EASA Regulations for Pilatus Aircraft PC-12

3 airworthiness directives and regulatory documents affecting Pilatus Aircraft PC-12.

EASA AD 2025-0271

Central Maintenance System — Central Computer / Primus APEX Operational Software — Modification

EASA Airworthiness Directive 2025-0271 is an official regulatory document addressing Pilatus PC-12/47E aeroplanes with specific serial numbers. It mandates modifications to the Central Maintenance System's Primus APEX Operational Software to enhance flight safety. The directive applies specifically to PC-12/47E aircraft equipped with certain software builds.

Dec 2, 2025

Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-12

EASA AD 2025-0201

Aeroplane Flight Manual — Section Normal Procedures / Loss of Avionics — Engine Indications During Engine Start — Amendment

EASA Airworthiness Directive 2025-0201 is an amendment concerning Pilatus PC-12/47E aeroplanes with manufacturer serial numbers 1720 and 2001 to 2999 inclusive. It addresses an issue during engine start where battery voltage drops cause avionics shutdown, resulting in loss of engine parameter indications including Interstage Turbine Temperature (ITT). This directive mandates updates to the Aeroplane Flight Manual to enhance engine start procedures.

Sep 18, 2025

Airworthiness DirectiveFlight OpsSafety MgmtPilatus Aircraft PC-12

EASA AD 2025-0182

Equipment and Furnishings — Emergency Exit / Passenger Service Unit Trim Panel Installation — Modification

EASA Airworthiness Directive 2025-0182 is issued for Pilatus PC-12/47E aeroplanes with manufacturer serial numbers 2001 to 2999 inclusive. It addresses the installation of emergency exit and passenger service unit (PSU) trim panels, specifically those lacking dual lock fastener tape with part numbers 917.47.28.046 and 917.47.28.045. The directive mandates modification of these PSU trim panels to prevent interference with emergency exit door operation.

Aug 25, 2025

Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-12