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EASA Regulations & Airworthiness Directives

Browse 4987 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320280Airbus A321276Airbus A319246Airbus A350214Airbus A330209All193Airbus A318185Airbus A380171Boeing 737170Airbus A340140Airbus A350-941125Airbus BD-500 (A220 Series)116Airbus Helicopters AS 332115Airbus Helicopters EC 225112Airbus Helicopters SA 330112Show all...

EASA AD 2024-0080

SUPERSEDED BY EASA AD 2026-0036

EASA Airworthiness Directive 2024-0080 is issued for Airbus A330-743L aeroplanes. It mandates compliance with updated Damage Tolerant Airworthiness Limitation Items (DT-ALI) as specified in the Airbus A330-700L Airworthiness Limitations Section Part 2 Revision 01 and Variation 1.1. This directive ensures continued airworthiness by requiring operators to follow new or more restrictive maintenance tasks.

Mar 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus A330-743L

EASA AD CF-2024-11

SUPERSEDED BY TCCA EMERGENCY AD CF-2025-29

The Canadian Airworthiness Directive CF-2024-11 is an urgent airworthiness directive affecting Bell Textron Canada Limited Model 429 helicopters with serial numbers 57001 and above. It addresses cracking in the anti-abrasion strips of the tail rotor blades, which could lead to catastrophic failure of the tail rotor and loss of directional thrust during critical flight phases. The directive mandates inspections, marking, and potential replacement of affected tail rotor blades to ensure continued airworthiness.

Mar 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBell 429Bell Textron Canada Limited 429

EASA AD US-2024-06-51

Engine - Torque Reference Tube Magnetic Insert Joint - Ultrasonic Inspection

The document titled 'Engine - Torque Reference Tube Magnetic Insert Joint - Ultrasonic Inspection' is a regulatory directive concerning the ultrasonic inspection of the magnetic insert joint in the torque reference tube of certain aircraft engines. It addresses the need for specific non-destructive testing to ensure the integrity and safety of this engine component. The directive is relevant to aviation maintenance and inspection professionals responsible for engine airworthiness.

Mar 25, 2024
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric CT7-2General Electric CT7-8

EASA AD 2024-0078

Equipment / Furnishings — AFT Galley Complex Lower Attachment Studs — Inspection / Replacement

EASA Airworthiness Directive 2024-0078 is issued for Airbus A350-941 and A350-1041 aeroplanes, addressing inspection and replacement of the aft galley complex lower attachment studs. The directive targets specific part numbers of lower attachment studs that secure the aft galley complex to the aircraft structure. It mandates inspections and replacement to ensure continued airworthiness and safety.

Mar 20, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD 2023-0132R1

Wings — Inboard Flap Trunnion — Inspection / Modification

EASA Airworthiness Directive 2023-0132R1 is an updated safety directive addressing inspection and modification requirements for the inboard flap trunnion on Airbus A350-941 aeroplanes, specifically serial numbers 0005 through 0046 excluding 0025 and 0033. The directive mandates inspections and potential modifications of affected trunnion arms made of forging aluminium 7037 to ensure structural integrity. It applies to specific part numbers installed on these aircraft.

Mar 20, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941

EASA AD 2024-0076

Wings — Ailerons — Inspection

EASA Airworthiness Directive 2024-0076 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Dassault Aviation Falcon 7X aeroplanes, including those modified as Falcon 8X. It mandates inspections of specific ailerons identified by part numbers and serial numbers to detect excessive trailing edge thickness that could compromise structural integrity. The directive provides detailed inspection and corrective action instructions based on Dassault Service Bulletins 7X-593 Revision 2 and 7X-594 Revision 1.

Mar 19, 2024
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 7XDassault Falcon 8X

EASA AD 2024-0075

Doors — Passenger Jettisonable Window Mechanism — Replacement

EASA Airworthiness Directive 2024-0075 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters H160 B models modified by EASA Supplemental Type Certificate 10080809. It addresses the replacement of passenger jettisonable window mechanisms due to potential safety issues with the self-locking nuts and cable kits in the window jettisoning system. The directive mandates corrective actions to ensure the continued airworthiness and safety of the affected helicopters.

