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EASA Regulations & Airworthiness Directives

Browse 274 EASA regulations with AI-powered summaries.

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EASA AD 2025-0120

Cabin Systems — Antenna Adapter Plate — Inspection

EASA Airworthiness Directive 2025-0120 is an airworthiness directive addressing inspection requirements for the antenna adapter plate and related parts installed on Airbus A319, A320, A321, A330, A350, and A380 aircraft models. The directive mandates repetitive general visual inspections of affected broadband antenna adapter plates to detect corrosion and cracks that could compromise aircraft safety. It applies to all manufacturer serial numbers of the specified Airbus models.

May 26, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321Airbus A330Airbus A350Airbus A380

EASA AD 2025-0111

Fuselage — Service Door Stop Fitting Hole — Inspection / Repair

EASA Airworthiness Directive 2025-0111 is issued for Airbus A318, A319, A320, and A321 aeroplanes, addressing inspection and repair requirements for the fuselage service door stop fitting holes at fuselage frames 16 and 20. This directive mandates repetitive rototest inspections and corrective actions to detect and repair cracks that could compromise structural integrity. It applies to both Current Engine Option (CEO) and New Engine Option (NEO) variants with specific applicability exceptions.

May 14, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0107

Fuselage — Frame 35 / Slidebox Junction — Inspection

EASA Airworthiness Directive 2025-0107 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 aeroplanes. The directive mandates inspections of the fuselage frame 35 and slidebox junction areas to detect cracks that could compromise structural integrity. It applies to all serial numbers except those with Airbus modifications 161341 or 161511 incorporated during production.

May 7, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321

EASA AD 2025-0096

Aircraft Flight Manual — Section Limitations — Amendment / Master Minimum Equipment List — Amendment / Pneumatic — High Pressure Bleed Valve — Replacement

The document titled 'Aircraft Flight Manual — Section Limitations — Amendment / Master Minimum Equipment List — Amendment / Pneumatic — High Pressure Bleed Valve — Replacement' applies to Airbus S.A.S. aircraft models A319, A320, and A321. It addresses updates to the Aircraft Flight Manual section limitations and the Master Minimum Equipment List, alongside the replacement procedure for the pneumatic high pressure bleed valve. These changes are specific to the Airbus A319/A320/A321 family.

Apr 28, 2025
OtherFlight OpsMaintenanceAirbus A319Airbus A320Airbus A321

EASA AD 2025-0083

Equipment/Furnishings — Cargo Bulkhead Frame 24A Vertical Members — Inspection

EASA Airworthiness Directive 2025-0083 is an official regulatory document addressing inspection requirements for the cargo bulkhead frame 24A vertical members on Airbus A318, A319, A320, and A321 aeroplanes. It mandates repetitive detailed inspections of the affected cargo bulkhead vertical member upper parts and fittings located behind the 80VU rack to ensure continued airworthiness. The directive applies to all manufacturer serial numbers of the specified Airbus models.

Apr 14, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0078

Fuselage — Centre Fuselage Skin and Forward Pressure Bulkhead — Inspection

EASA Airworthiness Directive 2025-0078 is an airworthiness directive addressing inspection requirements for the centre fuselage skin and forward pressure bulkhead on Airbus A318, A319, A320, and A321 aeroplanes. It applies to specific serial numbers and configurations, focusing on potential fatigue issues in critical fuselage areas. The directive mandates repetitive inspections and corrective actions to ensure structural integrity.

Apr 9, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0067

Fuselage — Centre Fuselage Frame Foot Joint — Inspection

EASA Airworthiness Directive 2025-0067 is an airworthiness directive addressing the Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes up to manufacturer serial number 09287 with Airbus modification 160286. It mandates inspections of the centre fuselage frame foot joint fastener holes to detect potential cracks that could affect structural integrity. The directive provides inspection intervals and corrective actions to maintain airworthiness.

Mar 28, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321

EASA AD 2025-0066

Fuselage — Pressure Panel at Centre Wing Box — Inspection

EASA Airworthiness Directive 2025-0066 is an airworthiness directive issued by EASA concerning Airbus A319, A320, and A321 aeroplanes with specific modifications embodied in production. It mandates inspections of the pressure panel at the centre wing box to detect potential fatigue-related cracks. The directive applies to various Airbus A319, A320, and A321 models up to manufacturer serial number 09287, excluding certain CEO aeroplanes with specific mods.

Mar 28, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2025-0068

SUPERSEDED BY EASA AD 2026-0017

EASA Airworthiness Directive 2025-0068 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses inspection and modification requirements for forward-facing galleys with specific part numbers to prevent damage-related failures that could compromise galley integrity during emergency landings. The directive mandates inspections and corrective actions to ensure galley safety and compliance.

