EASA Regulations for Pilatus PC-24

17 airworthiness directives and regulations affecting Pilatus PC-24.

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New ADs and bulletins for Pilatus PC-24, summarized like the ones below, every Monday.

EASA AD 2026-0149

Jul 28, 2026

Integrated Modular Avionics – Primus APEX DFZ Build 6.0 Software – Modification

EASA Airworthiness Directive 2026-0149 is an airworthiness directive affecting Pilatus PC-24 aeroplanes with manufacturer serial numbers 101 to 337 and 501 to 600. It mandates a software modification to the Integrated Modular Avionics Primus APEX DFZ system, updating from Build 5.3 or earlier to Build 6.0. This directive ensures continued safe operation by addressing flight director calculation errors during approach.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA PAD 26-075

Jun 18, 2026

Integrated Modular Avionics – Primus APEX DFZ Build 6.0 Software – Modification

EASA Airworthiness Directive PAD No. 26-075 is a proposed directive addressing the Primus APEX DFZ Build 6.0 software modification for Pilatus PC-24 aeroplanes, specifically those with manufacturer serial numbers 101 to 337 and 501 to 600. This directive targets the integrated modular avionics system to correct flight director calculation errors on affected aircraft. It applies to PC-24 aircraft equipped with earlier software versions and mandates software updates and flight manual amendments.

Proposed AD
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2024-0181R1

Sep 24, 2024

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.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2023-0219-E

Dec 19, 2023

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

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.

Airworthiness DirectiveSuperseded
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2022-0249

Dec 14, 2022

Navigation — Weather Radar System Redundant Wiring — Modification

EASA Airworthiness Directive 2022-0249 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus PC-24 aeroplanes with manufacturer serial numbers 231 to 252 inclusive, as well as MSN 254 and 255. The directive addresses a wiring issue in the weather radar system that could impact critical avionics components during a lightning strike. It mandates a modification to the redundant wiring of the weather radar system to ensure continued safe operation.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2022-0207

Oct 10, 2022

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

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.

Airworthiness DirectiveSuperseded
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2022-0122

Jun 24, 2022

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.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2020-0252

Nov 12, 2020

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.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2020-0202

Sep 22, 2020

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

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.

Airworthiness DirectiveSuperseded
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2020-0200

Sep 21, 2020

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.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2020-0160

Jul 16, 2020

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.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2020-0158

Jul 16, 2020

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.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2020-0096

Apr 29, 2020

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.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2020-0074

Mar 27, 2020

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

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.

Airworthiness DirectiveSuperseded
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2019-0293

Dec 4, 2019

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.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2019-0240

Sep 25, 2019

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.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24

EASA AD 2019-0166

Jul 15, 2019

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.

Airworthiness Directive
  • Pilatus Aircraft PC-24
  • Pilatus PC-24