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EASA Regulations & Airworthiness Directives

Browse 247 EASA regulations with AI-powered summaries.

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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.

Oct 22, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus 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.

Oct 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600Airbus A300-600ST (Beluga)Airbus A310Airbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus A340Airbus A300

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.

Oct 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus 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.

Oct 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus 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.

Oct 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321Airbus A330Airbus A350Airbus 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.

Aug 30, 2024
Agency DecisionMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus 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.

Aug 7, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus 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.

Aug 5, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus 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.

Jul 30, 2024
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus 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.

Jul 12, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus 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.

Jul 10, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus 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.

Jun 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600Airbus A300-600ST (Beluga)Airbus A310Airbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus A340Airbus A350Airbus A380

EASA AD 2024-0106

SUPERSEDED BY EASA AD 2024-0199

EASA Airworthiness Directive 2024-0106 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, A321, A330, A350, and A380 aeroplanes. It addresses corrosion and cracking issues found on broadband antenna adapter plates and related components installed on these aircraft models. The directive mandates inspections and corrective actions to ensure continued airworthiness and safety.

May 31, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321Airbus A330Airbus A350Airbus A380

EASA AD 2024-0091R1

Aircraft Flight Manual / Section Limitations — Amendment / Auto Flight — New Flight Guidance Standard — Modification

The document titled Aircraft Flight Manual / Section Limitations — Amendment / Auto Flight — New Flight Guidance Standard — Modification applies to AIRBUS S.A.S. aircraft models A319, A320, and A321. It introduces modifications to the aircraft flight manual sections related to auto flight systems by incorporating a new flight guidance standard. This amendment ensures that operators of these Airbus aircraft have updated procedural and operational information reflecting the latest auto flight system capabilities.

May 30, 2024
OtherFlight OpsSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2024-0105

Fuselage — Potable and Waste Water Service Panels — Modification

EASA Airworthiness Directive 2024-0105 is issued for Airbus A319 aeroplanes, specifically models A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, and A319-133, excluding those with certain Airbus modifications already embodied. The directive addresses modifications to the fuselage potable and waste water service panels to ensure structural integrity. It mandates compliance with Airbus Service Bulletin A320-53-1517 to correct identified fatigue issues.

May 30, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319

EASA AD 2024-0077

[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.

Apr 25, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0093

Engine — Non-Synchronous Vibration During Engine Operation — Monitoring

EASA Airworthiness Directive 2024-0093 addresses non-synchronous vibration (NSV) issues during operation of CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. The directive targets specific affected parts, notably bearing No. 3 spring finger housings with certain part numbers and serial numbers, to ensure ongoing engine safety and airworthiness. It mandates monitoring and corrective actions to prevent potential engine stalls and turbine failures.

Apr 22, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1ACFM International LEAP-1CAirbus A319Airbus A320Airbus A321

EASA AD 2024-0089

Fuselage — Main Landing Gear Bay Rear Panel — Inspections

EASA Airworthiness Directive 2024-0089 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aeroplanes. It mandates repetitive special detailed inspections of the main landing gear bay rear panel at specific stringer and frame locations to detect cracks. This directive applies to various models except those with certain Airbus modifications or service bulletins already embodied.

Apr 15, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2022-0096R2

SUPERSEDED BY EASA AD 2024-0091

EASA Airworthiness Directive 2022-0096R2 is an amendment addressing flight guidance system issues on Airbus A319, A320, and A321 aeroplanes equipped with certain Flight Guidance (FG) 2G and 3G standards. It mandates modifications to the aircraft flight manual and installation of updated FG software to prevent pitch-up attitudes and autopilot disconnections during go-around maneuvers, particularly when operating with high aft center of gravity and specific thrust configurations.

Apr 12, 2024
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2024-0068

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.

Mar 11, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321