EASA Regulations & Airworthiness Directives

Browse 253 EASA regulations with AI-powered summaries.

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EASA PAD 26-123

Oct 13, 2026

Fuselage – Forward Fuselage Skin Panels – Inspection

EASA Airworthiness Directive PAD No. 26-123 is a proposed directive addressing inspection requirements for forward fuselage skin panels on Airbus A319, A320, and A321 aircraft models. It applies to specific serial numbers and panel part numbers identified in the directive. The directive focuses on detecting potential structural integrity issues caused by production quality deviations and certain repair conditions affecting the fuselage panels.

Proposed AD
  • Airbus A319153N
  • Airbus A320251N252N271N
  • Airbus A321251NX252NX271NX272NX

EASA PAD 26-113

Sep 23, 2026

Engine – High Pressure Turbine Front Seal – Inspection

EASA Airworthiness Directive Proposal 26-113 is a regulatory document addressing the inspection of the High Pressure Turbine (HPT) front seal on CFM INTERNATIONAL S.A. CFM56-5B and CFM56-7B engine models. These engines are commonly installed on Airbus A318, A319, A320, and A321 series aircraft, as well as Boeing 737-600, 737-700, 737-800, 737-900, and 737-900ER series aircraft. The directive proposes a one-time on-wing borescope inspection to detect potential misalignment and cracks in the HPT front seal to prevent uncontained part release and possible engine or aircraft damage.

Proposed AD
  • CFM International CFM56-5B
  • CFM International CFM56-7B
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Boeing 737

EASA AD 2026-0182R1

Sep 22, 2026

Stabilizers – Elevators – Inspections / Replacement

EASA Airworthiness Directive 2026-0182R1 is an updated regulatory requirement addressing inspections and replacement of elevators on Airbus A319 and A321 NEO models. It applies to specific elevator part numbers that lack Airbus modification 35515, which could lead to structural integrity issues due to water ingress and disbonding. The directive mandates thermographic inspections and replacement of affected elevator parts to ensure continued airworthiness.

Airworthiness Directive
  • Airbus A319
  • Airbus A321
  • Airbus A319 NEO
  • Airbus A321 NEO

EASA AD 2026-0182

Sep 21, 2026

Stabilizers – Elevators – Inspections / Replacement

EASA Airworthiness Directive 2026-0182 is issued for Airbus A319 and A321 NEO aeroplanes addressing inspections and replacement of elevators without Airbus modification 35515. This directive targets elevators with specific part numbers that were incorrectly listed as eligible for installation, potentially affecting the structural integrity of the elevator. It mandates thermographic inspections and replacement of affected elevator parts to ensure continued airworthiness.

Airworthiness DirectiveSuperseded
  • Airbus A319
  • Airbus A321
  • Airbus A319 NEO
  • Airbus A321 NEO

EASA AD 2026-0176

Sep 11, 2026

Electrical Systems Installation – Battery Retaining Rods – Identification / Replacement

EASA Airworthiness Directive 2026-0176 is an aviation safety regulation addressing battery retaining rods on Airbus A318, A319, A320, and A321 aeroplanes. It applies to specific battery retaining rods with Part Number D9241023700000 manufactured by SUDAERO or unknown suppliers, focusing on identification, inspection, and replacement to prevent battery displacement. The directive mandates inspections and corrective actions to ensure continued airworthiness of affected aircraft.

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

EASA PAD 26-102

Sep 9, 2026

Fuselage – Cockpit Floor Structure – Inspections

EASA Airworthiness Directive Proposal 26-102 is a proposed regulation targeting Airbus A318, A319, A320, and A321 aeroplanes. It mandates inspections of the cockpit floor structure, specifically between cross beams Frame 8 and Frame 12, to detect mechanical damage such as cracks and missing fasteners. The directive aims to maintain structural integrity by addressing damage beyond corrosion in this critical fuselage area.

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

EASA PAD 26-093

Jul 31, 2026

Electrical Systems Installation – Battery Retaining Rods – Identification / Replacement

EASA Airworthiness Directive PAD No. 26-093 is a proposed directive addressing battery retaining rods on Airbus A318, A319, A320, and A321 aeroplanes. It focuses on identifying and replacing affected battery retaining rods with part number D9241023700000 that may have quality defects leading to potential battery displacement and electrical system failures. The directive applies to all manufacturer serial numbers of the specified Airbus models, including the A321-251NX and A321-271NX variants.

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

EASA AD 2026-0142

Jul 20, 2026

Wings – Main Landing Gear Support Rib 5 – Inspections

EASA Airworthiness Directive 2026-0142 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus A318, A319, A320, and A321 aeroplanes with specific manufacturer serial numbers. The directive mandates inspections of the main landing gear support rib 5 due to identified quality issues that could lead to fatigue damage and potential structural failure. It applies to affected parts listed by part and serial numbers in the directive's appendix.

