EASA Regulations & Airworthiness Directives

Browse 4980 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320278 Airbus A321274 Airbus A319245 Airbus A350213 Airbus A330209 All193 Airbus A318184 Airbus A380171 Boeing 737170 Airbus A340140 Airbus A350-941124 Airbus BD-500 (A220 Series)116 Airbus Helicopters AS 332115 Airbus Helicopters EC 225112 Airbus Helicopters SA 330112 Show all...

EASA AD 2026-0133

Fuselage – Centre Fuselage Forward Pressure Bulkhead – Inspection

EASA Airworthiness Directive 2026-0133 is an airworthiness directive addressing inspection requirements for the centre fuselage forward pressure bulkhead on Airbus A318, A319, A320, and A321 aeroplanes. It applies to various models and serial numbers except those with specific Airbus modifications embodied in production or service. The directive mandates repetitive rototest inspections of the forward pressure bulkhead hole C1 and provides an optional terminating modification.

Jul 8, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2026-0052R1

Instruments – Fuse Cover Attachment of Circuit Breaker Panel – Modification

EASA Airworthiness Directive 2026-0052R1 is a regulatory update addressing a safety issue in Airbus Helicopters AS 350 B2, AS 350 B3, and EC 130 B4 models. The directive mandates modification of the fuse cover attachment on the circuit breaker panel to prevent interference with the pilot pedal, which could impair yaw control. This AD applies to specific affected parts identified by part numbers and requires compliance with updated service bulletin instructions.

Jul 8, 2026

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

EASA AD 2026-0132

Rotors Flight Control – Upper Ball Bearing End of the Main Rotor Servo-Controls – Inspection

EASA Airworthiness Directive 2026-0132 is an airworthiness directive addressing the inspection of the upper ball bearing ends of the main rotor servo-controls on Airbus Helicopters AS 350 B3, AS 355 (F, F1, F2, N, NP), and EC 130 (B4, T2) models. The directive mandates a one-time and recurring inspection of the nut tightening torque on affected parts to prevent potential disconnection of the upper ball bearing end from the main rotor servo-controls. This AD applies to specific part numbers equipped with certain nut retainers and aims to ensure continued safe flight control operation.

Jul 8, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters AS 355Airbus Helicopters AS 350 B3Airbus Helicopters AS 355 FAirbus Helicopters AS 355 F1Airbus Helicopters AS 355 F2Airbus Helicopters AS 355 NAirbus Helicopters AS 355 NPAirbus Helicopters EC 130 B4Airbus Helicopters EC 130 T2

EASA AD 2025-0274R1

Fire Protection – Fire Panel – Inspection

EASA Airworthiness Directive 2025-0274R1 is a regulatory update addressing fire panel inspections on Airbus A318, A319, A320, and A321 aircraft. It targets specific fire panel part numbers that have been linked to incidents of engine fire switch self-releasing, which could cause uncommanded in-flight engine shutdowns. The directive mandates inspections, replacements, and installation requirements to ensure continued airworthiness and safety.

Jul 7, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD US-2026-13-03

Fuselage - Stringers and Stringer Splice Fittings - Inspection

The Federal Aviation Administration's Airworthiness Directive 2026-13-03 addresses certain Boeing 747-8F series airplanes. This directive mandates inspections of fuselage stringers and stringer splice fittings for cracking and the presence of radius fillers at specific fastener locations. It also requires applicable on-condition actions to ensure continued airworthiness.

Jul 7, 2026

Airworthiness DirectiveMaintenanceSafety MgmtBoeing 747Boeing 747-8F

EASA AD 2025-0158R2

Landing Gear – Main Landing Gear Door Actuators – Inspections

EASA Airworthiness Directive 2025-0158R2 is an updated regulatory requirement addressing inspections and corrective actions for main landing gear door actuators on Airbus A318, A319, A320, and A321 aircraft models. It targets actuators with specific part number 114122015 and serial numbers listed in Airbus Alert Operators Transmission A32N033-24, aiming to prevent landing gear extension issues caused by actuator assembly errors. The directive mandates repetitive inspections and eventual replacement or modification of affected parts to ensure continued airworthiness.

