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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 CF-2025-57

Stabilizers — Vertical Stabilizer Leading Edge Missing Clad Material

Canadian Airworthiness Directive CF-2025-57 addresses an issue with Bombardier Inc. model BD-700-2A12 aeroplanes, specifically serial numbers 70153 and 70160 through 70189. The directive concerns missing clad material on the vertical stabilizer leading edge, which can lead to corrosion and potential loss of structural integrity. It mandates inspections and protective coatings until the affected part is replaced.

Nov 20, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700

EASA AD CF-2023-38R1

Time Limits/Maintenance Checks — Introduction & Revision of the Airworthiness Limitations

Airworthiness Directive CF-2023-38R1 is a Canadian regulatory update affecting Bombardier Inc. BD-700-2A12 aeroplanes, specifically serial numbers 70005 through 70150. This directive introduces revisions to the Airworthiness Limitations (AWL) related to time limits and maintenance checks, ensuring continued airworthiness through updated maintenance requirements. It mandates compliance with the latest AWL Issue No. 017 as approved by Transport Canada.

Nov 20, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700

EASA AD 2025-0256

Wings — Centre Wing Box Frame 47 Angle Fittings — Inspection / Modification

EASA Airworthiness Directive 2025-0256 addresses inspection and modification requirements for the centre wing box frame 47 angle fittings on Airbus A300 F4-608ST aeroplanes. It mandates specific inspections and modifications to detect and correct cracks that could compromise the structural integrity of the aircraft's centre wing box. The directive applies to all manufacturer serial numbers of the A300 F4-608ST model.

Nov 20, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600ST (Beluga)

EASA AD 2018-0229R1

Wings — Centre Wing Box Frame 47 Angle Fittings — Inspection / Modification

EASA Airworthiness Directive 2018-0229R1 is a regulatory update addressing inspection and modification requirements for the centre wing box frame 47 angle fittings on Airbus A300-600 series aeroplanes. This directive applies to various A300-600 models except those already modified by Airbus Service Bulletin A300-57-6069. It mandates specific inspections and modifications to detect and correct cracks that could compromise the structural integrity of the aircraft's centre wing box.

Nov 20, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2025-0255

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

EASA Airworthiness Directive 2025-0255 is an amendment addressing the Airbus A300-600 aeroplanes. It mandates compliance with the updated Airworthiness Limitations Section Part 2, specifically the Damage Tolerant Airworthiness Limitations Items as defined in Airbus A300-600 ALS Part 2 Revision 4 Variation 4.3. This directive ensures continued airworthiness by enforcing new and more restrictive maintenance tasks for these aircraft.

Nov 19, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2025-0253

SUPERSEDED BY EASA AD 2025-0274

EASA Airworthiness Directive 2025-0253 is issued for Airbus A318, A319, A320, and A321 aeroplanes concerning fire panels with specific part numbers. The directive addresses the risk of engine fire switch self-releasing, which can cause uncommanded in-flight engine shutdown. It mandates inspection, replacement, and repair of affected fire panels to ensure continued airworthiness.

Nov 14, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD US-2025-23-51

SUPERSEDED BY FAA AD 2025-23-53

FAA Airworthiness Directive 2025-23-51 is a final rule addressing all Boeing Model MD-11 and MD-11F airplanes. It was issued following an accident where the left-hand engine and pylon detached during takeoff, prompting a safety directive to prevent further flight until inspections and corrective actions are completed. This directive aims to ensure continued safe flight and landing of these aircraft.

Nov 14, 2025
Airworthiness DirectiveSafety MgmtMaintenanceBoeing MD-11

EASA AD 2025-0252

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

EASA Airworthiness Directive 2025-0252 is an amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with updated maintenance tasks specified in the Airbus A380 Airworthiness Limitations Section Part 2, Damage Tolerant Airworthiness Limitation Items, Revision 11, Variation 11.2. This directive ensures continued airworthiness by incorporating new and more restrictive maintenance requirements.

Nov 14, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD CF-2025-58

Time Limits/Maintenance Checks (TLMC) — Airworthiness Limitations (AWL)

Airworthiness Directive CF-2025-58 is issued by Transport Canada and applies to Bombardier Inc. model BD-100-1A10 aeroplanes, specifically the Challenger 300 and Challenger 350 series. This directive mandates compliance with updated Time Limits/Maintenance Checks (TLMC) and Airworthiness Limitations (AWL) as published in Bombardier's TLMC manuals. It ensures that new or more restrictive maintenance tasks are performed to maintain the structural integrity and airworthiness of these aircraft.

Nov 14, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-100

EASA AD CF-2025-55

Navigation — 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace

The Canadian Airworthiness Directive CF-2025-55 addresses interference caused by 5G C-Band wireless broadband signals with radio altimeter systems on De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402 aircraft operating in Canadian airspace. It mandates specific operational limitations and modifications to ensure safe aircraft operation amid 5G deployment. The directive focuses on mitigating risks associated with erroneous radio altimeter data due to 5G signal interference.

Nov 12, 2025
Airworthiness DirectiveFlight OpsSafety MgmtDe Havilland Canada DHC-8

EASA AD CF-2025-54

Navigation — 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace affected by 5G C-Band wireless signals

Airworthiness Directive CF-2025-54 addresses interference issues between 5G C-Band wireless broadband signals and radio altimeter systems on De Havilland Aircraft of Canada DHC-8-100/-200/-300 aeroplanes operating in Canadian airspace. The directive mandates configuration of these aircraft as Radio Altimeter Tolerant (RAT) to ensure safe operation amid 5G C-Band deployments. It applies to all serial numbers of the specified aircraft models and focuses on mitigating erroneous radio altimeter data caused by 5G interference.

