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EASA Regulations & Airworthiness Directives

Browse 5,132 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320286 Airbus A321285 Airbus A319253 Airbus A350222 Airbus A330220 Airbus A318189 Airbus A380182 Boeing 737175 Airbus A340141 Airbus A350-941132 Airbus BD-500 (A220 Series)123 Airbus Helicopters AS 332119 Airbus Helicopters EC 225116 Airbus Helicopters SA 330116 Boeing 787114 Show all...

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.

Airworthiness Directive

Airbus 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.

Airworthiness Directive

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.

Safety Information Bulletin

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.

Airworthiness Directive

Bombardier 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.

Airworthiness Directive

Bombardier 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.

Airworthiness Directive

Polskie 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.

Airworthiness Directive

Dg 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.

Airworthiness Directive

Boeing 787

EASA AD BR-2025-10-01

Engine Feed Check Valve - Inspections / Functional Test

Brazilian Airworthiness Directive AD No. 2025-10-01 is issued by the Agência Nacional de Aviação Civil (ANAC) and applies to Embraer ERJ190-300 and ERJ190-400 aircraft equipped with Engine Feed Check Valve Part Number L85E38-003. The directive mandates inspections and functional tests of the engine feed check valves to address potential valve failures that could lead to engine flameout or fuel starvation. This AD ensures continued airworthiness and flight safety for affected aircraft registered in Brazil.

Airworthiness Directive

Embraer ERJ 190

EASA AD US-2025-20-03

Equipment / Furnishings - Lower Fitting Assemblies and Centerline Partition Threshold of Lavatories - Inspection / Revision of Maintenance Program

The document titled "Equipment / Furnishings - Lower Fitting Assemblies and Centerline Partition Threshold of Lavatories - Inspection / Revision of Maintenance Program" is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2025-20-03) addressing certain Boeing 787-8, 787-9, and 787-10 airplanes. It mandates inspections for corrosion on lower fitting assemblies and lavatory components and requires updates to the maintenance program to include inspections of lavatory vertical side forward fittings. This AD aims to ensure continued airworthiness and safety of the affected Boeing 787 models.

Airworthiness Directive

Boeing 787

EASA SIB BEA-2025-02

Fire Protection - Tube Replacement

The Special Airworthiness Bulletin BEA 2025-02 addresses corrosion issues found in the cargo compartment fire suppression system tubes of EMBRAER S.A. ERJ 190-400 aircraft. This bulletin provides information and recommendations regarding tube replacement to maintain fire protection system integrity. It is an informative bulletin and does not impose mandatory requirements or an Airworthiness Directive under RBAC 39.

Safety Information Bulletin

Embraer ERJ 190

EASA AD US-2025-20-04

Flight Controls - Aileron Trim Actuator - Repetitive Inspections / Modification

Airworthiness Directive 2025-20-04 is a final rule issued by the Federal Aviation Administration addressing The Boeing Company Model 757 airplanes. This directive mandates repetitive inspections of the aileron trim actuator bearing and attachment lug, and introduces a required modification involving changes to the lateral control box support assembly and installation of an aileron trim actuator bracket to terminate these inspections.

Airworthiness Directive

Boeing 757

EASA AD US-2025-20-11

Flight Controls - Attaching Rivets of the Pilot and Copilot Rudder Control Pushrods - Inspection

Flight Controls - Attaching Rivets of the Pilot and Copilot Rudder Control Pushrods - Inspection is a final rule airworthiness directive issued by the FAA for certain Textron Aviation Inc. Model B200GT, B200CGT, B300, and B300C airplanes. It addresses a safety issue involving the failure of rudder control pushrod rivets that could lead to loss of rudder control. The directive mandates inspection and replacement of incorrect rivets on the pilot and copilot rudder control pushrods.