Jul 7, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD US-2026-13-05

Air Conditioning - AFM Operating Procedures - Amendment

The Air Conditioning - AFM Operating Procedures - Amendment is an updated regulatory document concerning the Boeing 737 aircraft type. It provides revised operating procedures related to the air conditioning systems as specified in the Aircraft Flight Manual (AFM). This amendment aims to ensure continued safe and efficient operation of the affected Boeing 737 models.

Jul 6, 2026

OtherFlight OpsSafety MgmtBoeing 737

EASA AD 2026-0130

Electrical Systems Installation – Battery Retaining Rods – Identification / Replacement

EASA Airworthiness Directive 2026-0130 is an airworthiness directive addressing battery retaining rods on Airbus A318, A319, A320, and A321 aeroplanes. It mandates inspections and potential replacement or reidentification of affected battery retaining rods with Part Number D9241023700000 to prevent battery displacement and associated electrical system failures.

Jul 6, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2026-0131

Engine Fuel & Control – Electronic Engine Control Unit – Software Update; Engine Fuel & Control – Preference Injector – Non-extinguishing Test / Replacement

EASA Airworthiness Directive 2026-0131 addresses safety concerns for SAFRAN Helicopter Engines ARRIUS 2B2 engines, commonly installed on Airbus Helicopters Deutschland EC135 and EC635 models. The directive mandates software updates to the Electronic Engine Control Unit and introduces non-extinguishing tests and replacement requirements for the preference injector component. These measures aim to prevent engine flameouts caused by fuel coking and injector clogging.

Jul 6, 2026

Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIUS 2Airbus Helicopters EC135Airbus Helicopters EC635

EASA AD 26-083

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

EASA Airworthiness Directive PAD No. 26-083 is a proposed amendment addressing time limits and maintenance checks in the Airworthiness Limitations Section for CFM INTERNATIONAL CFM56-7B engines installed on Boeing 737-600, 737-700, 737-800, 737-900, and 737-900ER aircraft. The directive updates mandatory life limits and inspection tasks to ensure continued airworthiness of these engines. It applies to all serial numbers of multiple CFM56-7B engine variants.

Jul 6, 2026

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

EASA AD 2025-0094R1

Electrical Power – Overhead Panel Wires Interference – Inspection / Modification

EASA Airworthiness Directive 2025-0094R1 is issued for Leonardo S.p.A. AB139 and AW139 helicopters, addressing interference issues between electrical cables and connectors in the overhead panel. The directive mandates inspections and modifications to prevent potential cable damage that could lead to fire and loss of helicopter control. It applies to all serial numbers from 31201 onward, focusing on Long Nose helicopter configurations.

Jul 3, 2026

Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters AB139Leonardo S.P.A. Helicopters AW139Leonardo AB139Leonardo AW139

EASA AD 2025-0171R2

Engine – High Pressure Turbine Rotor Stage 1 Blade – Inspection

EASA Airworthiness Directive 2025-0171R2 is an updated regulatory requirement addressing inspections of high pressure turbine (HPT) rotor stage 1 blades on CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. The directive mandates repetitive borescope inspections of specific affected turbine blades to detect cracks and prevent potential in-flight engine failures. It applies to multiple LEAP-1A engine variants and specifies affected part numbers for inspection and corrective actions.

Jul 3, 2026

Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1ACFM International LEAP-1CAirbus A319Airbus A320Airbus A321

EASA AD CF-2026-26

Fuselage – Corrosion on Waste Box, Waste Access Doubler and Waste Service Door of Aft Waste Service Port

The Canadian Airworthiness Directive CF-2026-26 addresses corrosion issues on the waste box, waste access doubler, and waste service door of the aft waste service port on Airbus Canada Limited Partnership (ACLP) aircraft models BD-500-1A10 and BD-500-1A11. This directive mandates inspections, repairs, and application of protective coatings to prevent structural damage caused by corrosion. It applies to aircraft with specific serial numbers ranging from 50001 to 50047 for BD-500-1A10 and 55001 to 55063 for BD-500-1A11.

