Pilatus PC-24: Your Own Pilatus Jet
The PC-24 is quite simply unique. It is the first ever business jet to combine the versatility of a turboprop with the cabin size of a medium light jet and the performance of a light jet. The PC-24 is so special that it doesn’t fit into existing categories of business jet. That is why Pilatus had to create a category of its own: the Super Versatile Jet (SVJ) category. The PC-24 was developed from the outset for off-road use. Its outstanding performance on short country airfields opens up an incredible amount of flexibility and new possibilities.
Attributes
Land where no business jet has ever landed before
Approximately 10,650 airfields the world over can be approached by aircraft which can operate on runways with a length of 954 meters (3,130 feet). If the aircraft only requires a runway length of 893 metres (2,930 feet), that number increases by another 880 airports. In both cases, these figures refer to airfields with paved runways. If all airfields with a runway length of at least 893 meters are added together (2,930 feet), whether with paved or unpaved runways, the number rises to almost 20,000 airfields!
With the PC-24 you therefore have access to almost twice as many airfields around the world in comparison with the jets currently on the market. This means that you can fly closer to your destination, as you are able to take off and land on small airfields with shorter runways. In this way, you avoid the usual administrative work at large airports, and reduce the transfers on the ground to the absolute minimum.
Cabin
Flying on cloud nine
Only the highest quality materials are used to create an interior that is able to fulfil the highest of expectations. Every single element has been carefully selected to offer each passenger an incomparable flying experience. The spacious cabin with its flat floor provides sufficient space for all passengers, air crew and baggage.
Technical specifications
Performance
| Standard | Metric | |
| Balanced field length (MTOW, sea level, dry paved runway) |
2,930 ft | 893 m |
| Landing distance over 50 ft (15 m) obstacle (MLW, sea level, dry paved runway) |
2,375 ft | 724 m |
| Max. rate of climb (MTOW, sea level, 200 KCAS) | 4,070 ft/min | 20.70 m/s |
| Max. cruise speed (flight level 280) | 440 KTAS | 815 km/h |
| Range with 4 passengers (800 lb payload, LRC, NBAA IFR reserves of 100 nm + 30 min VFR)* |
2,000 nm | 3,704 km |
| Max. certified altitude | 45,000 ft | 13,716 m |
| Stall speed (landing configuration, MLW) | 82 KIAS | 151 km/h |
Weights
| Basic operating weight* | 11,720 lb | 5,316 kg |
| Max. take-off weight | 18,300 lb | 8,300 kg |
| Max. landing weight | 16,900 lb | 7,665 kg |
| Max. payload* | 2,500 lb | 1,134 kg |
| Max. payload with full fuel* | 715 lb | 324 kg |
*Executive configuration (6 seat), incl. one pilot
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