EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

EASA AD ISR-I-57-2021-12-3R1

Wings - Flaps - Fairing Seal Repair

Airworthiness Directive AD ISR I-57-2021-12-3R1 issued by the State of Israel Civil Aviation Authority addresses the GALP model G150 aircraft, serial numbers 201 through 326. This directive mandates inspection and repair of wing flap fairing seals to prevent flap fairing debonding, moisture intrusion, and corrosion of the wing lower skin at rib 3 and rib 11. The repair must be performed according to Gulfstream Service Bulletin No. 150-57-197 or later approved revisions.

Feb 1, 2024
Airworthiness DirectiveMaintenanceSafety MgmtGulfstream (Galp) G150Gulfstream G150

EASA AD ISR-I-57-2021-12-4R1

Wings - Flaps - Fairing Seal Repair

Airworthiness Directive ISR I-57-2021-12-4R1 issued by the State of Israel Civil Aviation Authority addresses the repair of wing flap fairing seals on GALP model G200 aircraft, serial numbers 004 through 250. The directive mandates inspection and resealing of the fillet seal between the wing structure and flap fairings to prevent flap fairing debonding, moisture intrusion, and corrosion of the wing lower skin at rib 3 and rib 11.

Feb 1, 2024
Airworthiness DirectiveMaintenanceSafety MgmtGulfstream (Galp) G200GALP G200

EASA SIB BEA-2024-01

FFE Ltd: Fire Suppression — Toilet Compartment Fire Extinguishers

FFE Ltd: Fire Suppression — Toilet Compartment Fire Extinguishers is a Special Airworthiness Bulletin (BEA 2024-01) issued to inform owners and operators about inspection recommendations for certain Toilet Compartment Fire Extinguishers FE-36 installed on Embraer ERJ 170, ERJ 190, EMB-135, EMB-145, EMB-545, and EMB-550 aircraft. The bulletin addresses fire extinguishers manufactured by FFE Ltd. with specific part numbers and serial numbers produced before June 12, 2023. It highlights a potential manufacturing defect that may cause leakage and loss of fire suppression capability.

Jan 31, 2024
Safety Information BulletinMaintenanceSafety MgmtEmbraer EMB-545Embraer EMB-550Embraer EMB-135Embraer EMB-145Embraer ERJ 170Embraer ERJ 190

EASA AD 2024-0036

SUPERSEDED BY EASA AD 2025-0292

EASA Airworthiness Directive 2025-0292 is an airworthiness directive concerning the Dassault Aviation Mystère-Falcon 900 aircraft. This directive supersedes previous regulations related to this aircraft type to ensure continued safety and compliance. It addresses specific maintenance and inspection requirements for the Mystère-Falcon 900 series.

Jan 31, 2024
Airworthiness DirectiveMaintenanceSafety MgmtDassault Mystère-Falcon 900Dassault Aviation Mystère-Falcon 900

EASA AD CF-2024-03

SUPERSEDED BY TCCA AD CF-2025-32

Canadian Airworthiness Directive CF-2024-03 is an emergency directive addressing cracking in the vertical stabilizer top end cap assembly of Bell Textron Canada Limited model 505 helicopters, serial number 65011 and subsequent. The directive mandates inspections and possible replacement of the stabilizer top end cap to prevent potential loss of directional control caused by parts detaching during flight.

Jan 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBell 505 (Jet Ranger X)Bell Textron Canada Limited 505

EASA AD BR-2023-07-01

[Correction] Equipment / Furnishings - Refreshment Center and Forward Cabinet - Modification

Brazilian Airworthiness Directive 2023-07-01 is an official correction and directive issued by the Agência Nacional de Aviação Civil (ANAC) affecting Embraer S.A. EMB-505 aircraft. It mandates the installation of structural reinforcements on the LH Refreshment Center and LH Forward Cabinet to ensure these components can withstand emergency landing loads. This directive applies to all EMB-505 airplanes as specified in Embraer Service Bulletin No. 505-25-0044.

