EASA Regulations & Airworthiness Directives

Browse 5,153 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 US-2024-16-07

Sep 19, 2024

Instruments / Navigation - Thrust Management / Displays and Crew Alerting Operational Program Software - Update

The document titled "Instruments / Navigation - Thrust Management / Displays and Crew Alerting Operational Program Software - Update" is a regulatory update concerning the software used in aircraft thrust management, navigation instruments, displays, and crew alerting systems. It addresses operational program software modifications that impact these avionics systems. The document does not specify particular aircraft types or engine models affected.

Other
  • Boeing 787

EASA SIB 2024-13

Sep 17, 2024

GARRECHT AVIONIK GMBH: Loss of Transponder Reply

EASA Safety Information Bulletin 2024-13 addresses the loss of transponder reply issue affecting Garrecht Avionik GmbH Mode-S Secondary Surveillance Radar transponders with specific part numbers including VT-0102, VT-0104, and VT-0201 models. The bulletin highlights detection problems reported by radar manufacturers and air navigation service providers due to an erroneous FPGA microcode firmware implementation. This issue impacts aircraft equipped with these transponders by reducing radar detection reliability under certain interrogation patterns.

Safety Information Bulletin

EASA AD 2024-0180

Sep 17, 2024

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 5 — Fuel Airworthiness Limitations — Amendment

EASA Airworthiness Directive 2024-0180 is an amendment addressing the Airworthiness Limitations Section Part 5 related to fuel airworthiness limitations for Airbus A350-941 and A350-1041 aeroplanes. This directive mandates compliance with new and more restrictive maintenance tasks and life limits as specified in Airbus A350 ALS Part 5 Variation 7.1. It applies to all manufacturer serial numbers of the affected Airbus A350 models.

Airworthiness Directive
  • Airbus A3509411041

EASA AD 2024-0101R1

Sep 13, 2024

Fuel — Engine Low Pressure Shut Off Valve Electrical Harness Routing — Modification

EASA Airworthiness Directive 2024-0101R1 is a regulatory update addressing the electrical harness routing of the engine low pressure shut off valve on Airbus A380-841, A380-842, and A380-861 aeroplanes. It applies to aircraft not modified with Airbus modification 77076 and covers both Engine Alliance GP7200 and Rolls-Royce RB211 Trent 900 engines. The directive aims to ensure compliance with safety requirements related to engine fuel isolation in case of uncontrolled engine rotor failure.

Airworthiness Directive
  • Airbus A380

EASA AD 2024-0179-E

Sep 13, 2024

Power Plant — Engine Mount Bolts — Replacement

EASA Airworthiness Directive 2024-0179-E is an emergency directive addressing the replacement of engine mount bolts on Elixir aeroplanes. It applies to all serial numbers of Elixir aircraft and targets specific engine mount bolts identified by part number PRD-00100696 marked "BUMAX". The directive mandates replacement of these bolts to ensure continued airworthiness and safety.

Airworthiness Directive
  • Elixir Aircraft Elixir
  • Elixir

EASA AD 2024-0177

Sep 13, 2024

Superseded by EASA AD 2026-0039

EASA Airworthiness Directive 2024-0177 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus Helicopters EC 175 B models. It mandates compliance with the updated Airworthiness Limitations Section (ALS) Revision 024 to ensure continued airworthiness of these helicopters. The directive consolidates and supersedes previous ADs related to maintenance tasks and life limits for critical components.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters EC175
  • Airbus Helicopters EC 175 B

EASA AD US-2024-15-05

Sep 12, 2024

Electrical Power - Electrical Support Bracket - Installation / Wire Bundles - Re-installation

Electrical Power - Electrical Support Bracket - Installation / Wire Bundles - Re-installation is a regulatory document addressing the installation and re-installation procedures for electrical support brackets and wire bundles in aircraft electrical power systems. The document aims to ensure proper mounting and secure wiring to maintain electrical system integrity and safety. No specific aircraft types, engine models, or part numbers are mentioned in the document.

Other
  • Boeing 767

EASA AD CF-2024-32

Sep 12, 2024

Electrical System Installation — Frame (FR) 51 Bulkhead Connectors - Inadequate Electrical Bonding

Canadian Airworthiness Directive CF-2024-32 addresses inadequate electrical bonding in the Frame (FR) 51 bulkhead connectors on Airbus Canada Limited Partnership (ACLP) aircraft models BD-500-1A10 and BD-500-1A11 with specified serial numbers. The directive mandates electrical bonding tests and corrective actions to ensure compliance with design limits and protect against electromagnetic interference, high-intensity radiated fields, and lightning strikes. This AD applies specifically to certain BD-500 series aircraft manufactured by ACLP.

Airworthiness Directive
  • Airbus BD-500 (A220 Series)
  • Airbus Canada Limited Partnership BD-500-1A10
  • Airbus Canada Limited Partnership BD-500-1A11

EASA AD 2024-0178

Sep 12, 2024

Engine — Intermediate Pressure Compressor Shaft Assembly / Front Air Seal — Inspection

EASA Airworthiness Directive 2024-0178 is an airworthiness directive addressing the inspection of the intermediate pressure compressor (IPC) shaft assembly front air seal on Rolls-Royce Trent 1000 and Trent 7000 engines. These engines are commonly installed on Boeing 787 and Airbus A330 aircraft. The directive mandates repetitive inspections to detect cracks that could lead to engine failure and potential safety risks.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT 7000
  • Boeing 787
  • Airbus A330

EASA AD 2024-0176

Sep 11, 2024

Superseded by EASA AD 2024-0192

EASA Airworthiness Directive 2024-0176 is issued for Fokker F28 Mark 0070 and Mark 0100 aeroplanes equipped with Collins Aerospace main landing gear pistons having specific part numbers. The directive addresses a crack found in the main landing gear piston modified by an Australian landing gear shop, which could lead to structural failure and landing gear collapse. It mandates inspections and replacement of affected parts to ensure continued airworthiness.