Mar 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters H160Airbus Helicopters H160 B

EASA AD 2024-0073

Equipment / Furnishings — Galley Lower Attachment Studs — Inspection — Maintenance Task

EASA Airworthiness Directive 2024-0073 is an airworthiness directive issued by EASA affecting Airbus A350-941 and A350-1041 aeroplanes manufactured on or before 31 December 2023. It addresses inspection and maintenance requirements for specific galley lower attachment studs with certain part numbers. The directive mandates a one-time inspection and corrective actions to ensure the safe installation of these studs.

Mar 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD 2024-0064R1

Stabilizers — Horizontal Stabilizer — Replacement

EASA Airworthiness Directive 2024-0064R1 is an updated regulatory requirement addressing the replacement of horizontal stabilizers on Airbus Helicopters EC 175 B models. It applies to all serial numbers of the EC 175 B and targets specific part numbers of horizontal stabilizers, fittings, and bolts. The directive mandates inspections and modifications to prevent potential loss of the horizontal stabilizer due to cracks, which could lead to loss of control of the helicopter.

Mar 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175Airbus Helicopters EC 175 B

EASA AD US-2024-05-51

SUPERSEDED BY FAA AD US-2024-06-51

FAA Airworthiness Directive 2024-05-51 is a final rule addressing certain General Electric Company Model CT7 and T700 series engines installed on various restricted category helicopters. This directive mandates inspections of the torque reference tube magnetic insert braze joint on the power turbine drive shaft assembly due to reported failures. The directive aims to ensure continued airworthiness and safety of affected aircraft by preventing potential loss of control.

Mar 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric CT7-2General Electric CT7-8General Electric Company Model CT7General Electric Company Model T700

EASA AD 2024-0072

Information Systems — Electronic Display Unit — Replacement

EASA Airworthiness Directive 2024-0072 is an airworthiness directive addressing the replacement of electronic display units (EDU) on Dassault Aviation Falcon 900EX, Falcon 2000EX, and Falcon 7X aircraft. The directive targets CMA-1310 EDUs with specific part numbers and modification statuses that have been found to have lithium-polymer battery swelling issues. It mandates replacement with modified units to ensure continued safe operation.

Mar 15, 2024
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 2000Dassault Falcon 7XDassault Falcon 900EXDassault Falcon 2000EX

EASA AD 2024-0071

Main Rotor — Swashplate— Inspection

EASA Airworthiness Directive 2024-0071 is an airworthiness directive addressing the inspection of the main rotor swashplate on Hélicoptères Guimbal Cabri G2 helicopters. It applies to all serial numbers of the Cabri G2 and focuses on inspecting swashplates with Part Number G41-00-000 for cracks. The directive mandates regular inspections to ensure continued airworthiness and prevent potential failure of the swashplate.

Mar 14, 2024
Airworthiness DirectiveMaintenanceSafety MgmtGuimbal, Helicopteres CABRIHélicoptères Guimbal Cabri G2

EASA AD 2024-0070

Oil — Front Bearing Housing Oil Feed Tube Assembly — Replacement

EASA Airworthiness Directive 2024-0070 is an airworthiness directive addressing Rolls-Royce Trent XWB-75, Trent XWB-79, Trent XWB-79B, and Trent XWB-84 engines installed on Airbus A350 aircraft. The directive mandates the replacement of front bearing housing oil feed tube assemblies with a specific serviceable part to ensure safe engine operation. It applies to all serial numbers of these engine models.

Mar 14, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT XWBAirbus A350

EASA AD US-2024-04-02

Tail Rotor - Tail Rotor Blade Tip Cap - Inspection

The Federal Aviation Administration Airworthiness Directive 2024-04-02 is a final rule addressing certain Robinson Helicopter Company Model R22, R22 Alpha, R22 Beta, R22 Mariner, R44, R44 II, and R66 helicopters. It focuses on inspecting tail rotor blade (TRB) tip caps with specific part and serial numbers for corrosion and requires removal of affected TRBs from service to prevent unsafe conditions.

