EASA Regulations & Airworthiness Directives

Browse 5057 EASA regulations with AI-powered summaries.

EASA AD 26-018

SAFRAN ELECTRONICS & DEFENSE BEACONS: Emergency Locator Transmitter — Modification

EASA Airworthiness Directive 26-018 is a proposed directive addressing the Safran Electronics & Defense Kannad 406 AF-Compact Emergency Locator Transmitter (ELT) models with part numbers S1840501-01 and S1840501-04. This directive applies to all serial numbers of these ELTs, which may be installed on any aircraft either during production or as an in-service modification. The directive focuses on modifying the ELT installation to correct an unsafe condition related to erroneous transmissions during distress signals.

Jan 29, 2026
Airworthiness DirectiveMaintenanceSafety Mgmt

EASA AD 26-016

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

EASA Airworthiness Directive 26-016 is a proposed amendment affecting Airbus A330 aeroplanes, including models A330-201 through A330-941. It updates the Airworthiness Limitations Section Part 1 related to Safe Life Airworthiness Limitation Items. This directive ensures continued airworthiness by mandating compliance with the latest Airbus A330 ALS Part 1 Revision 14.

Jan 29, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 26-015

Doors — Bulk Cargo Door Stop Screw — Ins

EASA Airworthiness Directive 26-015 is a proposed directive addressing the bulk cargo door stop screw on Airbus A350-941 and A350-1041 aeroplanes. It applies to aircraft with Airbus modification 103573 embodied in production but not modification 116251. The directive mandates repetitive inspections to detect missing heads on bulk cargo door stop screws to maintain structural integrity.

Jan 27, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350

EASA AD 2026-0020

Main Rotor — Main Rotor Pitch Rod End — Inspection

EASA Airworthiness Directive 2026-0020 is an airworthiness directive issued for Airbus Helicopters H160-B models. It mandates inspection of the main rotor pitch rod end bearings to detect potential defects that could compromise flight safety. The directive applies to all serial numbers of the H160-B helicopter and focuses on specific part numbers of the main rotor pitch rod end bearings.

Jan 27, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters H160

EASA AD 2026-0016

Flight Controls — Spoiler Electrical Control Unit — Replacement

EASA Airworthiness Directive 2026-0016 is an official regulatory document addressing the replacement of the Spoiler Electrical Control Unit (SPECU) on Dassault Aviation Falcon 7X aeroplanes, including those modified to Falcon 8X standard. The directive mandates the replacement of certain affected SPECUs to prevent hydraulic leakage and potential fire hazards. It applies to all serial numbers of Falcon 7X aircraft and specifies compliance requirements for operators.

Jan 26, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 7X

EASA AD 26-013

Fuselage — Door Frames Holes — Inspection

EASA Airworthiness Directive 26-013 is a proposed directive addressing inspection requirements for door frame holes on Airbus A300-600 and A310 aeroplanes. It mandates repetitive high frequency eddy current inspections of specific seal retainer run out rivet holes at frames 56A, 57A, and 73A on both left-hand and right-hand sides. The directive applies to all manufacturer serial numbers of the affected aircraft models.

Jan 26, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600Airbus A310

EASA AD 2026-0019

Fuselage — Ram Air Turbine Rod Assembly — Inspection

EASA Airworthiness Directive 2026-0019 is an informational document concerning the inspection of the Ram Air Turbine rod assembly on the Airbus A400M fuselage. Since there are currently no Airbus A400M aircraft in civil service, this directive is not publicly available and is intended for military airworthiness authorities and the design approval holder. The document serves as a recommendation for military authorities to issue their own applicable airworthiness directives.

Jan 26, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Military A400M

EASA SIB BEA-2026-01

Ice and Rain Protection - Replacement of Pitot #3 Heater Wiring

BEA 2026-01 is a Special Airworthiness Bulletin issued by ANAC addressing the replacement of Pitot #3 heater wiring on Embraer S.A. EMB-145 and EMB-135BJ aircraft models. The bulletin recommends incorporating Embraer Service Bulletins SB145-30-0058 and SB145LEG-30-0024 to upgrade the wiring gauge and related components. This bulletin applies to multiple EMB-145 and EMB-135 variants and aims to improve electrical safety in the ice and rain protection system.

Jan 26, 2026
Safety Information BulletinMaintenanceSafety MgmtEmbraer EMB-135Embraer EMB-145

EASA AD 26-014

Rotors Flight Control — Collective Stick Torque Tube Assembly — Inspection / Replacement

EASA Airworthiness Directive 26-014 is a proposed directive addressing the inspection and replacement of the collective stick torque tube assembly on Leonardo S.p.A. A119 and AW119MKII helicopters up to serial number 14999 inclusive. The directive targets affected torque tube assemblies with Part Number 109-0011-03-105 due to manufacturing defects that could impair helicopter control. It mandates inspections, corrective actions, and eventual replacement with serviceable parts to ensure continued airworthiness.

Jan 26, 2026
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119

EASA AD 2026-0018

Wings — Main Landing Gear Trunnion Block Fuse Pins and Retaining Pins — Inspection

EASA Airworthiness Directive 2026-0018 is an official directive addressing Airbus A350-941 aeroplanes with specific manufacturer serial numbers. It mandates inspection of the main landing gear trunnion block fuse pins and retaining pins due to a serialization non-conformity issue. The directive ensures the traceability and continued airworthiness of these critical landing gear components.

Jan 26, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350

EASA AD 2026-0017

Equipment / Furnishings — Galley — Inspection

EASA Airworthiness Directive 2026-0017 is an inspection directive addressing forward-facing galley equipment on Airbus A318, A319, A320, and A321 aeroplanes. It mandates inspections and corrective actions for specific galley part numbers to prevent damage such as delamination and corrosion that could lead to trolley detachment during emergency landings. The directive applies to all serial numbers of the affected aircraft models.

