EASA Regulations & Airworthiness Directives

Browse 5059 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 2026-0154

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

EASA Airworthiness Directive 2026-0154 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 14. This directive ensures continued airworthiness by mandating replacement of life-limited parts and maintenance program revisions.

Jul 31, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2026-0155

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

EASA Airworthiness Directive 2026-0155 is an amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with the updated Airworthiness Limitations Section Part 2, Damage Tolerant Airworthiness Limitation Items (DT-ALI) Revision 12 to ensure continued airworthiness. This directive updates maintenance requirements and intervals for these aircraft models.

Jul 31, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2026-0156

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3, Certification Maintenance Requirements – Amendment

EASA Airworthiness Directive 2026-0156 is an amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with the updated Airbus A380 Airworthiness Limitations Section Part 3, Certification Maintenance Requirements Revision 08 to ensure continued airworthiness. This directive applies to all manufacturer serial numbers of the affected Airbus A380 models.

Jul 31, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2026-0157

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 4, System Equipment Maintenance Requirements – Amendment

EASA Airworthiness Directive 2026-0157 is an amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 4, System Equipment Maintenance Requirements, requiring compliance with Airbus A380 ALS Part 4, SEMR Revision 17. This directive ensures mandatory maintenance tasks and life limits are followed to maintain continued airworthiness.

Jul 31, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD 2026-0152

Air Conditioning – Vapor Cycle Air Conditioning System – Inspection

EASA Airworthiness Directive 2026-0152 is an airworthiness directive addressing the vapor cycle air conditioning system on MBB-BK117 C-1 helicopters. It mandates recurring inspections of the louver box assembly, part number 117-820014, due to a reported in-flight detachment caused by incorrect installation. The directive applies to all serial numbers of the affected helicopter model and aims to prevent potential in-flight loss of parts and reduced helicopter control.

Jul 30, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117MBB-BK117 C-1

EASA AD 26-091

Engine – Fan Blades – Inspection

EASA Airworthiness Directive 26-091 is a proposed directive addressing inspection requirements for fan blades on CFM International CFM56-7B engines installed on Boeing 737-600, 737-700, 737-800, and 737-900 aircraft. It mandates ultrasonic inspections of specific fan blades to detect cracks and prevent potential fan blade failure. The directive applies to all serial numbers of affected engine models and specifies compliance times and inspection intervals.

Jul 30, 2026

Airworthiness DirectiveMaintenanceSafety MgmtCFM International CFM56-7BBoeing 737-600Boeing 737-700Boeing 737-800Boeing 737-900

EASA AD 2026-0151

Main Rotor Drive – Rotor Hub-Shaft – Inspection

EASA Airworthiness Directive 2026-0151 is an official safety directive addressing the inspection of the main rotor drive rotor hub-shaft on Airbus Helicopters Deutschland GmbH MBB-BK117 D-3 and D-3m helicopters. The directive mandates visual and eddy current inspections of specific rotor hub-shaft parts (MP/N D623M1501203 and D623M1501204) to detect cracks that could lead to main rotor transmission failure. This AD applies to all serial numbers of the affected helicopter models.

Jul 30, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters MBB-BK 117Airbus Helicopters MBB-BK117 D-3Airbus Helicopters MBB-BK117 D-3m

EASA AD US-2026-15-05

Wings - Airworthiness Limitation Section - Amendment

The Wings - Airworthiness Limitation Section - Amendment is a final rule airworthiness directive issued by the FAA affecting Textron Aviation Inc. Model B300 and B300C airplanes. It mandates revisions to the Airworthiness Limitations section of the aircraft maintenance manual to update inspection intervals for detecting cracks in the wing spar and supporting structures. This directive addresses safety concerns related to structural integrity for airplanes operating at different maximum takeoff weights.

Jul 30, 2026

Airworthiness DirectiveMaintenanceSafety MgmtTextron Aviation 300 (Super King Air)Textron Aviation B300Textron Aviation B300C

EASA AD ISR-I-52-2026-07-32

Doors - Main Entrance Door Fittings – Discard and Replace

Airworthiness Directive AD ISR I-52-2026-07-32 issued by the Civil Aviation Authority of Israel addresses the G280 model aircraft. It mandates the discard and replacement of main entrance door fittings due to reported failures during door operation. The directive also updates maintenance manual revisions related to door fittings and landing gear torque links.

Jul 29, 2026

Airworthiness DirectiveMaintenanceSafety MgmtGulfstream (Galp) G280Gulfstream G280

EASA AD BR-2026-07-03

Structures - Wing Tips Cracks - Inspection

Brazilian Airworthiness Directive AD No. 2026-07-03 is a regulatory document issued by the Agência Nacional de Aviação Civil (ANAC) that applies to all Embraer S.A. ERJ 170-200 aircraft equipped with specific left-hand and right-hand wingtip components. The directive mandates inspections for cracks in the wing spar and adjacent skin areas to ensure structural integrity and flight safety.