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

EASA AD 2026-0136

Jul 10, 2026

Flights Controls – Trimmable Horizontal Stabilizer Actuator Ballscrew Lower Splines – Inspection / Replacement

EASA Airworthiness Directive 2026-0136 is an airworthiness directive addressing corrosion issues in the trimmable horizontal stabilizer actuator (THSA) ballscrew lower splines on Airbus A318, A319, A320, and A321 aircraft. It applies to specific THSA part numbers that may suffer corrosion leading to potential loss of control of the airplane. The directive mandates inspections and possible replacement of affected parts to ensure continued airworthiness.

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

EASA AD 2026-0134

Jul 8, 2026

Flight Controls – Elevator Aileron Computer – Replacement

EASA Airworthiness Directive 2026-0134 is an airworthiness directive addressing the replacement of the Elevator Aileron Computer (ELAC) on Airbus A319, A320, and A321 aeroplanes. It applies to specific ELAC part numbers associated with these aircraft models and aims to ensure continued safe flight control operation. The directive updates previous requirements related to ELAC replacement and installation.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2026-0133

Jul 8, 2026

Fuselage – Centre Fuselage Forward Pressure Bulkhead – Inspection

EASA Airworthiness Directive 2026-0133 is an airworthiness directive addressing inspection requirements for the centre fuselage forward pressure bulkhead on Airbus A318, A319, A320, and A321 aeroplanes. It applies to various models and 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.

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

EASA AD 2025-0274R1

Jul 7, 2026

Fire Protection – Fire Panel – Inspection

EASA Airworthiness Directive 2025-0274R1 is a regulatory update addressing fire panel inspections on Airbus A318, A319, A320, and A321 aircraft. It targets specific fire panel part numbers that have been linked to incidents of engine fire switch self-releasing, which could cause uncommanded in-flight engine shutdowns. The directive mandates inspections, replacements, and installation requirements to ensure continued airworthiness and safety.

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

EASA AD 2025-0158R2

Jul 7, 2026

Landing Gear – Main Landing Gear Door Actuators – Inspections

EASA Airworthiness Directive 2025-0158R2 is an updated regulatory requirement addressing inspections and corrective actions for main landing gear door actuators on Airbus A318, A319, A320, and A321 aircraft models. It targets actuators with specific part number 114122015 and serial numbers listed in Airbus Alert Operators Transmission A32N033-24, aiming to prevent landing gear extension issues caused by actuator assembly errors. The directive mandates repetitive inspections and eventual replacement or modification of affected parts to ensure continued airworthiness.

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

EASA AD 2026-0130

Jul 6, 2026

Electrical Systems Installation – Battery Retaining Rods – Identification / Replacement

EASA Airworthiness Directive 2026-0130 is an airworthiness directive addressing battery retaining rods on Airbus A318, A319, A320, and A321 aeroplanes. It mandates inspections and potential replacement or reidentification of affected battery retaining rods with Part Number D9241023700000 to prevent battery displacement and associated electrical system failures.

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

EASA AD 2025-0171R2

Jul 3, 2026

Engine – High Pressure Turbine Rotor Stage 1 Blade – Inspection

EASA Airworthiness Directive 2025-0171R2 is an updated regulatory requirement addressing inspections of high pressure turbine (HPT) rotor stage 1 blades on CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. The directive mandates repetitive borescope inspections of specific affected turbine blades to detect cracks and prevent potential in-flight engine failures. It applies to multiple LEAP-1A engine variants and specifies affected part numbers for inspection and corrective actions.

Airworthiness Directive
  • CFM International LEAP-1A
  • CFM International LEAP-1C
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2025-0237R1

Jun 24, 2026

[Correction] Equipment / Furnishings – 80 VU Rack Attachments – Inspection / Repair

The document titled '[Correction] Equipment / Furnishings – 80 VU Rack Attachments – Inspection / Repair' is a correction notice related to Airbus S.A.S. aircraft models A318, A319, A320, and A321. It addresses inspection and repair procedures for the 80 VU rack attachments used in these aircraft. The correction ensures accurate maintenance guidelines for these specific equipment components.

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

EASA AD 2026-0120

Jun 23, 2026

Fuselage – Lateral Window Frame – Inspections

EASA Airworthiness Directive 2026-0120 is an airworthiness directive addressing inspections of the fuselage lateral window frame on Airbus A319, A320, and A321 NEO aircraft models. It mandates repetitive high frequency eddy current inspections of the horizontal upper stiffeners at fuselage frame 4 to detect cracks and requires corrective actions if discrepancies are found. This directive applies to specific MSN aircraft except those with certain Airbus modifications embodied in production.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A321 NEO

EASA AD 2026-0037

Feb 25, 2026

Equipment/Furnishings — Evacuation Slide/Inflation Hose Assemblies — Replacement

EASA Airworthiness Directive 2026-0037 is an official safety directive addressing evacuation slide inflation hose assemblies on Airbus A318, A319, A320, and A321 aircraft. It targets specific inflation hose assemblies and door evacuation slides identified by part and serial numbers that have been found to fail during emergency evacuations. The directive mandates the replacement of affected evacuation slides to ensure proper inflation and safe evacuation.

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

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