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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 — France (2), Qatar (2).

Max speed
787km/h
Range
3,700km
Produced
100units
Avg unit price
$12 million
Active worldwide
4+20 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
Similar Aircraft
Pilatus PC-24 vs

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. The French Navy received the first of three leased PC-24s in May 2026, replacing the Falcon 10 Mer for instrument-flight training and liaison, and Spain has selected the type to replace the Cessna Citations of its Air and Space Force and naval air arm.

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 6 October 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 in service with 2 countries, with approximately 4 aircraft in active service. The largest operators include France and Qatar. 2 more have it on order. 3 countries have operated it in all.
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.
Latest Data Updates
  1. OCT 62026 Updated French Navy service entry and Spanish selection added
  2. AUG 52026 Updated Powerplant updated in a site-wide editorial pass
  3. JUL 272026 Updated Name updated
  4. APR 72026 Updated Sources and cross-references refreshed
  5. JAN 122026 Updated Range updated in a site-wide editorial pass