EASA Regulations for Pilatus Aircraft PC-24

19 airworthiness directives and regulations affecting Pilatus Aircraft PC-24.

EASA AD 2026-0008

Ice and Rain Protection — Windows, Windshields and Doors / Left-Hand Windshield Heating Solid State Relay — Modification / Replacement

EASA Airworthiness Directive 2026-0008 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus PC-24 aeroplanes with specific serial numbers and service bulletin configurations. It addresses an issue with the left-hand windshield heating solid state relay (SSR) that may fail during emergency conditions. The directive mandates modification and replacement of the affected SSR to ensure proper ice and rain protection on windows, windshields, and doors.

Jan 15, 2026

Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-24

EASA AD 2025-0211

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2025-0211 is an amendment concerning the time limits and maintenance checks in the Airworthiness Limitations Section for Pilatus PC-24 aeroplanes. This directive updates the mandatory maintenance tasks and life limits to ensure continued airworthiness of all PC-24 aircraft. It applies to all manufacturer serial numbers of the Pilatus PC-24 and references the latest approved Aircraft Maintenance Manual revisions.

Sep 26, 2025

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EASA AD 2024-0240

Aeroplane Flight Manual — Section Normal Procedures / Flight Director Lateral Offset — Amendment

EASA Airworthiness Directive 2024-0240 is an amendment concerning the Aeroplane Flight Manual Section Normal Procedures / Flight Director Lateral Offset for Pilatus PC-24 aeroplanes. It addresses an issue with inaccurate flight director calculations on approach caused by certain software versions. This directive applies to all PC-24 aircraft serial numbers and mandates updates to the flight manual procedures.

Dec 10, 2024

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EASA AD 2024-0181R1

Flight Controls — Rudder Trim Tab Installation / Threaded Bolts — Replacement

EASA Airworthiness Directive 2024-0181R1 is an updated regulatory requirement addressing the installation and replacement of rudder trim tab threaded bolts on Pilatus PC-24 aeroplanes, specifically those with manufacturer serial numbers 101 and above. The directive mandates replacing affected short rudder-trim control rod assemblies with serviceable parts to prevent potential failure of titanium bolts. This directive applies to the rudder trim tab installation and threaded bolts identified by specific part numbers.

Sep 24, 2024

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EASA AD 2023-0219-E

SUPERSEDED BY EASA AD 2024-0181

EASA Airworthiness Directive 2023-0219-E is an emergency directive affecting Pilatus PC-24 aeroplanes with manufacturer serial numbers 101 and up. It addresses the replacement and inspection of threaded titanium bolts, part number 527.20.24.489, installed on the rudder trim tab short control rods to prevent potential failure. The directive mandates inspections and periodic replacements to ensure continued airworthiness.

Dec 19, 2023

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EASA AD 2023-0038

Airplane Flight Manual — Section Normal Procedures / Electrical Burning Smell in Cabin — Amendment

The Airplane Flight Manual — Section Normal Procedures / Electrical Burning Smell in Cabin — Amendment applies to the PILATUS AIRCRAFT LTD PC-24 aircraft. This amendment updates the normal procedures section of the flight manual to address the occurrence of an electrical burning smell in the cabin. It provides revised guidance for flight crews to identify and respond to this specific electrical issue.

Feb 14, 2023

OtherFlight OpsSafety MgmtPilatus Aircraft PC-24PILATUS PC-24

EASA AD 2022-0207

SUPERSEDED BY EASA AD 2025-0211

EASA Airworthiness Directive 2022-0207 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Pilatus PC-24 aeroplanes. It mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the Pilatus PC-24 Aircraft Maintenance Manual Chapter 04-00-00, Document Number 02378 Issue 005 Revision 29. This directive ensures continued airworthiness by enforcing new and more restrictive maintenance requirements.

Oct 10, 2022

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EASA AD 2022-0122

Equipment / Furnishings — Stretcher Trolley Installation — Modification

EASA Airworthiness Directive 2022-0122 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning the installation of stretcher trolleys on Pilatus PC-24 aeroplanes, specifically those with manufacturer serial numbers 105, 106, 118, 169, and others modified by EASA STC 10067483 revision 2 or earlier. The directive addresses safety issues related to the mattress height below the left-hand Over-Wing Exit sill that could impede emergency evacuation. It mandates modifications to the stretcher trolley installation and updates to emergency procedures.

Jun 24, 2022

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EASA AD 2020-0252

Fuel — Fuel Drain System — Modification

EASA Airworthiness Directive 2020-0252 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus Aircraft Ltd PC-24 aeroplanes with manufacturer serial numbers 101 to 184 inclusive. The directive mandates modifications to the fuel drain system to address safety concerns. It specifically targets the fuel drain pipe routing and installation of a drain mast to improve system performance.

