EASA Regulations & Airworthiness Directives

Browse 189 EASA regulations with AI-powered summaries.

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EASA AD 2025-0032

Feb 10, 2025

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.

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

EASA AD 2025-0033

Feb 10, 2025

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.

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

EASA AD 2024-0247

Dec 18, 2024

Superseded by EASA AD 2025-0041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.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A340

EASA AD 2024-0231

Dec 4, 2024

Superseded by EASA AD 2025-0083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.

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

EASA AD 2024-0217

Nov 18, 2024

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.

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

EASA AD 2024-0216

Nov 15, 2024

Superseded by EASA AD 2025-0158

EASA Airworthiness Directive 2024-0216 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 main landing gear door actuators, specifically those with Part Number 114122015 and listed serial numbers, which may cause jamming or inability to open the landing gear doors during maintenance. The directive mandates inspections and corrective actions to ensure safe operation of the landing gear.

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

EASA AD 2024-0208

Oct 25, 2024

Superseded by EASA AD 2025-0030

EASA Airworthiness Directive 2024-0208 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with updated damage tolerant airworthiness limitations as specified in Airbus A318/A319/A320/A321 Airworthiness Limitations Section Part 2 Revision 10 Variation 10.3. This directive ensures continued airworthiness by requiring operators to incorporate new or more restrictive maintenance tasks.

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

EASA AD 2024-0203

Oct 22, 2024

Flight Controls — Trimmable Horizontal Stabilizer Actuator — Replacement

EASA Airworthiness Directive 2024-0203 is an airworthiness directive addressing the replacement of trimmable horizontal stabilizer actuators (THSA) on Airbus A318, A319, A320, and A321 aircraft models, including the newly certified A321-253NY. The directive mandates the replacement of affected THSA parts identified by serial numbers to ensure continued safe operation of the flight controls. It applies to all manufacturer serial numbers of the specified aircraft models.

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

EASA AD 2024-0198

Oct 18, 2024

Oxygen — Chemical Oxygen Generators — Replacement

EASA Airworthiness Directive 2024-0198 is an official regulatory document addressing the replacement of chemical oxygen generators in various Airbus aeroplanes, including models A310, A300, A318, A319, A320, A321, A330, and A340. The directive targets specific oxygen generators with part numbers E63320-00, E63340-00, and E63440-00 that have known activation failures. It mandates replacement of these affected parts to ensure continued airworthiness and safety.

Airworthiness Directive
  • Airbus A310
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A340
  • Airbus A300600600ST (Beluga)

EASA AD 2024-0197

Oct 18, 2024

Oxygen — SafeLav Gaseous Oxygen Container — Replacement

EASA Airworthiness Directive 2024-0197 is issued for Airbus A318, A319, A320, A321, A330, and A340 aeroplanes concerning the SafeLav gaseous oxygen container (SLGOC). The directive addresses a production deficiency in certain SLGOC batches that may cause oxygen flow activation failure due to a missing heat treatment on the actuation pin. This AD applies to specific part numbers and serial numbers of SLGOCs installed on these aircraft models.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A340

EASA AD 2024-0196

Oct 18, 2024

Pneumatic — Overheat Detection System Sensing Elements — Inspection

EASA Airworthiness Directive 2024-0196 is an airworthiness directive addressing the inspection of pneumatic overheat detection system sensing elements on Airbus A318, A319, A320, and A321 aeroplanes. It applies to specific part numbers of continuous fire detectors produced before January 31, 2021, which may fail to detect thermal bleed leak events properly. The directive mandates inspection and, if necessary, replacement of affected parts to ensure continued airworthiness.

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

EASA AD 2020-0104R1-CN

Aug 30, 2024

CANCELLED: Oxygen — Oxygen Supply Solenoid Valve — Inspection / Replacement

EASA Airworthiness Directive Cancellation Notice 2020-0104R1-CN cancels the previous AD 2020-0104R1 concerning the inspection and replacement of oxygen supply solenoid valves on Airbus A318, A319, A320, and A321 aircraft. The affected parts are specific solenoid valves with part numbers DVE90-06 or DVE90-07 manufactured up to 2016. This cancellation applies to all manufacturer serial numbers of these aircraft models.

