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 2024-0023

Jan 23, 2024

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.

Airworthiness Directive
  • Airbus A330

EASA AD 2024-0022

Jan 23, 2024

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.

Other
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD CF-2024-02

Jan 23, 2024

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.

Airworthiness Directive
  • Diamond Aircraft Industries DA 62
  • Diamond Aircraft Industries Inc. DA 62

EASA SIB SAFO24001

Jan 22, 2024

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.

Safety Information Bulletin
  • Boeing 737

EASA SIB 2024-02

Jan 22, 2024

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.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD US-2024-02-51

Jan 19, 2024

[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.

Regulation
  • Boeing 7379

EASA AD BR-2023-01-01R1

Jan 18, 2024

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.

Airworthiness Directive
  • Embraer ERJ 190
  • Embraer ERJ190-300
  • Embraer ERJ190-400

EASA AD 2024-0020

Jan 17, 2024

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.

Airworthiness Directive
  • Airbus A340541542642643

EASA AD 2024-0021

Jan 17, 2024

Wings – Ailerons – Inspection

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.

Airworthiness DirectiveSuperseded
  • Dassault Falcon 7X
  • Dassault Falcon 8X

EASA AD CF-2024-01

Jan 12, 2024

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.

Airworthiness Directive
  • De Havilland Canada DHC-8
  • De Havilland DHC-8-401
  • De Havilland DHC-8-402

EASA AD 2024-0017

Jan 11, 2024

Aircraft Flight Manual — Amendment

EASA Airworthiness Directive 2024-0017 is an amendment concerning the Aircraft Flight Manual for Zakłady Lotnicze Margański & Mysłowski S.A. MDM-1 “Fox” and MDM-1P “Fox-P” sailplanes. It addresses safety issues related to spin recovery procedures during aerobatic flights. The directive applies to all serial numbers of these sailplanes.

Airworthiness Directive
  • Secint Air Support Poland Sp. Z.O.O. MDM-1 Fox
  • Zakłady Lotnicze Margański & Mysłowski S.A. MDM-1 Fox
  • Zakłady Lotnicze Margański & Mysłowski S.A. MDM-1P Fox-P

EASA AD 2024-0016

Jan 11, 2024

Flight Controls – Trimmable Horizontal Stabilizer Actuator / Electric Load Sensing Device – Modification

EASA Airworthiness Directive 2024-0016 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330 and A340 aeroplanes. It addresses modifications to the Trimmable Horizontal Stabilizer Actuator (THSA) and the installation of an Electric Load Sensing Device (ELSD) to improve safety monitoring of the actuator's secondary load path. This directive applies to various Airbus A330 and A340 models with specific manufacturer serial numbers.

Airworthiness DirectiveSuperseded
  • Airbus A330
  • Airbus A340

EASA AD 2024-0018

Jan 11, 2024

Indicating / Recording Systems — Control Unit — Inspection

EASA Airworthiness Directive 2024-0018 is an airworthiness directive addressing inspection and modification requirements for the control units of Airbus Helicopters AS 350 B2/B3, EC 130 B4, and EC 120 B models. It mandates inspection, cleaning, and corrective actions for affected control units to prevent short circuits that could impair multiple systems including the Emergency Floatation System (EFS). This directive applies to all serial numbers of the specified helicopter models.

Airworthiness Directive
  • Airbus Helicopters AS 350
  • Airbus Helicopters EC 130
  • Airbus Helicopters EC 120 B
  • Airbus Helicopters AS 350 B2
  • Airbus Helicopters AS 350 B3
  • Airbus Helicopters EC 130 B4

EASA AD 2024-0019

Jan 11, 2024

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

EASA Airworthiness Directive 2024-0019 is an amendment addressing the time limits and maintenance checks for SAFRAN Helicopter Engines RTM 322-01/9 and RTM 322-01/9A models, commonly installed on NH Industries NH90 military helicopters. This directive mandates compliance with updated Airworthiness Limitations Sections (ALS) in the engine maintenance manuals to ensure continued airworthiness. It applies to all serial numbers of these engine models and requires operators to follow revised maintenance tasks and life limits.

Airworthiness DirectiveSuperseded
  • Safran RTM 322
  • NH Industries NH90

EASA AD US-2023-25-10

Jan 10, 2024

Equipment / Furnishings - Seat Track Fitting Nuts - Re-torque

The Federal Aviation Administration Airworthiness Directive 2023-25-10 is a final rule addressing certain Boeing 787-8, 787-9, and 787-10 airplanes. It mandates re-torquing of the free-standing flight attendant seat track fitting nuts due to a quality issue where these nuts were found under-torqued during production. This directive aims to ensure the structural integrity of flight attendant seats to prevent safety hazards.

Airworthiness Directive
  • Boeing 7878910

EASA AD US-2024-01-02

Jan 10, 2024

Fuselage - Aft Fuselage Sloping Longerons - Records Review / Inspection

The Federal Aviation Administration's Airworthiness Directive 2024-01-02 addresses Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 382 series and C-130 series airplanes. This directive concerns aft fuselage sloping longerons that may have been exposed to excessive heat during manufacturing, potentially reducing their mechanical strength and compromising structural integrity. The AD applies to specific part numbers and requires inspections and records reviews to ensure airworthiness.

Airworthiness Directive
  • Lockheed Martin Corporation 382 (Hercules)
  • Lockheed Martin 382
  • Lockheed Martin C-130

EASA AD 2024-0013

Jan 10, 2024

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

EASA Airworthiness Directive 2024-0013 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642, and A340-643 aeroplanes. It mandates compliance with updated safe life airworthiness limitations as specified in Airbus A340 Airworthiness Limitations Section Part 1 Revision 12. This directive ensures the continued airworthiness of these aircraft by enforcing maintenance and replacement tasks based on the latest approved limitations.

Airworthiness DirectiveSuperseded
  • Airbus A340211212213311312313541542642643

EASA AD 2024-0014

Jan 10, 2024

Time Limits / Maintenance Checks – System Equipment Maintenance Requirements – ALS Part 4 – Amendment

EASA Airworthiness Directive 2024-0014 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A330 aeroplane models including A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343, A330-841, and A330-941. This directive mandates compliance with updated system equipment maintenance requirements as specified in Airbus A330 Airworthiness Limitations Section Part 4 Revision 9. It ensures continued airworthiness by requiring operators to follow new or more restrictive maintenance tasks and life limits for components.

Airworthiness DirectiveSuperseded
  • Airbus A330201202203223223F243243F301302303321322323341342343841941