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EASA Regulations & Airworthiness Directives

Browse 4983 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320278Airbus A321274Airbus A319245Airbus A350213Airbus A330209All193Airbus A318184Airbus A380171Boeing 737170Airbus A340140Airbus A350-941124Airbus BD-500 (A220 Series)116Airbus Helicopters AS 332115Airbus Helicopters EC 225112Airbus Helicopters SA 330112Show all...

EASA AD 2025-0121

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 1, Safe Life Airworthiness Limitations Items — Amendment

EASA Airworthiness Directive 2025-0121 is an amendment concerning the Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 1, Safe Life Airworthiness Limitations Items, requiring compliance with the latest Airbus A380 ALS Revision 13. This directive mandates replacement of life-limited parts and updates to the Aircraft Maintenance Programme to ensure continued airworthiness.

May 28, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA SIB 2025-04

Use of Protective Breathing Equipment

EASA Safety Information Bulletin 2025-04 provides guidance on the use of Protective Breathing Equipment (PBE) for air crew members. It applies to National Competent Authorities, aircraft operators, training organisations, and PBE manufacturers. The bulletin emphasizes proper training, usage, and limitations of PBEs, which protect crew from smoke, toxic fumes, and harmful gases during firefighting, smoke events, and dangerous goods incidents.

May 28, 2025
Safety Information BulletinTrainingSafety Mgmt

EASA SIB 2025-05

Development and Usage of Procedures for Visual Manoeuvring with Prescribed Tracks Relying on Required Navigation Performance

EASA Safety Information Bulletin 2025-05 is a guidance document addressing the development and use of Procedures for Visual Manoeuvring with Prescribed Tracks relying on Required Navigation Performance (RNP). It targets aircraft operators, air navigation service providers, aerodrome operators, flight procedure designers, design approval holders, and national competent authorities. The bulletin focuses on enhancing safety and predictability during visual manoeuvring by integrating RNP-based guidance, applicable to various aircraft equipped with compatible Flight Management Systems.

May 27, 2025
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB 2025-03

Passenger and Crew Awareness on the Risks of Lithium Batteries

EASA Safety Information Bulletin No. 2025-03 is a guidance document addressing passenger and crew awareness on the risks associated with lithium batteries carried on commercial passenger aircraft. It applies to aircraft operators, aerodrome operators, ground handling service providers, and National Competent Authorities. The bulletin highlights the dangers posed by portable electronic devices and transportation devices powered by lithium batteries, including e-cigarettes and power banks, and provides recommendations to mitigate these risks during air operations.

May 27, 2025
Safety Information BulletinSafety MgmtTraining

EASA AD 2025-0120

Cabin Systems — Antenna Adapter Plate — Inspection

EASA Airworthiness Directive 2025-0120 is an airworthiness directive addressing inspection requirements for the antenna adapter plate and related parts installed on Airbus A319, A320, A321, A330, A350, and A380 aircraft models. The directive mandates repetitive general visual inspections of affected broadband antenna adapter plates to detect corrosion and cracks that could compromise aircraft safety. It applies to all manufacturer serial numbers of the specified Airbus models.

May 26, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321Airbus A330Airbus A350Airbus A380

EASA AD US-2025-10-04

Engine - High Pressure Turbine Shroud / Low Pressure Turbine Nozzle Assemblies - Inspection

The Federal Aviation Administration's Airworthiness Directive 2025-10-04 addresses all General Electric Company Model CF34-10E2A1, CF34-10E5, CF34-10E5A1, CF34-10E6, CF34-10E6A1, CF34-10E7, and CF34-10E7-B engines equipped with specific high-pressure turbine shroud/low-pressure turbine nozzle assemblies. This directive mandates inspections and rework due to failed retention features of support air ducts discovered during engine disassembly. The AD aims to prevent combustion case failure that could lead to engine separation and potential loss of the airplane.

May 26, 2025
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric CF34-10

EASA AD G-2025-0003

Time Limits / Maintenance Checks — Airworthiness Limitations Section Amendment

The UK Civil Aviation Authority Airworthiness Directive G-2025-0003 is an amendment concerning the Time Limits and Maintenance Checks within the Airworthiness Limitations Section for BAE Systems BAe 146 and AVRO 146-RJ aeroplanes. It updates the mandatory maintenance tasks and life limits to ensure continued airworthiness of all models and serial numbers of these aircraft. The directive includes revised maintenance manuals and associated documents applicable from 5 June 2025.

May 26, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBae Systems (Operations) AVRO146RJBae Systems (Operations) BAE146

EASA AD 2025-0119

Time Limits / Maintenance Checks — Time Limits Manual / Maintenance Programme — Amendment

EASA Airworthiness Directive 2025-0119 is an amendment concerning the Rolls-Royce Trent XWB series engines installed on Airbus A350 aircraft. It updates the Time Limits Manual and Maintenance Programme requirements for Trent XWB-75, Trent XWB-79, Trent XWB-79B, Trent XWB-84, and Trent XWB-97 engines to ensure continued airworthiness. The directive mandates compliance with the latest maintenance tasks and life limits as specified in the revised Rolls-Royce Trent XWB Time Limits Manual Revision 061.

May 26, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT XWB

EASA AD CF-2019-39R1

Fuel System — Fuel Tank Connection Hose Deterioration

Canadian Airworthiness Directive CF-2019-39R1 addresses fuel tank connection hose deterioration in Diamond Aircraft Industries Inc. models DA 40, DA 40 D, DA 40 F, and DA 40 NG aeroplanes. The directive mandates inspection and replacement of affected fuel tank connection hoses and removal of any detached rubber parts found in the fuel system. It applies to all serial numbers of these aircraft models and references specific Mandatory Service Bulletins for compliance.

