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Pilatus PC-24

Swiss light business jet, operational since 2015, known for versatility across multiple deployments including charter services. Key figures: top speed 787 km/h, range 3,700 km, service ceiling 13,716 m, max takeoff weight 8,005 kg, unit price $12M, built 100. In service with 2 air forces as of 2026 — Qatar (2), France (1).

Max speed
787km/h
Range
3,700km
Produced
100units
Avg unit price
$12 million
Active worldwide
3+2 on order
Pilatus PC-24 military training aircraft side profile drawing
Side profile · Pilatus PC-24 · length 16.8 m
Technical SpecificationsVersion: PC-24
Length16.8 m (55.1 ft)
Wingspan17 m (55.8 ft)
Height5.3 m (17.4 ft)
Wing area30.9 m² (332.7 sqft)
Empty weight4,967 kg (10,950 lbs)
Max. takeoff weight8,005 kg (17,648 lbs)
Powerplant2 × turbofans Williams FJ44-4A 1,529 kgf each
PerformanceVersion: PC-24
Maximum speed787 km/h (489 mph)
Operational range3,700 km (2,299 mi)
Service ceiling13,716 m (45,000 ft)
Climb rate20.7 m/s (67.9 ft/s)
Takeoff distance820 m (2,690 ft)
Operators — 2026
ActiveOn order
All Operators
🇨🇭 Switzerland· 🇫🇷 France· 🇶🇦 Qatar

Description

Following the PC-12 single-engine turboprop program, Pilatus Aircraft initiated the PC-24 program in 2007 to develop a twin-engine jet with greater range and speed while retaining rough-field capability. The development was funded using existing company resources and the program was publicly mentioned in Pilatus' May 2011 annual report. The PC-24 was formally introduced on 21 May 2013, at the European Business Aviation Convention & Exhibition (EBACE) in Geneva. The first of three prototypes, P01, was rolled out on 1 August 2014. Prototype P01 was used for exploring the flight envelope, P02 for avionics and autopilot integration testing, and P03 served as a representative production model incorporating improvements. The first flight occurred on 11 May 2015, from Buochs Airport, Switzerland. The PC-24 received EASA and FAA type certification on 7 December 2017. The first customer delivery to PlaneSense was on 7 February 2018.

Design

The Pilatus PC-24 is a low-wing cantilever monoplane powered by two Williams FJ44-4A turbofans mounted on the rear fuselage sides. It features a T-tail and retractable tricycle landing gear. The wing incorporates a double-slotted flap system, contributing to a stall speed of 81 knots at maximum landing weight. The trailing link landing gear has a long stroke, and the dual-wheel main wheels operate at 70 psi pressure. The wing flaps feature replaceable, abradable surfaces. The high-mounted engines are positioned to minimize debris ingestion. Pilatus collaborated with Honeywell on the Advanced Cockpit Environment, utilizing the Honeywell Primus Epic 2 avionics system, designed to support single-pilot certification. The cabin accommodates up to ten passengers and one or two pilots and has three exits: a front left passenger door, overwing emergency exits, and a rear left cargo door.

The PC-24's primary function is passenger and cargo transport. Its design facilitates operation from short and rough airstrips. The aircraft has a maximum payload capacity of 1,406 kg (3,100 lb) and a large cargo door.

Operational History

The PC-24 has seen diverse operational use. The Royal Flying Doctor Service of Australia operates PC-24 aircraft as air ambulances, equipped with medical interiors. The Qatar Emiri Air Force operates two PC-24s for governmental transport. Sweden's Svenskt Ambulansflyg operates six PC-24s for medical evacuation.

Variants

Main Variants:

  • PC-24: The baseline production model, capable of operating from short and unpaved runways.

  • PC-24 medevac: Configured as an air ambulance, capable of accommodating three beds and medical equipment.

  • PC-24 (modified): Features updated designs with lighter seats, touchscreen-controlled avionics, and optional galleys.

  • PC-24 steep approach certified: Approved for steep approaches, including operations at a 5.5° approach angle.

  • PC-24 rough field operation certified: Certified for operations on grass, wet earth, and snow-covered surfaces.

Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 5 August 2026. Suggest a change

Frequently Asked Questions

What type of aircraft is the Pilatus PC-24?
The Pilatus PC-24 is a military training aircraft aircraft developed by Pilatus and entered service in 2018.
What is the maximum speed of the Pilatus PC-24?
The Pilatus PC-24 has a maximum speed of 787 km/h (489 mph).
What is the range of the Pilatus PC-24?
The Pilatus PC-24 has an operational range of 3,700 km (2,299 miles). This range can vary based on payload, altitude, and mission profile.
When did the Pilatus PC-24 first fly?
The Pilatus PC-24 made its first flight on May 11, 2015. It entered operational service in 2018.
How many Pilatus PC-24 have been built?
Approximately 100 units of the Pilatus PC-24 have been produced since it entered service in 2018.
Which countries operate the Pilatus PC-24?
The Pilatus PC-24 is operated by 2 countries with approximately 3 aircraft in active service. The largest operators include Qatar and France.
How much does a Pilatus PC-24 cost?
The Pilatus PC-24 has an estimated unit cost of approximately $12.0 million. Actual prices vary based on configuration, quantity ordered, and included support packages.
What is the service ceiling of the Pilatus PC-24?
The Pilatus PC-24 has a service ceiling of 13,716 meters (45,000 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
Compare This Aircraft
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Latest Data Updates
  1. AUG 52026 Updated Powerplant updated in a site-wide editorial pass
  2. JUL 272026 Updated Name updated
  3. APR 72026 Updated Sources and cross-references refreshed
  4. JAN 122026 Updated Range updated in a site-wide editorial pass