Jan 25, 2024
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer EMB-505 (Phenom 300)Embraer EMB-505

EASA AD 2024-0027

SUPERSEDED BY EASA AD 2024-0230

EASA Airworthiness Directive 2024-0027 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aeroplanes, including both Current Engine Option (CEO) and New Engine Option (NEO) models. It addresses potential fatigue cracking in the bottom wing skin manhole access panel attachment holes between Rib 13 and Rib 26 on both left and right wings. The directive mandates inspections and corrective actions to ensure structural integrity of the wings.

Jan 25, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2024-0026

Engine — High Pressure Turbine — Rotor Interstage Seal — Replacement

EASA Airworthiness Directive 2024-0026 is an airworthiness directive addressing the replacement of the High Pressure Turbine Rotor Interstage Seal on CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. The directive targets specific affected parts identified by part number 2466M68P02 and certain serial numbers. It mandates replacement of these parts to ensure continued safe operation of the engines.

Jan 24, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1ACFM International LEAP-1CAirbus A319Airbus A320Airbus A321

EASA AD 2024-0025

Placards and Markings — Cargo Height Limitation — Implementation / Cargo Loading Procedure — Amendment

EASA Airworthiness Directive 2024-0025 addresses cargo height limitations and cargo loading procedures for ATR 42 and ATR 72 aircraft modified by EASA STC 10069551 Rev. 1 or EASA STC 2004-2872. This directive mandates modifications to the cargo compartment and updates to the cargo loading procedures to ensure safe operation. The directive applies specifically to aircraft converted from passenger to Class E Cargo configurations by Sabena Technics BGC.

Jan 24, 2024
Airworthiness DirectiveMaintenanceSafety MgmtATR ATR42ATR ATR72ATR 42ATR 72

EASA AD 2024-0024

THOMMEN AIRCRAFT EQUIPMENT AG: Navigation — Digital Air Data Computer — Replacement

EASA Airworthiness Directive 2024-0024 is issued for Thommen Aircraft Equipment AG AC32 Digital Air Data Computers installed on aircraft including the AW 189, Pilatus PC-21, and Cessna 550, among others with Supplemental Type Certificates. The directive addresses a known issue with certain AC32.() digital air data computers that may stop functioning at temperatures below -20°C. It mandates the replacement of affected units to ensure continued safe navigation data provision.

Jan 24, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAgustaWestland AW 189Pilatus PC-21Cessna 550

EASA AD 2024-0023

Equipment / Furnishings — Galley 4 Aft Bulkhead Cover Panel — Replacement

EASA Airworthiness Directive 2024-0023 is an official safety directive addressing certain Airbus A330 models, specifically A330-243, A330-302, A330-343, and A330-941 aeroplanes with specified manufacturer serial numbers. The directive mandates the replacement of aft bulkhead cover panels installed in galley 4 that were manufactured from non-conforming materials. This replacement ensures compliance with fire safety standards and maintains the aircraft's certification requirements.

Jan 23, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD 2024-0022

Landing Gear — Nose Landing Gear — Repair Assessment

Landing Gear — Nose Landing Gear — Repair Assessment is a regulatory document concerning the Airbus S.A.S. A319, A320, and A321 aircraft types. It addresses the assessment procedures for repairs related to the nose landing gear to ensure continued airworthiness and safety. The document provides guidance on evaluating repair conditions and standards for these specific aircraft models.

Jan 23, 2024
OtherMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD CF-2024-02

Stabilizers — Horizontal Stabilizer — Incorrect Torque Specified for Attachment Bolts

Canadian Airworthiness Directive CF-2024-02 addresses an incorrect torque specification for the horizontal stabilizer attachment bolts on Diamond Aircraft Industries Inc. model DA 62 aeroplanes, serial numbers 62.C001 through 62.C044 and 62.008 through 62.203. This directive mandates corrective actions to ensure the structural integrity of the horizontal stabilizer. It applies specifically to the DA 62 aircraft series.

Jan 23, 2024
Airworthiness DirectiveMaintenanceSafety MgmtDiamond Aircraft Industries DA 62Diamond Aircraft Industries Inc. DA 62

EASA SIB SAFO24001

Boeing 737-900ER Mid-Cabin Door Plug Inspection

The Safety Alert for Operators SAFO 24001 titled Boeing 737-900ER Mid-Cabin Door Plug Inspection informs operators about inspection recommendations for the Boeing 737-900ER fuselage plug assembly. It highlights the similarity between the 737-900ER and the 737-9 MAX mid-cabin door plug designs and addresses safety concerns following an incident involving a 737-9 MAX. The document applies to all operators under 14 CFR Parts 91, 91K, 121, 125, 129, and 135 operating the Boeing 737-900ER aircraft.

