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EASA Regulations & Airworthiness Directives

Browse 5057 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320281Airbus A321277Airbus A319247Airbus A350216Airbus A330211All198Airbus A318186Airbus A380178Boeing 737172Airbus A340140Airbus A350-941126Airbus BD-500 (A220 Series)119Airbus Helicopters AS 332118Airbus Helicopters EC 225115Airbus Helicopters SA 330115Show all...

EASA AD 26-031

Instruments — Fuse Cover Attachment of Circuit Breaker Panel — Modification

EASA Airworthiness Directive 26-031 is a proposed directive addressing a modification to the fuse cover attachment on the circuit breaker panel of Airbus Helicopters AS 350 B2, AS 350 B3, and EC 130 B4 models. The directive targets specific fuse covers with part numbers 350A76-2395-20, 350A76-2395-21, and 350A76-2395-23 that are part of certain control units. It aims to enhance safety by preventing interference with the pilot pedal controls.

Feb 20, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130

EASA AD 2026-0032

Tail Rotor — Tail Rotor Blades — Inspection

EASA Airworthiness Directive 2026-0032 is an airworthiness directive addressing inspection requirements for tail rotor blade assemblies on Airbus Helicopters Deutschland GmbH EC135 and EC635 helicopter models. It specifically targets tail rotor blade assemblies with part numbers L642A2002111 and L642A2002112 due to risks of intergranular corrosion and potential cracks. The directive mandates repetitive inspections to ensure continued airworthiness and safety.

Feb 19, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC135Airbus Helicopters 635

EASA AD 2026-0031

Tail Rotor — Tail Rotor Blades — Inspection

EASA Airworthiness Directive 2026-0031 is issued for Airbus Helicopters Deutschland GmbH EC135 and EC635 helicopter models. It mandates repetitive inspections of tail rotor blade assemblies with part number L642A2002121 due to risks of intergranular corrosion that may cause cracks and potential rupture. The directive applies to all variants and serial numbers of the affected helicopter models.

Feb 19, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC135Airbus Helicopters 635

EASA AD CF-2026-08

Equipment/Furnishings — Overhead Stowage Compartment — Handle Rod Disconnected

EASA Airworthiness Directive CF-2026-08 is a regulatory document addressing a safety issue in Airbus Canada Limited Partnership (ACLP) aircraft models BD-500-1A10 and BD-500-1A11. The directive focuses on the overhead stowage compartments where the handle rod may become disconnected, potentially preventing access to emergency equipment. This AD applies to specific serial numbers of these aircraft models and mandates corrective action to ensure safety.

Feb 12, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)

EASA AD CF-2026-09

Ice and Rain Protection — Engine Cowl Anti-Ice — Ejector Pipe Chafing

EASA Airworthiness Directive CF-2026-09 addresses ice and rain protection issues related to engine cowl anti-ice ejector pipe chafing on MHI RJ Aviation ULC model CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 aircraft. The directive mandates inspections and potential replacement of the ejector pipe and seal to prevent ice accumulation and engine shutdown. It applies to all serial numbers of the affected aircraft models.

Feb 12, 2026
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)

EASA AD 2026-0029

Tail Rotor Drive — Tail Gear Box Input Flange — Functional Checks

EASA Airworthiness Directive 2026-0029 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters SA 365 N models. It mandates repetitive functional checks on the tail gear box input flange, specifically part number 365A33500000, to ensure continued safe operation of the tail rotor drive system.

Feb 12, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SAAirbus Helicopters AS 365Airbus Helicopters EC 155

EASA AD 26-030

Time Limits / Maintenance Checks — Airworthiness Limitation Section Part 4, System Equipment Maintenance Requirements — Amendment

EASA Airworthiness Directive 26-030 is a proposed amendment affecting Airbus A330 aeroplanes, including models A330-201 through A330-941. It updates the Airworthiness Limitation Section Part 4, which covers System Equipment Maintenance Requirements, to ensure continued airworthiness. The directive applies to all manufacturer serial numbers and references Airbus A330 ALS Part 4 SEMR Revision 11.

Feb 12, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 26-028

Air Conditioning — Air Conditioning Pack — Inspection

EASA Airworthiness Directive 26-028 is a proposed directive addressing the inspection of the air conditioning pack exhaust plenum on Dassault Aviation Falcon 7X aeroplanes, including those modified to Falcon 8X standard. The directive targets specific exhaust plenum parts with Part Numbers 6112C020 and 6146C770 due to reported damage. It mandates inspections to ensure the structural integrity of the affected components.

Feb 11, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 7X

EASA AD 2024-0215R1

Main Rotor — Hub Sleeves — Inspection

EASA Airworthiness Directive 2024-0215R1 is an updated directive addressing inspection requirements for main rotor hub sleeves on Airbus Helicopters EC 225 LP models. It mandates repetitive inspections and, if necessary, replacement of affected main rotor hub sleeves with part number 332A31-3071-00 and associated blade pins to prevent structural failure. This directive applies to all serial numbers of the EC 225 LP helicopter.

Feb 11, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

EASA AD 2026-0027

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2026-0027 is an amendment concerning the time limits and maintenance checks detailed in the Airworthiness Limitations Section for SAFRAN Helicopter Engines ARRIUS 2B2 engines. These engines are commonly installed on Airbus Helicopters Deutschland EC135 and EC635 models. The directive updates mandatory maintenance tasks and life limits to ensure continued airworthiness of these engines.

