EASA Regulations & Airworthiness Directives

Browse 284 EASA regulations with AI-powered summaries.

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EASA AD 2026-0028

Feb 11, 2026

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 — Damage Tolerant Airworthiness Limitation Items — Amendment

EASA Airworthiness Directive 2026-0028 is an amendment concerning the Airbus A318, A319, A320, and A321 aircraft family. It addresses updates to the Airworthiness Limitations Section Part 2, specifically the Damage Tolerant Airworthiness Limitation Items. This directive mandates compliance with revised maintenance tasks and intervals to ensure continued airworthiness of these aircraft models.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA PAD 26-022

Feb 4, 2026

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 1, Safe Life Airworthiness Limitation Items — Amendment

EASA Airworthiness Directive 26-022 is a proposed amendment addressing the Time Limits and Maintenance Checks in the Airworthiness Limitations Section Part 1 for Airbus A318, A319, A320, and A321 aeroplanes. It applies to all manufacturer serial numbers of these models and updates the safe life airworthiness limitation items. The directive ensures continued airworthiness by mandating compliance with the latest Airbus ALS Part 1, Revision 11 issue 2.

Proposed AD
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA PAD 26-023

Feb 4, 2026

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

EASA Airworthiness Directive 26-023 is a proposed amendment affecting Airbus A318, A319, A320, and A321 aeroplanes. It updates the Airworthiness Limitations Section Part 3, Certification Maintenance Requirements, introducing new and more restrictive maintenance tasks and limitations. This directive applies to all manufacturer serial numbers of the specified Airbus A320 family models.

Proposed AD
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA PAD 26-024

Feb 4, 2026

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

EASA Airworthiness Directive 26-024 is a proposed amendment addressing time limits and maintenance checks for Airbus A318, A319, A320, and A321 aeroplanes. It updates the Airworthiness Limitations Section Part 4 concerning System Equipment Maintenance Requirements. This directive applies to all manufacturer serial numbers of the specified Airbus A320 family models.

Proposed AD
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA PAD 26-025

Feb 4, 2026

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

EASA Airworthiness Directive 26-025 is a proposed amendment affecting Airbus A318, A319, A320, and A321 aeroplanes. It updates the Airworthiness Limitations Section Part 5 related to Fuel Airworthiness Limitations, applying to all manufacturer serial numbers of these aircraft models. The directive mandates compliance with the latest Airbus ALS Part 5, Revision 10, to ensure continued airworthiness.

Proposed AD
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2026-0017

Jan 23, 2026

Equipment / Furnishings — Galley — Inspection

EASA Airworthiness Directive 2026-0017 is an inspection directive addressing forward-facing galley equipment on Airbus A318, A319, A320, and A321 aeroplanes. It mandates inspections and corrective actions for specific galley part numbers to prevent damage such as delamination and corrosion that could lead to trolley detachment during emergency landings. The directive applies to all serial numbers of the affected aircraft models.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA PAD 25-196

Dec 17, 2025

Fuselage — Forward Fuselage Skin Panels — Inspection

EASA Airworthiness Directive Proposal 25-196 is a regulatory document addressing inspection requirements for forward fuselage skin panels on specific Airbus A319, A320, and A321 aircraft models. It applies to certain serial numbers and targets panels with potential thickness deviations identified by an Airbus supplier. The directive mandates inspections and possible corrective actions to ensure structural integrity.

Proposed AD
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0274

Dec 11, 2025

[Correction] Fire Protection — Fire Panel — Inspection

The document titled '[Correction] Fire Protection — Fire Panel — Inspection' is a correction notice related to the Airbus S.A.S. aircraft types A318, A319, A320, and A321. It addresses inspection procedures for the fire protection fire panel systems on these specific Airbus models. The correction aims to clarify or amend previous instructions to ensure proper maintenance and safety compliance.

Correction
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0275

Dec 9, 2025

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.

Other
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0254R1

Dec 5, 2025

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.

Airworthiness Directive
  • Airbus A320
  • Airbus A321

EASA AD 2025-0268-E

Nov 28, 2025

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.

Airworthiness DirectiveSuperseded
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0258

Nov 21, 2025

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.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0253

Nov 14, 2025

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.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0248

Nov 6, 2025

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.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0207R1

Oct 30, 2025

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.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0237

Oct 27, 2025

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.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0234

Oct 23, 2025

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.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0151R2

Sep 12, 2025

Equipment / Furnishings — Escape Slide Inflation Reservoir Regulator Valve — Inspection / Modification

EASA Airworthiness Directive 2025-0151R2 is an updated regulatory document addressing safety concerns related to the escape slide inflation reservoir regulator valve on Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes. It mandates inspection, modification, and replacement of affected reservoirs and orifice fittings to prevent uncommanded deployment of escape slides during flight. The directive applies to all manufacturer serial numbers of the specified aircraft models.

Airworthiness Directive
  • Airbus A321

EASA AD 2025-0158R1

Sep 12, 2025

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.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0193

Sep 8, 2025

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.

Airworthiness Directive
  • Airbus A320
  • Airbus A321