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EASA Regulations & Airworthiness Directives

Browse 274 EASA regulations with AI-powered summaries.

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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SUPERSEDED BY EASA AD 2024-0091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

EASA AD 2024-0067-E

Engine — Life Limited Parts — Replacement

EASA Airworthiness Directive 2024-0067-E is an emergency directive addressing life limited parts replacement for CFM International CFM56 series engines, including models CFM56-2, -3, -5, -5B, -5C, and -7B. These engines are commonly installed on Airbus A318, A319, A320, A321, A340, and Boeing 737 series aircraft from the 300 to 900ER variants. The directive targets specific compressor discharge pressure seals, high-pressure compressor stage 3 disks, and high-pressure turbine rear shafts identified as affected parts due to potential damage from improper maintenance.

Mar 9, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCFM International CFM56-2CFM International CFM56-3CFM International CFM56-5CFM International CFM56-5BCFM International CFM56-5CCFM International CFM56-7BAirbus A318Airbus A319Airbus A320Airbus A321Airbus A340Boeing 737

EASA AD 2024-0066

Time Limits / Maintenance Checks — Safe Life Airworthiness Limitations Items — ALS Part 1 — Amendment

EASA Airworthiness Directive 2024-0066 is an amendment concerning the Airbus A318, A319, A320, and A321 aircraft models. It updates the Safe Life Airworthiness Limitations Items in the Airworthiness Limitations Section Part 1, Revision 09, to ensure continued airworthiness through mandatory maintenance tasks and life limits. This directive applies to all serial numbers of the specified Airbus A320 family aircraft.

Mar 8, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0057

SUPERSEDED BY EASA AD 2025-0151

EASA Airworthiness Directive 2024-0057 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes. It addresses inspection and replacement requirements for escape slide and offwing slide inflation reservoir venting holes orifice fittings with specific part numbers. The directive ensures continued airworthiness by mandating inspections and corrective actions for affected parts to prevent potential in-flight deployment failures.

Feb 28, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321Airbus A321-251NXAirbus A321-252NXAirbus A321-253NXAirbus A321-271NXAirbus A321-272NX

EASA AD 2024-0046

SUPERSEDED BY EASA AD 2025-0032

EASA Airworthiness Directive 2024-0046 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with the Airbus A318/A319/A320/A321 Airworthiness Limitations Section Part 4 Revision 09, which includes system equipment maintenance requirements and life limits for components. This directive ensures continued airworthiness by requiring operators to follow updated maintenance tasks and replacement schedules.

Feb 19, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0047

SUPERSEDED BY EASA AD 2025-0033

EASA Airworthiness Directive 2024-0047 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 fuel airworthiness limitations specified in Airbus Airworthiness Limitations Section Part 5 Revision 08. The directive ensures continued airworthiness by requiring maintenance tasks and life limit replacements as per the latest approved maintenance program.

Feb 19, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0048

SUPERSEDED BY EASA AD 2024-0057

EASA Airworthiness Directive 2024-0048 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX, and A321-272NX aeroplanes. It addresses a potential unsafe condition related to the escape slide and offwing slide inflation reservoir venting holes, specifically concerning certain orifice fittings installed on these reservoirs. The directive mandates inspection and possible replacement of affected parts to ensure continued airworthiness.

Feb 16, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321Airbus A321-251NXAirbus A321-252NXAirbus A321-253NXAirbus A321-271NXAirbus A321-272NX

EASA AD 2024-0038

SUPERSEDED BY EASA AD 2025-0068

EASA Airworthiness Directive 2024-0038 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses inspection and modification requirements for forward-facing galley parts with specific part numbers to prevent damage that could lead to trolley detachment during emergency landings. This directive applies to all manufacturer serial numbers of the listed aircraft models.