Agency Decision
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0147R1

Aug 7, 2024

Fuselage — Centre Fuselage Forward Pressure Bulkhead — Inspection

EASA Airworthiness Directive 2024-0147R1 is an updated regulatory requirement addressing inspection and reinforcement of the centre fuselage forward pressure bulkhead on Airbus A318, A319, A320, and A321 aircraft. It mandates repetitive inspections for fatigue damage at frame 35 (or 35.8 for A321) and requires modification to reinforce the bulkhead to ensure structural integrity. This directive applies to all serial numbers except those with specific Airbus modifications embodied in production or service.

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

EASA AD 2019-0069R2

Aug 5, 2024

[Correction] Equipment / Furnishings — Overhead Stowage Compartments — Modification

EASA Airworthiness Directive 2019-0069R2 is a regulatory document addressing the modification of overhead stowage compartments (OHSC) and pivoting OHSC (POHSC) on Airbus A318, A319, A320, and A321 aircraft. The directive mandates modifications to improve the robustness of these compartments to prevent detachment caused by loose or missing screws. This AD applies specifically to various Airbus A320 family models as listed in the applicable service bulletins.

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

EASA SIB 2011-28R1

Jul 30, 2024

Maintenance of Emergency Evacuation Systems

EASA Safety Information Bulletin 2011-28R1 is an airworthiness bulletin addressing the maintenance of emergency evacuation systems on Airbus A318, A319, A320, and A321 aircraft. It emphasizes the importance of proper maintenance and reporting of malfunctions in evacuation systems such as slides, slides/rafts, and door mechanisms to ensure their reliability during emergencies. The bulletin updates references to the latest Airbus service publications and reinforces the need for accurate data collection during system testing and deployments.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0097R2

Jul 12, 2024

Superseded by EASA AD 2025-0189

EASA Airworthiness Directive 2024-0097R2 is a regulatory update addressing inspection and maintenance requirements for Airbus A318, A319, A320, and A321 aircraft. It focuses on the main landing gear (MLG) door hinge and actuator fittings on the keel beam to detect and prevent cracks that could lead to in-flight detachment of MLG doors. The directive applies to both Current Engine Option (CEO) and New Engine Option (NEO) variants, specifying inspection methods and intervals.

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

EASA AD 2024-0135

Jul 10, 2024

Fuselage — Centre Fuselage — Keel Beam Bottom Panel — Inspection

EASA Airworthiness Directive 2024-0135 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates inspections of the keel beam bottom panel in the centre fuselage due to detected cracks during fatigue testing. The directive applies to specific aircraft configurations and serial numbers, excluding those with certain Airbus modifications or service bulletins already embodied.

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

EASA AD US-2024-11-01

Jun 26, 2024

Electrical Power - Nickel-Cadmium Batteries during Aeroplane Parking or Storage - Replacement

The Electrical Power - Nickel-Cadmium Batteries during Aeroplane Parking or Storage - Replacement is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2024-11-01) that applies to various Airbus SAS airplane models including A300, A310, A318, A319, A320, A321, A330, A340, A350, and A380 series equipped with certain parts manufacturer approval (PMA) nickel-cadmium (Ni-Cd) batteries. This AD addresses the issue of reduced battery endurance performance during airplane parking or storage periods. It mandates replacement of affected PMA Ni-Cd batteries with serviceable parts to ensure electrical power reliability during abnormal or emergency conditions.

Airworthiness Directive
  • Airbus A300600600ST (Beluga)
  • Airbus A310
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A340
  • Airbus A350
  • Airbus A380

EASA AD 2024-0077

Apr 25, 2024

[Correction] Fuselage — Pressure Panel Longitudinal Beams — Inspection / Repair / Modification

EASA Airworthiness Directive 2024-0077 is a regulatory document addressing inspection, repair, and modification requirements for the pressure panel longitudinal beams on Airbus A318, A319, A320, and A321 aircraft. It targets all manufacturer serial numbers except those with Airbus modification 151574 embodied in production. The directive aims to ensure structural integrity by mandating inspections and corrective actions related to fatigue cracks found around fasteners connecting the pressure panel to the flexible bracket at fuselage frame 36.

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

EASA AD 2024-0068

Mar 11, 2024

Fuselage — Lateral Cockpit Window Frame Upper Stiffener — Inspection

EASA Airworthiness Directive 2024-0068 is an inspection directive affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates special detailed inspections of the lateral cockpit window frame upper stiffener at fuselage frame 4 to detect cracks that could compromise structural integrity. The directive applies to specific aircraft configurations excluding those with certain Airbus modifications embodied in production or service.

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