EASA Regulations & Airworthiness Directives

Browse 4968 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320278 Airbus A321274 Airbus A319245 Airbus A350213 Airbus A330209 All193 Airbus A318184 Airbus A380171 Boeing 737170 Airbus A340140 Airbus A350-941124 Airbus BD-500 (A220 Series)116 Airbus Helicopters AS 332115 Airbus Helicopters EC 225112 Airbus Helicopters SA 330112 Show all...

EASA AD 2025-0288R1

Engine – Low Pressure Compressor Blades – Removal from Service

EASA Airworthiness Directive 2025-0288R1 is an updated regulatory requirement 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 non-conforming repairs, posing a risk of blade cracking and potential engine failure. It mandates inspections, removal, and replacement of these parts to ensure continued airworthiness.

Jun 26, 2026

Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 700Airbus A330

EASA AD 2026-0122

Flight Controls – Droop Nose Geared Rotary Actuator Ring – Inspection / Replacement

EASA Airworthiness Directive 2026-0122 is an airworthiness directive applicable to Airbus A350-941 and A350-1041 aeroplanes. It addresses inspection and replacement requirements for the droop nose geared rotary actuator ring, specifically part number 4776A0000-03, due to identified corrosion issues. The directive mandates inspection and corrective actions to ensure continued safe operation of the affected flight control components.

Jun 26, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD CF-2026-33R1

Pneumatic – High Pressure Valve - Butterfly Clip Failure

The Pneumatic – High Pressure Valve - Butterfly Clip Failure Emergency Airworthiness Directive CF-2026-33R1 issued by Transport Canada applies to Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft models. It addresses the issue of missing or broken butterfly clips on high pressure valves that can cause bleed system isolation failure, hot air leakage, and potential structural damage. This directive mandates compliance with specific Minimum Equipment List (MEL) items to mitigate safety risks.

Jun 25, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A10Airbus Canada BD-500-1A11

EASA AD 2025-0237R1

[Correction] Equipment / Furnishings – 80 VU Rack Attachments – Inspection / Repair

The document titled '[Correction] Equipment / Furnishings – 80 VU Rack Attachments – Inspection / Repair' is a correction notice related to Airbus S.A.S. aircraft models A318, A319, A320, and A321. It addresses inspection and repair procedures for the 80 VU rack attachments used in these aircraft. The correction ensures accurate maintenance guidelines for these specific equipment components.

Jun 24, 2026

CorrectionMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2026-0121-E

Engine – Propeller Gearbox – Inspection

EASA Airworthiness Directive 2026-0121-E is an emergency directive addressing the inspection of propeller gearboxes installed on BRP-Rotax 912, 912 i, and 914 series engines used in various general aviation aircraft. The directive mandates a one-time inspection to verify the presence of the oil spray nozzle assembly and securing screws in the propeller gearbox. It applies to all serial numbers of the affected engines and gearboxes as specified in the associated BRP-Rotax Alert Service Bulletin ASB-2026-001R00.

Jun 24, 2026

Airworthiness DirectiveMaintenanceSafety MgmtBrp-Rotax Gmbh & Co Kg 912 ABrp-Rotax Gmbh & Co Kg 912 FBrp-Rotax Gmbh & Co Kg 912 SBrp-Rotax Gmbh & Co Kg 912 iScBrp-Rotax Gmbh & Co Kg 914 F

EASA AD 2026-0120

Fuselage – Lateral Window Frame – Inspections

EASA Airworthiness Directive 2026-0120 is an airworthiness directive addressing inspections of the fuselage lateral window frame on Airbus A319, A320, and A321 NEO aircraft models. It mandates repetitive high frequency eddy current inspections of the horizontal upper stiffeners at fuselage frame 4 to detect cracks and requires corrective actions if discrepancies are found. This directive applies to specific MSN aircraft except those with certain Airbus modifications embodied in production.

Jun 23, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321Airbus A321 NEO

EASA AD CF-2026-33

Pneumatic – High Pressure Valve - Butterfly Clip Failure

The Pneumatic – High Pressure Valve - Butterfly Clip Failure Emergency Airworthiness Directive CF-2026-33 issued by Transport Canada applies to Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft models. This directive addresses the failure of butterfly clips on high pressure valves which may lead to bleed system isolation issues, hot air leaks, and potential structural overheating. It prohibits dispatching affected aircraft under certain Minimum Equipment List (MEL) items until corrective actions are taken.

