Pilatus PC-12
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Image:US Immigration and Customs Enforcement aircraft.jpg The Pilatus PC-12 is a single-engine turboprop passenger and cargo aircraft manufactured by Pilatus Aircraft of Switzerland. The main market for the aircraft is corporate transport and regional airliner operators.
As with many other Pilatus aircraft, the PC-12 is powered by a single Pratt & Whitney Canada PT6A-67B turboprop engine. It has a flight crew of one or two pilots, although it is certified for single pilot IFR operations.
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History
Pilatus announced the development of the PC-12 at the National Business Aircraft Association's annual convention in October 1989. The first flight of the first of two prototypes took place on 31 May 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 FAA approval followed on 15 July 1994.
Versions
The PC-12 is available in the following configurations:
- Nine-seat standard passenger airliner.
- Six-seat executive corporate transport.
- Four-seat passenger/cargo combination.
- All-cargo transport.
There is also a PC-12M (the M stands for multipurpose) version, based on the basic PC-12, but equipped with a more powerful electrical generation system in order to enable the integration of additional power-consuming equipment. This enables the PC-12M to perform special mission tasks 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 Eagle military special missions platform.
Users
Most PC-12s are currently 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 nations. This has opened up a new potential market for the PC-12 as a regional airliner, in order to replace older twin piston-engined aircraft.
More than 600 PC-12s have been sold as of Feb. 2006.
Military Users
- South Africa.
Specifications (PC-12)
Note: These statistics are for the standard configuration (9 passenger PC-12). There is also a 6 passenger Executive version, and a cargo version.
General characteristics
- Crew: one or two pilots
- Capacity: 9 passengers standard, 6 executive
- Length: 14.40 m (47 ft 3 in)
- Wingspan: 16.23 m (53 ft 3 in)
- Height: 4.26 m (14 ft 0 in)
- Tail wingspan: 5.20 m (17 ft 1 in)
- Wing area: 25.81 m² (277.8 ft²)
- Wing loading: 174.3 kg/m² (35.7 lb/ft²)
- Empty: 2,661 kg (5,867 lb)
- Loaded: 4,500 kg (9,921 lb)
- Maximum takeoff: 4,500 kg (9,920 lb)
- Maximum landing: 4,500 kg (9,920 lb)
- Maximum payload: 1,400 kg (2,973 lb)
- Maximum payload full fuel: 539 kg (1,189 lb)
- Powerplant: 1x Pratt & Whitney Canada PT6A-67B turboprop, 895 kW (1,200 shp)
- Propeller: Hartzell HC - E4A - 3D/E10477K – 4 blade aluminum
- Propeller diameter: 2.67 m (8 ft 9 in)
- Propeller RPM: 1,700 rpm constant speed
Performance
- Maximum speed: 500 km/h (312.5 mph) (270 KTAS)
- Stall speed, landing configuration: 120 km/h (74.8 mph) (65 KCAS)
- Range 0 passenger: 4,149 km (2,593 mi) (2,239 NM)
- Range 9 passenger: 2,804 km (1,753 mi) (1,513 NM)
- Service ceiling: 9,150 m (30,000 ft)
- Rate of climb: 512 m/min (1,680 ft/min)at sea level
- Power loading: 3.7 kg/shp (8.2 lb/shp)
- Takeoff distance over 15 m (50 ft) obstacle: 701 m (2,300 ft)
- Takeoff distance ground roll: 450 m (1,475 ft)
- Landing distance over 15 m (50 ft) obsacle: 558 m (1,830 ft)
- Landing distance ground roll: 228 m (945 ft)
Related content
Related development:
Comparable aircraft:
Designation sequence: P-2 - P-3 - PC-6 - PC-7 - PC-9 - PC-11 - PC-12 - PC-21
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