Jul 3, 2026

Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada Limited Partnership BD-500-1A10Airbus Canada Limited Partnership BD-500-1A11

EASA SIB 2022-02R4

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

The EASA Safety Information Bulletin 2022-02R4 is an updated advisory addressing the increase in Global Navigation Satellite System (GNSS) jamming and spoofing incidents affecting communication, navigation, and surveillance systems in aviation. It highlights the impact on flight operations, particularly in regions near conflict or geopolitical risk zones, and provides guidance for National Competent Authorities, air operators, ATM/ANS providers, and manufacturers. The bulletin does not target specific aircraft or engine models but focuses on GNSS-dependent systems broadly.

Jul 3, 2026

Safety Information BulletinFlight OpsSafety Mgmt

EASA AD 2026-0129

Main Rotor Drive – Main Gearbox Flexible Mounting Plate – Maintenance Task

EASA Airworthiness Directive 2026-0129 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 C, C1, L, and L1 models. It mandates maintenance on the main gearbox flexible mounting plate, specifically part numbers 332A38010600 and 332A38010620, to ensure proper torque on attachment bolts. This directive addresses a maintenance task correction related to helicopters performing external load transport with loads of 2.5 tons or less.

Jul 3, 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 2026-0123

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

EASA Airworthiness Directive 2026-0123 is an amendment concerning time limits and maintenance checks in the Airworthiness Limitations Section for GE Aviation Czech H75, H80, and H85 engine models. This directive applies to these engines installed on aircraft such as the Aircraft Industries L410-UVP-E20, L410-NG, Do 28 series, Thrush S-2R series, and Viking Air DHC-3 Otter. It mandates compliance with updated maintenance tasks and life limits to ensure continued airworthiness.

Jul 3, 2026

Airworthiness DirectiveMaintenanceSafety MgmtGe Aviation Czech H75, H80, H85Aircraft Industries L410-UVP-E20Aircraft Industries L410-NGDornier Do 28Thrush S-2RViking Air DHC-3 Otter

EASA AD 2026-0128

Engine Fuel & Control – Hydromechanical Metering Unit – Replacement

EASA Airworthiness Directive 2026-0128 is an official safety 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 identified by part number 01648511170 and certain serial numbers listed in the AD. It mandates the replacement of affected HMUs to prevent engine fuel flow issues that could lead to uncommanded engine shutdowns.

Jul 2, 2026

Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIUS 1Airbus Helicopters AS 355 N

EASA AD 26-082

Flight Controls – Roll Spoiler Actuator Mount – Inspection

EASA Airworthiness Directive Proposal PAD No. 26-082 addresses the inspection of roll spoiler actuator mounts on Dornier 328-100 aeroplanes. The directive targets corrosion issues found around the pivot-bearing area of the roll spoiler actuator mounts, which could affect flight control. It applies to all manufacturer serial numbers of Dornier 328-100 aircraft.

Jul 2, 2026

Airworthiness DirectiveMaintenanceSafety MgmtDeutsche Aircraft Gmbh Dornier 328Dornier 328-100

EASA AD 26-081

Fire Protection – Pyrotechnical Cartridge – Inspection

EASA Airworthiness Directive PAD No. 26-081 is a proposed directive addressing fire protection inspections for pyrotechnical cartridges installed on Dassault Aviation Mystère-Falcon and Fan Jet Falcon aeroplanes. It applies to all serial numbers of Fan Jet Falcon, Mystère-Falcon 20-( )5 series, Mystère-Falcon 200, and 20 GF models. The directive mandates repetitive inspections and potential replacement of specific pyrotechnical cartridges to ensure fire extinguishing capability.

Jul 1, 2026

Airworthiness DirectiveMaintenanceSafety MgmtDassault Fan Jet FalconDassault MystÃ¨re-Falcon 20Dassault MystÃ¨re-Falcon 20GFDassault 200Dassault Mystère-Falcon 20-( )5Dassault Mystère-Falcon 200Dassault 20 GF

EASA AD 2026-0124

Flight Controls – Aileron Hinge / Cotter Pins – Inspection

EASA Airworthiness Directive 2026-0124 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Tecnam P2006T and P2006T NG aeroplanes. It mandates inspection of the aileron hinge assemblies and cotter pins to ensure their integrity and prevent potential detachment of the ailerons. This directive applies to specific serial numbers of these aircraft models and aims to maintain flight safety by addressing a critical flight control component issue.

Jul 1, 2026

Airworthiness DirectiveMaintenanceSafety MgmtTecnam P2006TTecnam P2006T NG