairchild Hiller. In service with the U.S. Air Force, it received the designation AU-23A Peacemaker. In U.S. Army use, it was designated UV-20 Chiricahua.

Operational history

The PC-6 is famous in the aviation world for its Short Take-off and Landing (STOL) performance on almost any type of terrain - it can take-off within a distance of 195 metres (640 ft) and land within a distance of 130 metres (427 ft) while carrying a payload of 1,500 kg (3,300 lb) (The length of a soccer field is enough, Pilatus test pilots were able to land on not much more than 50 metres (164 ft) of space). Thanks to its STOL performance, the PC-6 holds the world record for highest landing by a fixed wing aircraft, at 5,750 metres (18,865 ft), on the Dhaulagiri glacier in Nepal.

Variants

  • PC-6 Porter.
  • PC-6B Turbo-Porter.
  • AU-23A Peacemaker: Armed version for the U.S. Air Force during the Vietnam War.
  • UV-20 Chiricahua: U.S. Army version.
  • PC-8 Twin Porter: Twin-engined version flown in 1967, but not subsequently developed.

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This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Pilatus PC-6 Porter of Wikipedia ( authors )

Specifications (B2-H4 Turbo Porter)

  • Passengers : Up to 10.
  • Length : 35 ft 9 in (or 10.9 m).
  • Height : 10 ft 5 in (or 3.18 m).
  • Wing span : 52 ft (or 15.85 m).
  • Wing area : 325 sq ft (or 30.19 m²).
  • Max take-off weight : 6,173 lb (or 2,800 kg).
  • Max landing weight : 5,864 lb (or 2,660 kg).
  • Max zero fuel weight : 5,291 lb (or 2,400 kg).
  • Dry Operating weight : 2,800 lb (or 1,270 kg).
  • Max payload : 2,227 lb (or 1,010 kg).
  • Fuel : 170 gal (or 644 l).
  • Max Speed : 155 mph (or 135 kts or 249 km/h).
  • Service ceiling : 25,000 ft (or 7,620 m).
  • Max range : 932 mi (or 810 nm or 1,500 km).
  • Engines : P&WC PT6A-27.
  • Power : 680 hp (or 507 kW).

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This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Pilatus PC-6 Porter of Wikipedia ( authors )
Pilatus PC-6 Porter : Your comments on this subject
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