Product Overview
Based on feedback from PC-12 customers, the PC-24 features increased range, speed, and short runway capability. As compared to other business jets in this class, the Pilatus PC-24 achieves this goal with less than 3,000 feet of takeoff distance and 2,120 feet of landing distance.
As of August 2023, 17% of Pilatus PC-24 ownership comes from the pre-owned market, the other 83% from new. 6.3% of those are currently for sale, with the majority (85%) under an exclusive broker agreement. For those on the market, the average sale time is eight months.
Brief History
The Pilatus PC-24 received FAA and EASA type certifications in December 2017 and is certified for single pilot operation. The introduction of the PC-24 was the first entry by Pilatus into the Business Jet Market.
Worldwide Appeal
There are 206 Pilatus PC-24 jets in operation worldwide. The majority of those (177) are wholly owned with five in shared ownership, and 24 in fractional ownership. 6% are currently leased. North America has the largest percentage of wholly owned Pilatus PC-24 aircraft (56%), followed by Europe (29%). Jetfly Aviation SA, Luxembourg owns the largest fleet of Pilatus PC-24 aircraft with 12.
Highlights
Performance
Two Williams International FJ44-4A-QPM engines power the Pilatus PC-24 each offering 3,420lbst of thrust and using a combined 160 gallons per hour (GPH). The range of the PC-24 is 2,030 nm operating under NBAA rules using IFR 4 passengers with available fuel.
Interior
The cabin volume for the Pilatus PC-24 is 501 cubic feet. Typical configuration features 8 passenger seats and 1 crew seat.
Speed
| Maximum Cruise Speed: | 438 kts |
811 km/hr
|
||
| Long-range Speed: |
358 kts
|
663 km/hr
|
Airfield Performance
| Takeoff distance: | 2,930 ft (983 m) |
(SL, ISA, MTOW)
|
||
| Landing distance: | 2,120 ft (646 m) |
(SL, ISA, MLW)
|
Operating Altitude
| Maximum operating altitude: | 45,000 ft (13,716 m) |
Noise Level (EPNdB)
| Takeoff: |
92.o
|
|---|---|
| Approach: | 78.2 |
| Lateral: | 90.4 |
Weights
| A. | Maximum ramp weight: | 18,400 lb (8,346 kg) | ||
| B. | Maximum takeoff weight: | 18,300 lb (8,301 kg) | ||
| C. | Maximum landing weight: | 16,900 lb (7,666 kg) | ||
| D. | Maximum zero fuel weight: | 14,220 lb (6,450 kg) | ||
| E. | Standard basic operating weight: | 11,720 lb (5,316 kg) |
ADS-B OUT
It is assumed that the Pilatus PC-24 that are based in the US have ADS-B Out installed.
Derivative Models
None
Range Report
Contact Us at +1 919 941 8400 or [email protected] to request a custom range report including detailed aircraft comparisons.
Aircraft For Sale
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