RegNotify

EASA Regulations for Airbus A320

280 airworthiness directives and regulations affecting Airbus A320.

EASA AD 2025-0275

Aircraft Flight Manual / Normal Procedure Ground Engine Operation in Icing Condition — Amendment

The Aircraft Flight Manual / Normal Procedure Ground Engine Operation in Icing Condition — Amendment is an update applicable to AIRBUS S.A.S. aircraft models A319, A320, and A321. This amendment addresses procedures related to ground engine operation under icing conditions to ensure safe and efficient aircraft handling. It provides revised guidance to pilots and maintenance personnel for these specific Airbus aircraft types.

Dec 9, 2025
OtherFlight OpsMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2025-0254R1

Wing — Main Landing Gear Retraction Actuator Fitting — Inspection

EASA Airworthiness Directive 2025-0254R1 is an updated safety directive addressing inspection requirements for the main landing gear retraction actuator fitting on the rear spar of Airbus A320 and A321 aeroplanes. It applies to specific A320 and A321 models except those modified with certain Airbus service bulletins or modifications. The directive mandates detailed inspections and corrective actions to detect and repair fatigue cracks and corrosion that could compromise structural integrity.

Dec 5, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A320Airbus A321

EASA AD 2025-0268-E

Flight Controls — Elevator Aileron Computer — Replacement

EASA Airworthiness Directive 2025-0268-E is an emergency directive addressing the replacement of the Elevator Aileron Computer (ELAC) on Airbus A319, A320, and A321 aeroplanes. It applies to specific models and serial numbers equipped with the affected ELAC B L104. The directive mandates the installation of a serviceable ELAC B L103+ to ensure continued safe flight control operation.

Nov 28, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

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 SIB 2025-08

Failure of the Digital Radio and Audio Integrated Management System on the Airbus A320 NEO and A330 Family Aeroplanes

The EASA Safety Information Bulletin 2025-08 addresses failures of the Digital Radio and Audio Integrated Management System (DRAIMS) on Airbus A320 NEO and A330 family aeroplanes. These failures can cause partial or total loss of radio communications, transponder, and Airborne Collision Avoidance System (ACAS) functionality, impacting flight safety and Air Traffic Control operations. The bulletin raises awareness of these issues and provides information on temporary procedures and ongoing software modifications.

Oct 20, 2025
Safety Information BulletinFlight OpsSafety MgmtAirbus A320Airbus A330

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 2025-0193

Fuselage — Forward and Aft Upper Corner Bulk Cargo Door Section 16 and 17 — Inspection / Modification

EASA Airworthiness Directive 2025-0193 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A320 and A321 aeroplanes. It addresses inspection and modification requirements for the forward and aft upper corner bulk cargo door areas at fuselage sections 16 and 17. The directive applies specifically to certain A320 and A321 models operated or to be operated in Extended Service Goal (ESG) conditions.

Sep 8, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus 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