May 22, 2025
Airworthiness DirectiveMaintenanceSafety MgmtDiamond Aircraft Industries, DA 40

EASA AD CF-2025-27

Fuselage — Cracks on Aft Wing to Body Fairing Structure

Canadian Airworthiness Directive CF-2025-27 addresses cracks found on the aft wing to body fairing (WTBF) structure of Airbus Canada Limited Partnership (ACLP) Model BD-500-1A10 and BD-500-1A11 aircraft. This directive mandates inspections, load adjustments of tie-rods, and structural reinforcements to prevent loss of WTBF integrity. It applies to specific serial number ranges of these aircraft models.

May 22, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)

EASA AD 2025-0117

Fuselage — Bracket Supporting Flap Shaft Catcher — Inspection

EASA Airworthiness Directive 2025-0117 is an airworthiness directive addressing the Airbus A350-1041 aeroplanes with specific manufacturer serial numbers. It mandates inspection of the fuselage bracket supporting the flap shaft catcher to detect incorrect installation that could cause misalignment and potential flap surface detachment. The directive applies to affected left-hand and right-hand side brackets identified by part numbers V5393528020000 and V5393528020100.

May 19, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350

EASA AD 2025-0116

Main Rotor — Swashplate Assembly — Modification

EASA Airworthiness Directive 2025-0116 is issued for Airbus Helicopters AS 332 C, C1, L, L1, and L2 models, addressing the main rotor swashplate assembly. The directive mandates modifications to the swashplate assembly to prevent failure of the scissors link caused by ball joint-cups assembly seizure. This AD ensures continued airworthiness and safe operation of affected helicopters.

May 19, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

EASA AD 2025-0115

Equipment / Furnishings — Fuselage / Belly Fairing Mounted Emergency Evacuation Escape Slides — Inspection / Replacement

EASA Airworthiness Directive 2025-0115 is an airworthiness directive addressing inspection and replacement requirements for fuselage and belly fairing mounted emergency evacuation escape slides installed on Airbus A380-841, A380-842, and A380-861 aeroplanes. The directive targets specific slide parts with part numbers 103004-xxx, 103007-xxx, and 103008-xxx, focusing on those affected by adhesive degradation and seam failures. It mandates inspections, pressure testing, and replacement of affected slides to ensure continued airworthiness and safety.

May 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD 2025-0109

SUPERSEDED BY EASA AD 2025-0117

EASA Airworthiness Directive 2025-0109 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-1041 aeroplanes with specific manufacturer serial numbers. The directive mandates inspection of the fuselage bracket supporting the flap shaft catcher to detect incorrect installation that could lead to flap surface detachment. This AD applies to certain left-hand and right-hand side brackets identified by part numbers V5393528020000 and V5393528020100.

May 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350

EASA AD US-2025-07-10

Engine Controls - Engine Indicating and Crew Alerting System - Dispatch Prohibition; Full Authority Digital Engine Control (FADEC) Integrated Circuit Microprocessor - Replacement; Electronic Engine Control FADEC - Software Upgrade

The document titled "Engine Controls - Engine Indicating and Crew Alerting System - Dispatch Prohibition; Full Authority Digital Engine Control (FADEC) Integrated Circuit Microprocessor - Replacement; Electronic Engine Control FADEC - Software Upgrade" is a final rule Airworthiness Directive issued by the FAA affecting General Electric Company Model GE90-110B1 and GE90-115B engines. It addresses unsafe conditions related to engine thrust control and FADEC microprocessor degradation by mandating operational restrictions, hardware replacements, and software upgrades.

May 15, 2025
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtGeneral Electric GE90

EASA AD 2025-0114

Equipment / Furnishings — Lavatory Floor Fittings — Inspection

EASA Airworthiness Directive 2025-0114 is an airworthiness directive issued by EASA concerning Airbus A330-841 and A330-941 aeroplanes. It addresses inspection requirements for lavatory floor fittings installed in SAFRAN D/E and L/M, S/T, Hs/Ks lavatories to detect corrosion and prevent potential detachment of lavatory modules. The directive mandates repetitive general visual inspections and corrective actions to ensure continued airworthiness.

May 15, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD US-2025-09-12

Fuselage - Seat Tracks above the Electronics Equipment Bays - Inspection

Fuselage - Seat Tracks above the Electronics Equipment Bays - Inspection is a final rule airworthiness directive issued by the FAA affecting certain Boeing 787-8, 787-9, and 787-10 airplanes. It addresses water leakage from the potable water system causing water ingress into the electronics equipment bays due to missing or improperly installed sealant, moisture barrier tape, or tape dams above the seat tracks. The directive mandates inspections and corrective actions to ensure the safety of the affected aircraft.

May 15, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787

EASA AD 2025-0111

Fuselage — Service Door Stop Fitting Hole — Inspection / Repair

EASA Airworthiness Directive 2025-0111 is issued for Airbus A318, A319, A320, and A321 aeroplanes, addressing inspection and repair requirements for the fuselage service door stop fitting holes at fuselage frames 16 and 20. This directive mandates repetitive rototest inspections and corrective actions to detect and repair cracks that could compromise structural integrity. It applies to both Current Engine Option (CEO) and New Engine Option (NEO) variants with specific applicability exceptions.

May 14, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2025-0110

Stabilizers — Horizontal Stabilizer Front Box, Centre Box and Front Spar Web — Inspection

EASA Airworthiness Directive 2025-0110 is an airworthiness directive affecting ATR 42-500 and ATR 72-212A aeroplanes. It mandates inspections of the horizontal stabilizer front box, centre box, front spar web, and related structural components to detect loose fasteners and cracks. The directive applies to specific manufacturer serial numbers as listed in ATR service bulletins.

May 14, 2025
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72