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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320262Airbus A321257Airbus A319229Airbus A350206Airbus A330197All177Airbus A318172Boeing 737164Airbus A380162Airbus A340136Airbus A350-941119Airbus Helicopters AS 332110Airbus Helicopters EC 225107Airbus Helicopters SA 330107Boeing 787106Show all...

EASA AD BR-2026-01-01

Engines Operation in Ground Freezing Fog - Operational Limitations Revision

The Brazilian Airworthiness Directive 2026-01-01 is a regulatory document issued by ANAC addressing operational limitations for Embraer ERJ190-300 and ERJ190-400 aircraft equipped with PW1900 family engines. It mandates restrictions on engine operation during ground freezing fog conditions to prevent compressor stalls in PW1100 engines. This directive aims to enhance flight safety by mitigating risks of multiple engine failures during critical flight phases.

Jan 9, 2026
Airworthiness DirectiveFlight OpsSafety MgmtEmbraer ERJ 190

EASA AD CF-2025-67

Time Limits/Maintenance Checks (TLMC) — New and Revised Airworthiness Limitations (AWL) Tasks

Canadian Airworthiness Directive CF-2025-67 addresses new and revised Airworthiness Limitations (AWL) tasks for Airbus Canada Limited Partnership (ACLP) aircraft models BD-500-1A10 and BD-500-1A11. This directive mandates compliance with updated time limits and maintenance checks to ensure continued airworthiness. It applies to all serial numbers 50001 and subsequent for BD-500-1A10, and 55001 and subsequent for BD-500-1A11.

Jan 9, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)

EASA AD US-2025-25-07

Turbine Engine - High-Pressure Turbine (HPT) Stage 1 and HPT Stage 2 Disks - Replacement

The Federal Aviation Administration's Airworthiness Directive 2025-25-07 addresses certain General Electric Company Model GE90-90B, GE90-94B, GE90-110B1, and GE90-115B engines. It requires replacement of specific high-pressure turbine (HPT) stage 1 and stage 2 disks suspected to contain iron inclusion in the powder metal material. This directive aims to prevent premature fracture and uncontained failure of these turbine disks.

Jan 9, 2026
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric GE90

EASA AD ISR-I-35-26-01-01

Potential of arcing, fire and/or loss of crew oxygen supply due to insufficient clearances between electrical wiring and flexible oxygen hose

Airworthiness Directive AD ISR I-35-26-01-01 issued by the Civil Aviation Authority of Israel addresses a safety issue on Boeing 747-400 freighter aircraft converted under CAAI STC SA-151 or SA-152 and their validated equivalents. The directive highlights the risk of arcing, fire, and loss of crew oxygen supply caused by insufficient clearance between electrical wiring and the flexible crew oxygen hose. It requires inspection and corrective action to prevent potential hazards related to chafing and damage to oxygen hoses and electrical wiring.

Jan 1, 2026
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 747Israel Aerospace Industries CAA Israel STC SA151Israel Aerospace Industries CAA Israel STC SA152

EASA SIB 2025-11

[Correction] Chemical Oxygen Generator Instructions for Disposal

EASA Safety Information Bulletin 2025-11 is a correction notice regarding the disposal instructions for B/E Aerospace Systems chemical oxygen generators with specific part numbers. It reminds operators that these generators have a certified service life of 15 years and must be activated and disposed of at the end of their life, even if unused. The bulletin also references EASA Airworthiness Directive 2024-0198 related to certain batches of generators with reduced starter powder reactivity.

Dec 26, 2025
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2025-0298-E

Main Rotor — Swashplate — Inspection

EASA Airworthiness Directive 2025-0298-E is an emergency directive addressing the inspection of the main rotor swashplate on MBB-BK117 D-3 and D-3m helicopters. It mandates repetitive inspections of the swashplate bolts, specifically those with Part Number D623M2050206, due to reported excessive wear that could lead to bolt rupture and reduced helicopter control. The directive applies to all serial numbers of the affected helicopter models.

Dec 23, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117

EASA AD 2025-0296

Tail Rotor Drive — Tail Drive Line Rear Shaft and Damper — Inspections

EASA Airworthiness Directive 2025-0296 is an airworthiness directive affecting all Airbus Helicopters H160-B serial numbers. It mandates inspections of the tail rotor drive line rear shaft and damper components, including specific part numbers such as tail rotor drive shafts P/N U651A1100102 and U651A1100103, rear damper P/N U651A2200103, and damper brackets P/N U535A2121207 and U535A2121208. The directive addresses potential unsafe conditions related to premature wear and contact between the rear shaft and damper.

Dec 23, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters H160

EASA AD 2025-0295

AIRCRAFT CABIN MODIFICATION - Equipment / Furnishings — Pallet Net — Limitation

EASA Airworthiness Directive 2025-0295 is an official regulatory document addressing safety concerns related to Aircraft Cabin Modification GmbH pallet nets, part number 5010-2M4N-()-()()(), used on various large aeroplanes for passenger and freight transport. The directive prohibits the use of these pallet nets manufactured on or before 20 May 2025 due to reported degradation issues. This AD applies to all serial numbers of the affected pallet nets and aims to prevent potential in-flight cargo release.

Dec 22, 2025
Airworthiness DirectiveMaintenanceSafety Mgmt

EASA AD 2025-0293

Fuselage — Inner Flange Glare Frames — Inspection

EASA Airworthiness Directive record for Fuselage — Inner Flange Glare Frames — Inspection provides information related to Airbus A400M military aeroplanes. Since there are currently no Airbus A400M aircraft in civil service, no public AD document exists. This record serves as a recommendation for military authorities responsible for the affected aircraft.

