EASA Regulations & Airworthiness Directives

Browse 5061 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320281 Airbus A321277 Airbus A319247 Airbus A350216 Airbus A330211 All198 Airbus A318186 Airbus A380178 Boeing 737172 Airbus A340140 Airbus A350-941126 Airbus BD-500 (A220 Series)119 Airbus Helicopters AS 332118 Airbus Helicopters EC 225115 Airbus Helicopters SA 330115 Show all...

EASA AD 2026-0117R1

Engine – Low Pressure Turbine Discs – Inspection

EASA Airworthiness Directive 2026-0117R1 is an updated safety directive addressing inspection requirements for low pressure turbine stage 3 and stage 4 discs on Rolls-Royce Trent 1000 engines, commonly installed on Boeing 787 aircraft. The directive mandates inspections to detect cracks caused by rubbing contact with interstage static seals to prevent potential turbine disc failure. It applies to all serial numbers of Trent 1000-A2 through Trent 1000-L2 engine variants.

Aug 12, 2026

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

EASA AD 2026-0163

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

EASA Airworthiness Directive 2026-0163 is an operational limitation directive affecting Airbus A350-941 and A350-1041 aeroplanes. It addresses issues with the GLU-2100 Global Navigation Satellite System Clock Oscillator, specifically certain units with untested oscillators that may cause erroneous position information. The directive prohibits operation and installation of affected GLU-2100 units unless modified according to Collins Aerospace instructions.

Aug 12, 2026

Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA SIB SAIB-2026-10R1

Equipment / Furnishings - Restraint Systems

The FAA Special Airworthiness Information Bulletin SAIB: 2026-10R1 addresses airworthiness concerns related to torso restraint systems and safety belts installed in general aviation aircraft. It highlights failures in restraint assemblies, particularly at the shoulder harness Y-junction, that have contributed to serious injuries and fatalities in multiple accidents involving general aviation airplanes such as the Aeronca 7AC. The bulletin provides guidance on compliance with Technical Standard Orders TSO-C114 and TSO-C22g for restraint performance.

Aug 11, 2026

Safety Information BulletinSafety MgmtMaintenanceAeronca 7AC

EASA AD 2026-0145R1

Flight Controls – Maintenance and Avionics Interface Computer Software – Modification

EASA Airworthiness Directive 2026-0145R1 is issued for Dassault Aviation Falcon 7X aeroplanes, serial numbers 2 through 400 inclusive, that have not embodied modification M1000. This directive addresses maintenance and avionics interface computer software modifications related to flight controls, specifically targeting the inboard slats extension failure issue during landing. It mandates updates to the Maintenance and Avionics Interface Computer (MAIC) software and amendments to the Aeroplane Flight Manual (AFM).

Aug 11, 2026

Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 7X

EASA AD 2026-0162

Flight Controls – Roll Spoiler Actuator Mount – Inspection

EASA Airworthiness Directive 2026-0162 is an airworthiness directive addressing the inspection of roll spoiler actuator mounts on Dornier 328-100 aeroplanes. It mandates a one-time inspection to detect corrosion around the pivot-bearing area of the roll spoiler actuator mount, which is difficult to detect due to its concealed location. The directive applies to all manufacturer serial numbers of Dornier 328-100 aircraft and requires reporting of inspection results to Deutsche Aircraft GmbH.

Aug 11, 2026

Airworthiness DirectiveMaintenanceSafety MgmtDeutsche Aircraft Gmbh Dornier 328Dornier 328-100

EASA AD 2026-0150

Lights – Emergency Power Supply Unit Battery Pack – Life Limit Implementation / Functional Check

The document titled 'Lights – Emergency Power Supply Unit Battery Pack – Life Limit Implementation / Functional Check' is an informational record created by EASA regarding the Airbus A400M aircraft. It clarifies that no Airworthiness Directive (AD) exists for this aircraft in civil service because there are currently no Airbus A400M aeroplanes in civil operation. The legally binding requirements for this subject are issued by the relevant military airworthiness authorities depending on the country of registration.

Aug 11, 2026

Safety Information BulletinMaintenanceSafety MgmtAirbus Military A400MAirbus A400M

EASA AD 26-094

Rotor(s) – Main Rotor Yoke – Inspection

EASA Airworthiness Directive Proposal 26-094 is a proposed directive addressing the inspection of main rotor yokes on Leonardo S.p.A. AB412 and AB412 EP helicopters. It targets specific main rotor yokes manufactured by Bell Helicopter Textron that may have manufacturing defects leading to structural damage. The directive requires a one-time inspection and potential replacement of affected parts to ensure continued airworthiness.

