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EASA Regulations & Airworthiness Directives

Browse 5061 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320281Airbus A321277Airbus A319247Airbus A350216Airbus A330211All198Airbus A318186Airbus A380178Boeing 737172Airbus A340140Airbus A350-941126Airbus BD-500 (A220 Series)119Airbus Helicopters AS 332118Airbus Helicopters EC 225115Airbus Helicopters SA 330115Show all...

EASA AD 2023-0148R1

Main Rotor Drive – Main Gearbox – Replacement; Placards and Markings – ENG1 Training Idle Switch – Installation / Operational Restriction

EASA Airworthiness Directive 2023-0148R1 is issued for Airbus Helicopters EC 225 LP models addressing issues with the main rotor drive main gearbox (MGB) and installation of placards related to the ENG1 Training Idle switch. It applies to specific MGB part numbers and configurations that have shown wear and broken roller cages, potentially reducing engine power transfer capability during one engine inoperative (OEI) conditions. The directive mandates inspections, replacements, placard installations, and operational restrictions to ensure continued airworthiness and safe helicopter operation.

Jul 24, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters EC 225 LP

EASA AD 26-090

Tail Rotor – Tail Rotor Blade – Service Life Limit Amendment / Replacement

EASA Airworthiness Directive Proposal 26-090 is a regulatory document addressing the tail rotor blade service life limit for Airbus Helicopters EC 175 B models. It applies to all serial numbers of EC 175 B helicopters and focuses on tail rotor blades with part number M641A1001104. The directive proposes an amendment to the service life limit of these tail rotor blades based on new flight load assessments.

Jul 24, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175Airbus Helicopters EC 175 B

EASA AD 2026-0145

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

EASA Airworthiness Directive 2026-0145 is issued for Dassault Aviation Falcon 7X aeroplanes, serial numbers 2 through 400 inclusive, addressing flight controls maintenance and avionics interface computer software modifications. This directive mandates updates to the Maintenance and Avionics Interface Computers (MAIC) software and amendments to the Airplane Flight Manual (AFM) to enhance crew awareness of inboard slat configuration during failures. It supersedes a previous emergency AD related to the same issue.

Jul 23, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 7X

EASA AD 2026-0147

Main Rotor Drive – Main Rotor Mast – Inspection

EASA Airworthiness Directive 2026-0147 is an airworthiness directive addressing the inspection of the main rotor drive and main rotor mast on Hélicoptères Guimbal Cabri G2 helicopters. It applies to all serial numbers of the Cabri G2 and focuses on inspecting specific main gear boxes with part numbers G21-10-000 through G21-10-003. The directive mandates inspections to detect cracks and corrosion that could compromise the main rotor mast's structural integrity.

Jul 23, 2026
Airworthiness DirectiveMaintenanceSafety MgmtGuimbal, Helicopteres CABRIHélicoptères Guimbal Cabri G2

EASA AD 26-088

Tail Rotor Drive – Tail Gear Box and Chip Detector – Inspection

EASA Airworthiness Directive Proposal 26-088 is a regulatory document addressing inspection requirements for the tail rotor drive tail gear box (TGB) and chip detector on Leonardo S.p.A. helicopters, specifically models A109AII, A109C, A109E, A109K2, A109LUH, A109S, and AW109SP. The directive targets TGB assemblies with part number 109-0442-01 manufactured by Turbomecanica, requiring repetitive inspections to detect abnormal wear. This directive aims to ensure continued airworthiness and safety of the affected helicopter models.

Jul 23, 2026
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119Leonardo A109AIILeonardo A109CLeonardo A109ELeonardo A109K2Leonardo A109LUHLeonardo A109SLeonardo AW109SP

EASA CZIB CZIB-2026-08

Airspace of Jordan

The EASA Conflict Zone Information Bulletin (CZIB) titled 'Airspace of Jordan' addresses the heightened risks for civil aviation within the FIR Amman (OJAC) airspace at all altitudes and flight levels. It highlights increased military activity, including missile and drone attacks, which pose significant dangers to all aircraft operating in this region. The bulletin applies to all air operators subject to Commission Regulation (EU) 965/2012 and third Country Operators authorized by EASA under TCO authorizations.

