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EASA Regulations & Airworthiness Directives

Browse 5032 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 2025-0290

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2025-0290 is an amendment addressing time limits and maintenance checks in the Airworthiness Limitations Section for Dassault Aviation Falcon 900EX aeroplanes, including the Falcon 900EX Easy, Falcon 900LX, and Falcon 900DX models. This directive applies to aircraft with serial numbers 97 and 120 and above and mandates compliance with updated maintenance tasks and life limits as specified in the latest Aircraft Maintenance Manual. It ensures continued airworthiness by enforcing mandatory maintenance requirements.

Dec 19, 2025
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 900EX

EASA AD 2025-0206R1

Engine — High Pressure Turbine Blades — Inspection

EASA Airworthiness Directive 2025-0206R1 is a regulatory update concerning the inspection of high pressure turbine (HPT) blades on Rolls-Royce Trent 1000 engines installed on Boeing 787 aircraft. It mandates repetitive on-wing borescope inspections of specific HPT blades to detect cracks and requires corrective actions including engine removal and blade replacement if cracks exceed defined limits. The directive applies to multiple Trent 1000 engine variants and aims to ensure continued airworthiness and safety.

Dec 18, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT 1000

EASA AD 2025-0285

Wings — Main Wing Spar — Inspection

EASA Airworthiness Directive 2025-0285 is an airworthiness directive addressing the inspection of the main wing spars on AMS-FLIGHT d.o.o. CARAT A powered sailplanes, specifically serial numbers CA005 to CA010 inclusive and CA032. The directive mandates a one-time inspection of the bonding between the upper spar cap and the spar web on both left-hand and right-hand main wing spars to ensure structural integrity. This AD applies to aircraft certified under TCDS number EASA.A.448.

Dec 18, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAms - Flight CARAT A

EASA AD 2025-0286

Aircraft Flight Manual — Emergency Procedure Section — Amendment; Master Minimum Equipment List — Amendment; Communications — Digital Radio and Audio Integrating Management System — Modification

EASA Airworthiness Directive 2025-0286 is an amendment addressing Airbus A330-941 aeroplanes with specific manufacturer serial numbers. It mandates updates to the Aircraft Flight Manual emergency procedures, amendments to the Master Minimum Equipment List, and modifications to the Communications system involving the Digital Radio and Audio Integrating Management System. This directive ensures continued airworthiness and operational safety of affected Airbus A330 aircraft.

Dec 17, 2025
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtAirbus A330

EASA AD 2025-0288

Engine — Low Pressure Compressor Blades — Removal from Service

EASA Airworthiness Directive 2025-0288 is an official regulatory document addressing the removal from service of certain low pressure compressor blades installed on Rolls-Royce Deutschland RB211 Trent 700 engines, commonly found on Airbus A330 aircraft. The directive identifies specific part numbers and serial numbers of affected compressor blades that have undergone erroneous repairs, leading to potential blade cracking. It mandates inspections and removal of these parts to ensure continued airworthiness and safety.

Dec 17, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 700

EASA AD 25-196

Fuselage — Forward Fuselage Skin Panels — Inspection

EASA Airworthiness Directive Proposal 25-196 is a regulatory document addressing inspection requirements for forward fuselage skin panels on specific Airbus A319, A320, and A321 aircraft models. It applies to certain serial numbers and targets panels with potential thickness deviations identified by an Airbus supplier. The directive mandates inspections and possible corrective actions to ensure structural integrity.

Dec 17, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2025-0287

Powerplant — Fuel Draining System — Inspection

EASA Airworthiness Directive 2025-0287 is an airworthiness directive addressing Airbus Helicopters AS 355 series, including AS 355 E, F, F1, F2, N, and NP models. It mandates inspections and corrective actions for the fuel draining system's rear cargo compartment hoses, specifically part number 350A21010123, to prevent potential damage from hot air leakage and fire risks. The directive includes operational checks, installation of thermal paper, and silicone tape application to affected parts.

Dec 17, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 355

EASA AD 2025-0289

Wings — Centre Wing Box Fastener Holes at Frame 40 Vertical Web — Inspection

EASA Airworthiness Directive 2025-0289 is an airworthiness directive issued by EASA concerning Airbus A330-743L aeroplanes. It mandates inspections of the centre wing box fastener holes at Frame 40 vertical web to detect cracks that could compromise the structural integrity of the aircraft's centre fuselage. The directive applies to all manufacturer serial numbers of the Airbus A330-743L.

Dec 17, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 2025-0284

Flight Controls — Rudder Control System / Drive — Inspection

EASA Airworthiness Directive 2025-0284 is an airworthiness directive addressing the rudder control system drive inspection for Airbus Defence and Space GmbH Bölkow BO 208 and BO 209 aeroplanes. It mandates repetitive inspections and corrosion inhibitor applications on specific rudder drive parts identified by part numbers 208-31014 and 209-35264. The directive applies to all serial numbers of the BO 208 C Junior, BO 209 MONSUN, and BO 209 S models.

Dec 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Defence & Space Gmbh Bölkow BO 208Airbus Defence & Space Gmbh Bölkow BO 209

EASA AD 25-194

Fuel — Fuel Low Pressure Shut-Off Valve — Leak Check

EASA Airworthiness Directive Proposal PAD No. 25-194 addresses fuel low pressure shut-off valve leak checks on Airbus A330 and A340 aeroplanes. It applies to specific models including A330-243, A330-243F, A330-341, A330-342, A330-343, A330-743L, A330-841, A330-941, and A340-211 through A340-643 series. The directive targets certain fuel low pressure shut-off valve part numbers to prevent fuel leaks that could lead to fire hazards.