Dec 19, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Military A400M

EASA AD CF-2025-68

Landing Gear — Degraded Anti-Skid Performance on a Contaminated Runway

The Canadian Airworthiness Directive CF-2025-68 addresses degraded anti-skid performance on contaminated runways for Airbus Canada Limited Partnership BD-500-1A11 aircraft, serial numbers 55001 to 55388, 55390 to 55397, 55399, and 55402. This directive mandates corrective action to improve braking system software to prevent wheel lockup and loss of directional control during landing on contaminated surfaces.

Dec 19, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)

EASA AD 2025-0290

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2025-0290 is an amendment addressing time limits and maintenance checks in the Airworthiness Limitations Section for Dassault Aviation Falcon 900EX aeroplanes, including the Falcon 900EX Easy, Falcon 900LX, and Falcon 900DX models. This directive applies to aircraft with serial numbers 97 and 120 and above and mandates compliance with updated maintenance tasks and life limits as specified in the latest Aircraft Maintenance Manual. It ensures continued airworthiness by enforcing mandatory maintenance requirements.

Dec 19, 2025
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 900EX

EASA AD 2025-0291

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2025-0291 is an amendment concerning the Dassault Aviation Falcon 900EX aeroplanes, serial numbers 1 to 119 except 97. It updates the Airworthiness Limitations Section (ALS) in the Aircraft Maintenance Manual, Chapter 5-40, Revision 20, to ensure continued airworthiness through mandatory maintenance tasks and life-limited part replacements. This directive applies to Falcon 900EX aircraft operated under European regulations.

Dec 19, 2025
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 900EX

EASA AD 2025-0206R1

Engine — High Pressure Turbine Blades — Inspection

EASA Airworthiness Directive 2025-0206R1 is a regulatory update concerning the inspection of high pressure turbine (HPT) blades on Rolls-Royce Trent 1000 engines installed on Boeing 787 aircraft. It mandates repetitive on-wing borescope inspections of specific HPT blades to detect cracks and requires corrective actions including engine removal and blade replacement if cracks exceed defined limits. The directive applies to multiple Trent 1000 engine variants and aims to ensure continued airworthiness and safety.

Dec 18, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000

EASA AD 2025-0285

Wings — Main Wing Spar — Inspection

EASA Airworthiness Directive 2025-0285 is an airworthiness directive addressing the inspection of the main wing spars on AMS-FLIGHT d.o.o. CARAT A powered sailplanes, specifically serial numbers CA005 to CA010 inclusive and CA032. The directive mandates a one-time inspection of the bonding between the upper spar cap and the spar web on both left-hand and right-hand main wing spars to ensure structural integrity. This AD applies to aircraft certified under TCDS number EASA.A.448.

Dec 18, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAms - Flight CARAT A

EASA AD 2025-0286

Aircraft Flight Manual — Emergency Procedure Section — Amendment; Master Minimum Equipment List — Amendment; Communications — Digital Radio and Audio Integrating Management System — Modification

EASA Airworthiness Directive 2025-0286 is an amendment addressing Airbus A330-941 aeroplanes with specific manufacturer serial numbers. It mandates updates to the Aircraft Flight Manual emergency procedures, amendments to the Master Minimum Equipment List, and modifications to the Communications system involving the Digital Radio and Audio Integrating Management System. This directive ensures continued airworthiness and operational safety of affected Airbus A330 aircraft.

Dec 17, 2025
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtAirbus A330

EASA AD 2025-0288

Engine — Low Pressure Compressor Blades — Removal from Service

EASA Airworthiness Directive 2025-0288 is an official regulatory document addressing the removal from service of certain low pressure compressor blades installed on Rolls-Royce Deutschland RB211 Trent 700 engines, commonly found on Airbus A330 aircraft. The directive identifies specific part numbers and serial numbers of affected compressor blades that have undergone erroneous repairs, leading to potential blade cracking. It mandates inspections and removal of these parts to ensure continued airworthiness and safety.

Dec 17, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 700

EASA AD 25-196

Fuselage — Forward Fuselage Skin Panels — Inspection

EASA Airworthiness Directive Proposal 25-196 is a regulatory document addressing inspection requirements for forward fuselage skin panels on specific Airbus A319, A320, and A321 aircraft models. It applies to certain serial numbers and targets panels with potential thickness deviations identified by an Airbus supplier. The directive mandates inspections and possible corrective actions to ensure structural integrity.

Dec 17, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2025-0287

Powerplant — Fuel Draining System — Inspection

EASA Airworthiness Directive 2025-0287 is an airworthiness directive addressing Airbus Helicopters AS 355 series, including AS 355 E, F, F1, F2, N, and NP models. It mandates inspections and corrective actions for the fuel draining system's rear cargo compartment hoses, specifically part number 350A21010123, to prevent potential damage from hot air leakage and fire risks. The directive includes operational checks, installation of thermal paper, and silicone tape application to affected parts.

Dec 17, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 355

EASA AD 2025-0289

Wings — Centre Wing Box Fastener Holes at Frame 40 Vertical Web — Inspection

EASA Airworthiness Directive 2025-0289 is an airworthiness directive issued by EASA concerning Airbus A330-743L aeroplanes. It mandates inspections of the centre wing box fastener holes at Frame 40 vertical web to detect cracks that could compromise the structural integrity of the aircraft's centre fuselage. The directive applies to all manufacturer serial numbers of the Airbus A330-743L.

Dec 17, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330