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EASA Regulations & Airworthiness Directives

Browse 4987 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320280Airbus A321276Airbus A319246Airbus A350214Airbus A330209All193Airbus A318185Airbus A380171Boeing 737170Airbus A340140Airbus A350-941125Airbus BD-500 (A220 Series)116Airbus Helicopters AS 332115Airbus Helicopters EC 225112Airbus Helicopters SA 330112Show all...

EASA SIB CASA-2024-03

Inboard Flap Spigot Tube and Mid and Outboard Flap Corrosion

Transport Canada Civil Aviation Safety Alert CASA 2024-03 addresses corrosion issues affecting the inboard flap spigot tubes and the internal structure of the mid and outboard flaps on Bombardier Inc. aeroplanes models BD-700-1A10 and BD-700-1A11. The alert highlights the need for inspections and corrective actions to mitigate corrosion risks in these specific aircraft components. It recommends incorporating related Maintenance Review Board Report and Aircraft Maintenance Manual tasks into the approved maintenance schedule.

May 13, 2024
Safety Information BulletinMaintenanceSafety MgmtBombardier BD-700

EASA SIB SAIB-2024-02

Wing Spar - Inspection

Special Airworthiness Information Bulletin SAIB: 2024-02 is an FAA informational bulletin addressing potential cracks and hole-quality issues in the wing rear attach beam assembly of Revo Incorporated Model Colonial C-1, Colonial C-2, Lake LA-4 series, Lake Model 250, and Lake 270 Turbo Renegade aircraft. The bulletin highlights inspection areas and provides guidance to owners, operators, and maintenance personnel to identify and address these concerns. This bulletin is not a mandatory directive but serves as a safety alert.

May 13, 2024
Safety Information BulletinMaintenanceSafety MgmtRevo, C-1Revo, C-2

EASA AD 2024-0100

SUPERSEDED BY EASA AD 2024-0233

EASA Airworthiness Directive 2024-0100 is issued for Airbus Helicopters AS 332 C, C1, L, and L1 models equipped with dual hoist installation and de-icing systems. It addresses a vibration issue around 12 Hz frequency observed after retrofit of the de-icing system, which could lead to structural failure or loss of control. The directive mandates removal or operational limitations related to the dual hoist and de-icing systems to mitigate this unsafe condition.

May 10, 2024
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 BR-2023-08-03R2

Windows - Cockpit Side Windows - Inspection / Replacement

Brazilian Airworthiness Directive AD No. 2023-08-03R02 is an official regulatory document issued by the Agência Nacional de Aviação Civil (ANAC) that applies to Embraer S.A. airplanes model EMB-545 and EMB-550 equipped with cockpit side windows having Part Numbers NP-200402-7 or NP-200402-8. The directive mandates inspection and replacement procedures for these cockpit side windows to address safety concerns. It provides detailed inspection methods and replacement requirements to prevent potential in-flight depressurization due to window failure.

May 8, 2024
Airworthiness DirectiveMaintenanceSafety MgmtEmbraer EMB-545Embraer EMB-550

EASA AD US-2024-06-01

Fuselage - Skin and Bear Strap at the Forward Galley Door Cutout - Inspection

Federal Aviation Administration Airworthiness Directive 2024-06-01 is a final rule addressing certain Boeing 737-600, -700, -700C, -800, -900, and -900ER airplanes. It mandates inspections of the fuselage skin and bear strap at the forward galley door cutout forward upper corner due to reported cracks caused by high operating stresses. The directive aims to ensure structural integrity and prevent potential rapid decompression.

May 6, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-600Boeing 737-700Boeing 737-700CBoeing 737-800Boeing 737-900Boeing 737-900ER

EASA AD 2024-0099

SUPERSEDED BY EASA AD 2025-0115

EASA Airworthiness Directive 2024-0099 is an airworthiness directive issued for Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses issues with fuselage and belly fairing mounted emergency evacuation escape slides, specifically those with certain part numbers and serial numbers that have shown seam failures during proof pressure testing after overhaul. The directive mandates replacement and inspection requirements to ensure the continued airworthiness of these emergency slides.

