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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320262Airbus A321257Airbus A319229Airbus A350206Airbus A330197All177Airbus A318172Boeing 737164Airbus A380162Airbus A340136Airbus A350-941119Airbus Helicopters AS 332110Airbus Helicopters EC 225107Airbus Helicopters SA 330107Boeing 787106Show all...

EASA AD 2024-0231

SUPERSEDED BY EASA AD 2025-0083

EASA Airworthiness Directive 2024-0231 is an airworthiness directive applicable to Airbus A318, A319, A320, and A321 aeroplanes. It mandates repetitive detailed inspections of the cargo bulkhead frame 24A vertical members and female fittings located behind the 80VU rack to detect elongation and potential damage. The directive aims to prevent possible system failures caused by affected parts hitting the 80VU rack, which could lead to reduced control of the aircraft.

Dec 4, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA AD CF-2024-39

Flight Controls — Uncommanded and Unarrested Flap Movement

Canadian Airworthiness Directive CF-2024-39 addresses the issue of uncommanded and unarrested flap movement in Bombardier Inc. model CL-600-1A11, CL-600-2A12, and CL-600-2B16 aeroplanes. This directive mandates updates to the Aircraft Flight Manual (AFM) to provide flight crews with specific procedures to follow if such flap movements occur. The directive aims to enhance flight safety by mitigating risks associated with flap control system failures.

Dec 3, 2024
Airworthiness DirectiveFlight OpsSafety MgmtBombardier CL-600 (Challenger)

EASA AD 2024-0230

Wings — Bottom Wing Skin Panel 2 — Inspection

EASA Airworthiness Directive 2024-0230 is an airworthiness directive addressing inspection requirements for the bottom wing skin panel 2 on Airbus A319, A320, and A321 aeroplanes, including both Current Engine Option (CEO) and New Engine Option (NEO) models. It mandates detailed inspections of specific wing areas prone to fatigue cracking, particularly around the bottom wing skin manhole access panel number 2 between ribs 13 and 26. The directive applies to all manufacturer serial numbers of the affected aircraft models.

Dec 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD 2024-0201R1

Wings — Outer Wing Bottom Buttstrap — Inspections

EASA Airworthiness Directive 2024-0201R1 is an updated regulatory requirement addressing inspections of the outer wing bottom buttstrap on Airbus A319, A320, and A321 aeroplanes. It mandates repetitive special detailed inspections of the wing surface area between rib 19 and rib 21 forward of stringer 8 on both left and right sides to detect cracks that could compromise structural integrity. This directive applies to all manufacturer serial numbers of the specified Airbus models.

Dec 2, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A320Airbus A321

EASA AD US-2024-20-07

Equipment / Furnishings - Emergency Float Kit Activation Handle - Repetitive Inspections / Replacement

The document titled 'Equipment / Furnishings - Emergency Float Kit Activation Handle - Repetitive Inspections / Replacement' is a regulatory directive addressing the maintenance requirements for the emergency float kit activation handle on certain aircraft. It mandates repetitive inspections and replacement procedures to ensure the proper functioning of this critical safety equipment. The directive applies to aircraft equipped with the specified emergency float kit activation handle assemblies.

Nov 29, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters AS 350Airbus Helicopters EC 130Airbus Helicopters EC 120 BAirbus Helicopters BO 105Airbus Helicopters EC135Airbus Helicopters 635Airbus Helicopters MBB-BK 117Bell 206Bell 407Bell Textron Inc. (Bti) 210Bell Textron Inc. (Bti) 212Bell Textron Inc. (Bti) 412Leonardo S.P.A. Helicopters AB212Leonardo S.P.A. Helicopters AB412Md Helicopters Inc (Mdhi) 369Md Helicopters Inc (Mdhi) 500NRobinson R44 (Raven)Robinson R66Sikorsky S-76

EASA AD 2024-0175

[Correction] Engine — Fuel Nozzle — Replacement

EASA Airworthiness Directive 2024-0175 is a corrective directive addressing the replacement of fuel injection nozzles on CFM International LEAP-1A32 engines installed on specific Airbus A321-251NX aircraft. The directive targets fuel nozzles with part numbers 2085M31G02, 2085M31G03, and 2085M31G05 due to accelerated coking issues. This AD mandates timely replacement to maintain engine performance and safety.

