(Pilatus) PC-12 @·AIRCRAFTUBE

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Pilatus PC-12

Design and development

Pilatus announced the development of the PC-12 at the annual convention of the National Business Aviation Association (NBAA) in October 1989. The two prototypes were completed on 1 May 1991, with the first flight taking place on May 31, 1991. Certification of the type was originally planned for mid-1991 but a redesign of the wings (increase of wing span and addition of winglets to ensure performance guarantees were met) delayed this. Swiss certification finally took place on 30 March 1994, and U.S. Federal Aviation Administration approval followed on 15 July 1994.

As with many other Pilatus aircraft, the PC-12 is powered by a single Pratt & Whitney Canada PT6 turboprop engine (the PT6A-67B). It is certified for single-pilot IFR operations, though operators may choose to utilize a second flight crew member. Pilatus offers the PC-12 in a standard nine-seat airliner form, in a four-passenger seat/freight Combi version, and as a six-seat corporate transport with an option for a seven-seat by adding a three-seat bench in place of seats five and six. A pure freighter model is under consideration.

The PC-12M (Multipurpose) is based on the PC-12, but equipped with a more powerful electrical generation system that enables addition of additional power-consuming equipment. This enables the PC-12M to perform missions such as flight inspection, air ambulance, parachutist dropping, aerial photography, and aerial surveillance. This version is marketed in the United States as the PC-12 Spectre paramilitary special missions platform.

Pilatus announced the PC-12NG (Next Generation) at the 2006 NBAA meeting in Orlando, and officially launched it during the NBAA 2007 in Atlanta. The NG features a more powerful Pratt & Whitney PT6A-67P engine with better climb performance and an increase in maximum cruise speed to 280 kts TAS. The NG also features a Honeywell APEX glass cockpit. The revised cockpit includes automatic pressurization control as well as cursor controlled inputs to the navigation system. The PC-12 NG winglets have also been modified from the original version.

Operational history

Commercial, corporate, and private use

Most PC-12s are used as corporate transports, but recent regulatory changes in Australia, Brazil, Canada, and the United States have cleared single engine turboprops such as the PC-12 for regional passenger transport operations in those countries. This opens a new market for the PC-12 as a regional airliner that would replace older twin piston-engined aircraft.

PlaneSense, a New Hampshire-based fractional ownership company, is the largest fractional operator of PC-12s in the world, operating 34 PC-12s.

In 1994, the Royal Flying Doctor Service of Australia was the launch customer of the PC-12 and now operates more than 36 PC-12 aircraft across Australia.

U.S. Air Force operations

The U-28A is the United States Air Force variant of the PC-12 for intra-theater support of special operations forces. The 319th Special Operations Squadron is stationed at Hurlburt Field, Florida at the headquarters of the Air Force Special Operations Command. The 34th Special Operations Squadron (SOS) was activated on 9 April 2010 as the second U-28A unit at Hurlburt Field. Both squadrons operate as part of the 1st Special Operations Wing/ 1st Special Operations Group (SOG) at Hurlburt Field. The U-28A / Pilatus PC-12 is also operated by the 318th Special Operations Squadron as part of the 27th Special Operations Wing at Cannon Air Force Base, New Mexico.

Variants

  • PC-12/41 : Original production variant certified in 1994 has a Pratt & Whitney Canada PT6A-67B engine. Most, if not all of the /41s have been upgraded to /45s.
  • PC-12/45 : Certified in 1996 has a Pratt & Whitney Canada PT6A-67B engine, maximum takeoff weight increased to 4,500 kg (9,921 lb).
  • PC-12/47 : Certified in 2005 has a Pratt & Whitney Canada PT6A-67B engine, maximum takeoff weight increased to 4,740 kg (10,450 lb).
  • PC-12/47E : Variant certified in 2008 has upgraded avionics and a Pratt & Whitney Canada PT6A-67P engine. Sometimes known by its trade name PC-12 NG (Next Generation).
  • PC-12M Spectre : Paramilitary special missions platform marketed in the United States, originally called "Eagle".
  • U-28A : United States military designation for the PC-12.

Accidents and incidents

On 22 March 2009, a PC-12/45 with the aircraft registration number N128CM, owned by the Eagle Cap Leasing of Enterprise, Oregon, crashed on approach to the Bert Mooney Airport in Butte, Montana. The aircraft had departed from Oroville, California, and diverted from the original destination of Bozeman, Montana for unknown reasons. The NTSB recovered a computer memory chip from the aircraft that contained essential aircraft and engine performance data. From it, they concluded that icing in the fuel system had prevented the normally balanced flow of fuel from the wings. The pilot had delayed a precautionary landing until one wing was full of fuel and the other was empty, and then lost control of the PC-12 while maneuvering to land. All 14 people on board were killed: one pilot and 13 passengers, seven of whom were young children.

On 8 February 2011 at 4:31, a Pilatus PC-12, operated by Majuba Aviation, disappeared from Air Traffic Control's radar. On Wednesday 9 February, wreckage believed to be that of the missing plane was found just off the shore of Robberg Nature Reserve, close to Plettenberg Bay. Both crew members and all seven passengers, including Italtile CEO Gianpaolo Ravazzotti and Prima Bella MD Salvatore Di Bella, were killed in the accident.

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This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Pilatus PC-12 of Wikipedia ( authors )

Specifications

  • Passengers : 9.
  • Length : 47 ft 2 in (14.38 m).
  • Height : 13 ft 11 in (4.24 m).
  • Wing span : 53 ft 2 in (16.21 m).
  • Wing area : 278 sq ft (25.83 m²).
  • Max take-off weight : 9,921 lb (4,500 kg).
  • Max landing weight : 9,921 lb (4,500 kg).
  • Max zero fuel weight : 9,039 lb (4,100 kg).
  • Dry Operating weight : 5,930 lb (2,690 kg).
  • Max payload : 3,109 lb (1,410 kg).
  • Fuel : 400 gal (1,514 l).
  • Cruising Speed : 276 mph (240 kts - 444 km/h).
  • Max Speed : 295 mph (256 kts - 475 km/h).
  • Service ceiling : 30,000 ft (9,144 m).
  • Max range : 1,590 mi (1,382 nm - 2,559 km).
  • Engine : Pratt & Whitney Canada PT6A-67B.
  • Power : 1,200 hp (895 kW).

— — — = = — — —

This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Pilatus PC-12 of Wikipedia ( authors )
Pilatus PC-12 : Your comments on this subject
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