Mar 28, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0041

Flight Controls — Trimmable Horizontal Stabilizer Actuator — Modification

The Flight Controls — Trimmable Horizontal Stabilizer Actuator — Modification is an airworthiness directive issued by AIRBUS S.A.S. affecting multiple aircraft types including the A318, A319, A320, A321, A330, and A340. This document addresses modifications related to the trimmable horizontal stabilizer actuator system to ensure continued safe flight control operations. It applies specifically to the listed Airbus aircraft models equipped with the affected actuator components.

Feb 18, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus A340

EASA AD 2025-0037

SUPERSEDED BY EASA AD 2025-0118

EASA Airworthiness Directive 2025-0037 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aeroplanes with specific Airbus modifications embodied. The directive addresses issues related to loss of synchronization between radio management panels, which can result in loss of radio communications, transponder functionality, and standby navigation. It requires amendments to the Aircraft Flight Manual to include procedures to manage these failures.

Feb 12, 2025
Airworthiness DirectiveFlight OpsSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2025-0031

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 3 — Certification Maintenance Requirements — Amendment

EASA Airworthiness Directive 2025-0031 is an amendment addressing the Time Limits and Maintenance Checks in the Airworthiness Limitations Section Part 3 for Airbus A318, A319, A320, and A321 aeroplanes. It applies to all manufacturer serial numbers of these models and mandates compliance with updated Certification Maintenance Requirements. The directive ensures continued airworthiness by requiring operators to follow the latest Airbus ALS Part 3 Revision 10 maintenance tasks and intervals.

Feb 10, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0032

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 4 — System Equipment Maintenance Requirements — Amendment

EASA Airworthiness Directive 2025-0032 is an amendment addressing the Time Limits and Maintenance Checks in the Airworthiness Limitations Section Part 4 for Airbus A318, A319, A320, and A321 aeroplanes. It applies to all manufacturer serial numbers of these models and mandates compliance with updated system equipment maintenance requirements. This directive ensures continued airworthiness by enforcing specific maintenance tasks and life limits.

Feb 10, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0033

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 5 — Fuel Airworthiness Limitations — Amendment

EASA Airworthiness Directive 2025-0033 is an amendment addressing time limits and maintenance checks in the Airworthiness Limitations Section Part 5 related to fuel airworthiness limitations for Airbus A318, A319, A320, and A321 aeroplanes. It applies to all manufacturer serial numbers of these models and mandates compliance with Airbus A318/A319/A320/A321 ALS Part 5 Revision 09. The directive ensures continued airworthiness by enforcing updated maintenance tasks and life limits for fuel system components.

Feb 10, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0247

SUPERSEDED BY EASA AD 2025-0041

EASA Airworthiness Directive 2024-0247 is issued for Airbus A318, A319, A320, A321, A330, and A340 aeroplanes. It addresses issues related to Trimmable Horizontal Stabilizer Actuators (THSA) that have erroneous accumulated life data in their release certificates. This directive applies to specific THSA parts identified by Collins Aerospace and Airbus documentation.

Dec 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus A340

EASA AD 2024-0231

SUPERSEDED BY EASA AD 2025-0083

EASA Airworthiness Directive 2024-0231 is an airworthiness directive applicable to Airbus A318, A319, A320, and A321 aeroplanes. It mandates repetitive detailed inspections of the cargo bulkhead frame 24A vertical members and female fittings located behind the 80VU rack to detect elongation and potential damage. The directive aims to prevent possible system failures caused by affected parts hitting the 80VU rack, which could lead to reduced control of the aircraft.

Dec 4, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0230

Wings — Bottom Wing Skin Panel 2 — Inspection

EASA Airworthiness Directive 2024-0230 is an airworthiness directive addressing inspection requirements for the bottom wing skin panel 2 on Airbus A319, A320, and A321 aeroplanes, including both Current Engine Option (CEO) and New Engine Option (NEO) models. It mandates detailed inspections of specific wing areas prone to fatigue cracking, particularly around the bottom wing skin manhole access panel number 2 between ribs 13 and 26. The directive applies to all manufacturer serial numbers of the affected aircraft models.

Dec 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2024-0201R1

Wings — Outer Wing Bottom Buttstrap — Inspections

EASA Airworthiness Directive 2024-0201R1 is an updated regulatory requirement addressing inspections of the outer wing bottom buttstrap on Airbus A319, A320, and A321 aeroplanes. It mandates repetitive special detailed inspections of the wing surface area between rib 19 and rib 21 forward of stringer 8 on both left and right sides to detect cracks that could compromise structural integrity. This directive applies to all manufacturer serial numbers of the specified Airbus models.

Dec 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2024-0217

Fuselage — Double Joggle Area at Frame 16 and Frame 20 — Inspection

EASA Airworthiness Directive 2024-0217 is an airworthiness directive addressing inspection requirements for the fuselage double joggle areas at frame 16 and frame 20 on Airbus A318, A319, A320, and A321 aeroplanes. It applies to various models of these aircraft except those with specific Airbus modifications or service bulletins embodied. The directive mandates special detailed inspections and corrective actions to detect and address cracks that could compromise fuselage structural integrity.

Nov 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321