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EASA Regulations & Airworthiness Directives

Browse 274 EASA regulations with AI-powered summaries.

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EASA AD 2023-0074

Wings — Centre Wing Box Rear Lower Spar and Slanted Beam — Inspection

EASA Airworthiness Directive 2023-0074 is an airworthiness directive issued by EASA affecting Airbus A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 aeroplanes. It mandates a one-time inspection of the centre wing box rear lower spar junction area and the slanted beam connection at fuselage frame 42 to detect potential fatigue cracks. The directive aims to ensure structural integrity by addressing high fatigue stress identified during certification and stress analysis.

Apr 5, 2023
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321Airbus A321-111Airbus A321-112Airbus A321-131Airbus A321-211Airbus A321-212Airbus A321-213Airbus A321-231Airbus A321-232

EASA AD US-2021-21-02

SUPERSEDED BY FAA AD 2024-11-01

FAA Airworthiness Directive 2021-21-02 is a final rule addressing certain Airbus SAS airplanes including models A318, A319, A320, A321, A330 series, A340 series, and A380-800 series equipped with parts manufacturer approval (PMA) nickel-cadmium (Ni-Cd) batteries. This directive targets the reduction in battery capacity caused by repetitive disconnection and reconnection of these PMA Ni-Cd batteries during airplane parking or storage.

Mar 28, 2023
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus A340Airbus A380Airbus A380-800

EASA AD 2022-0165R1

Aircraft Flight Manual — Section Abnormal Procedures — Amendment; Ice and Rain Protection / Pneumatic — MMEL Amendment; Pneumatic — Bleed Monitoring Computer Electrical Connection — Modification

EASA Airworthiness Directive 2022-0165R1 is an amendment addressing the electrical grounding issue in the Over-Heat Detection System (OHDS) on Airbus A320 and A321 aircraft, specifically models A320-251N, A320-253N, A321-251N, A321-253N, A320-271N, A321-271N, and A321-272N. This directive mandates modifications to the Bleed Monitoring Computer electrical connections, updates to the Aircraft Flight Manual (AFM) abnormal procedures, and amendments to the Master Minimum Equipment List (MMEL) to ensure continued safe operation. The directive applies to aircraft not incorporating Airbus modifications 161978 or 161979 in production.

Feb 28, 2023
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtAirbus A320Airbus A321

EASA AD 2022-0204R1

[Correction] Landing Gear — Main Landing Gear Sliding Tube — Inspection / Replacement

EASA Airworthiness Directive 2022-0204R1 is a regulatory update addressing inspection and replacement requirements for the main landing gear (MLG) sliding tubes on Airbus A318, A319, A320, and A321 aircraft. The directive targets specific MLG sliding tubes and shock absorbers identified by part and serial numbers due to reported cracks caused by manufacturing defects and abnormal overhaul processes. It mandates detailed and special inspections as well as replacement procedures to ensure continued airworthiness and safety.

Feb 17, 2023
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2023-0029

Equipment / Furnishings — Galley / Container End Stop — Replacement

EASA Airworthiness Directive 2023-0029 is issued for Airbus A318, A319, A320, and A321 aeroplanes equipped with certain affected galleys or stowage units. The directive addresses the replacement and modification of galley/container end stops and waste compartment doors to prevent potential failures that could lead to container detachment or release of waste bins during critical flight phases. This AD applies to various galley part numbers and serial numbers identified in the Aircraft Inspection Report.

Feb 1, 2023
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2023-0014

Doors — On-board Entrance Stairs / Motoreductor Units — Replacement

EASA Airworthiness Directive 2023-0014 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses the replacement of specific motoreductor units installed on the on-board entrance stairs to ensure continued safe operation. The directive applies to motoreductor units with part numbers 4255417, 4394656, or 4339747 installed on these aircraft models.

Jan 18, 2023
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2023-0009

Fuselage — Cockpit Lateral Window Frames — Inspection

EASA Airworthiness Directive 2023-0009 mandates repetitive special detailed inspections of the cockpit lateral window frame vertical stiffeners on Airbus A318, A319, A320, and A321 aircraft, excluding certain modified configurations. The directive addresses potential cracks that could compromise fuselage structural integrity. It applies to all manufacturer serial numbers except those with specific Airbus modifications embodied in production or service.

Jan 16, 2023
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2023-0008

SUPERSEDED BY EASA AD 2024-0031

EASA Airworthiness Directive 2023-0008 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 airworthiness limitations related to damage tolerant items as specified in Airbus ALS Part 2 Variation 9.2. This directive ensures continued airworthiness by requiring operators to follow revised maintenance tasks and limitations.

Jan 16, 2023
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2022-0266

Electric and Electronic Common Installation — Cockpit Panel Bracket — Inspection

EASA Airworthiness Directive 2022-0266 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates detailed inspections of the 10VU rack side fittings on cockpit panel brackets to detect cracks that could affect primary flight and navigation displays. The directive applies to all manufacturer serial numbers except those with Airbus modification 157335 embodied in production.

Dec 22, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2006-0135-CN

CANCELLED: Hydraulic Power — Ram Air Turbine — Speed Limitation

EASA Airworthiness Directive 2006-0135-CN is a cancellation notice affecting Airbus A318, A319, A320, and A321 aeroplanes equipped with Hamilton Sundstrand Ram Air Turbine (RAT) Part Numbers 762308, 762308A, or 766352. This document cancels the previous AD 2006-0135 which imposed speed limitations during flight tests with the RAT deployed due to a risk of RAT imbalance and potential structural damage. The cancellation reflects that all affected counterweights have been recovered and the original unsafe condition is no longer present.

