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Most commercial jetliners have a service (or certified) ceiling of under 45,000 ft (13,700 m) [3] and some business jets about 51,000 ft (15.5 km; 9.7 mi). [4] Before its retirement, the Concorde supersonic transport (SST) (as well as the Tupolev Tu-144 before it was retired) routinely flew at 60,000 ft (18.3 km; 11.4 mi).
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.
A PC-21 landing at RAF Fairford, England, 2010. In the Armament Program 2006, the Swiss Parliament approved an initial purchase of the PC-21 for the Swiss Air Force.By April 2008, four PC-21 have been accepted by the Swiss Air Force following the passing of acceptance trials, and flight operations were set to start in July that year. [19]
The Pilatus PC-24 is a light business jet produced by Pilatus Aircraft of Switzerland. Following the success of the PC-12 single engine turboprop, work on the twin engine jet began in 2007 for greater range and speed, keeping the rough-field capability.
The Citation V (Model 560) is a development of the Citation S/II, retaining the supercritical airfoil and swept wing roots of that aircraft, but with a 1.5 ft (46 cm) fuselage stretch and recontoured interior for increased passenger space. [2]
There is a long-standing convention within WikiProject:Aircraft that specifications for US, Canadian and UK aircraft (for the UK periods differ - e.g. RAF aircraft until post war used mph, FAA aircraft operated in knots) should be given as English units first, and all others as SI units first.
A sectional chart is a two-sided chart created from a Lambert Conformal Conic Projection [1] with two defined standard parallels. The scale is 1:500,000, with a contour interval of 500 feet. The size of each sectional is designed to be "arm's width" when completely unfolded.
The aircraft is predominantly made from wood, with some steel parts and doped aircraft fabric. Its 19.50 ft (5.9 m) span wing employs a Wainfan 16% symmetrical airfoil and has a wing area of 75.55 sq ft (7.019 m 2). The wing has almost full-span ailerons that produce rolls of 360° per second. The wing has no flaps. Other features include a low ...