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EASA Regulations & Airworthiness Directives

Browse 186 EASA regulations with AI-powered summaries.

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EASA AD 2018-0218

SUPERSEDED BY EASA AD 2021-0228

EASA Airworthiness Directive 2018-0218 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates repetitive internal and external inspections of the center and outer wing box at the Rib 1 junction due to non-compliant taperlok fasteners that could compromise structural integrity. The directive includes detailed inspection thresholds and intervals to ensure continued airworthiness.

Oct 26, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2018-0231

SUPERSEDED BY EASA AD 2024-0047

EASA Airworthiness Directive 2018-0231 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 as specified in the Airbus Airworthiness Limitations Section Part 5 Revision 05. This directive applies to all manufacturer serial numbers of the listed Airbus A320 family models.

Oct 25, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2018-0189

Navigation — Back Up Speed Scale / Aircraft Flight Manual — Amendment

EASA Airworthiness Directive 2018-0189 is an amendment applicable to Airbus A318, A319, A320, and A321 aeroplanes. It addresses the reliability of airspeed information displayed on the Primary Flight Display under extreme icing conditions by mandating amendments to the Aircraft Flight Manual related to the Back-Up Speed Scale function. This directive ensures flight crews receive accurate operational procedures to manage potential erroneous airspeed indications caused by angle of attack sensor blockages.

Aug 30, 2018
Airworthiness DirectiveFlight OpsSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2018-0180

SUPERSEDED BY EASA AD 2020-0067

EASA Airworthiness Directive 2018-0180 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses the airworthiness limitations related to the Certification Maintenance Requirements as specified in the Airbus Airworthiness Limitations Section Part 3 Revision 06. This directive ensures that operators comply with updated maintenance tasks and intervals to maintain aircraft safety.

Aug 27, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2018-0060R1

Oxygen — Crew Oxygen / Oxygen Pipe Corrosion — Inspection

EASA Airworthiness Directive 2018-0060R1 is a regulatory document addressing corrosion issues in crew oxygen pipe assemblies with Part Number D3511032000640 installed on Airbus A318, A319, A320, and A321 aircraft. The directive mandates inspection and replacement of affected oxygen pipes from specific batch numbers to ensure continued airworthiness and safety of the oxygen supply system for flight crew members. It applies to various manufacturer serial numbers including certain A320 and A321 NEO models.

Jul 19, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2018-0135R1

SUPERSEDED BY EASA AD 2022-0204

EASA Airworthiness Directive 2018-0135R1 is an updated directive addressing the inspection and replacement of Main Landing Gear (MLG) sliding tubes on Airbus A318, A319, A320, and A321 aeroplanes. It applies to specific MLG sliding tubes identified by part and serial numbers in Safran and Airbus service bulletins. The directive mandates repetitive inspections and corrective actions to prevent potential sliding tube failure that could lead to landing gear collapse.

Jul 6, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2018-0136

SUPERSEDED BY EASA AD 2020-0258

EASA Airworthiness Directive 2018-0136 is an airworthiness directive issued by the European Aviation Safety Agency addressing the Airbus A318, A319, and A320 aircraft models. It focuses on inspecting the main landing gear sliding tubes that were last overhauled between 27 October 2003 and 21 September 2009 to detect cracks that could lead to landing gear collapse. The directive mandates repetitive visual inspections and replacement of affected parts if cracks are found.

Jun 26, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320

EASA AD 2018-0131

SUPERSEDED BY EASA AD 2022-0266

EASA Airworthiness Directive 2022-0266 addresses safety requirements for Airbus S.A.S. aircraft models A318, A319, A320, and A321. This directive supersedes previous related airworthiness directives to ensure continued airworthiness and operational safety of these aircraft types. It provides updated instructions and mandates for inspections or modifications as necessary.

Jun 19, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2018-0091

Fuselage — Belly Fairing and Keel Beam Side Panel Attachment Angles — Inspection / Replacement / Repair

EASA Airworthiness Directive 2018-0091 is an airworthiness directive affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses inspection, replacement, and repair requirements for the belly fairing and keel beam side panel attachment titanium angles to ensure structural integrity. The directive mandates repetitive detailed inspections and corrective actions to detect and fix cracks in these components.

Apr 20, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2015-0135R3

Navigation — Angle of Attack Sensors — Replacement

EASA Airworthiness Directive 2015-0135R3 is an amendment addressing the replacement of Angle of Attack (AOA) sensors on Airbus A318, A319, A320, and A321 aircraft. It applies to various AOA sensor part numbers from manufacturers including Thales, UTC Aerospace, and SEXTANT/THOMSON. The directive mandates modifications to ensure continued safe operation by preventing loss of control caused by blocked or malfunctioning AOA sensors.

Mar 13, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2018-0023

[Correction] Doors — Main Landing Gear Fixed Fairing Assembly - Inspection

EASA Airworthiness Directive 2018-0023 is a corrective directive addressing inspection requirements for the main landing gear fixed fairing assembly on Airbus A318, A319, A320, and A321 aircraft. It applies to all manufacturer serial numbers of these models and focuses on preventing in-flight loss of the main landing gear fixed and hinged fairings due to fatigue cracking and corrosion. The directive mandates inspections, replacements, and modifications to ensure continued airworthiness and safety.