Jul 22, 2026
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB 2022-02R4

[Correction] Global Navigation Satellite System Outage and Alterations Leading to Communication / Navigation / Surveillance Degradation

EASA Safety Information Bulletin 2022-02R4 is a correction and revision addressing the increase in Global Navigation Satellite System (GNSS) jamming and spoofing incidents affecting communication, navigation, and surveillance in various flight information regions. It applies to National Competent Authorities, Air Traffic Management and Air Navigation Service providers, air operators, and manufacturers of aircraft and ATM/ANS equipment. The bulletin highlights operational impacts such as degraded position, navigation, and timing data, which can affect flight safety and air traffic control communications.

Jul 22, 2026
Safety Information BulletinFlight OpsSafety Mgmt

EASA AD 26-087

Indicating / Recording Systems – Integrated Control Panels – Inspection

EASA Airworthiness Directive PAD No. 26-087 is a proposed directive addressing inspection requirements for fire integrated control panels (ICP) on Airbus A350-941 and A350-1041 aeroplanes. The directive focuses on the ICP Functional Item Number 245VM with Part Number 727-7206-03, which may suffer internal damage leading to in-flight engine shutdown. This directive applies to all manufacturer serial numbers of the affected aircraft models.

Jul 21, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD 2026-0144

Stabilizers – Rudder Outer Skin – Inspection

EASA Airworthiness Directive 2026-0144 is an airworthiness directive addressing inspection requirements for the rudder outer skin on certain Airbus A320 and A321 aircraft models. It applies specifically to Airbus A320-251N, A320-252N, A321-252NX, and A320-271N aeroplanes with specified manufacturer serial numbers. The directive mandates inspections to detect dents caused by storage trolleys during production that could lead to structural damage and reduced control of the aircraft.

Jul 21, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A320Airbus A321

EASA AD 2026-0143

Engine – Intermediate Pressure Compressor Shaft Assembly / Front Air Seal – Inspection

The document titled 'Engine – Intermediate Pressure Compressor Shaft Assembly / Front Air Seal – Inspection' is a technical directive concerning Rolls-Royce Deutschland Ltd & Co KG Trent 1000 and Trent 7000 engine models. It addresses inspection requirements for the intermediate pressure compressor shaft assembly and the front air seal components. This directive is intended to ensure the continued airworthiness and safety of affected engines installed on various aircraft.

Jul 20, 2026
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD 2026-0142

Wings – Main Landing Gear Support Rib 5 – Inspections

EASA Airworthiness Directive 2026-0142 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus A318, A319, A320, and A321 aeroplanes with specific manufacturer serial numbers. The directive mandates inspections of the main landing gear support rib 5 due to identified quality issues that could lead to fatigue damage and potential structural failure. It applies to affected parts listed by part and serial numbers in the directive's appendix.

Jul 20, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2026-0141

Engine Oil – Lubrication / Scavenge Oil Pumps – Installation Criteria

EASA Airworthiness Directive 2026-0141 addresses installation criteria for lubrication and scavenge oil pumps on Rolls-Royce Trent 7000 series engines, which are commonly installed on Airbus A330 NEO aircraft. The directive applies to specific affected parts with certain part numbers and aims to prevent engine in-flight shutdowns caused by early-life failure of internal components in these pumps. It mandates compliance with installation criteria outlined in Rolls-Royce Alert Non-Modification Service Bulletin TRENT 1000 79-AK868.

Jul 17, 2026
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 7000Airbus A330 NEO

EASA AD US-2026-13-07

Equipment/Furnishings - Doorway Support Bracket - Installation

The Federal Aviation Administration's Airworthiness Directive 2026-13-07 addresses certain Boeing 787-8, 787-9, and 787-10 airplanes. It mandates modifications to the doorway support bracket assemblies to prevent door assist handles from detaching during pre-flight checks. The directive includes installation of new retainers, placards or part markings, inspections, and on-condition corrective actions to ensure safety.