Nov 23, 2022
Airworthiness DirectiveSafety MgmtMaintenanceAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2022-0213R1

Doors — Passenger Door / External Handle Mechanism — Cleaning / Lubrication

EASA Airworthiness Directive 2022-0213R1 is an updated regulatory requirement addressing the cleaning and lubrication of the passenger door external handle mechanism on Airbus A318, A319, A320, and A321 aircraft. The directive targets specific affected doors where corrosion protection compound caused sticky mechanisms, potentially impairing door operation and emergency evacuation. This AD applies to all manufacturer serial numbers of the listed Airbus models.

Nov 8, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2022-0185

Fuel — Engine Low Pressure Shut Off Valve Electrical Harness Routing — Modification

EASA Airworthiness Directive 2022-0185 is an airworthiness directive issued by EASA affecting Airbus A319, A320, and A321 aircraft equipped with International Aero Engines PW1100 series or CFM International LEAP-1A series engines. The directive addresses the electrical harness routing of the engine low pressure shut off valve (LPSOV) to enhance protection against uncontained engine rotor failure. It applies to all manufacturer serial numbers except those with Airbus modification 167036 embodied in production.

Sep 5, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2022-0176

SUPERSEDED BY EASA AD 2025-0151

EASA Airworthiness Directive 2022-0176 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 safety issue related to the escape slide inflation reservoir regulator valve protective cover that may cause uncommanded door 3 escape slide release during flight. The directive mandates modification of affected parts to prevent deployment of a non-inflated escape slide.

Aug 24, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A321Airbus A321-251NXAirbus A321-252NXAirbus A321-253NXAirbus A321-271NXAirbus A321-272NX

EASA AD 2022-0147

SUPERSEDED BY EASA AD 2024-0196

EASA Airworthiness Directive 2022-0147 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses potential defects in certain overheat detection system (OHDS) sensing elements manufactured before 31 January 2021, which may fail to detect thermal bleed leak events properly. The directive mandates inspection and possible replacement of these affected parts to ensure continued airworthiness.

Aug 17, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2022-0032R1

SUPERSEDED BY EASA AD 2023-0093

EASA Airworthiness Directive 2022-0032R1 is an amendment addressing the braking and steering control units (BSCU) on Airbus A318, A319, A320, and A321 aeroplanes. It focuses on BSCUs with Part Number E21327307, which have shown failures leading to loss of anti-skid function, alternate braking mode, and nose wheel steering. The directive updates operational procedures and maintenance requirements to mitigate these risks.

Jul 29, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2022-0151

SUPERSEDED BY EASA AD 2024-0068

EASA Airworthiness Directive 2022-0151 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 horizontal upper stiffeners of the lateral cockpit window frame at fuselage frame 4 to detect cracks that could compromise fuselage structural integrity. The directive applies to specific Airbus models and serial numbers, excluding certain configurations with specific Airbus modifications.

Jul 26, 2022
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2022-0009R1

Engine — High Pressure Turbine Rotor Stage 1 Blade — Inspection

EASA Airworthiness Directive 2022-0009R1 is an updated safety directive addressing inspection requirements for high pressure turbine 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 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.

Jul 19, 2022
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1ACFM International LEAP-1CAirbus A319Airbus A320Airbus A321

EASA AD 2022-0139

Engine — High Pressure Turbine Nozzle Assembly and Stator Stationary Seal — Inspection

EASA Airworthiness Directive 2022-0139 is an official regulatory document addressing the inspection of the high pressure turbine nozzle assembly and stator stationary seal on CFM International LEAP-1A engines. This directive applies specifically to various LEAP-1A engine models installed on Airbus A319, A320, and A321 aircraft. It mandates a one-time inspection to detect potential damage caused by non-synchronous vibrations that could affect engine safety and performance.

Jul 7, 2022
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1ACFM International LEAP-1CAirbus A319Airbus A320Airbus A321

EASA AD 2022-0115

Fuselage — Cargo Compartment Fitting Brackets, Tack and Rivet Holes — Inspection / Repair

The document titled 'Fuselage — Cargo Compartment Fitting Brackets, Tack and Rivet Holes — Inspection / Repair' is an AIRBUS S.A.S. type designation applicable to the A319, A320, and A321 aircraft models. It addresses inspection and repair procedures related to the fitting brackets and associated tack and rivet holes in the cargo compartment of these Airbus aircraft. The document provides guidance to ensure structural integrity and safety of the fuselage in the cargo area.

Jun 20, 2022
OtherMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2022-0113

Engine — Stages 6-10 Compressor Rotor Spools and High Pressure Turbine Rotor Stage 1 Disks — Replacement

EASA Airworthiness Directive 2022-0113 is an airworthiness directive addressing CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. It mandates the replacement of specific compressor rotor spools (Stages 6-10) and high pressure turbine rotor stage 1 disks identified as affected parts due to potential manufacturing defects. The directive aims to ensure continued airworthiness and prevent engine part failure.

Jun 17, 2022
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1ACFM International LEAP-1CAirbus A319Airbus A320Airbus A321