Pilatus PC-12 | |
|---|---|
| Maa | Sveitsi |
| Rooli | Matkustaja- ja rahtilentokoneet |
| Ensimmäinen lento | 31. toukokuuta 1991 |
| Rakennettu | 2000+ |
Nniiden Pilatus PC-12 on paineistettu, yksimoottorinen potkuriturbiinikone, jonka on valmistanut Pilatus Aircraft of Stans, Sveitsi vuodesta 1991. Se on suunniteltu korkean suorituskyvyn hyötylentokoneeksi, jossa on suuri perän rahtiovi päämatkustajan oven lisäksi
Lähde: Pilatus PC-12 Wikipediassa
| Pilatus PC-12 Kävele ympäriinsä | |
|---|---|
| Valokuvaaja | Vladimir Jakubov |
| Lokalisointi | Tyynenmeren rannikon unelmakoneet 2010 |
| Valokuvat | 59 |
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Odota, etsitään Pilatus P-12 puolestasi ...
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General Characteristics
The Pilatus PC-12 is a highly successful, single-engine turboprop aircraft known for its versatility, reliability, and low operating costs. It is used globally for corporate transport, air ambulance, cargo, and regional airline services, often operating from short, unpaved runways.
| Property | Typical Value (PC-12 NGX Variant) |
|---|---|
| Rooli | Utility/Executive Transport, Air Ambulance |
| Valmistaja | Pilatus Aircraft Ltd (Stans, Switzerland) |
| First Flight | May 31, 1991 |
| miehistö | 1 or 2 pilots |
| Kapasiteetti | Up to 9 passengers |
| Siipiväli | 16.23 m (53 ft 3 in) |
| Max Takeoff Weight | 4,740 kg (10,450 lb) |
Design and Powerplant
- Engine: One Pratt & Whitney Canada PT6E-67XP turboprop engine (NGX model).
- Power Output: Flat-rated to 895 kW (1,200 shp). The PT6 is famous for its reliability and power-to-weight ratio.
- Construction: Conventional low-wing cantilever monoplane with retractable tricycle landing gear.
- Fuselage Feature: The PC-12 is instantly recognizable for its large, aft cargo door (1.35 m x 1.32 m), which facilitates the loading of oversized cargo, stretchers, or palletized goods.
- Cockpit (NGX): Features the modern Honeywell Epic 2.0 integrated avionics system, offering a digital, glass cockpit experience with advanced safety features.
Performance and Safety
- Maximum Cruise Speed: 537 km/h (290 knots) at 20,000 ft.
- Maximum Range: Approximately 3,339 km (1,803 nautical miles) with reserves.
- Service Ceiling: 9,144 m (30,000 ft).
- Short Field Capability: Renowned for excellent Short Take-off and Landing (STOL) performance, requiring less than 800 meters (2,600 ft) to clear a 50 ft obstacle.
- Single-Engine Safety: The PC-12’s single-engine configuration is offset by the PT6’s historically low in-flight shutdown rate, making it a very safe aircraft, often operating under single-engine IFR rules comparable to twins.
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