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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

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EASA AD 2019-0044R1

Wings — Centre Section Frame 40 Forward Fitting Radius at Tension Bolt Junction — Inspection / Repair

The document titled 'Wings — Centre Section Frame 40 Forward Fitting Radius at Tension Bolt Junction — Inspection / Repair' is an Airworthiness Directive issued by AIRBUS S.A.S. specifically for the Airbus A300-600 aircraft. It addresses inspection and repair requirements for the forward fitting radius at the tension bolt junction on the centre section frame 40 of the wing. The directive aims to ensure structural integrity and safety of the affected aircraft component.

Oct 22, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2025-0231

Fire Protection — Pyrotechnical Cartridge — Inspection

EASA Airworthiness Directive 2025-0231 is an airworthiness directive addressing the inspection of pyrotechnical cartridges used in the fire protection system of Airbus Helicopters SA 330 J helicopters. It mandates repetitive inspections of specific pyrotechnical cartridges identified by part and serial numbers to ensure their proper function in activating engine fire extinguishers. The directive applies to all serial numbers of the SA 330 J helicopter model.

Oct 21, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225

EASA AD 2025-0230-E

Powerplant — Turbocharger and Intercooler Hoses — Inspection/Replacement

EASA Airworthiness Directive 2025-0230-E is an emergency directive addressing inspection and replacement requirements for turbocharger and intercooler hoses on Textron Aviation Inc. (formerly Cessna) Model 182M, 182N, 182P, 182Q, 182R, and Reims-manufactured F182P and F182Q aeroplanes equipped with SMA SR305-230 series engines. The directive targets specific intercooler inlet/outlet hoses with defined part numbers to prevent potential engine power loss. It mandates inspections and replacements to ensure continued airworthiness.

Oct 21, 2025
Airworthiness DirectiveMaintenanceSafety MgmtTextron Aviation 182 (Skylane)Textron Aviation F182

EASA AD 2021-0281R3

Aircraft Flight Manual / Engine Bleed Air System — Amendment / Pneumatic — Engine Bleed Air System — Maintenance Tasks

EASA Airworthiness Directive 2021-0281R3 is an amendment addressing the engine bleed air system on Airbus A330 series aeroplanes, including models A330-201 through A330-743L. It mandates updates to the Aircraft Flight Manual and maintenance tasks related to the pneumatic engine bleed air system to mitigate risks of engine bleed system over-temperature and valve malfunctions. The directive applies to all manufacturer serial numbers of the affected A330 variants.

Oct 20, 2025
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtAirbus A330

EASA SIB 2025-08

Failure of the Digital Radio and Audio Integrated Management System on the Airbus A320 NEO and A330 Family Aeroplanes

The EASA Safety Information Bulletin 2025-08 addresses failures of the Digital Radio and Audio Integrated Management System (DRAIMS) on Airbus A320 NEO and A330 family aeroplanes. These failures can cause partial or total loss of radio communications, transponder, and Airborne Collision Avoidance System (ACAS) functionality, impacting flight safety and Air Traffic Control operations. The bulletin raises awareness of these issues and provides information on temporary procedures and ongoing software modifications.

Oct 20, 2025
Safety Information BulletinFlight OpsSafety MgmtAirbus A320Airbus A330

EASA AD 2025-0229

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2025-0229 is an amendment concerning the Dassault Aviation Falcon 7X aeroplanes, including those modified with Dassault modification M1000 (Falcon 8X). It updates the Airworthiness Limitations Section (ALS) of the maintenance manual, specifically Chapter 5-40 (DGT 107838) Revision 14, to ensure continued airworthiness through mandatory maintenance tasks and life limit replacements.

Oct 20, 2025
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 7X

EASA AD 2007-0201R1

Engine — High Pressure and Intermediate Pressure Turbine Bearing Oil Vent Tubes — Inspection / Cleaning / Replacement

EASA Airworthiness Directive 2007-0201R1 is a regulatory document addressing inspection, cleaning, and replacement requirements for the high pressure and intermediate pressure turbine bearing oil vent tubes on Rolls-Royce RB211 Trent 700 series engines, commonly installed on Airbus A330 aircraft. The directive aims to prevent engine failures caused by carbon build-up and oil vent tube blockages that can lead to turbine blade release and internal fires.

