EASA Regulations & Airworthiness Directives

Browse 5,158 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350222Airbus A330220Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941132Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787115Show all...

EASA AD 2024-0227

Nov 27, 2024

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.

Airworthiness Directive
  • CFM International LEAP-1B

EASA AD 2024-0225

Nov 26, 2024

Engine – Forward Outer Seal, High-Pressure Compressor Stages 6-10 Compressor Rotor Spools and High-Pressure Turbine Rotor Stage 1 Disks – Replacement

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.

Airworthiness DirectiveSuperseded
  • CFM International LEAP-1A
  • CFM International LEAP-1C

EASA AD 2024-0226

Nov 26, 2024

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.

Airworthiness Directive
  • CFM International LEAP-1B

EASA AD US-2024-20-03

Nov 26, 2024

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.

Airworthiness Directive
  • Robinson R22
  • Robinson R44 (Raven)

EASA AD 2024-0224

Nov 26, 2024

Flight Controls – Spoiler Electrical Control Unit – Replacement

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.

Airworthiness DirectiveSuperseded
  • Dassault Falcon 7X

EASA AD 2023-0189R1

Nov 26, 2024

Pneumatic – Trent XWB Engine Bleed Air Supply System T-Duct – Replacement

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.

Airworthiness DirectiveSuperseded
  • Airbus A350

EASA AD 2024-0223

Nov 26, 2024

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.

Airworthiness Directive
  • Airbus Helicopters H160

EASA AD US-2024-19-15

Nov 25, 2024

[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.

Correction

EASA SIB CASA-2024-12

Nov 22, 2024

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.

Safety Information Bulletin
  • Bombardier CL-600 (Challenger)

EASA AD 2024-0221

Nov 22, 2024

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.

Airworthiness Directive

EASA AD 2024-0220

Nov 20, 2024

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.

Safety Directive
  • Airbus A350

EASA AD US-2024-23-06

Nov 20, 2024

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.

Airworthiness Directive
  • Md Helicopters Inc (Mdhi) 369
  • Md Helicopters Inc (Mdhi) 500N
  • Md Helicopters Inc (Mdhi) 600N

EASA SIB CASA-2024-11

Nov 19, 2024

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.

Safety Information Bulletin
  • MHI RJ Aviation CL-600 (Regional Jet)

EASA AD 2024-0217

Nov 18, 2024

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.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0219

Nov 18, 2024

Navigation — VOR/LOC Antenna Coupler — Operational Limitation / Inspection

EASA Airworthiness Directive 2024-0219 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Dassault Aviation Falcon 2000EX aeroplanes with specific serial numbers. It addresses the VOR/LOC antenna coupler installation, which if incorrect, can cause navigation instrument errors during ILS approaches. The directive mandates inspection and operational limitations to ensure flight safety.

Airworthiness Directive
  • Dassault Falcon 2000

EASA AD CF-2024-38

Nov 15, 2024

Flight Controls — Horizontal Stabilizer Trim Actuator (HSTA) — Incomplete Overhaul

Canadian Airworthiness Directive CF-2024-38 addresses an incomplete overhaul issue with the Horizontal Stabilizer Trim Actuator (HSTA) on Bombardier Inc. model BD-100-1A10 aircraft. The directive applies to HSTA part numbers C47100-004 and C47100-005 and requires verification and possible replacement of affected units. This directive aims to ensure continued safe flight by preventing potential failure of HSTA components.

Airworthiness Directive
  • Bombardier BD-100

EASA AD 2024-0216

Nov 15, 2024

Landing Gear – Main Landing Gear Door Actuators – Inspections

EASA Airworthiness Directive 2024-0216 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses issues with certain main landing gear door actuators, specifically those with Part Number 114122015 and listed serial numbers, which may cause jamming or inability to open the landing gear doors during maintenance. The directive mandates inspections and corrective actions to ensure safe operation of the landing gear.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0214

Nov 14, 2024

Time Limits / Maintenance Checks — Safe Life Airworthiness Limitations Items — ALS Part 1 — Amendment

EASA Airworthiness Directive 2024-0214 is an amendment addressing the Airbus A340 series, including models A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642, and A340-643. This directive updates the Safe Life Airworthiness Limitations Items in the Airbus A340 Airworthiness Limitations Section (ALS) Part 1, Revision 13. It mandates compliance with revised maintenance tasks and life limits to ensure continued airworthiness.

Airworthiness Directive
  • Airbus A340

EASA AD 2024-0212

Nov 13, 2024

Rotorcraft Flight Manual — Normal Procedures — Amendment

EASA Airworthiness Directive 2024-0212 is an amendment concerning the Rotorcraft Flight Manual normal procedures for Leonardo S.p.A. AB412 and AB412EP helicopters. The directive addresses a safety issue related to cracked main gearbox support cases reported on similar Bell Textron Inc. Model 412 helicopters. It mandates updates to the flight manual procedures to mitigate the risk of structural failure and loss of helicopter control.

Airworthiness Directive
  • Leonardo S.P.A. Helicopters AB212
  • Leonardo S.P.A. Helicopters AB412