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Pilatus PC-6A Turbo Porter

One of the most successful
aircraft of its class, the piston engined
Pilatus PC-6 Porter featured a strong and
reliable airframe, excellent short take off
and landing (STOL) capability and excellent
load-carrying capacity. A total of 50 Porters
were built before production changed to the
turboprop-powered PC-6A-H1, first flown on
May 2nd 1961. Turbo Porters have enjoyed
great success around the world and have been
operated by various air arms, including those
of Australia, Switzerland, Dubai, Indonesia, Iran,
Oman and Sudan.
A single PC-6A Turbo Porter arrived
in Israel in 1962 and was used by the 100th light transport
squadron at Sde-Dov for utility, liaison and ambulance
duties. Another Turbo Porter was procured in 1968 after
a crash disabled the first example. The Turbo Porter
was retired from service in 1973 and is currently on
display at the IAF Museum in Hatzerim.
Specification: Pilatus PC-6A-H1
Type: STOL utility transport.
Powerplant: one Turbomeca Astazou
IIE turboprop engine.
Performance: max speed - 280km/h,
cruising speed - 213km/h, max range - 926km, service
ceiling - 7,620m.
Weights: empty - 1,270kg, max take
off - 2,800kg.
Dimensions: length - 11.00m, height
- 3.20m, span - 15.87m.
Armament: none.
Source: The
Israeli Air Force - IDF/AF [Unofficial] |
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