Jun 23, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A10Airbus Canada BD-500-1A11

EASA AD CF-2026-07R1

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

The Canadian Airworthiness Directive CF-2026-07R1 titled 'Ice and Rain Protection – Engine Cowl Anti-Ice – Ejector Pipe Chafing' applies to all serial numbers of the MHI RJ Aviation ULC model CL-600-2B19 aircraft. It addresses chafing damage to the engine cowl anti-ice ejector pipe and seal, which can lead to system degradation, ice accumulation, and potential engine shutdown. The directive mandates inspections and corrective actions to ensure continued airworthiness.

Jun 22, 2026

Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)MHI RJ Aviation ULC CL-600-2B19

EASA AD CF-2026-09R1

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

The Canadian Airworthiness Directive CF-2026-09R1 addresses ice and rain protection specifically concerning engine cowl anti-ice systems on MHI RJ Aviation ULC aircraft models CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25. It mandates inspections and potential replacements of the reactive exhaust pipe and sealing joint to prevent damage caused by chafing, which could lead to ice accumulation, engine ingestion of ice, and engine shutdown.

Jun 22, 2026

Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)MHI RJ Aviation ULC CL-600-2C10MHI RJ Aviation ULC CL-600-2C11MHI RJ Aviation ULC CL-600-2D15MHI RJ Aviation ULC CL-600-2D24MHI RJ Aviation ULC CL-600-2E25

EASA AD CF-2026-27

Nacelles/Pylons – Upper and Side Pylon Link Assemblies - Replacement

Canadian Airworthiness Directive CF-2026-27 addresses the replacement of upper and side pylon link assemblies on Airbus Canada Limited Partnership model BD-500-1A11 and BD-500-1A10 aircraft. The directive targets assemblies potentially manufactured from incorrect titanium alloy material, which could compromise structural integrity. It mandates verification and replacement of affected parts to ensure continued airworthiness.

Jun 22, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A11Airbus Canada BD-500-1A10

EASA AD 2026-0118

Rotors Flight Control – Tail Rotor Actuator – Inspection

EASA Airworthiness Directive 2026-0118 is issued for Airbus Helicopters SA 365 N, SA 365 N1, AS 365 N2, and AS 365 N3 models. It addresses inspection and modification requirements for tail rotor actuators with part numbers 704A47135036 or 704A47135059 to prevent interference that could block tail rotor pedal control. The directive mandates inspections and modifications to ensure safe yaw control of affected helicopters.

Jun 22, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SAAirbus Helicopters AS 365Airbus Helicopters EC 155Airbus Helicopters SA 365 NAirbus Helicopters SA 365 N1Airbus Helicopters AS 365 N2Airbus Helicopters AS 365 N3

EASA AD 2026-0119-E

Wings – Wing Mid Spars – Inspection

EASA Airworthiness Directive 2026-0119-E is an emergency directive addressing inspection requirements for the wing mid spars on Airbus A380-841, A380-842, and A380-861 aeroplanes with specific manufacturer serial numbers. It mandates special detailed inspections to detect cracks that could compromise wing structural integrity. The directive applies to certain serial numbers grouped into two categories with different compliance times.

Jun 22, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 26-074

Electrical Power – Direct Current Electrical Master Box – Inspection

EASA Airworthiness Directive PAD No. 26-074 is a proposed directive addressing the inspection of the direct current electrical master box on Airbus Helicopters AS 332 C, C1, L, and L1 models. It targets the printed circuit boards with part number GC11050 and serial numbers up to 400, aiming to prevent electrical short circuits that could affect the helicopter's DC power supply system.

Jun 19, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA AD 2026-0117

Engine – Low Pressure Turbine Discs – Inspection

EASA Airworthiness Directive 2026-0117 is an airworthiness directive addressing inspection requirements for Rolls-Royce Trent 1000 series engines installed on Boeing 787 aircraft and potentially other types. It mandates inspections of low pressure turbine stage 3 and stage 4 discs, specifically parts with P/N KH36323 and KH33943, to detect cracks caused by rubbing contact with interstage static seals. The directive aims to prevent turbine disc failure and potential damage to the aircraft.