Oct 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 700

EASA AD 2025-0226

Engine — Propeller Gear Box / Referenced Flight Cycles — Recalculation / Replacement

The document titled "Engine — Propeller Gear Box / Referenced Flight Cycles — Recalculation / Replacement" is an explanatory statement related to the absence of an Airworthiness Directive (AD) for the Europrop International GmbH TP400-D6 engine. It clarifies that no Europrop TP400-D6 engines are currently in civil service, and therefore, no public AD exists. The document serves as an informational record provided by EASA to military authorities and design approval holders.

Oct 16, 2025
OtherMaintenanceSafety MgmtEpi Europrop International Gmbh TP400-D6

EASA AD ISR-I-05-2025-10-1

G150 Airworthiness Limitations Section Revision

The G150 Airworthiness Limitations Section Revision is an Airworthiness Directive issued by the Civil Aviation Authority of Israel that applies to all G150 model aircraft. This directive mandates updates to the Aircraft Maintenance Manual (AMM) to revision 30 or later, reflecting changes in inspection procedures and intervals. It aims to ensure continued airworthiness and safety compliance for G150 operators.

Oct 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtGulfstream (Galp) G150

EASA AD 2025-0227

Main Rotor — Upper and Lower H Legs — Service Life Limit

EASA Airworthiness Directive 2025-0227 is issued for Airbus Helicopters EC 175 B models, addressing the service life limits of the main rotor upper and lower H legs. This directive mandates replacement of affected parts that have reached or are nearing 10 years since manufacture to prevent potential structural failure. It applies to all serial numbers of the EC 175 B helicopter and updates previous service life limitations.

Oct 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters EC175

EASA SIB SAIB-2025-10

Propeller Controlling System

The FAA Special Airworthiness Information Bulletin SAIB: 2025-10 addresses potential pitch change yoke fractures in Hamilton Sundstrand Corporation Model 247F-3 propellers installed on Xi'an Aircraft Industrial Corporation Model MA60 airplanes. This bulletin highlights an airworthiness concern specific to the Xi’an Model MA60, which is not FAA type certificated, and does not apply to other airplanes with 247F series propellers. The document provides information and recommendations but does not mandate regulatory action.

Oct 16, 2025
Safety Information BulletinMaintenanceSafety MgmtHamilton Sundstrand 247F

EASA AD 2025-0225-E

SUPERSEDED BY EASA EMERGENCY AD 2025-0230-E

EASA Airworthiness Directive 2025-0225-E is an emergency directive addressing the inspection and replacement of turbocharger and intercooler hoses on Textron Aviation Inc. Model 182M through 182R and Reims F182P and F182Q aeroplanes equipped with SMA SR305-230 engine installations under EASA STC 10013975. The directive targets specific intercooler inlet/outlet hoses identified by part numbers SP01170459-0, SP01170385-1, SP01170460-0, SP01170386-1, 1500004183-1, and 1500004182-1. It mandates inspections and replacement to prevent engine power loss due to damaged hoses.

Oct 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtTextron Aviation 182 (Skylane)Textron Aviation F182

EASA AD 2025-0224

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 / Damage Tolerant Airworthiness Limitations Items — Amendment

EASA Airworthiness Directive 2025-0224 is an amendment addressing the Airbus A310 aeroplanes. It mandates the incorporation of new damage tolerant airworthiness limitations tasks introduced in the Airbus A310 Airworthiness Limitations Section Part 2 Damage Tolerant Airworthiness Limitations Items Revision 4 Variation 4.1. This directive ensures continued airworthiness by updating maintenance requirements for all certified Airbus A310 models.