Nov 28, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1ACFM International LEAP-1C

EASA AD 2024-0227

Engine — High-Pressure Stage 2 Compressor Stator Seal and Rotor Seal Teeth — In-Shop Inspection

EASA Airworthiness Directive 2024-0227 is an airworthiness directive addressing certain CFM International LEAP-1B engine models installed on Boeing 737-8, 737-8200, and 737-9 aircraft. The directive mandates in-shop inspections of the high-pressure stage 2 compressor stator seals and rotor seal teeth to detect manufacturing defects that could lead to damage and reduced aircraft control. This AD applies specifically to engines with certain serial numbers and requires compliance by December 11, 2024.

Nov 27, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1B

EASA AD 2024-0226

Engine — High-Pressure Compressor Stages 6-10 Spools and High-Pressure Turbine Rotor Stage 1 Disks — Replacement

EASA Airworthiness Directive 2024-0226 is an airworthiness directive addressing the replacement of high-pressure compressor stages 6-10 spools and high-pressure turbine rotor stage 1 disks in CFM International LEAP-1B engines. These engines are commonly installed on Boeing 737-8, 737-8200, and 737-9 aircraft. The directive mandates replacement of affected parts to ensure continued airworthiness and safety.

Nov 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1B

EASA AD US-2024-20-03

Flight Controls - Governor Controller - Replacement

The Federal Aviation Administration's Airworthiness Directive 2024-20-03 addresses Robinson Helicopter Company Model R22 Beta, R22 Mariner, R44, and R44 II helicopters equipped with governor controller part number D270-1, Revisions A through E. This directive mandates the replacement of these governor controllers due to engine governor failures caused by water intrusion. The AD aims to enhance flight safety by preventing loss of engine speed governing during critical flight phases.

Nov 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtRobinson R22Robinson R44 (Raven)

EASA AD 2024-0225

SUPERSEDED BY EASA AD 2025-0243

EASA Airworthiness Directive 2024-0225 is an airworthiness directive addressing certain CFM International LEAP-1A engine models installed on Airbus A319, A320, and A321 aircraft. It mandates the replacement of forward outer seals, high-pressure compressor stages 6-10 compressor rotor spools, and high-pressure turbine rotor stage 1 disks that are affected by manufacturing defects. The directive aims to ensure continued airworthiness and prevent potential engine part failures.

Nov 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1ACFM International LEAP-1C

EASA AD 2023-0189R1

SUPERSEDED BY EASA AD 2025-0259

EASA Airworthiness Directive 2023-0189R1 is a revision addressing the Airbus A350-941 and A350-1041 aeroplanes equipped with Trent XWB engines. It focuses on the replacement and inspection of the Engine Bleed Air System (EBAS) T-Duct, part number RR03-11011-001, due to a manufacturing quality issue that could lead to cracking and potential engine failure. The directive mandates compliance with Airbus and Rolls-Royce service bulletins to ensure continued airworthiness.

Nov 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350

EASA AD 2024-0224

SUPERSEDED BY EASA AD 2026-0016

EASA Airworthiness Directive 2024-0224 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Dassault Aviation Falcon 7X aeroplanes, including those modified to Falcon 8X standard. It addresses issues related to the Spoiler Electrical Control Unit (SPECU) with Part Number 051243-01, which may cause hydraulic leakage and potential fire hazards. The directive mandates replacement of affected SPECUs to ensure continued airworthiness and safety.

Nov 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtDassault Falcon 7X

EASA AD 2024-0223

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2024-0223 is an amendment addressing the time limits and maintenance checks for Airbus Helicopters H160-B helicopters. It mandates compliance with the Airworthiness Limitations Section (ALS) Revision 016 to ensure continued airworthiness of all H160-B serial numbers. The directive applies to all configurations of the H160-B helicopter and requires adherence to updated maintenance tasks and life limits.

Nov 26, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters H160

EASA AD US-2024-19-15

[Correction] SAFRAN AEROSYSTEMS - Oxygen Cylinder and Valve Assemblies - Inspection / Replacement

Correction SAFRAN AEROSYSTEMS - Oxygen Cylinder and Valve Assemblies - Inspection / Replacement is a regulatory correction document concerning the inspection and replacement procedures for oxygen cylinder and valve assemblies manufactured by SAFRAN AEROSYSTEMS. The document addresses safety and maintenance requirements for these specific oxygen system components used in aircraft. It aims to ensure continued airworthiness and operational safety by providing updated instructions for maintenance and inspection.

