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EASA Regulations & Airworthiness Directives

Browse 285 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320286 Airbus A321285 Airbus A319253 Airbus A350222 Airbus A330220 Airbus A318189 Airbus A380182 Boeing 737175 Airbus A340141 Airbus A350-941132 Airbus BD-500 (A220 Series)123 Airbus Helicopters AS 332119 Airbus Helicopters EC 225116 Airbus Helicopters SA 330116 Boeing 787114 Show all...

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EASA AD 2024-0247

Superseded by EASA AD 2025-0041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

Superseded by EASA AD 2025-0083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 2024-0230

Wings — Bottom Wing Skin Panel 2 — Inspection

EASA Airworthiness Directive 2024-0230 is an airworthiness directive addressing inspection requirements for the bottom wing skin panel 2 on Airbus A319, A320, and A321 aeroplanes, including both Current Engine Option (CEO) and New Engine Option (NEO) models. It mandates detailed inspections of specific wing areas prone to fatigue cracking, particularly around the bottom wing skin manhole access panel number 2 between ribs 13 and 26. The directive applies to all manufacturer serial numbers of the affected aircraft models.

Airworthiness Directive

Airbus A319
Airbus A320
Airbus A321

EASA AD 2024-0201R1

Wings — Outer Wing Bottom Buttstrap — Inspections

EASA Airworthiness Directive 2024-0201R1 is an updated regulatory requirement addressing inspections of the outer wing bottom buttstrap on Airbus A319, A320, and A321 aeroplanes. It mandates repetitive special detailed inspections of the wing surface area between rib 19 and rib 21 forward of stringer 8 on both left and right sides to detect cracks that could compromise structural integrity. This directive applies to all manufacturer serial numbers of the specified Airbus models.

Airworthiness Directive

Airbus A319
Airbus A320
Airbus A321

EASA AD 2024-0217

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

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

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

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 2024-0204

Fuselage — Rivet Holes at Frame 64 — Inspection

EASA Airworthiness Directive 2024-0204 is issued for Airbus A319 and A320 aeroplanes, specifically models A319-112, A319-132, A320-214, A320-232, A320-233, A320-251N, and A320-271N. This directive mandates inspection of rivet holes at frame 64 of the fuselage to detect and correct potential fatigue damage. The directive applies to all manufacturer serial numbers listed in the AD's appendix.

Airworthiness Directive

Airbus A319
Airbus A320

EASA AD 2024-0198

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

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

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 2024-0199

Superseded by EASA AD 2025-0120

EASA Airworthiness Directive 2024-0199 is an update addressing corrosion and cracks found in broadband antenna adapter plates and related parts on Airbus A319, A320, A321, A330, A350, and A380 aircraft models. The directive mandates inspections and corrective actions to ensure the continued airworthiness of these aircraft. It applies to all serial numbers of the affected Airbus models and includes new provisions for the recently certified A321-253NY variant.

Airworthiness DirectiveSuperseded

Airbus A319
Airbus A320
Airbus A321
Airbus A330
Airbus A350
Airbus A380

EASA AD 2020-0104R1-CN

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

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

[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

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

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

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

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