Jul 17, 2026
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787Boeing 787-8Boeing 787-9Boeing 787-10

EASA AD 26-086

Fuselage – Splice of Frame X5295 – Inspection

EASA Airworthiness Directive Proposal 26-086 is a proposed directive addressing Airbus Helicopters EC 225 LP models with specific modifications related to the fuselage splice at frame X5295. It requires inspection of the upper splice plates to verify their material composition and mandates corrective actions if discrepancies are found. This directive aims to ensure the structural integrity of the helicopter frame by correcting maintenance records and inspection programs.

Jul 17, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters EC 225 LP

EASA AD CF-2026-35

Engine – Exhaust – Turbine Exhaust Frame Cracks - Inspection

The Canadian Airworthiness Directive CF-2026-35 is an urgent regulatory document addressing turbine exhaust frame (TEF) cracks in Pratt & Whitney Canada PW210A, PW210A1, and PW210S engines. It mandates initial and periodic general visual inspections of the TEF to detect circumferential cracks caused by thermal stress and material durability issues. This directive updates previous requirements to include different inspection thresholds based on TEF material composition.

Jul 16, 2026
Airworthiness DirectiveMaintenanceSafety MgmtPratt & Whitney Canada PW210

EASA AD CF-2026-06R1

Landing Gear – Main Landing Gear Aft Door Mechanism – Lock Link Apex Pin/Bolt Fracture

Canadian Airworthiness Directive CF-2026-06R1 addresses the fracture risk of the lock link apex pin/bolt in the main landing gear aft door mechanism on De Havilland DHC-8-401 and DHC-8-402 aircraft, serial numbers 4001 and 4003 through 4633. The directive mandates inspections and replacement of specific apex pins and bolts to prevent asymmetric landing gear extension caused by pin or bolt failure. It applies to apex pin P/N 46852-1 and apex bolt NAS6207-17D, requiring installation of a new pin P/N 46857-1.

Jul 16, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDe Havilland Canada DHC-8De Havilland DHC-8-401De Havilland DHC-8-402

EASA AD CF-2026-34

Water/Waste – Waste Service Panel Ball Valve Leakage - Installation

Canadian Airworthiness Directive CF-2026-34 addresses a corrosion issue caused by leakage from the waste service panel ball valve on Airbus Canada Limited Partnership (ACLP) aircraft models BD-500-1A10 and BD-500-1A11. The directive applies to specific serial numbers of these models and mandates corrective action to prevent structural damage. This directive aims to enhance aircraft safety by preventing waste water leakage that can lead to cabin pressure loss or structural failure.

Jul 16, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A10Airbus Canada BD-500-1A11

EASA AD 2026-0140

Flight Controls – Flap Actuator – Inspections / Modification

EASA Airworthiness Directive 2026-0140 is an airworthiness directive affecting all serial numbers of Diamond Aircraft Industries GmbH DA 50 C aeroplanes. It addresses issues with the flap actuator that could cause flap extension failure and reduced aileron control. The directive mandates inspections and modifications to the flap actuator to ensure continued safe operation.

Jul 15, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDiamond Aircraft Industries DA 50Diamond Aircraft Industries GmbH DA 50 C

EASA AD 26-085

Navigation – GLU-2100 Global Navigation Satellite System Clock Oscillator – Operational Limitation

EASA Airworthiness Directive PAD No. 26-085 is a proposed directive addressing an operational limitation for the GLU-2100 Global Navigation Satellite System Clock Oscillator installed on Airbus A350-941 and A350-1041 aeroplanes. It identifies certain affected GLU-2100 units with specific part and serial numbers that may cause erroneous aircraft position information without warning. The directive applies to all manufacturer serial numbers of these aircraft models.

Jul 15, 2026
Airworthiness DirectiveFlight OpsSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD G-2026-0002

Time Limits / Maintenance Checks – Airworthiness Limitations – Amendment / Implementation

The Civil Aviation Authority Airworthiness Directive G-2026-0002 is an amendment addressing time limits and maintenance checks for BAE Systems Jetstream 4100 series aeroplanes. It updates mandatory airworthiness limitations and structural repair inspections to ensure continued safe operation of these aircraft. This directive applies to all models and serial numbers of the Jetstream 4100 series.

Jul 15, 2026
Airworthiness DirectiveMaintenanceSafety MgmtBae Systems (Operations) Jetstream 4100BAE Systems Jetstream 4100