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EASA Regulations & Airworthiness Directives

Browse 245 EASA regulations with AI-powered summaries.

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EASA AD 2025-0258

Landing Gear — Nose Landing Gear Sliding Tube — Inspection

EASA Airworthiness Directive 2025-0258 is an airworthiness directive addressing the nose landing gear sliding tube on Airbus A318, A319, A320, and A321 aeroplanes. It mandates inspection of specific nose landing gear sliding tubes with part number 50-3752016-00 and certain serial numbers for overheat damage and cracks. The directive applies to all affected serial numbers listed and requires corrective actions if discrepancies are found.

Nov 21, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0253

SUPERSEDED BY EASA AD 2025-0274

EASA Airworthiness Directive 2025-0253 is issued for Airbus A318, A319, A320, and A321 aeroplanes concerning fire panels with specific part numbers. The directive addresses the risk of engine fire switch self-releasing, which can cause uncommanded in-flight engine shutdown. It mandates inspection, replacement, and repair of affected fire panels to ensure continued airworthiness.

Nov 14, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0248

Equipment / Furnishings — Overhead Stowage Compartments — Inspection / Repair

EASA Airworthiness Directive 2025-0248 is an airworthiness directive issued by the European Union Aviation Safety Agency addressing Airbus A318, A319, A320, and A321 aeroplanes equipped with ARIES overhead stowage compartments. The directive mandates inspection and repair of specific overhead stowage compartments to ensure their structural integrity. It applies to affected parts identified by certain part numbers and excludes aircraft with specific Airbus modifications embodied in production.

Nov 6, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0207R1

Fuselage — Seat Rail Connections Nylon Bushes — Replacement

EASA Airworthiness Directive 2025-0207R1 is an updated regulatory requirement addressing the replacement of nylon bushes with bronze bushes in the seat rail connections of Airbus A318, A319, A320, and A321 aircraft. This directive applies to all manufacturer serial numbers except those with Airbus modifications 152721 and 154725 incorporated. It aims to ensure continued airworthiness by mitigating risks associated with broken bolts in critical seat rail areas.

Oct 30, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0237

Equipment / Furnishings — 80 VU Rack Attachments — Inspection / Repair

EASA Airworthiness Directive 2025-0237 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes, including both Current Engine Option (CEO) and New Engine Option (NEO) models. The directive addresses inspection and repair requirements for the 80 VU rack attachments, which house critical flight control, communication, and radio-navigation computers. It mandates repetitive inspections and corrective actions to ensure the structural integrity of the 80 VU rack fittings and prevent potential system failures.

Oct 27, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0234

SUPERSEDED BY EASA AD 2025-0253

EASA Airworthiness Directive 2025-0234 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses issues with certain fire panels that may cause an uncommanded in-flight engine shutdown due to self-releasing engine fire switches. The directive mandates inspection and possible replacement of affected fire panels to ensure continued airworthiness and flight safety.

Oct 23, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0158R1

Landing Gear — Main Landing Gear Door Actuators — Inspections

EASA Airworthiness Directive 2025-0158R1 is a regulatory update addressing inspection and replacement requirements for main landing gear door actuators on Airbus A318, A319, A320, and A321 aircraft models. It targets actuators with part number 114122015 and specific serial numbers identified in Airbus Alert Operators Transmission A32N033-24 Revision 02. The directive aims to prevent landing gear extension issues caused by actuator assembly errors.

Sep 12, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0189

Fuselage — Centre Fuselage / Main Landing Gear Door Keel Beam Hinge and Actuator Fittings — Inspection

Fuselage — Centre Fuselage / Main Landing Gear Door Keel Beam Hinge and Actuator Fittings — Inspection is an airworthiness directive applicable to Airbus S.A.S. aircraft models A318, A319, A320, and A321. This document mandates inspections of the centre fuselage area focusing on the main landing gear door keel beam hinge and actuator fittings to ensure structural integrity and operational safety.

Sep 2, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0167R1

Landing Gear — Main Landing Gear Aft Pintle Pin — Replacement

EASA Airworthiness Directive 2025-0167R1 is an updated safety directive addressing the replacement of the Main Landing Gear (MLG) Aft Pintle Pin on Airbus A318, A319, A320, and A321 aircraft. The directive applies to specific part numbers D3215600500600 and D3215303000800 identified as affected due to manufacturing defects. It mandates replacement of these parts to prevent potential corrosion and cracking that could lead to landing gear collapse.