Aug 11, 2026

Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters AB212Leonardo S.P.A. Helicopters AB412Leonardo AB412Leonardo AB412 EP

EASA AD CF-2026-39

Tail Rotor – Tail Rotor Pitch Horn Fracture - Replacement

The Canadian Emergency Airworthiness Directive CF-2026-39 addresses a critical safety issue affecting Bell Textron Canada Limited model 222 helicopters, serial numbers 47006 through 47089. It mandates the replacement of tail rotor pitch horn Part Number 222-012-774-109 due to in-flight fatigue failure risks. The directive requires installation of serviceable parts P/N 222-012-705-105 or 222-012-705-107 to ensure continued safe operation.

Aug 11, 2026

Airworthiness DirectiveMaintenanceSafety MgmtBell 222Bell Textron Canada Limited 222

EASA AD US-2026-14-03

Engine - Engine Fuel Distribution - Replacement

The Federal Register Final Rule titled "Engine - Engine Fuel Distribution - Replacement" establishes a new airworthiness directive (AD 2026-14-03) issued by the FAA for certain General Electric Company GEnx engine models including GEnx-1B64, GEnx-1B67, GEnx-1B70 series, GEnx-1B74/75, GEnx-1B76, and GEnx-2B67 variants. This AD addresses a fuel leak issue caused by defective fuel tube hoses connecting the main fuel-oil heat exchanger, affecting engines installed on aircraft such as the Boeing 787-8. The directive mandates removal and replacement of affected fuel tube hoses to ensure continued airworthiness and safety.

Aug 10, 2026

Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric GEnxBoeing 787-8

EASA AD 2024-0004R1

Fuselage – Centre Fuselage Frame Assembly – Inspection / Repair / Modification

EASA Airworthiness Directive 2024-0004R1 is an updated regulation addressing inspection, repair, and modification requirements for the centre fuselage frame assembly on Leonardo S.p.A. A109 helicopters, including A109E, A109S (up to serial number 22199), and A109LUH models. The directive mandates repetitive inspections and structural reinforcement to ensure the integrity of the fuselage frame at station 1815, where cracks have been reported. It applies to all serial numbers within the specified helicopter models.

Aug 10, 2026

Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119Leonardo A109Leonardo A109ELeonardo A109SLeonardo A109LUH

EASA SIB AIR750-2026-06-S-5700-ACS

Lower Wing Skin Cracking

The Lower Wing Skin Cracking Airworthiness Concern Sheet issued by the Federal Aviation Administration (FAA) addresses reports of cracks in the lower wing skin cutouts near the main landing gear truss on Twin Commander aircraft models 500 series through 720. The document highlights Maintenance Alert MA23001 issued by Twin Commander Aircraft LLC, recommending recurring inspections to detect these cracks. It also references a related Australian Civil Aviation Safety Authority Airworthiness Directive AD/AC/92 for similar inspections on affected aircraft.

Aug 10, 2026

Safety Information BulletinMaintenanceSafety MgmtTwin Commander Aircraft 500Twin Commander Aircraft 520Twin Commander Aircraft 560Twin Commander Aircraft 560-FTwin Commander Aircraft 680Twin Commander Aircraft 690Twin Commander Aircraft 695Twin Commander Aircraft 720Twin Commander 500Twin Commander 520Twin Commander 560Twin Commander 680Twin Commander 690Twin Commander 700Twin Commander 720

EASA AD US-2026-15-11

Fuselage - Fuselage Skin / Bear Strap - Inspection

The Federal Aviation Administration's Airworthiness Directive 2026-15-11 addresses certain Boeing 737-8, 737-9, and 737-8200 airplanes. This directive requires inspections of the fuselage skin and bear strap near the forward galley door cutout due to reported cracks. The directive aims to maintain structural integrity and ensure safety by detecting and repairing cracks before they become critical.

Aug 7, 2026

Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-8Boeing 737-9Boeing 737-8200

EASA AD 2026-0161

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

The document titled 'Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment' is an amendment concerning the CFM INTERNATIONAL CFM56-7B engine model. It updates the airworthiness limitations section related to time limits and maintenance checks for this specific engine type. The amendment aims to ensure continued airworthiness and safe operation of aircraft equipped with the CFM56-7B engine.