Nov 12, 2025
Airworthiness DirectiveSafety MgmtDe Havilland Canada DHC-8

EASA AD CF-2025-53

Flight Controls — Incorrect Airplane Flight Manual (AFM) Approach Speed Adder and Landing Distance Factors for SLAT FAIL (Caution) Crew-Alerting System (CAS) Message Non-Normal Procedure

Airworthiness Directive CF-2025-53 is issued by Transport Canada and applies to Bombardier Inc. model BD-700-1A10 and BD-700-1A11 aircraft, including Global Express, Global Express XRS, Global 6000, Global 5000, and related variants. This directive addresses incorrect approach speed adders and landing distance factors in the Airplane Flight Manual (AFM) related to the SLAT FAIL (Caution) Crew-Alerting System (CAS) message non-normal procedure. The directive mandates updates to the AFM to ensure safe flight operations.

Nov 10, 2025
Airworthiness DirectiveFlight OpsSafety MgmtBombardier BD-700

EASA AD 2025-0250

Fuselage — Frame Inboard Boom — Inspection

EASA Airworthiness Directive 2025-0250 is an airworthiness directive addressing Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates a one-time inspection of the fuselage frame inboard boom area at specific wing spar joint locations to detect cracks that could compromise structural integrity. The directive also requires reporting inspection results to Fokker Services.

Nov 10, 2025
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28

EASA AD CF-2024-22R1

Navigation — Required Navigation Performance Authorization Required (RNP-AR) Approach Vertical Deviation

The Navigation — Required Navigation Performance Authorization Required (RNP-AR) Approach Vertical Deviation Airworthiness Directive CF-2024-22R1 applies to Bombardier Inc. model BD-700-2A12 aeroplanes, serial numbers 70005 through 70193. This directive addresses vertical deviation issues during RNP-AR approaches caused by partial engine thrust loss under certain conditions. It mandates updates to the Airplane Flight Manual to ensure safe approach containment and obstacle clearance.

Nov 10, 2025
Airworthiness DirectiveFlight OpsSafety MgmtBombardier BD-700

EASA AD 2025-0249-E

SUPERSEDED BY EASA EMERGENCY AD 2025-0262-E

EASA Airworthiness Directive 2025-0249-E is an emergency directive addressing the Airbus Helicopters EC 130 T2 and EC 130 B4 models. It mandates the replacement of the tail rotor drive centre shaft assembly, part number 350A34021401, due to potential fatigue cracking that could lead to failure of the tail rotor drive shaft and loss of yaw control. This directive applies to all serial numbers of the affected helicopter models.

Nov 7, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130

EASA AD 2025-0248

Equipment / Furnishings — Overhead Stowage Compartments — Inspection / Repair

EASA Airworthiness Directive 2025-0248 is an airworthiness directive issued by the European Union Aviation Safety Agency addressing Airbus A318, A319, A320, and A321 aeroplanes equipped with ARIES overhead stowage compartments. The directive mandates inspection and repair of specific overhead stowage compartments to ensure their structural integrity. It applies to affected parts identified by certain part numbers and excludes aircraft with specific Airbus modifications embodied in production.

Nov 6, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB CASA-2025-11

Part Number MS20220-3 Pulleys with Corroded and Dislodged Bearings

Part Number MS20220-3 Pulleys with Corroded and Dislodged Bearings is a Transport Canada Civil Aviation Safety Alert (CASA 2025-11) addressing corrosion issues in flight control pulleys and pulley bearing assemblies installed on De Havilland Canada (DHC) DASH 8 series 100/200/300/400 aircraft. The alert highlights multiple service difficulty reports involving corroded and seized pulleys causing stiff roll control and autopilot disconnection. It targets operators and maintenance personnel responsible for the affected flight control systems.

Nov 3, 2025
Safety Information BulletinMaintenanceSafety MgmtDe Havilland Canada DHC-8

EASA AD CF-2025-52

Navigation — 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in the contiguous United States of America (U.S.) airspace.

The Canadian Airworthiness Directive CF-2025-52 addresses interference caused by 5G C-Band wireless broadband signals with radio altimeter systems on De Havilland Aircraft of Canada Limited DHC-8-100, -200, and -300 series aircraft operating in the contiguous United States airspace. This directive mandates modifications to affected aircraft radio altimeters to ensure tolerance against 5G interference and introduces interim operational limitations. It specifically targets aircraft equipped with Honeywell RT-300 radio altimeters.

Oct 31, 2025
Airworthiness DirectiveMaintenanceSafety MgmtDe Havilland Canada DHC-8

EASA AD 2025-0026R1

Oxygen — Full-Face Quick Donning Masks — Functional Check

The document titled "Oxygen — Full-Face Quick Donning Masks — Functional Check" is an explanatory statement regarding the absence of an Airworthiness Directive (AD) for the Airbus A400M aeroplane in civil service. It clarifies that no publicly available AD exists because the Airbus A400M is not in civil operation, and the content is provided by EASA solely for information to military authorities and design approval holders. The applicable AD for this aircraft type is issued by the responsible military authority depending on the country of registration.

Oct 31, 2025
OtherMaintenanceSafety MgmtAirbus Military A400M

EASA AD 2025-0238

[Correction] Electrical Power — Ram Air Turbine — Replacement

EASA Airworthiness Directive 2025-0238 is a corrective directive addressing the replacement of the Ram Air Turbine (RAT) module on Airbus A350-941 and A350-1041 aeroplanes. It targets RAT modules identified by Part Number 1713586A that have been deployed and retracted in flight, due to corrosion issues affecting electrical power generation. This directive applies to all manufacturer serial numbers of the specified Airbus A350 models.

Oct 30, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350