Sep 2, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0185

Wings — Pylon Spigot Fitting — Inspections

EASA Airworthiness Directive 2025-0185 is an airworthiness directive addressing inspections of the pylon spigot fitting on Airbus A318, A319, A320, and A321 aeroplanes. It targets slotted nuts with Part Number D57250182200 installed on these aircraft to detect severe corrosion that could compromise wing and pylon structural integrity. The directive mandates repetitive visual inspections and corrective actions as necessary to maintain safety.

Aug 26, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0166

Fuselage — Inner Cap and Frame Flange at Frame 68 Stringer 22 — Inspections

The document titled 'Fuselage — Inner Cap and Frame Flange at Frame 68 Stringer 22 — Inspections' is a regulatory directive applicable to Airbus S.A.S. aircraft models A318, A319, A320, and A321. It addresses inspection requirements focused on the fuselage structure, specifically the inner cap and frame flange at frame 68 stringer 22. The directive aims to ensure structural integrity and continued airworthiness of these aircraft types.

Jul 30, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0210R1

SUPERSEDED BY EASA AD 2025-0166

EASA Airworthiness Directive 2025-0166 supersedes the previous directive affecting Airbus S.A.S. aircraft models A318, A319, A320, and A321. This directive addresses updated safety and maintenance requirements for these aircraft types to ensure continued airworthiness. It provides revised instructions and compliance measures relevant to operators and maintenance organizations.

Jul 22, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 25-104

Fuselage — Centre Fuselage Forward Pressure Bulkhead — Inspection

EASA Airworthiness Directive Proposal 25-104 is a regulatory document addressing inspection requirements for the centre fuselage forward pressure bulkhead on Airbus A318, A319, A320, and A321 aeroplanes. It applies to various serial numbers except those with specific Airbus modifications embodied in production or service. The directive mandates repetitive rototest inspections of the forward pressure bulkhead hole C1 and provides an optional terminating modification.

Jul 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0118R1

Aircraft Flight Manual — Amendment / Communications — Digital Radio and Audio Integrating Management System — Modification

The document titled 'Aircraft Flight Manual — Amendment / Communications — Digital Radio and Audio Integrating Management System — Modification' applies to AIRBUS S.A.S. aircraft models A319, A320, and A321. It addresses updates to the Aircraft Flight Manual related to the integration and modification of the digital radio and audio management systems on these aircraft types. The amendment ensures that the flight manual reflects the latest system capabilities and operational procedures.

Jul 15, 2025
OtherFlight OpsMaintenanceAirbus A319Airbus A320Airbus A321

EASA AD 2021-0177R3

Hydraulic Power — Pylon / Engine Interface Rods — Inspection / Replacement

EASA Airworthiness Directive 2021-0177R3 is a regulatory update addressing inspection and replacement requirements for hydraulic power pylon/engine interface rods installed on Airbus A319, A320, and A321 aircraft models. The directive applies to specific part numbers of interface rods and mandates repetitive detailed inspections and corrective actions to prevent potential fuel or hydraulic leaks caused by rod end damage. It also introduces optional terminating actions through modification to enhance safety and compliance.

Jul 15, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2025-0133

Aircraft Flight Manual / Cabin Crew Operating Manual / Cabin Crew Data — Amendment

The Aircraft Flight Manual / Cabin Crew Operating Manual / Cabin Crew Data — Amendment applies to AIRBUS S.A.S. A318 and A319 aircraft types. This amendment updates the existing manuals and data relevant to flight operations and cabin crew procedures for these specific aircraft models. It ensures that the documentation reflects the latest operational and safety information.

Jun 25, 2025
OtherFlight OpsSafety MgmtAirbus A318Airbus A319

EASA AD 2017-0098R2

Fuselage — Potable Water and Waste Water Service Panels — Reinforcement

EASA Airworthiness Directive 2017-0098R2 addresses reinforcement requirements for the potable water and wastewater service panels on Airbus A319, A320, and A321 aeroplanes. This directive applies to various models except those already modified with Airbus production modifications 160055 or 160056, or certain corporate jet variants. It mandates structural reinforcements to prevent fatigue cracks that could compromise aircraft integrity.

Jun 25, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

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 2025-0096

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