Airworthiness Directive

Textron Aviation 200 (Super King Air)
Textron Aviation 300 (Super King Air)

EASA AD US-2025-19-11

Landing Gear - Main Landing Gear Outer Cylinders - Records Check / Inspection

The Federal Aviation Administration (FAA) Airworthiness Directive 2025-19-11 addresses all Boeing Company Model 757-200, -200PF, and -200CB series airplanes. This directive requires a records check or inspection of the main landing gear (MLG) outer cylinders due to reports of improper grinding causing possible heat damage. The directive mandates replacement of any affected outer cylinders to ensure continued airworthiness.

Airworthiness Directive

Boeing 757

EASA AD US-2025-17-11

Rotors Flight Control - Tail Rotor Pedal Support Brackets - Repetitive Inspections

The Federal Register document titled "Rotors Flight Control - Tail Rotor Pedal Support Brackets - Repetitive Inspections" is a final rule airworthiness directive (AD 2025-17-11) issued by the FAA affecting MD Helicopters, LLC models 369 (Army YOH-6A), 369A (Army OH-6A), 369D, 369E, 369F, 369FF, 369H, 369HE, 369HM, 369HS, 500N, and 600N. This AD addresses multiple reports of cracked tail rotor pedal support brackets by requiring repetitive inspections and, depending on findings, replacement or refinishing of affected brackets. It also prohibits installation of certain magnesium cast tail rotor pedal support brackets to ensure continued airworthiness.

Airworthiness Directive

Md Helicopters Inc (Mdhi) 369
Md Helicopters Inc (Mdhi) 500N
Md Helicopters Inc (Mdhi) 600N

EASA AD 2025-0218

Equipment / Furnishings — Emergency Location Transmitter Mounting Tray — Replacement

The document titled 'Equipment / Furnishings — Emergency Location Transmitter Mounting Tray — Replacement' pertains to the Airbus Helicopters H160 model. It addresses the replacement requirements for the mounting tray of the emergency location transmitter installed on this helicopter type. This document is intended to ensure proper equipment configuration and airworthiness compliance for the affected aircraft.

Airworthiness Directive

Airbus Helicopters H160

EASA AD 2025-0219

Superseded by EASA AD 2026-0035

EASA Airworthiness Directive 2025-0219 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330-743L aeroplanes. It mandates compliance with updated airworthiness limitations specified in the Airbus A330-700L Airworthiness Limitations Section Part 1 Variation 0.4. The directive ensures the continued airworthiness of these aircraft by enforcing replacement of life-limited parts and maintenance program revisions.

Airworthiness DirectiveSuperseded

Airbus A330

EASA AD 2025-0216

Equipment / Furnishings — Doghouse Placard — Replacement

EASA Airworthiness Directive 2025-0216 is an airworthiness directive affecting Airbus A330 and A340 aeroplanes. It mandates the replacement of doghouse placards in the passenger cabin to provide clearer door lock handling instructions. This directive applies to specific batches of doghouses installed on these aircraft models.

Airworthiness Directive

Airbus A330
Airbus A340

EASA AD 2025-0217

Rotors Flight Control — Fork Lever — Inspection

EASA Airworthiness Directive 2025-0217 is an airworthiness directive addressing the inspection of the rotors flight control fork lever on Airbus Helicopters Deutschland GmbH BO105 and MBB-BK117 helicopter models. It mandates a one-time inspection of the fork lever part numbers 105-42122.01, 117-421221.01, and 117-421231.02 to detect cracks that could lead to part failure and potential loss of helicopter control.

Airworthiness Directive

Airbus Helicopters BO 105

EASA AD 2025-0215

Stabilizers — Vertical Stabilizer to Rudder Junction Ribs and Lugs —Inspection / Replacement (Wrong Material)

EASA Airworthiness Directive 2025-0215 is an airworthiness directive addressing the inspection and replacement of vertical stabilizer to rudder junction ribs and lugs on ATR 42-500 and ATR 72-212A aeroplanes. The directive targets specific affected parts manufactured with incorrect materials that may compromise structural integrity. It applies to all manufacturer serial numbers listed in the directive's appendix and requires inspections and potential replacement of affected components.

Airworthiness Directive

ATR ATR42
ATR ATR72