Feb 5, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0031

SUPERSEDED BY EASA AD 2025-0030

EASA Airworthiness Directive 2024-0031 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 Tolerance Airworthiness Limitations Items specified in the Airbus Airworthiness Limitations Section Part 2 Revision 10. This directive ensures continued airworthiness by requiring operators to follow new and/or more restrictive maintenance tasks.

Feb 1, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0030

SUPERSEDED BY EASA AD 2025-0031

EASA Airworthiness Directive 2024-0030 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with the updated Airbus Airworthiness Limitations Section (ALS) Part 3 Revision 09, which contains certification maintenance requirements essential for continued airworthiness. This directive applies to all manufacturer serial numbers of the specified Airbus A320 family models.

Jan 31, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0027

SUPERSEDED BY EASA AD 2024-0230

EASA Airworthiness Directive 2024-0027 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aeroplanes, including both Current Engine Option (CEO) and New Engine Option (NEO) models. It addresses potential fatigue cracking in the bottom wing skin manhole access panel attachment holes between Rib 13 and Rib 26 on both left and right wings. The directive mandates inspections and corrective actions to ensure structural integrity of the wings.

Jan 25, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2024-0026

Engine — High Pressure Turbine — Rotor Interstage Seal — Replacement

EASA Airworthiness Directive 2024-0026 is an airworthiness directive addressing the replacement of the High Pressure Turbine Rotor Interstage Seal on CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. The directive targets specific affected parts identified by part number 2466M68P02 and certain serial numbers. It mandates replacement of these parts to ensure continued safe operation of the engines.

Jan 24, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1ACFM International LEAP-1CAirbus A319Airbus A320Airbus A321

EASA AD 2024-0022

Landing Gear — Nose Landing Gear — Repair Assessment

Landing Gear — Nose Landing Gear — Repair Assessment is a regulatory document concerning the Airbus S.A.S. A319, A320, and A321 aircraft types. It addresses the assessment procedures for repairs related to the nose landing gear to ensure continued airworthiness and safety. The document provides guidance on evaluating repair conditions and standards for these specific aircraft models.

Jan 23, 2024
OtherMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA SIB 2024-02

Emergency Exit Safety Barriers Modification / Models Selection

EASA Safety Information Bulletin 2024-02 is an airworthiness bulletin addressing emergency exit safety barriers on Airbus A318, A319, A320, and A321 aircraft. It provides information on the different part numbers of safety barriers used during maintenance to prevent personnel from falling through open doors. The bulletin highlights concerns about the retention forces of certain upgraded barrier designs and introduces improved versions with enhanced nozzle ends.

Jan 22, 2024
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0002

Engine — High-Pressure Turbine Inner Stationary Seal — Inspection

EASA Airworthiness Directive 2024-0002 is an airworthiness directive addressing the inspection of the high-pressure turbine (HPT) inner stationary seal on CFM International CFM56-5B, CFM56-5C, and CFM56-7B engines. These engines are commonly installed on Airbus A318, A319, A320, A321, A340, and Boeing 737-600 through 737-900ER series aircraft. The directive mandates inspections and corrective actions to prevent potential damage caused by cracks and honeycomb separation in the affected seals.

Jan 4, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCFM International CFM56-5BCFM International CFM56-5CCFM International CFM56-7BAirbus A318Airbus A319Airbus A320Airbus A321Airbus A340Boeing 737-600Boeing 737-700Boeing 737-800Boeing 737-900ER

EASA AD 2023-0212

SUPERSEDED BY EASA AD 2024-0217

EASA Airworthiness Directive 2023-0212 is issued for Airbus A318, A319, A320, and A321 aeroplanes to address potential cracks in the fuselage double joggle areas at frames 16 and 20 on both right-hand and left-hand sides. The directive applies to both Current Engine Option (CEO) and New Engine Option (NEO) models, requiring special detailed inspections and optional modifications to reinforce affected areas. This directive ensures continued structural integrity and airworthiness of the affected Airbus aircraft models.

Dec 6, 2023
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321