Nov 25, 2024
CorrectionMaintenanceSafety Mgmt

EASA SIB CASA-2024-12

Electrical Shock Hazard

The Electrical Shock Hazard Safety Alert CASA 2024-12 is a Transport Canada Civil Aviation safety alert addressing a potential electrocution risk during maintenance of the potable water tank on Bombardier Inc. CL-600-2B16 Challenger 605 aircraft. This alert specifically affects Challenger 605 aircraft with serial numbers ranging from 5752 to 5988. It highlights incidents where maintenance personnel received electric shocks from exposed electrical connections on the baggage compartment heater thermostat.

Nov 22, 2024
Safety Information BulletinMaintenanceSafety MgmtBombardier CL-600 (Challenger)

EASA AD 2024-0221

Exhaust — Engine / Turbocharger Exhaust System / Components — Inspection

EASA Airworthiness Directive 2024-0221 is an airworthiness directive addressing inspection requirements for spot-welded, multi-segment v-band couplings installed at the tailpipe of turbocharger exhaust housing flanges on turbocharged reciprocating engine-powered aircraft. It applies to various aircraft including Piper PA-60 (Aerostar) series, Britten BN2 series, Cirrus SR22 and SR22T, and others listed in the directive's appendix. The directive establishes life limits and inspection protocols for these exhaust system components to ensure continued airworthiness.

Nov 22, 2024
Airworthiness DirectiveMaintenanceSafety Mgmt

EASA AD 2024-0220

Oxygen — Cabin Oxygen Containers — Inspection

The document titled 'Oxygen — Cabin Oxygen Containers — Inspection' is an AIRBUS S.A.S. directive specifically addressing the inspection requirements for cabin oxygen containers installed on the Airbus A350 aircraft. It outlines necessary procedures to ensure the safety and reliability of oxygen supply systems on this aircraft type. The directive aims to maintain compliance with airworthiness standards for the Airbus A350 fleet.

Nov 20, 2024
Safety DirectiveMaintenanceSafety MgmtAirbus A350

EASA AD US-2024-23-06

Rotorcraft Flight Control - Torque Tube Assembly and Roller Bearings - Inspection

The document titled 'Rotorcraft Flight Control - Torque Tube Assembly and Roller Bearings - Inspection' is a regulatory directive addressing the inspection requirements for torque tube assemblies and roller bearings in rotorcraft flight control systems. It focuses on ensuring the integrity and safety of these critical components to maintain flight control reliability. The directive applies specifically to affected rotorcraft models equipped with the specified torque tube assemblies and roller bearings.

Nov 20, 2024
Airworthiness DirectiveMaintenanceSafety MgmtMd Helicopters Inc (Mdhi) 369Md Helicopters Inc (Mdhi) 500NMd Helicopters Inc (Mdhi) 600N

EASA SIB CASA-2024-11

Localizer Tracking Anomaly

Transport Canada Civil Aviation Safety Alert CASA 2024-11 addresses a localizer tracking anomaly affecting MHI RJ Aviation ULC CRJ series aircraft, including CRJ100/200/440, Challenger 850, and CRJ550/700/701/702/705/900/1000 models. The alert highlights an issue where aircraft autopilots fail to complete planned turns to capture the localizer, causing overshoot of the localizer centerline during approaches, which can lead to missed approaches or the need for ATC vectors. This problem is known across all CRJ models and is more prevalent on long runways with narrower localizer beams, especially in urban areas with newer or updated localizer antennas.

Nov 19, 2024
Safety Information BulletinFlight OpsSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)

EASA AD 2024-0217

Fuselage — Double Joggle Area at Frame 16 and Frame 20 — Inspection

EASA Airworthiness Directive 2024-0217 is an airworthiness directive addressing inspection requirements for the fuselage double joggle areas at frame 16 and frame 20 on Airbus A318, A319, A320, and A321 aeroplanes. It applies to various models of these aircraft except those with specific Airbus modifications or service bulletins embodied. The directive mandates special detailed inspections and corrective actions to detect and address cracks that could compromise fuselage structural integrity.

Nov 18, 2024
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321