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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 US-2024-05-09

Fuselage - Station 1640 - Maintenance Records Check / Frame Web - Inspection

Federal Aviation Administration Airworthiness Directive 2024-05-09 is a final rule addressing certain Boeing 757-200, -200CB, and -300 series airplanes. It mandates inspections and maintenance record checks due to a reported crack at fuselage station 1640 frame web near the lower hinge intercostal tee clip center hole of the upper fastener row. The directive aims to ensure structural integrity by detecting and repairing potential cracks.

Apr 10, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757Boeing 757-200Boeing 757-200CBBoeing 757-300

EASA AD US-2024-04-09

Instruments - Wing Anti-Ice Valve / Autothrottle - Software Installation

Airworthiness Directive 2024-04-09 issued by the Federal Aviation Administration addresses certain Boeing 777-200, 777-200LR, 777-300, 777-300ER, and 777F series airplanes. It mandates software installation and configuration checks to resolve wing anti-ice valve failures and autothrottle disconnection issues that could compromise flight safety. The directive targets software updates to improve low-speed protection and response to unreliable airspeed events.

Apr 10, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 777Boeing 777-200Boeing 777-200LRBoeing 777-300Boeing 777-300ERBoeing 777F

EASA AD US-2024-05-11

Engine - High-Pressure Turbine 1st / 2nd Stage Hub / High Pressure Compressor 7th and 8th Stage Integrally Bladed Rotors / Rear Hub - Inspection / Replacement

Airworthiness Directive 2024-05-11 is a final rule issued by the Federal Aviation Administration addressing certain International Aero Engines, LLC Model PW1100G and PW1400G series engines. It mandates inspections and accelerated replacements of high-pressure turbine 1st and 2nd stage hubs, high-pressure compressor 7th and 8th stage integrally bladed rotors, and the HPC rear hub to mitigate risks associated with powdered metal anomalies. This directive aims to prevent uncontained failures that could lead to engine and aircraft damage.

Apr 9, 2024
Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines PW1100International Aero Engines PW1400

EASA AD 2024-0082

SUPERSEDED BY EASA AD 2025-0101

EASA Airworthiness Directive 2025-0101 is an informational document regarding Ratier-Figeac FH385 and FH386 series propellers. It clarifies that no such propellers are currently in civil service, and therefore, no public AD exists for them. The directive serves as a recommendation to military authorities responsible for aircraft equipped with these propellers.

Apr 9, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRatier-Figeac FH385Ratier-Figeac FH386

EASA AD 2024-0083

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

EASA Airworthiness Directive 2024-0083 is an amendment addressing the Airbus A300-600 aeroplanes equipped with Airbus modification 12046. It mandates compliance with new and more restrictive maintenance tasks introduced in the Airbus A300-600 Airworthiness Limitations Section Part 2 Revision 4 Variation 4.1. This directive ensures continued airworthiness by updating time limits and maintenance checks related to damage tolerant airworthiness limitation items.

Apr 9, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2024-0079

[Correction] Landing Gear — Body Landing Gear Rear Axle — Replacement

[Correction] Landing Gear — Body Landing Gear Rear Axle — Replacement is a correction document related to the Airbus S.A.S. A380 aircraft. It addresses the replacement procedures or requirements for the rear axle of the body landing gear on this specific aircraft model. The document ensures proper maintenance and safety standards for the landing gear component.

Apr 4, 2024
CRDMaintenanceSafety MgmtAirbus A380

EASA AD 2024-0081

SUPERSEDED BY EASA AD 2024-0096

EASA Airworthiness Directive 2024-0081 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting ATR 42-400, ATR 42-500, and various ATR 72 models. It addresses the inspection and testing requirements for the rudder travel limiting unit (TLU) lever, part number S2728183300200, due to potential corrosion and premature failure risks. The directive mandates repetitive inspections and conductivity tests to ensure continued safe operation of the affected aircraft.

Apr 4, 2024
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72ATR 42-400ATR 42-500ATR 72

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