The Pilatus PC-9 is a single-engine, low-wing, tandem-seat turboprop trainer designed and built by Pilatus Aircraft of Switzerland. It was developed as a more powerful evolution of the PC-7, with an enlarged cockpit, stepped ejection seats and a ventral airbrake, and has little structural commonality with its predecessor. The prototype first flew on 7 May 1984 and type certification came in September 1985. The PC-9 was designed to serve as both an initial and an advanced trainer without an intermediate type. More than 250 have been built in five variants, including Australian licence production by Hawker de Havilland and the Beechcraft T-6A Texan II developed with Beechcraft for the United States JPATS competition.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) EnginePratt & Whitney Canada PT6A-62 2 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Pilatus PC-9 (Wikipedia)
Of Make
Source Pilatus PC-9 (Wikipedia)
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Manufactured By
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designed and manufactured by Pilatus Aircraft of Switzerland
Originated In
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designed and manufactured by Pilatus Aircraft of Switzerland
Sources
1. Pilatus PC-9 (Wikipedia)
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designed and manufactured by Pilatus Aircraft of Switzerland
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designed and manufactured by Pilatus Aircraft of Switzerland
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The Pilatus PC-9 is a single-engine, low-wing tandem-seat turboprop training aircraft
Of Make: Pilatus Aircraft, Lead, maker
designed and manufactured by Pilatus Aircraft of Switzerland
In Group: Military Trainer Aircraft, Lead, role
designed and manufactured by Pilatus Aircraft of Switzerland
Exemplifies: Aviation, Lead, mode
designed and manufactured by Pilatus Aircraft of Switzerland
View the Source2. Aviastar: Pilatus PC-9, U-23 Peacemaker
AviastarPage text, first flight
The first PC-9 flew on May 7, 1984.
Specification, empty weight
Empty weight 1620 kg 3572 lb
Specification, take-off weight
Take-off weight 3200 kg 7055 lb
Specification, engine
ENGINE 1 x Pratt & Whitney Canada PT6A-62 turboprop, 857kW
Specification, engine type
ENGINE 1 x Pratt & Whitney Canada PT6A-62 turboprop, 857kW
Specification, maximum speed
Max. speed 556 km/h 345 mph
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