May 6, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380Airbus A380-841Airbus A380-842Airbus A380-861

EASA AD US-2024-06-14

Engine - High-pressure Compressor 2nd and 4th Stage Rotors - Replacement

The Federal Register document titled "Engine - High-pressure Compressor 2nd and 4th Stage Rotors - Replacement" is a final rule airworthiness directive (AD 2024-06-14) issued by the FAA affecting International Aero Engines, LLC Model PW1124G1-JM, PW1127G-JM, PW1127GA-JM, PW1129G-JM, PW1130G-JM, PW1133G-JM, and PW1133GA-JM engines. It addresses potential degradation and fracture risks in the high-pressure compressor 2nd and 4th stage rotors due to improper cleaning procedures. The AD mandates replacement of certain affected rotors to ensure continued airworthiness and safety.

May 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines PW1100International Aero Engines PW1400

EASA AD US-2024-07-05

Fuselage - Station 1640 Frame Web Between S-14 and S-15 - Inspection / Maintenance Records Check

The Federal Aviation Administration's Airworthiness Directive 2024-07-05 is a final rule addressing certain Boeing 757-200, 757-200CB, and 757-300 airplanes. It mandates inspections or maintenance records checks for liner holes in the fuselage at station 1640 frame web between stringers S-14 and S-15 due to detected cracks. The directive aims to ensure structural integrity by requiring corrective actions when necessary.

May 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 757Boeing 757-200Boeing 757-200CBBoeing 757-300

EASA AD G-2024-0001-E

Hot Air Balloons - Envelopes with Polyester Filled Aramid (Kevlar) Load Tapes — Removal from Service

The Civil Aviation Authority Emergency Airworthiness Directive G-2024-0001-E addresses safety concerns for all types and models of hot air balloon envelopes manufactured by Lindstrand Technologies Limited after March 2017 that are fitted with optional Polyester Filled Aramid (Kevlar) Load Tapes. This directive mandates inspections and potential removal from service due to significant degradation of the load tapes. It applies specifically to hot air balloons with these load tapes and aims to prevent unsafe conditions caused by ultraviolet damage to the Kevlar core.

May 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtLindstrand Technologies Series 1Lindstrand Technologies Series 2Lindstrand Technologies Series RLindstrand Technologies Limited Hot Air Balloons

EASA AD CF-2023-68R1

Stabilizer — Horizontal Stabilizer — Jamming of the Horizontal Stabilizer Trim Actuator

Airworthiness Directive CF-2023-68R1 addresses the jamming issue of the Horizontal Stabilizer Trim Actuator (HSTA) on Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft. The directive mandates lubrication and inspection procedures to prevent water intrusion and freezing in the HSTA ballscrew assembly, which can cause loss of pitch trim capability. This directive applies to specific serial numbers of the affected models and updates previous requirements.

May 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A10Airbus Canada BD-500-1A11

EASA AD 2024-0098

SUPERSEDED BY EASA AD 2024-0129

EASA Airworthiness Directive 2024-0098 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes. It mandates inspection of the forward cargo door piano hinges 2 and 3 due to potential cracking risks. This directive applies to specific manufacturer serial numbers and aims to ensure continued structural integrity of the affected aircraft.

May 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD 2024-0095

Fuselage — Bulk Cargo Door Frames — Inspection / Repair

EASA Airworthiness Directive 2024-0095 is issued for Airbus A330-202, A330-203, and A330-243 aircraft modified with specific EASA Supplemental Type Certificates related to MRTT and FSTA configurations. The directive addresses inspection and repair requirements for bulk cargo door frames, specifically focusing on potential fatigue cracks in door fitting attachment holes due to certain surface treatments. It mandates inspections and corrective actions to ensure continued airworthiness of affected aircraft.

Apr 30, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330

EASA AD CF-2024-13

Hydraulic Power — Improperly Torqued Rudder Power Control Unit Hydraulic Fittings

Canadian Airworthiness Directive CF-2024-13 addresses hydraulic power issues related to improperly torqued rudder Power Control Unit (PCU) hydraulic fittings on Airbus Canada Limited Partnership BD-500-1A11 aircraft, specifically serial numbers 55170, 55172, and 55174 through 55183. The directive mandates corrective actions to prevent hydraulic fluid leakage that could lead to loss of hydraulic systems. It applies to these specific aircraft models and serial numbers.