Jan 23, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD US-2026-01-03

Main Landing Gear - Airworthiness Limitations — Revision

EASA Airworthiness Directive US-2026-01-03 is a final rule issued by the FAA affecting all Gulfstream Aerospace Corporation Model GVII-G500 and GVII-G600 airplanes. It mandates revisions to the existing maintenance or inspection programs to incorporate new and more restrictive airworthiness limitations related to the main landing gear. This directive addresses updated safe life limits and corrected part numbers for critical components to ensure continued airworthiness.

Jan 23, 2026
Airworthiness DirectiveMaintenanceSafety MgmtGulfstream Aerospace Corporation GVII

EASA AD US-2026-01-02

Wings — Airworthiness Limitations — Revision

EASA AD US-2026-01-02 is a final airworthiness directive issued by the FAA for all Gulfstream Aerospace Corporation Model GVI airplanes. It mandates revisions to the maintenance or inspection programs to incorporate new and more restrictive airworthiness limitations. The directive aims to prevent failure of principal structural elements and maintain the structural integrity of the aircraft throughout their service life.

Jan 23, 2026
Airworthiness DirectiveMaintenanceSafety MgmtGulfstream Aerospace Corporation GVI

EASA SIB CASA-2025-13

A220 PW1500G Oil System Inspection after Oil Debris Monitoring (ODM) Indication

The Transport Canada Civil Aviation Safety Alert CASA 2025-13 addresses inspection requirements for the A220 aircraft models BD-500-1A10 and BD-500-1A11 equipped with PW1500G engines. It highlights potential engine issues caused by debris from the number 4 bearing compartment detected through Oil Debris Monitoring (ODM) indications. The alert aims to inform owners, operators, and maintainers about these risks and recommended corrective actions.

Jan 22, 2026
Safety Information BulletinMaintenanceSafety MgmtAirbus BD-500 (A220 Series)

EASA SIB SAIB-2026-02

Elevator Tab Control System

The Special Airworthiness Information Bulletin SAIB 2026-02 is an FAA advisory concerning the elevator tab control system on Textron Aviation Inc. Model 1900D airplanes, including those registered under previous type certificate holders such as Beechcraft Corporation and Raytheon Aircraft Company. It addresses a potential airworthiness concern related to the elevator pitch trim actuator that may experience water ingress and freezing, leading to pitch trim jams during flight.

Jan 22, 2026
Safety Information BulletinSafety MgmtMaintenanceTextron Aviation 1900 (Airliner)

EASA AD CF-2026-03

Equipment/Furnishings — Emergency Locator Transmitter (ELT) G-Switch Jumper Wire missing

EASA Airworthiness Directive CF-2026-03 addresses a safety issue affecting Diamond Aircraft Industries Inc. Model DA20-C1 aeroplanes equipped with the Artex 1000 Emergency Locator Transmitter (ELT). The directive mandates inspection and correction of a missing jumper wire in the ELT's G-Switch circuit to ensure proper activation during impact events. This AD aims to maintain the reliability of emergency locator equipment on affected aircraft.

Jan 22, 2026
Airworthiness DirectiveMaintenanceSafety MgmtDiamond Aircraft Industries, DA20

EASA AD 26-009

Landing Gear — Main Landing Gear Bogie Pivot Pin and Bushes — Inspection

EASA Airworthiness Directive 26-009 is a proposed directive addressing the inspection of main landing gear bogie pivot pins and bushes on Airbus A350-941 aeroplanes. It mandates repetitive detailed inspections to detect damage caused by frictional heating and potential cracking. The directive applies to all manufacturer serial numbers of the Airbus A350-941 and aims to prevent main landing gear collapse.

Jan 22, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350

EASA AD 2026-0015-E

Stabilizers — Horizontal Stabilizer — Inspections

EASA Airworthiness Directive 2026-0015-E is an emergency directive addressing inspections of the horizontal stabilizer on Airbus Helicopters AS 332 and EC 225 models. It mandates inspections of metallic horizontal stabilizers, specifically those with part numbers 332A1310XXXX for AS 332 helicopters and all metallic horizontal stabilizers for EC 225 helicopters. The directive aims to prevent loss of control caused by potential failure of the horizontal stabilizer.

Jan 22, 2026
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

EASA AD BR-2012-08-03R1

Cockpit Door Passive Lock Striker - Quick Release Pin and Hinges / Replacement

EASA Airworthiness Directive BR-2012-08-03R1 is a Brazilian regulatory document issued by ANAC that mandates replacement of the cockpit door passive lock striker, quick-release pin, and hinges on specific Embraer ERJ 190 series aircraft models. It applies to ERJ 190-100 ECJ, STD, LR, IGW (except post-mod SB190-25-0270 freighter configuration), SR, and ERJ 190-200 STD, LR, and IGW airplanes as identified in Embraer Service Bulletins dated August 1, 2011. The directive aims to ensure continued airworthiness and safety of these aircraft by addressing a known issue with cockpit door hinges.

Jan 20, 2026
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer ERJ 190

EASA AD US-2026-01-06

Fuselage - Cargo Barrier Fitting Link - Inspection

EASA AD US-2026-01-06 is a final airworthiness directive issued by the FAA addressing certain Boeing 787-9 and 787-10 airplanes. It requires inspection of cargo barrier fitting links to verify the titanium alloy material used, due to concerns that some fittings may have been manufactured with incorrect titanium alloy. The directive mandates use of high frequency eddy current or handheld X-ray fluorescence spectrometer inspections to determine material compliance and specifies replacement if necessary.

Jan 20, 2026
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787