Jul 29, 2026

Airworthiness DirectiveMaintenanceSafety MgmtEmbraer ERJ 170Embraer ERJ 170-200

EASA AD G-2026-0003

Crew Safety – Crewman Restraint – Inspection

Civil Aviation Authority Airworthiness Directive G-2026-0003 addresses the inspection of IRVINGQ Lightweight Search and Rescue Harnesses, specifically part numbers MRIIGQ2779 and MRIASE2494. These harnesses are used in emergency rescue operations on multiple aircraft types and incorporate a quick release system critical for crew safety. The directive mandates inspection to ensure correct assembly of the Crewman Restraint Release Assembly to prevent potential failure in emergency disconnection.

Jul 28, 2026

Airworthiness DirectiveMaintenanceSafety Mgmt

EASA SIB 2026-08

Diode Cooler Assembly Insulation - Inspection

EASA Safety Information Bulletin 2026-08 is an airworthiness bulletin addressing inspection of diode cooler assembly insulation on small aeroplanes certified under CS-23, including the Piper PA-28RT-201T Arrow IV. The bulletin highlights an in-flight fire incident caused by electrical failure due to insulation faults in the diode cooler assembly and references related investigations and FAA guidance. It provides safety information and recommendations to prevent similar electrical failures.

Jul 28, 2026

Safety Information BulletinMaintenanceSafety MgmtPiper PA-28RT-201T

EASA AD 2026-0148

Electrical Power – Direct Current Electrical Master Box – Inspection

EASA Airworthiness Directive 2026-0148 is an airworthiness directive addressing Airbus Helicopters AS 332 C, C1, L, and L1 models. It mandates inspection of the direct current electrical master box, specifically the printed circuit boards with part number GC11050 and serial numbers up to 400, to prevent electrical short-circuits that could lead to loss of DC power and control of the helicopter.

Jul 28, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA AD BR-2026-07-02

Engine Pylons Drainage

Brazilian Airworthiness Directive AD No. 2026-07-02 issued by ANAC addresses safety concerns on Embraer S.A. ERJ 190-300 and ERJ 190-400 aircraft. The directive mandates modifications to the engine pylons' drainage system to prevent hydraulic fluid leakage that could lead to fire. It applies to specific serial numbers referenced in Embraer Service Bulletin SB190E2-54-0009.

Jul 28, 2026

Airworthiness DirectiveMaintenanceSafety MgmtEmbraer ERJ 190Embraer ERJ 190-300Embraer ERJ 190-400

EASA AD 2026-0149

Integrated Modular Avionics – Primus APEX DFZ Build 6.0 Software – Modification

EASA Airworthiness Directive 2026-0149 is an airworthiness directive affecting Pilatus PC-24 aeroplanes with manufacturer serial numbers 101 to 337 and 501 to 600. It mandates a software modification to the Integrated Modular Avionics Primus APEX DFZ system, updating from Build 5.3 or earlier to Build 6.0. This directive ensures continued safe operation by addressing flight director calculation errors during approach.

Jul 28, 2026

Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-24Pilatus PC-24

EASA AD BR-2026-07-01

SUPERSEDED BY ANAC BRAZIL AD 2026-07-02

Brazilian Airworthiness Directive 2026-07-01 is issued by the Agência Nacional de Aviação Civil (ANAC) and applies to Embraer S.A. ERJ 190-300 and ERJ 190-400 aircraft as specified in Embraer Service Bulletin SB190E2-54-0009. This directive addresses a potential fire risk caused by hydraulic fluid leakage migrating to high-temperature areas in the pylon assembly. It mandates specific modifications to the drain tubes and installation of shrouds and seals on the pylons to mitigate this risk.

Jul 28, 2026

Airworthiness DirectiveMaintenanceSafety MgmtEmbraer ERJ 190Embraer ERJ 190-300Embraer ERJ 190-400

EASA AD 2026-0146

Equipment / Furnishings – Mechanical Dropping Control – Inspection

EASA Airworthiness Directive 2026-0146 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 350 B2, AS 350 B3, AS 355 N, AS 355 NP, and EC 130 B4 models. The directive addresses inspection requirements for the mechanical dropping control system, specifically the dropping control part number 704A41811037, to prevent unintended load release during cargo operations.

Jul 24, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 355Airbus Helicopters AS 350 B2Airbus Helicopters AS 350 B3Airbus Helicopters AS 355 NAirbus Helicopters AS 355 NPAirbus Helicopters EC 130 B4

EASA AD 26-089

Fuselage – Centre Fuselage – Modification

EASA Airworthiness Directive PAD No. 26-089 is a proposed directive addressing Airbus A330 aircraft modified with the Elbe Flugzeugwerke GmbH Supplemental Type Certificate 10063798 for Passenger-to-Freighter conversion. It targets specific serial-numbered A330 aeroplanes to correct a structural issue involving non-conforming fasteners on brackets supporting the P2F Bypass Ducts in the centre fuselage. The directive aims to ensure continued airworthiness and prevent potential fuel leakage and structural integrity risks.

Jul 24, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

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