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The Pilatus PC-12 is a pressurized, single-engined, turboprop aircraft manufactured by Pilatus Aircraft of Stans, Switzerland since 1991. It was designed as a high-performance utility aircraft that incorporates a large aft cargo door in addition to the main passenger door.
The prototype PC-12 was flown on 31 May 1991. [9] On 30 March 1994, the Swiss Federal Office of Civil Aviation issued the type certificate for the PC-12; [26] The first PC-12 Eagle surveillance aircraft was built in 1995, further developments led to the PC-12 Spectre; amongst other customers, it was adopted by the United States Air Force as the ...
Pilatus PC-7 Turbo Trainer: PT6A-25C: 783: 750: Embraer EMB 312 Tucano Pilatus PC-7 Mk.II M PZL-130 Orlik / TC-II Turbo-Orlik PT6A-27: 715: 680: Beechcraft Model 99A, B99 De Havilland Canada DHC-6 Twin Otter 300 Harbin Y-12 (CATIC / HAIG) Embraer EMB 110 Bandeirante Let L-410 Turbolet Pilatus PC-6/B Turbo-Porter: PT6A-28: 715: 680: Embraer EMB ...
Data from Textron General characteristics Crew: 1-2 Capacity: 7-9 passengers/1,100 lb (500 kg) full fuel payload Length: 48 ft 9 in (14.86 m) Wingspan: 54 ft 3 in (16.54 m) Height: 15 ft 2 in (4.62 m) Cabin height: 58 in (150 cm) Cabin width: 63 in (160 cm) Cabin length: 16 ft 9 in (5.11 m) Powerplant: 1 × General Electric Catalyst turboprop, 1,300 hp (970 kW) Propellers: 5-bladed McCauley, 8 ...
[12] [8] It was initially deployed on a 20-hour flight test program to contrast computer simulations against data from the prototype's real-world flight performance; during each of these flights, telemetry data was gathered inflight by a specially-equipped Pilatus PC-12 chase plane. [3]
Accidents and incidents involving the Pilatus PC-12 (2 P) O. Lists of Pilatus aircraft operators (1 P) Pages in category "Pilatus aircraft"
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 2,820 lbf (12.5 kN) thrust FJ44-3A was introduced in 2004. In 2005, a new low end version, the FJ44-1AP, was introduced, with a 1,965 lbf (8.74 kN) takeoff thrust. Released in 2007 was the new 3,600 lbf (16 kN) thrust FJ44-4. In 2010 this engine was in use on the Cessna CJ4, and since 2018 also on the new Pilatus PC-24.