Oct 16, 2025
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A310

EASA AD 2025-0222

AEROSPACE & DEFENSE OXYGEN SYSTEMS SaS (Part of SAFRAN AEROSYSTEMS): Portable Breathing Equipment — Operational Instructions

EASA Airworthiness Directive 2025-0222 addresses Portable Breathing Equipment (PBE) Part Numbers 15-40F-11 and 15-40F-80 manufactured by Aerospace & Defense Oxygen Systems, part of SAFRAN Aerosystems. This directive applies to PBEs installed on any aircraft, whether during production or in-service modifications. It mandates updated operational instructions to ensure correct usage of the PBE.

Oct 13, 2025
Airworthiness DirectiveFlight OpsSafety Mgmt

EASA SIB 2025-07

Continuous Use of Stop Bars

EASA Safety Information Bulletin No. 2025-07 titled Continuous Use of Stop Bars addresses the use of stop bars at aerodromes to prevent runway incursions. The bulletin applies to aerodrome operators, aerodrome air traffic control service providers, national competent authorities, and EASA member states. It highlights that continuous use of stop bars, beyond low-visibility conditions, can significantly reduce runway incursions involving commercial aircraft.

Oct 13, 2025
Safety Information BulletinSafety Mgmt

EASA AD CF-2025-50

Flight Controls — Roll Control Input-Modules (RCIMs) Incorrect Installation

The Canadian Airworthiness Directive CF-2025-50 addresses incorrect installation of Roll Control Input-Modules (RCIMs) on Bombardier Inc. model BD-700-1A10 and BD-700-1A11 aircraft, serial numbers 9002 through 9998 and 60001 through 60184. This directive mandates compliance with updated Aircraft Maintenance Manual procedures and requires replacement and testing of certain RCIM part numbers to ensure proper roll control function and prevent loss of aircraft control.

Oct 13, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700

EASA AD CF-2025-49

Wings — Low Clearance Between Fuel Vent Tube Installation and Surrounding Systems and Structures in Right Wing

Airworthiness Directive CF-2025-49 addresses low clearance issues between the fuel vent tube installation and surrounding systems in the right wing of Bombardier Inc. model BD-700-2A12 aeroplanes, serial numbers 70005 through 70179. The directive mandates corrective actions to prevent potential ignition sources in the fuel tank caused by lightning strikes. It requires compliance with Bombardier Service Bulletin 700-57-7537 Revision No. 01 or later approved revisions.

Oct 13, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBombardier BD-700

EASA AD 2025-0221-E

Flight Controls — Rudder Control System / Bracket to Frame 29 — Inspection

EASA Airworthiness Directive 2025-0221-E is an emergency directive addressing the rudder control system bracket to frame 29 on Polskie Zakłady Lotnicze Sp.z.o.o. PZL M28 02 (including M28 02-W variant) and PZL M28 05 aeroplanes. It mandates a one-time inspection of the frame 29 and rudder control unit mounting components to detect damage that could compromise rudder control. This directive applies to all serial numbers of the affected aircraft models.

Oct 10, 2025
Airworthiness DirectiveMaintenanceSafety MgmtPolskie Zaklady Lotnicze (Pzl) Mielec M28

EASA AD 2025-0220

Flight Manual — Amendment; Powerplant — Operational Restriction; Placards and Markings — Placards — Installation

EASA Airworthiness Directive 2025-0220 addresses safety concerns for DG-1000T powered sailplanes related to propeller adapter rings. It applies to all serial numbers of DG-1000T sailplanes and introduces operational restrictions on the powerplant, flight manual amendments, and placard installations to prevent propeller separation incidents. The directive also specifies part installation restrictions and optional modifications to improve safety.

Oct 10, 2025
Airworthiness DirectiveFlight OpsMaintenanceSafety MgmtDg Aviation Gmbh DG-1000

EASA AD US-2025-18-02

Oxygen - Passenger Service Unit Oxygen Panel Assemblies - Inspection

The Federal Aviation Administration's Airworthiness Directive 2025-18-02 addresses an unsafe condition affecting all Boeing 787-8, 787-9, and 787-10 airplanes. This directive requires inspection of passenger service unit (PSU) oxygen panel assemblies installed in the forward-most position of a center stow bin due to the risk of oxygen supply tubing becoming kinked. The AD prohibits installation of affected parts and mandates corrective actions to ensure safety.

Oct 10, 2025
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 787