Pilatus PC-24 airworthiness directives

• AD 2026-17-11

  Effective 2026-10-20

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by a report that a solid-state relay used in the left-hand windshield heating system may allow reverse current flow when in the OFF position.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency AD 2026-0008, dated January 15, 2026 (EASA AD 2026-0008).

• AD 2026-07-10

  Effective 2026-05-19

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by a revision to the airworthiness limitations section (ALS) of the existing aircraft maintenance manual (AMM) introducing new and more restrictive instructions and maintenance tasks.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, all serial numbers, certificated in any category.

• AD 2025-20-02

  Effective 2025-12-30

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by a report of an inaccurate flight director calculation on approach.

  This AD applies to Pilatus Aircraft Ltd Model PC-24 airplanes, certificated in any category.

• AD 2025-10-10

  Effective 2025-07-07

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by a determination that the titanium threaded bolts installed at the forward end of the short rudder trim tab actuating rods could be subject to unexpectedly high oscillating loads due to aerodynamic forces acting on the rudder trim tab.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0181R1, dated September 24, 2024 (EASA AD 2024-0181R1).

• AD 2023-26-05

  Effective 2024-01-03 · superseded or removed

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by a determination that the titanium threaded bolts installed at the forward end of the short rudder trim tab actuating rods could be subject to unexpectedly high oscillating loads due to aerodynamic forces acting on the rudder trim tab.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 Airplanes, as identified in European Union Aviation Safety Agency (EASA) Emergency AD 2023-0219-E, dated December 19, 2023 (EASA Emergency AD 2023-0219-E), certificated in any category.

• AD 2023-15-06

  Effective 2023-09-27

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, all serial numbers, certificated in any category.

• AD 2023-12-04

  Effective 2023-08-07

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by a report that an incorrect wiring arrangement was detected around the weather radar system.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, serial numbers 231 through 252 inclusive and serial numbers 254 and 255, certificated in any category.

• AD 2023-11-05

  Effective 2023-07-18 · superseded or removed

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, all serial numbers, certificated in any category.

• AD 2022-08-09

  Effective 2022-06-14

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by a failure of the dual ethernet communication channel on a dual-channel data concentration and processing unit, which triggered the opening of electronic circuit breakers that caused several unintended system activations.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, all serial numbers, certificated in any category.

• AD 2021-26-21

  Effective 2022-02-25

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, serial numbers 101 through 184, certificated in any category.

• AD 2021-11-12

  Effective 2021-07-15

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, serial numbers (S/Ns) 101 through 162, S/N 164, S/N 165, S/N 167, and S/N 168, certificated in any category.

• AD 2021-10-28

  Effective 2021-07-15 · superseded or removed

  Pilatus Aircraft Ltd. Airplanes

  The FAA is issuing this AD to prevent reduction in the structural integrity of the airframe and components, as well as an unrecognized failure of the manual pitch trim.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, all serial numbers, certificated in any category.

• AD 2021-06-01

  Effective 2021-05-04

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by a report that electronic circuit breakers (ECBs) were found in a locked state after maintenance, but before flight.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, all serial numbers, certificated in any category.

• AD 2021-04-03

  Effective 2021-03-30

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by a reported occurrence where, during production, cockpit and cabin evaporator filters produced with degraded fire retardant properties were installed on some Model PC- 24 airplanes.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, all serial numbers, certificated in any category, with any of the following evaporator filter assemblies installed, or if the part number (P/N) of the evaporator filter assembly is unknown: (1) Cockpit filter assembly P/N 959.90.20.291 (PC24EC-6068-1); (2)...

• AD 2021-01-05

  Effective 2021-03-30

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by electrical harness installations on some PC-24 airplanes in production that did not comply with the approved design.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, serial numbers 101 through 160 inclusive, certificated in any category.

• AD 2020-24-01

  Effective 2020-12-28

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.

  This airworthiness directive (AD) applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, serial numbers 101 through 125 inclusive, certificated in any category.

• AD 2020-22-17

  Effective 2020-12-14

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by an occurrence of movement of the aft fuel pipe within the coupling when system pressure was applied.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, all serial numbers, certificated in any category, with a flexible saddle clamp part number (P/N) 946.33.22.004 installed between frame 34 and 36.

• AD 2020-21-12

  Effective 2020-12-08

  Pilatus Aircraft Ltd. Airplanes

  This AD was prompted by a report that after exposure to low temperatures, the vinyl grommets that hold the upper panel assembly in position on the left-hand (LH) and right-hand (RH) emergency exits can become rigid.

  This AD applies to Pilatus Aircraft Ltd. Model PC-24 airplanes, all serial numbers, with an emergency exit grommet part number (P/N) 944.87.32.001 installed, certificated in any category.

Pilatus PC-24: price, specs and every tail

AD data from the Federal Register and the FAA. Data: Radar, FAA aircraft registry file of 2026-10-09.