EASA Regulations &amp; Airworthiness Directives

Superseded by EASA AD 2025-0122

EASA Airworthiness Directive 2024-0033 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 mandates compliance with updated airworthiness limitations specified in the Dassault Falcon 7X Aircraft Maintenance Manual, Airworthiness Limitations Section, Revision 12. This directive ensures continued airworthiness by enforcing maintenance tasks and life limits for components.

Dassault Falcon 7X

EASA AD 2024-0034

Superseded by EASA AD 2025-0290

EASA Airworthiness Directive SUPERSEDED BY EASA AD 2025-0290 is a regulatory document related to the Dassault Aviation Falcon 900EX aircraft. The directive has been superseded by a newer airworthiness directive numbered 2025-0290. No further technical details or specific requirements are available due to the document content extraction failure.

Dassault Falcon 900EX

EASA AD 2024-0035

Superseded by EASA AD 2025-0291

EASA Airworthiness Directive 2024-0035 is issued for Dassault Aviation Falcon 900EX aeroplanes, serial numbers 1 to 119 except 97. This directive mandates compliance with updated airworthiness limitations specified in the Dassault Falcon 900EX Aircraft Maintenance Manual, Chapter 5-40, Airworthiness Limitations Section, Revision 19. It ensures continued airworthiness by enforcing maintenance tasks and life limits on components.

Dassault Falcon 900EX

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Superseded by EASA AD 2025-0292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.

Dassault MystÃ¨re-Falcon 900
Dassault Aviation Mystère-Falcon 900

EASA AD 2024-0029

Jan 29, 2024

Engine Oil — Lubrication / Scavenge Oil Pumps — Installation Criteria

The document titled 'Engine Oil — Lubrication / Scavenge Oil Pumps — Installation Criteria' issued by ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG pertains to the installation requirements for lubrication and scavenge oil pumps on the Trent 7000 engine model. It provides specific criteria to ensure proper installation and functioning of these critical engine components. This document is relevant for operators and maintenance organizations working with aircraft powered by the Trent 7000 engine.

OtherSuperseded

Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000

EASA AD CF-2024-03

Jan 26, 2024

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.

Bell 505 (Jet Ranger X)
Bell Textron Canada Limited 505

EASA AD BR-2023-07-01

Jan 25, 2024

[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.

Embraer EMB-505 (Phenom 300)
Embraer EMB-505

EASA AD 2024-0027

Jan 25, 2024

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.

Airbus A319
Airbus A320
Airbus A321

EASA AD 2024-0026

Jan 24, 2024

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.

CFM International LEAP-1A
CFM International LEAP-1C
Airbus A319
Airbus A320
Airbus A321

EASA AD 2024-0025

Jan 24, 2024

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.

ATR ATR42
ATR ATR72
ATR 42
ATR 72

EASA AD 2024-0024

Jan 24, 2024

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.

AgustaWestland AW 189
Pilatus PC-21
Cessna 550

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.

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.

Safety Information Bulletin

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.

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.

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.

Airbus A340541542642643

EASA AD 2024-0021

Jan 17, 2024

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.