Jun 19, 2026

Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Boeing 787

EASA AD CF-2026-24

Fire Protection – Main Wheel Well Bin Sensing Element – Incompatible Connector Nut - Replacement

Canadian Airworthiness Directive CF-2026-24 addresses a fire protection issue related to the main wheel well bin sensing element on Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft. The directive mandates the replacement of incompatible connector nuts that have shown corrosion, which could compromise the fire detection system. This AD applies to specific serial numbers of these aircraft models.

Jun 19, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A10Airbus Canada BD-500-1A11

EASA AD CF-2026-25

Indicating/Recording System – Misleading Caution Messages Posted on Engine Indicating and Crew Alerting System during Air Driven Generator Deployment

Canadian Airworthiness Directive CF-2026-25 addresses misleading caution messages displayed on the Engine Indicating and Crew Alerting System (EICAS) during Air Driven Generator (ADG) deployment in MHI RJ Aviation ULC aircraft models CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25. The directive mandates updates to the Aircraft Flight Manual (AFM) to correct message logic and clarify procedures during emergency power conditions.

Jun 19, 2026

Airworthiness DirectiveFlight OpsSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)MHI RJ Aviation ULC CL-600-2C10MHI RJ Aviation ULC CL-600-2C11MHI RJ Aviation ULC CL-600-2D15MHI RJ Aviation ULC CL-600-2D24MHI RJ Aviation ULC CL-600-2E25

EASA AD US-2026-13-51

Power Plant - Engine Mount System - Inspection

Emergency Airworthiness Directive FAA AD 2026-13-51 addresses a critical safety issue affecting Gulfstream Aerospace Corporation Model GVIII-G700 and GVIII-G800 airplanes. The directive focuses on inspecting the engine mount system, specifically the engine thrust strut mounts, due to reports of broken hollow pin caps caused by missing or displaced sleeve bushings. This condition risks structural failure of the engine mount system and possible in-flight engine separation.

Jun 19, 2026

Airworthiness DirectiveMaintenanceSafety MgmtGulfstream Aerospace Corporation GVIIIGulfstream Aerospace Corporation GVIII-G700Gulfstream Aerospace Corporation GVIII-G800

EASA AD US-2026-12-07

Auto Flight - Mode Control Panel - Replacement

The Federal Aviation Administration's Airworthiness Directive 2026-12-07 is a final rule addressing certain Boeing 787-8, 787-9, and 787-10 airplanes. It mandates replacement of the existing mode control panel (MCP) with an updated version to prevent uncommanded changes to the MCP selected altitude. This directive aims to enhance flight safety by mitigating risks of controlled flight into terrain or mid-air collisions.

Jun 18, 2026

Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787Boeing 787-8Boeing 787-9Boeing 787-10

EASA AD 26-076

Flight Controls – Maintenance and Avionics Interface Computer Software – Modification; Airplane Flight Manual – Amendment

EASA Proposed Airworthiness Directive 26-076 addresses Dassault Aviation Falcon 7X aeroplanes, serial numbers 2 through 400 inclusive, that have not incorporated modification M1000. This directive focuses on maintenance and avionics interface computer software modifications and amendments to the Airplane Flight Manual to improve flight control safety. It supersedes a previous emergency AD and mandates software upgrades and procedural updates to ensure proper crew awareness of inboard slat configurations during flight.

Jun 18, 2026

Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 7X

EASA AD 26-075

Integrated Modular Avionics – Primus APEX DFZ Build 6.0 Software – Modification

EASA Airworthiness Directive PAD No. 26-075 is a proposed directive addressing the Primus APEX DFZ Build 6.0 software modification for Pilatus PC-24 aeroplanes, specifically those with manufacturer serial numbers 101 to 337 and 501 to 600. This directive targets the integrated modular avionics system to correct flight director calculation errors on affected aircraft. It applies to PC-24 aircraft equipped with earlier software versions and mandates software updates and flight manual amendments.

Jun 18, 2026

Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-24Pilatus PC-24