Feb 5, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2018-0007R1

Flight Controls — Elevator Aileron Computers — Replacement / Software Update

EASA Airworthiness Directive 2018-0007R1 is a regulatory update addressing the replacement and software update of Elevator Aileron Computers (ELAC) on Airbus A318, A319, A320, and A321 aircraft. The directive targets ELAC units to improve Angle of Attack (AoA) probe monitoring and prevent potential flight control issues. It applies to all manufacturer serial numbers of these Airbus models and mandates specific software upgrades and hardware replacements.

Jan 19, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2017-0257R1

SUPERSEDED BY EASA AD 2018-0189

EASA Airworthiness Directive 2017-0257R1 is an amendment affecting Airbus A318, A319, A320, and A321 aircraft equipped with the Back-Up Speed Scale (BUSS) function. This directive mandates an amendment to the Airplane Flight Manual (AFM) to incorporate new operational procedures addressing potential erroneous airspeed indications caused by pitot probe icing and angle of attack sensor blockages. The directive ensures flight crews have reliable airspeed information below flight level 250.

Jan 9, 2018
Airworthiness DirectiveFlight OpsSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2017-0251

SUPERSEDED BY EASA AD 2020-0085

EASA Airworthiness Directive 2017-0251 is an airworthiness directive issued by the European Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes equipped with CFM56-5A/5B engines. It addresses the issue of broken aft engine mount inner retainers caused by vibration and surface finish defects, which could lead to in-flight loss of an engine mount link. The directive mandates inspections, part identification, replacement, and modification of affected engine mount assemblies to ensure continued airworthiness.

Dec 15, 2017
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB 2010-10R1

Fuel Tank Safety — Flammability Reduction System (FRS) for High Flammability Exposure Fuel Tanks

EASA Safety Information Bulletin 2010-10R1 is an informational document addressing fuel tank safety through the introduction of Flammability Reduction Systems (FRS) for high flammability exposure fuel tanks. It applies to Airbus A318, A319, A320, A321, A330, A340 and Boeing 737, 767, and 777 aircraft with center wing tanks manufactured from January 1, 2012. The bulletin provides background on the safety improvements following the TWA Flight 800 accident and outlines regulatory requirements for new production aircraft fuel tanks.

Nov 28, 2014
Safety Information BulletinSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus A340Boeing 737Boeing 767Boeing 777

EASA SIB NM-14-21

Honeywell RTA 44D VHF Transceivers — Frequency Interference / Spurious Transmissions

The FAA Special Airworthiness Information Bulletin SAIB: NM-14-21 addresses frequency interference and spurious transmissions issues associated with Honeywell RTA 44D VHF transceivers installed on Airbus A318, A319, A320, and A321 series airplanes. The bulletin informs operators and maintenance personnel about off-frequency transmissions that can interfere with air traffic control communications but do not currently warrant an airworthiness directive. It highlights the affected Honeywell transceiver part numbers 064-50000-0202 and 064-50000-0505 and provides background on the issue and mitigation recommendations.

Sep 17, 2014
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB 2014-02

WITHDRAWN _ SEE FAA SAIB NM-14-21

EASA Safety Information Bulletin SIB No. 2014-02 addresses frequency interference caused by spurious transmissions from Honeywell RTA-44D Very High Frequency (VHF) transceivers. The affected transceivers, identified by part numbers 064-50000-0202 and 064-50000-0505 without MOD 22 incorporated, are installed on Airbus A318, A319, A320, and A321 aircraft. This bulletin informs operators about the issue and provides recommendations to mitigate the interference.

Jan 17, 2014
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB 2013-03

Seat Track Monument Fittings Replacement

EASA Safety Information Bulletin SIB No: 2013-03 titled 'Seat Track Monument Fittings Replacement' addresses concerns related to seat track lower attachment fittings Part Number ABS1262C010 installed on Airbus A318, A319, A320, A321, A330-243, and A330-343 aircraft. The bulletin informs operators about engineering static load test failures indicating these fittings may not meet required load specifications. It highlights that while Airbus-installed fittings comply with certification requirements, fittings installed via Supplemental Type Certificate modifications may pose a safety risk.

Jan 28, 2013
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321Airbus A330-243Airbus A330-343

EASA SIB 2012-16R1

Hydraulic Systems — Implementation of automatic Power Transfer Unit inhibition logic

EASA Safety Information Bulletin 2012-16R1 is an informational bulletin addressing hydraulic system improvements on Airbus A318, A319, A320, and A321 aircraft. It informs operators about the implementation of automatic Power Transfer Unit (PTU) inhibition logic designed to prevent overheating and failure of a second hydraulic system following a single hydraulic system failure with fluid loss. The bulletin references Airbus Service Bulletins that provide retrofit and activation instructions for this safety enhancement.

Nov 21, 2012
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB 2012-17

CFM International CFM56-5B engines — High Cycle Fatigue Failure of Low Pressure Turbine Active Clearance Control Fuel Manifolds

EASA Safety Information Bulletin 2012-17 is an advisory document addressing high cycle fatigue failure of Low Pressure Turbine Active Clearance Control (LPTACC) fuel manifolds on CFM International CFM56-5B turbofan engines. These engines are installed on Airbus A318, A319, A320, and A321 aircraft. The bulletin aligns with FAA Special Airworthiness Information Bulletin NE-12-29 and informs European operators and maintenance organizations about the issue and recommended actions.

Sep 20, 2012
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321