EASA AD 2025-0182
Equipment and Furnishings — Emergency Exit / Passenger Service Unit Trim Panel Installation — Modification
Summary
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.
What Changed
This new airworthiness directive introduces a mandatory modification for affected PSU trim panels installed above emergency exit doors on certain Pilatus PC-12/47E aircraft. It requires inspection and modification or replacement of the affected parts to ensure the emergency exit door can be opened from inside the aircraft without obstruction. The directive also prohibits installation of affected parts on any aeroplane after the effective date.
Why It Matters
This directive is critical for aviation professionals as it addresses a safety risk where the emergency exit door could be blocked by incorrectly installed PSU trim panels, potentially preventing evacuation during emergencies. Operators and maintenance organizations must ensure compliance to maintain airworthiness and passenger safety. Non-compliance could lead to regulatory penalties and increased risk during emergency situations.
What To Do
Operators of Pilatus PC-12/47E aeroplanes with serial numbers 2001 to 2999 must inspect and modify affected PSU trim panels within 12 months of 8 September 2025, following Pilatus Service Bulletin 25-059 instructions. Alternatively, replacing the affected part with a compliant part is acceptable. Installation of affected parts is prohibited after the effective date unless modified as required.