Aug 7, 2026

Airworthiness DirectiveMaintenanceSafety MgmtCFM International CFM56-7B

EASA SIB 2026-09

Inadequate Protection of SBAS-Based Instrument Approach Procedures

EASA Safety Information Bulletin 2026-09 addresses the inadequate protection of Satellite-Based Augmentation System (SBAS) based instrument approach procedures, specifically those using APV-I and Precision Approach Category I criteria. The bulletin highlights that some published Localiser Performance with Vertical Guidance (LPV) procedures may not provide the intended obstacle clearance protection for all eligible aircraft due to assumptions in navigation system performance. This affects flight procedure design providers, air traffic services, and aircraft operators involved with SBAS-based approaches.

Aug 6, 2026

Safety Information BulletinFlight OpsSafety Mgmt

EASA SD SD-2026-01

Inadequate Protection of SBAS-Based Instrument Approach Procedures

EASA Safety Directive 2026-01 addresses the inadequate obstacle clearance protection in Satellite-Based Augmentation System (SBAS) based instrument approach procedures, specifically those using LPV minima. This directive affects Flight Procedure Design providers and Air Traffic Services providers holding EASA approvals, focusing on procedures for aircraft eligible to fly RNP APCH operations to LPV minima. It highlights discrepancies in current ICAO design criteria assumptions that may compromise safety during missed approach phases.

Aug 6, 2026

Safety DirectiveFlight OpsSafety Mgmt

EASA AD CF-2026-37

Time Limits / Maintenance Checks – Airworthiness Limitation Items – Amendment

Canadian Airworthiness Directive CF-2026-37 is an amendment addressing Time Limits and Maintenance Checks for Airworthiness Limitation Items (ALI) on De Havilland Aircraft of Canada Limited DHC-8-401 and DHC-8-402 models. It mandates compliance with updated and more restrictive maintenance tasks as defined in the DHC Maintenance Requirements Manual PSM 1-84-7 Part 2. The directive applies to all serial numbers of these aircraft models and includes detailed inspection requirements for various structural components.

Aug 6, 2026

Airworthiness DirectiveMaintenanceSafety MgmtDe Havilland Canada DHC-8De Havilland Aircraft of Canada Limited DHC-8-401De Havilland Aircraft of Canada Limited DHC-8-402

EASA AD CF-2026-09R2

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

Airworthiness Directive CF-2026-09R2 addresses ice and rain protection issues related to engine cowl anti-ice ejector pipe chafing on MHI RJ Aviation ULC model CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 aircraft. This directive mandates inspections and potential replacement of the ejector pipe and seal to prevent ice accumulation and engine shutdown. It applies to all serial numbers of the affected aircraft models.

Aug 5, 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 2026-0128

[Correction] Engine Fuel & Control – Hydromechanical Metering Unit – Replacement

EASA Airworthiness Directive 2026-0128 is a corrective directive addressing the replacement of Hydromechanical Metering Units (HMUs) on SAFRAN Helicopter Engines ARRIUS 1A models, commonly installed on Airbus Helicopters AS 355 N twin-engine helicopters. The directive targets specific HMUs with part number 0164851170 identified as having a torn constant delta P valve diaphragm, which could cause fuel flow drift and potential engine shutdown. It mandates replacement of affected HMUs to ensure continued airworthiness and safe engine operation.

Aug 3, 2026

Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIUS 1Airbus Helicopters AS 355 N

EASA AD 2026-0158

Fire Protection – Pyrotechnical Cartridge – Inspection

EASA Airworthiness Directive 2026-0158 is an airworthiness directive addressing fire protection pyrotechnical cartridges installed on Dassault Aviation Mystère-Falcon and Fan Jet Falcon aeroplanes. It mandates repetitive inspections and potential replacement of specific pyrotechnical cartridge parts identified by part and batch numbers to ensure fire extinguishing capability. The directive applies to all serial numbers of Fan Jet Falcon, Mystère-Falcon 20-( )5 series, Mystère-Falcon 200, and 20 GF aeroplanes.

Aug 3, 2026

Airworthiness DirectiveMaintenanceSafety MgmtDassault Fan Jet FalconDassault MystÃ¨re-Falcon 20Dassault MystÃ¨re-Falcon 20GFDassault 200Dassault Mystère-Falcon

EASA AD 26-092

Power Plant – Air Intake Cowl – Nacelle Anti-ice Duct Female Socket – Inspection

EASA Airworthiness Directive PAD No. 26-092 is a proposed directive addressing inspection requirements for the air intake cowl nacelle anti-ice duct female socket on Airbus A380-861 aeroplanes equipped with SAFRAN engine nacelles. It targets potential structural failures caused by excessive wear in the female socket of the anti-ice duct. The directive applies to all manufacturer serial numbers of the Airbus A380 and references specific Airbus and SAFRAN service bulletins for inspection procedures.

Aug 3, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380