Dec 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus A340

EASA AD US-2025-23-03

Engine Strut Structure / Thermal Switch - Inspection

The document titled "Engine Strut Structure / Thermal Switch - Inspection" is a final rule airworthiness directive (AD 2025-23-03) issued by the Federal Aviation Administration (FAA) affecting certain Boeing Company Model 757 airplanes. It addresses issues related to precooler failures and latent failures of overheat detection thermal switches that could cause heat damage to the engine strut structure. The AD mandates inspections, tests, and replacements to ensure continued airworthiness and safety.

Dec 15, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757

EASA AD US-2025-25-04

Equipment / Furnishings - Escape Slide Assembly - Inspection

The Equipment / Furnishings - Escape Slide Assembly - Inspection is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2025-25-04) that applies to The Boeing Company Model 737-600, -700, -700C, -800, -900, -900ER, 737-8, 737-9, and 737-8200 airplanes. This directive addresses the inspection and replacement of certain escape slide assemblies to prevent uncommanded inflation inside the slide compartment, which could cause injury or impede emergency evacuation.

Dec 15, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737

EASA AD 2023-0147R2

Time Limits / Maintenance Checks — Main Gearbox Suspension Bar Pins / Fittings — Re-calculation of Life Limits / Replacement / Modification; Fuselage — Main Gearbox Suspension Bar Pins / Fittings — Replacement / Modification

EASA Airworthiness Directive 2023-0147R2 is an updated regulatory document addressing the main gearbox suspension bar pins and fittings on Airbus Helicopters AS 332 L2 and EC 225 LP models. It provides revised instructions for recalculating life limits, replacing affected parts, and performing modifications to ensure continued airworthiness. The directive applies to specific part numbers of pins and fittings related to the main gearbox suspension bars.

Dec 15, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

EASA AD 2025-0261R1

Engine Fuel and Control — Fuel Pump — Replacement

EASA Airworthiness Directive 2025-0261R1 is a regulatory update addressing the Rolls-Royce Trent XWB-97 engines. It mandates the replacement of certain fuel pumps, specifically those with Part Number G5020FPU02 and affected serial numbers, due to identified fatigue damage that could impair engine thrust. This directive ensures continued airworthiness by requiring operators to replace affected fuel pumps within specified flight hour or cycle limits.

Dec 12, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg TRENT XWB

EASA AD 2025-0282

Equipment / Furnishings — Emergency Locator Transmitter — Rotorcraft Flight Manual — Amendment / Operational Restrictions / Modification

EASA Airworthiness Directive 2025-0282 is an airworthiness directive affecting Hélicoptères Guimbal Cabri G2 helicopters, specifically serial numbers 1003 to 1389 except 1383 and 1388. It addresses issues related to the Emergency Locator Transmitter (ELT) installation and requires amendments to the Rotorcraft Flight Manual and modifications to the ELT antenna installation.

Dec 12, 2025
Airworthiness DirectiveMaintenanceSafety MgmtGuimbal, Helicopteres CABRI

EASA AD 2025-0274

[Correction] Fire Protection — Fire Panel — Inspection

The document titled '[Correction] Fire Protection — Fire Panel — Inspection' is a correction notice related to the Airbus S.A.S. aircraft types A318, A319, A320, and A321. It addresses inspection procedures for the fire protection fire panel systems on these specific Airbus models. The correction aims to clarify or amend previous instructions to ensure proper maintenance and safety compliance.

Dec 11, 2025
CorrectionMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SD SD-2025-02R1

Flight Procedure Design software used in the calculation of final approach minima for non-precision approaches

EASA Safety Directive 2025-02R1 addresses a critical safety issue related to the Flight Procedure Design and Management (FPDAM) software used in calculating final approach minima for non-precision approaches. The directive highlights that certain versions of the FPDAM software, including version 10.10.2.152, may produce obstacle clearance altitudes/heights (OCA/H) that are too low, potentially compromising obstacle clearance. This affects Flight Procedure Design service providers and Air Traffic Services providers contracting these services across Europe.

Dec 11, 2025
Safety DirectiveSafety Mgmt

EASA AD 2025-0247R1

Fuselage — Forward and Aft Cargo Door Piano Hinges — Inspection

EASA Airworthiness Directive 2025-0247R1 is an updated regulatory requirement for Airbus A350-941 and A350-1041 aeroplanes concerning the inspection of forward and aft cargo door piano hinges. This directive mandates repetitive inspections of specific piano hinges and related structures to detect cracks, damage, or sheared fasteners that could compromise the structural integrity of the aircraft fuselage. The directive applies to all manufacturer serial numbers of the affected Airbus A350 models.

Dec 11, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350

EASA AD 2025-0281

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2025-0281 is an amendment addressing the time limits and maintenance checks for Pilatus PC-6 aeroplanes. It mandates compliance with updated airworthiness limitations specified in the latest approved Aircraft Maintenance Manual and Airworthiness Limitations Section documents. This directive applies to all manufacturer serial numbers of the PC-6 aircraft.

Dec 11, 2025
Airworthiness DirectiveMaintenanceSafety MgmtPilatus Aircraft PC-6