EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320262 Airbus A321257 Airbus A319229 Airbus A350206 Airbus A330197 All177 Airbus A318172 Boeing 737164 Airbus A380162 Airbus A340136 Airbus A350-941119 Airbus Helicopters AS 332110 Airbus Helicopters EC 225107 Airbus Helicopters SA 330107 Boeing 787106 Show all...

EASA AD 2026-0037

Equipment/Furnishings — Evacuation Slide/Inflation Hose Assemblies — Replacement

EASA Airworthiness Directive 2026-0037 is an official safety directive addressing evacuation slide inflation hose assemblies on Airbus A318, A319, A320, and A321 aircraft. It targets specific inflation hose assemblies and door evacuation slides identified by part and serial numbers that have been found to fail during emergency evacuations. The directive mandates the replacement of affected evacuation slides to ensure proper inflation and safe evacuation.

Feb 25, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2026-0035

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

EASA Airworthiness Directive 2026-0035 is an amendment addressing time limits and maintenance checks for Airbus A330-743L aeroplanes. It updates the Airworthiness Limitations Section Part 1 concerning Safe Life Airworthiness Limitation Items to ensure continued airworthiness. This directive applies to all manufacturer serial numbers of the Airbus A330-743L model.

Feb 25, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 2026-0036

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

EASA Airworthiness Directive 2026-0036 is an amendment addressing the Airworthiness Limitations Section Part 2 for Airbus A330-743L aeroplanes. It mandates compliance with updated damage tolerant airworthiness limitation items to ensure continued airworthiness of these aircraft. The directive applies to all Airbus A330-743L serial numbers and updates maintenance requirements.

Feb 25, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 26-032

Hydraulic Power — Engine-driven Pump — Software Update / Modification; Aircraft Flight Manual — Abnormal and Emergency Procedures — Amendment

EASA Airworthiness Directive 26-032 is a proposed directive addressing hydraulic power issues related to the engine-driven pump software and Aircraft Flight Manual amendments for Airbus A350-941 and A350-1041 aeroplanes. It applies to aircraft except those with Airbus modifications 116830 and 117811 incorporated in production. The directive focuses on updating software and replacing affected engine-driven pumps to prevent overheating and potential hydraulic system failures.

Feb 23, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350

EASA AD 26-033

Powerplant — Engine Shock Mounts — Replacement

EASA Airworthiness Directive 26-033 is a proposed directive addressing the replacement of engine shock mounts on Tecnam P2006T and P2006T NG aeroplanes. It targets engine shock mounts with Part Number CONO21-BS from specific manufacturing batches 49-24 and 11-25. The directive aims to ensure continued airworthiness by mandating replacement and inspection of these parts.

Feb 23, 2026

Airworthiness DirectiveMaintenanceSafety MgmtTecnam P2006T

EASA AD 2026-0034

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

EASA Airworthiness Directive 2026-0034 is an amendment concerning the Airbus A350-941 and A350-1041 aeroplanes. It addresses updates to the Airworthiness Limitations Section Part 2, specifically the Damage Tolerant Airworthiness Limitation Items (DT-ALI). This directive mandates compliance with new and more restrictive maintenance tasks introduced in Variation 11.1 of the Airbus A350 ALS Part 2 document.

Feb 23, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350

EASA AD 2026-0033

Engine — High-Pressure Turbine Inner Stationary Seal — Inspection

EASA Airworthiness Directive 2026-0033 is issued for CFM International CFM56-5B, CFM56-5C, and CFM56-7B engines installed on aircraft including Airbus A318, A319, A320, A321, A340 and Boeing 737-600 through 737-900ER series. The directive mandates inspections of the high-pressure turbine inner stationary seal and the rotating air high-pressure turbine front seal to detect cracks or honeycomb separation. It addresses potential risks of seal failure that could lead to uncontained engine damage and possible harm to the aircraft.

Feb 20, 2026

Airworthiness DirectiveMaintenanceSafety MgmtCFM International CFM56-5BCFM International CFM56-5CCFM International CFM56-7B

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