Apr 30, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus BD-500 (A220 Series)Airbus Canada BD-500-1A11

EASA SIB SAIB-2024-03

Rudder Control System

The Special Airworthiness Information Bulletin SAIB: 2024-03 is an FAA informational document addressing a rudder control system concern for Air Tractor, Inc. Model AT-802 airplanes, serial numbers 802-0001 through 802-1099, equipped with a two-seat cockpit, spray valve control handle, and rear cockpit rudder pedals. It highlights a potential interference issue between the rear left rudder pedal and spray valve control pushrod that may affect control during landing. This bulletin does not mandate corrective action but provides safety recommendations.

Apr 29, 2024
Safety Information BulletinSafety MgmtAir Tractor AT-600Air Tractor AT-800

EASA AD 2024-0094

ULTRAMAGIC, S.A.: Restraint Systems / Occupant Restraint Harnesses — Inspection

EASA Airworthiness Directive 2024-0094 addresses inspection requirements for Ultramagic, S.A. occupant restraint harnesses, specifically part number CI-C-1302, commonly installed on Ultramagic hot air balloons. The directive mandates inspection and potential replacement of leg lanyard tapes with incorrectly positioned adjustment buckles that compromise safety. This AD applies to all hot air balloons equipped with these harnesses, regardless of installation method.

Apr 26, 2024
Airworthiness DirectiveMaintenanceSafety Mgmt

EASA AD 2024-0077

[Correction] Fuselage — Pressure Panel Longitudinal Beams — Inspection / Repair / Modification

EASA Airworthiness Directive 2024-0077 is a regulatory document addressing inspection, repair, and modification requirements for the pressure panel longitudinal beams on Airbus A318, A319, A320, and A321 aircraft. It targets all manufacturer serial numbers except those with Airbus modification 151574 embodied in production. The directive aims to ensure structural integrity by mandating inspections and corrective actions related to fatigue cracks found around fasteners connecting the pressure panel to the flexible bracket at fuselage frame 36.

Apr 25, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD 2023-0013R1

Flight Controls — Rudder Steering Bracket — Inspections / Modification

EASA Airworthiness Directive 2023-0013R1 is an updated regulatory requirement addressing inspection and modification of the rudder steering bracket on Diamond Aircraft Industries DA 42 series aeroplanes, including DA 42, DA 42 M, DA 42 NG, and DA 42 M-NG models. The directive mandates inspections and corrective actions related to the rudder T-yoke bolt to prevent potential loss of rudder control. It applies to all manufacturer serial numbers of these aircraft.

Apr 25, 2024
Airworthiness DirectiveMaintenanceSafety MgmtDiamond Aircraft Industries DA 42Diamond Aircraft Industries DA 42 MDiamond Aircraft Industries DA 42 NGDiamond Aircraft Industries DA 42 M-NG

EASA AD US-2024-06-03

Electrical Power - P6 Panel / Standby Power Control Unit - Installation

Airworthiness Directive 2024-06-03 is a final rule issued by the Federal Aviation Administration (FAA) addressing certain Boeing 737-8 and 737-9 airplanes. It mandates the installation of two bonding jumpers from the P6 panel structure to the primary structure to prevent failure of the standby power control unit (SPCU). This directive aims to maintain critical flightcrew instrumentation and displays by ensuring redundant grounding paths.

Apr 22, 2024
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-8Boeing 737-9

EASA AD 2024-0093

Engine — Non-Synchronous Vibration During Engine Operation — Monitoring

EASA Airworthiness Directive 2024-0093 addresses non-synchronous vibration (NSV) issues during operation of CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. The directive targets specific affected parts, notably bearing No. 3 spring finger housings with certain part numbers and serial numbers, to ensure ongoing engine safety and airworthiness. It mandates monitoring and corrective actions to prevent potential engine stalls and turbine failures.

Apr 22, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1ACFM International LEAP-1CAirbus A319Airbus A320Airbus A321

EASA SIB 2024-07

Front Electric Sustainer Wiring — Inspection / Modification

EASA Safety Information Bulletin 2024-07 is an airworthiness bulletin addressing inspection and modification of the Front Electric Sustainer (FES) wiring on specific powered sailplanes. The affected aircraft include the Discus-2cFES, Ventus-2cFES, Ventus-2c modified with FES under EASA flight conditions 60037733, and Ventus-3F powered sailplanes. The bulletin highlights a potential issue with brass screws used in the FES wiring that may fail due to excessive tightening torque.

Apr 22, 2024
Safety Information BulletinMaintenanceSafety MgmtSchempp Hirth Flugzeugbau Discus Powered SailplanesSchempp Hirth Flugzeugbau Ventus Powered Sailplanes