Jan 22, 2024
Safety Information BulletinMaintenanceSafety MgmtBoeing 737

EASA SIB 2024-02

Emergency Exit Safety Barriers Modification / Models Selection

EASA Safety Information Bulletin 2024-02 is an airworthiness bulletin addressing emergency exit safety barriers on Airbus A318, A319, A320, and A321 aircraft. It provides information on the different part numbers of safety barriers used during maintenance to prevent personnel from falling through open doors. The bulletin highlights concerns about the retention forces of certain upgraded barrier designs and introduces improved versions with enhanced nozzle ends.

Jan 22, 2024
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD US-2024-02-51

[Final Rule] Doors - Mid-Cabin Door Plug - Inspection

The Final Rule titled 'Doors - Mid-Cabin Door Plug - Inspection' approves a Method of Compliance (MOC) to FAA Emergency Airworthiness Directive 2024-02-51 for Boeing Model 737-9 airplanes equipped with a mid-cabin door plug. This rule provides specific inspection instructions and corrective actions to ensure the mid-cabin door plug meets type design requirements. It applies exclusively to the Boeing 737-9 aircraft listed in the referenced AD.

Jan 19, 2024
RegulationMaintenanceSafety MgmtBoeing 737Boeing 737-9

EASA AD BR-2023-01-01R1

Aeroplane Flight Manual - Section 2 Limitations - Amendment

The Brazilian Airworthiness Directive AD No. 2023-01-01R1 - EMBRAER / 39-1540 is an amendment issued by the Agência Nacional de Aviação Civil (ANAC) affecting Embraer S.A. airplanes models ERJ190-300 and ERJ 190-400. It addresses flight manual limitations related to stall warning system activation and angle of attack limiter engagement under certain gust conditions. This directive updates operational requirements to enhance flight safety for these aircraft.

Jan 18, 2024
Airworthiness DirectiveFlight OpsSafety MgmtEmbraer ERJ 190Embraer ERJ190-300Embraer ERJ190-400

EASA AD 2024-0020

Indicating and Recording Systems — Flight Warning Computer Software — Modification

EASA Airworthiness Directive 2024-0020 is an official regulatory document addressing Airbus A340-541, A340-542, A340-642, and A340-643 aeroplanes. It mandates modifications to the Flight Warning Computer software to enhance safety related to the landing gear system. The directive applies to all manufacturer serial numbers of these Airbus A340 models.

Jan 17, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A340Airbus A340-541Airbus A340-542Airbus A340-642Airbus A340-643

EASA AD 2024-0021

SUPERSEDED BY EASA AD 2024-0076

EASA Airworthiness Directive 2024-0021 is issued for Dassault Aviation Falcon 7X aeroplanes, including those modified as Falcon 8X in production. It mandates inspection of specific ailerons with certain part numbers and serial numbers due to potential excessive trailing edge thickness that could compromise structural integrity. The directive provides detailed inspection and corrective action instructions based on Dassault Service Bulletins 7X-593 Revision 1 and 7X-594.

Jan 17, 2024
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 7XDassault Falcon 8X

EASA AD CF-2024-01

Landing Gear — Main Landing Gear — Brake Fuse/Shuttle Valve Assembly — Failure Caused by Assembly Error

Canadian Airworthiness Directive CF-2024-01 addresses a failure in the brake fuse/shuttle valve assembly caused by a factory assembly error affecting De Havilland Aircraft of Canada Limited DHC-8-401 and DHC-8-402 aeroplanes, serial numbers 4001, 4003, and subsequent. The directive mandates inspection and possible replacement of affected fuse/shuttle valve assemblies to prevent loss of critical landing gear and braking functions. This AD aims to ensure continued safe operation of the affected aircraft models.

Jan 12, 2024
Airworthiness DirectiveMaintenanceSafety MgmtDe Havilland Canada DHC-8De Havilland DHC-8-401De Havilland DHC-8-402