Nov 12, 2020

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EASA AD 2020-0202

SUPERSEDED BY EASA AD 2022-0207

EASA Airworthiness Directive 2020-0202 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Pilatus PC-24 aeroplanes. It mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the Pilatus PC-24 Aircraft Maintenance Manual Chapter 04-00-00. The directive ensures continued airworthiness by requiring operators to follow new and more restrictive maintenance tasks and life limits.

Sep 22, 2020

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EASA AD 2020-0200

Integrated Modular Avionics — Utility Management System — Software Update

EASA Airworthiness Directive 2020-0200 is an official safety directive addressing Pilatus PC-24 aeroplanes equipped with the Integrated Modular Avionics Utility Management System. It mandates a software update to the Utility Management System to resolve critical failures affecting environmental controls, oxygen mask deployment, and autopilot functions. This directive applies to all PC-24 aircraft with software version Build 7 or earlier installed.

Sep 21, 2020

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EASA AD 2020-0194

Powerplant — Engine Attachment Hardware — Inspection / Replacement

Powerplant — Engine Attachment Hardware — Inspection / Replacement is a regulatory document concerning the inspection and replacement procedures for engine attachment hardware on the PILATUS AIRCRAFT LTD PC-24 aircraft. It addresses maintenance requirements to ensure the integrity and safety of the engine mounting components. The document aims to provide clear guidance for operators and maintenance organizations on maintaining compliance and aircraft airworthiness.

Sep 8, 2020

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EASA AD 2020-0160

Air Conditioning — Cockpit and Cabin Evaporator Filters — Replacement

EASA Airworthiness Directive 2020-0160 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Pilatus PC-24 aeroplanes. It addresses the replacement of cockpit and cabin evaporator filter assemblies that were incorrectly installed during production and do not meet the required fire retardant standards. The directive mandates replacing these affected filters with serviceable parts to ensure continued airworthiness and safety.

Jul 16, 2020

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EASA AD 2020-0158

Air Vehicle Wiring — Electrical Harness Installation — Modification

EASA Airworthiness Directive 2020-0158 is an official regulatory document addressing electrical harness installation modifications on Pilatus Aircraft Ltd PC-24 aeroplanes, specifically those with manufacturer serial numbers 101 to 160 inclusive. The directive mandates changes to ensure compliance with approved design standards to maintain airworthiness and safety.

Jul 16, 2020

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EASA AD 2020-0096

Airplane Flight Manual — Section Normal Procedures / Electronic Circuit Breaker — Amendment

EASA Airworthiness Directive 2020-0096 is an amendment to the Airplane Flight Manual Section Normal Procedures concerning the Electronic Circuit Breaker for Pilatus PC-24 aeroplanes. This directive applies to all PC-24 aircraft serial numbers and mandates changes to the preflight check procedures to address a specific safety issue. The directive was issued by EASA to ensure continued airworthiness and safe operation of the affected aircraft.

Apr 29, 2020

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EASA AD 2020-0074

SUPERSEDED BY EASA AD 2020-0202

EASA Airworthiness Directive 2020-0074 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Pilatus PC-24 aeroplanes. It mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the Pilatus PC-24 Aircraft Maintenance Manual Chapter 4, including corrected certification maintenance requirements. This directive ensures the continued airworthiness and safety of the PC-24 fleet by addressing previously incorrect maintenance task implementations.

Mar 27, 2020

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EASA AD 2019-0293

Equipment and Furnishings — Emergency Exits / Grommets — Replacement

EASA Airworthiness Directive 2019-0293 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus Aircraft Ltd PC-24 aeroplanes. It addresses the replacement of vinyl grommets used in the emergency exits, which may become rigid after exposure to low temperatures. The directive applies to all PC-24 aircraft serial numbers and mandates replacing affected grommets to ensure emergency exits function properly during evacuation.

Dec 4, 2019

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EASA AD 2019-0240

Fuel — Saddle Clamps / Motive-Flow Fuel Pipes — Replacement / Alignment

EASA Airworthiness Directive 2019-0240 is an airworthiness directive issued by EASA affecting all Pilatus PC-24 aeroplanes. It addresses the replacement and alignment of flexible saddle clamps and motive-flow fuel pipes installed between frame 34 and 36 to prevent potential fuel leaks. The directive mandates the replacement of specific flexible saddle clamps with fixed saddle clamps to ensure continued airworthiness and safety.

Sep 25, 2019

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EASA AD 2019-0166

Ice and Rain Protection — Pitot and Static Electrical Wiring Splices — Replacement

EASA Airworthiness Directive 2019-0166 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus Aircraft Ltd PC-24 aeroplanes with manufacturer serial numbers 101 through 125. The directive addresses the replacement of specific pitot and static electrical wiring splices to prevent potential safety hazards. It mandates the replacement of affected electrical wiring splices with serviceable parts to ensure continued safe operation of the aircraft.

Jul 15, 2019

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