Feb 11, 2026
Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIUS 2

EASA AD 2026-0028

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 — Damage Tolerant Airworthiness Limitation Items — Amendment

EASA Airworthiness Directive 2026-0028 is an amendment concerning the Airbus A318, A319, A320, and A321 aircraft family. It addresses updates to the Airworthiness Limitations Section Part 2, specifically the Damage Tolerant Airworthiness Limitation Items. This directive mandates compliance with revised maintenance tasks and intervals to ensure continued airworthiness of these aircraft models.

Feb 11, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0297R1

AEROSPACE & DEFENSE OXYGEN SYSTEMS SaS (Part of SAFRAN AEROSYSTEMS): Portable Breathing Equipment — Removal From Service

EASA Airworthiness Directive 2025-0297R1 is issued for Aerospace & Defense Oxygen Systems SaS Portable Breathing Equipment (PBE) Part Numbers 15-40F-11 and 15-40F-80 manufactured between November 2015 and March 2017. This directive mandates the removal from service of affected PBEs due to a manufacturing defect that may prevent oxygen delivery during use. The affected PBEs may be installed on any aircraft either during production or in-service modifications.

Feb 10, 2026
Airworthiness DirectiveMaintenanceSafety Mgmt

EASA AD 26-029

Stabilizers — NACA Vent Intake Panel — Modification

EASA Airworthiness Directive 26-029 is a proposed directive addressing Airbus A330 series aeroplanes, specifically models A330-202, A330-243, A330-243F, A330-302, A330-323, A330-343, A330-841, and A330-941 with certain modifications. The directive focuses on modifying the NACA vent intake panel installation on the stabilizers to prevent potential fuel leaks. This action is intended to enhance safety by reducing the risk of fire due to lightning ignition.

Feb 10, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 2026-0025

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 — Damage Tolerant Airworthiness Limitation Items — Amendment

EASA Airworthiness Directive 2026-0025 is an amendment affecting Airbus A330 series aeroplanes, including models A330-201 through A330-941. It mandates compliance with updated airworthiness limitations related to Damage Tolerant Airworthiness Limitation Items as specified in Airbus A330 Airworthiness Limitations Section Part 2 Revision 08 Issue 02. This directive ensures continued airworthiness by enforcing maintenance tasks and intervals approved by EASA.

Feb 10, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 2026-0026

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 — Damage Tolerant Airworthiness Limitation Items — Amendment

EASA Airworthiness Directive 2026-0026 is an amendment concerning the Airbus A340 series, including models A340-211, -212, -213, -311, -312, -313, -541, -542, -642, and -643. It updates the Airworthiness Limitations Section Part 2 related to Damage Tolerant Airworthiness Limitation Items. This directive mandates compliance with revised maintenance tasks to ensure continued airworthiness of these aircraft.

Feb 10, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A340

EASA AD 2025-0294R1

B/E AEROSPACE FISCHER GmbH: Medical Seats — Modification

EASA Airworthiness Directive 2025-0294R1 is issued for B/E Aerospace Fischer GmbH Medical Seats, specifically Part Number 9613-1-35-( ) with certain serial numbers. These seats are installed on helicopters including Airbus Helicopters Deutschland EC135, MBB-BK 117, Bell Textron Canada 429, and Bell Textron 412. The directive addresses a safety issue related to the swivel unit installed on these medical seats.

Feb 9, 2026
Airworthiness DirectiveMaintenanceSafety Mgmt

EASA AD 26-026

Equipment / Furnishings — Personal Locator Beacons installed on Emergency Life-Rafts — Operational Check

EASA Airworthiness Directive 26-026 is a proposed directive addressing the operational check of Personal Locator Beacons (PLBs) installed on emergency life-rafts of Airbus Helicopters EC 175 B models. It applies to all serial numbers of EC 175 B helicopters and focuses on specific PLB part numbers U256M30T1001 and 704A45737082. The directive aims to ensure the functionality of these PLBs to enhance safety during emergency situations.

Feb 9, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175

EASA AD 26-027

Fuel — Quantity Indicating Placard — Modification

EASA Airworthiness Directive 26-027 is a proposed directive addressing fuel quantity indicating placard modifications for Vulcanair P.68 "Victor" and P.68B "Victor" aeroplanes, serial numbers 1 to 182 inclusive. It targets specific fuel level indicators and placards to ensure accurate fuel quantity readings and warnings. The directive applies to aircraft with certain fuel tank configurations and requires updates to the Aircraft Flight Manual.

Feb 9, 2026
Airworthiness DirectiveMaintenanceSafety MgmtVulcanair P.68

EASA SIB 2026-01

Landing Gear - Degraded Anti-Skid Performance on Contaminated Runways

EASA Safety Information Bulletin 2026-01 is an airworthiness bulletin addressing degraded anti-skid performance on contaminated runways for Airbus Canada Limited Partnership BD-500-1A11 model aeroplanes, specifically serial numbers 55001 through 55388, 55390 through 55397, 55399, and 55402. The bulletin highlights safety concerns related to locked wheels and reduced braking performance under certain runway contamination conditions. It references related Transport Canada directives and service bulletins aimed at mitigating these risks.

Feb 9, 2026
Safety Information BulletinMaintenanceSafety MgmtAirbus BD-500 (A220 Series)

EASA AD 2025-0228R1

Standard Practices and Structures — DECOMATIC Titanium Bolts — Replacement

EASA Airworthiness Directive 2025-0228R1 addresses the replacement of DECOMATIC titanium bolts used in the standard practices and structures of Dassault Aviation Falcon 2000, Falcon 7X, and Falcon 900EX aircraft. This directive focuses on ensuring the continued airworthiness and structural integrity of these aircraft models by mandating specific bolt replacements. It applies directly to operators and maintenance organizations responsible for these Dassault Falcon aircraft types.

Feb 6, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 2000Dassault Falcon 7XDassault Falcon 900EX