Mar 14, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRobinson R22Robinson R44 (Raven)Robinson R66Robinson R22 AlphaRobinson R22 BetaRobinson R22 MarinerRobinson R44Robinson R44 II

EASA SIB 2024-05

Incorrect Computation of the Hybrid Flight Path Angle by LCR-100 Attitude Heading Reference System

EASA Safety Information Bulletin 2024-05 addresses an incorrect computation of the Hybrid Flight Path Angle by the Northrop Grumman LITEF GmbH LCR-100 Attitude Heading Reference System (AHRS) with specific software part numbers. The issue affects units with modification 28 and/or 29 when zero values are stored for Lever Arms to Centre of Gravity in the Installation Data Module. This bulletin informs type certificate and supplemental type certificate holders about the erroneous data output affecting ARINC Labels 263, 134, and 262.

Mar 13, 2024
Safety Information BulletinSafety MgmtMaintenance

EASA AD 2024-0069-E

Engine — High Pressure Compressor / Stage 1 and 2 Rotor Path Liners — Inspection

EASA Airworthiness Directive 2024-0069-E is an emergency directive addressing inspection requirements for the high pressure compressor stage 1 and 2 rotor path liners on Rolls-Royce Deutschland RB211-524H-36 and RB211-524H-T-36 engines, commonly installed on Boeing 767 aircraft. The directive mandates borescope inspections to detect potential damage that could lead to engine surges and dual engine shutdown. It applies to all manufacturer serial numbers of the affected engines.

Mar 12, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211-524Boeing 767

EASA AD 2024-0068

Fuselage — Lateral Cockpit Window Frame Upper Stiffener — Inspection

EASA Airworthiness Directive 2024-0068 is an inspection directive affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates special detailed inspections of the lateral cockpit window frame upper stiffener at fuselage frame 4 to detect cracks that could compromise structural integrity. The directive applies to specific aircraft configurations excluding those with certain Airbus modifications embodied in production or service.

Mar 11, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2024-0067-E

Engine — Life Limited Parts — Replacement

EASA Airworthiness Directive 2024-0067-E is an emergency directive addressing life limited parts replacement for CFM International CFM56 series engines, including models CFM56-2, -3, -5, -5B, -5C, and -7B. These engines are commonly installed on Airbus A318, A319, A320, A321, A340, and Boeing 737 series aircraft from the 300 to 900ER variants. The directive targets specific compressor discharge pressure seals, high-pressure compressor stage 3 disks, and high-pressure turbine rear shafts identified as affected parts due to potential damage from improper maintenance.

Mar 9, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCFM International CFM56-2CFM International CFM56-3CFM International CFM56-5CFM International CFM56-5BCFM International CFM56-5CCFM International CFM56-7BAirbus A318Airbus A319Airbus A320Airbus A321Airbus A340Boeing 737

EASA AD CF-2024-10

Flight Controls — Elevator Power Control Unit Bracket Cracks

Canadian Airworthiness Directive CF-2024-10 addresses cracks found in the elevator power control unit (PCU) brackets and elevator front spar on De Havilland Aircraft of Canada Limited model DHC-8-401 and DHC-8-402 aeroplanes, serial numbers 4001 and 4003 through 4580. The directive mandates inspections and corrective actions to prevent potential elevator jamming and loss of pitch control. It applies to specific parts including the horizontal stabilizer rear spar assembly P/N 85517044 and elevator structure assembly P/N 85527021.

Mar 8, 2024
Airworthiness DirectiveMaintenanceSafety MgmtDe Havilland Canada DHC-8De Havilland Aircraft of Canada DHC-8-401De Havilland Aircraft of Canada DHC-8-402

EASA AD 2021-0217R1

SUPERSEDED BY EASA AD 2024-0116

EASA Airworthiness Directive 2021-0217R1 is an amendment concerning Rolls-Royce Deutschland Ltd & Co KG Trent XWB-75, Trent XWB-79, Trent XWB-79B, and Trent XWB-84 engines, commonly installed on Airbus A350 aircraft. This directive mandates compliance with updated airworthiness limitations and maintenance instructions specified in the Rolls-Royce Trent XWB Time Limits Manual. It ensures continued airworthiness by enforcing mandatory inspections and life-limited part replacements.

Mar 8, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT XWBAirbus A350