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In 2013, Pilatus created a new overseas entity, Pilatus Aircraft Industry (China) Co., Ltd, to manufacture both the PC-6 and PC-12 aircraft in Chongqing, China; this company was run as a joint partnership between Pilatus and Beijing Tian Xing Jian Yu Science Co., Ltd. [36] In 2014, the majority of PC-6s delivered that year were to Chinese ...
This is an accepted version of this page This is the latest accepted revision, reviewed on 18 December 2024. Classified advertisements website Craigslist Inc. Logo used since 1995 Screenshot of the main page on January 26, 2008 Type of business Private Type of site Classifieds, forums Available in English, French, German, Dutch, Spanish, Italian, Portuguese Founded 1995 ; 29 years ago (1995 ...
The aircraft's fuselage was of fabric-covered steel-tube construction; the wing, which was braced to the fuselage by steel V-struts, was of wooden construction. [ 1 ] [ 2 ] It was powered by a 190 hp (140 kW) Lycoming GO-435 engine (later replaced by a 240 hp (180 kW) GO-435-C2a) driving a two-bladed variable-pitch propeller. [ 3 ]
The Pilatus PC-21 is an advanced single-engine trainer aircraft; it is often referred to by Pilatus as being the "Twenty-first Century Trainer". [3] [4] The type can be applied for various training capacities, including basic flying training, advanced flight training, full mission management training, and embedded simulation/emulation.
The aircraft are painted in the bold red, white and blue scheme, with a large "R" symbol on the tail. The RAAF has since adopted this scheme (minus the "R") for all its PC-9 trainers, except for the PC-9s at ARDU and FAC, [ clarification needed ] which allows an aircraft to be swapped into or out of the team to equalise fleet airframe hours by ...
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The Pilatus PC-9 is a single-engine, low-wing tandem-seat turboprop training aircraft designed and manufactured by Pilatus Aircraft of Switzerland.. Developed as a more powerful evolution of the preceding Pilatus PC-7, the PC-9 features an enlarged cockpit and a ventral airbrake while possessing only a low level of structural commonality with its predecessor.
The aircraft would have a total length of 13.50 m, a height of 6.08 meters and a wingspan of 19 meters. The machine should be able to transport 16 people, or nearly 2 tons of cargo. It had been equipped with a fixed landing gear and two Garrett TPE-331 or Pratt & Whitney PT6A-27 turboprop engines.