Airworthiness DirectiveSuperseded
  • Fokker F28
  • Fokker F28 Mark 0070
  • Fokker F28 Mark 0100

EASA SIB 2024-12

Sep 10, 2024

Use of Balloon Pilot Restraint Systems

EASA Safety Information Bulletin 2024-12 addresses the use of pilot restraint systems in hot air balloons. It highlights safety concerns related to hard landings where pilots may be lifted or lose balance, increasing the risk of falling out of the basket. The bulletin applies specifically to hot air balloons and recommends the installation and use of approved pilot restraint systems, including for training balloons with both instructor and student restraints.

Safety Information BulletinSuperseded

EASA AD 2024-0174-E

Sep 5, 2024

Superseded by EASA AD 2024-0182R1

EASA Airworthiness Directive 2024-0174-E is an emergency directive addressing Rolls-Royce Trent XWB-97 engines installed on Airbus A350-1041 aircraft. It mandates a one-time inspection of specific main fuel manifold hoses to detect damage that could lead to engine fire. The directive applies to all Trent XWB-97 engines except those with certain serial numbers listed in the document.

Airworthiness DirectiveSuperseded
  • Rolls-Royce Deutschland Ltd & Co Kg TRENT XWB
  • Airbus A350-1041

EASA SIB BEA-2024-05

Sep 4, 2024

Indicating/Recording Systems: Load 7.5 version for PRIMUS EPIC field-loadable software system

BEA 2024-05 is a Special Airworthiness Bulletin addressing the PRIMUS EPIC field-loadable software system Load 7.5 version for EMBRAER S.A. ERJ 190-300 and ERJ 190-400 airplanes. It informs the civil aviation community about improvements and fixes in this software version, including safety-related corrections. The bulletin is informative and does not impose mandatory requirements or an Airworthiness Directive under RBAC 39 at this time.

Safety Information Bulletin
  • Embraer ERJ 190

EASA SIB BEA-2024-04

Sep 4, 2024

Pneumatic: New software for Pneumatic System Controller (PSC)

BEA 2024-04 is a Special Airworthiness Bulletin addressing a software update for the Pneumatic System Controller (PSC) on EMBRAER S.A. EMB-545 and EMB-550 airplanes. The bulletin informs about a potential dual bleed failure and cabin depressurization issue related to the PSC software. It provides guidance to prevent this failure without imposing mandatory requirements.

Safety Information Bulletin
  • Embraer EMB-545
  • Embraer EMB-550

EASA AD 2024-0173

Sep 4, 2024

Superseded by EASA AD 2026-0011

EASA Airworthiness Directive 2024-0173 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters EC 155 B and EC 155 B1 models. It addresses the modification of jettisonable windows and seals on the sliding doors and fixed panels to ensure proper emergency egress capability. This directive mandates specific modifications to improve safety during emergency evacuations.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA
  • Airbus Helicopters AS 365
  • Airbus Helicopters EC 155
  • Airbus Helicopters EC 155 B
  • Airbus Helicopters EC 155 B1

EASA AD CF-2024-30

Sep 4, 2024

Superseded by TCCA AD CF-2025-12

Canadian Airworthiness Directive CF-2024-30 is issued for Airbus Canada Limited Partnership BD-500-1A10 and BD-500-1A11 aircraft equipped with Pratt & Whitney PW1500G engines. It addresses a software protection logic issue related to large leaks in the engine bleed duct that could lead to dual engine failure. The directive mandates updates to the Airplane Flight Manual (AFM) non-normal procedures to include manual isolation of the opposite engine in such events.

Airworthiness Directive
  • Airbus BD-500 (A220 Series)
  • Airbus Canada BD-500-1A10
  • Airbus Canada BD-500-1A11

EASA SIB 2024-11

Sep 3, 2024

Continuing Airworthiness of Aerazur AIR 12 A (M2) Towing Hook

EASA Safety Information Bulletin 2024-11 is an airworthiness bulletin addressing the continuing airworthiness of the Aerazur AIR 12 A (M2) towing hook, part number 55509-B. This towing hook is installed on various aeroplanes including DAHER AEROSPACE MS 890 and Rallye 235 series, CEAPR HR 100, R 1180 T/TD, and DR 200/300/400 series aircraft. The bulletin provides information on a towing accident caused by a defective towing hook and highlights inspection and maintenance recommendations.

Safety Information BulletinSuperseded

EASA AD 2020-0104R1-CN

Aug 30, 2024

CANCELLED: Oxygen — Oxygen Supply Solenoid Valve — Inspection / Replacement

EASA Airworthiness Directive Cancellation Notice 2020-0104R1-CN cancels the previous AD 2020-0104R1 concerning the inspection and replacement of oxygen supply solenoid valves on Airbus A318, A319, A320, and A321 aircraft. The affected parts are specific solenoid valves with part numbers DVE90-06 or DVE90-07 manufactured up to 2016. This cancellation applies to all manufacturer serial numbers of these aircraft models.

Agency Decision
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA SIB 2023-08R1

Aug 30, 2024

Reporting of Occurrences Involving Human Interventions Linked to Flight Deck Design, Operating Procedures, Training, or a Combination Thereof

EASA Safety Information Bulletin 2023-08R1 is a revision of the previous SIB 2023-08 and addresses the reporting of occurrences involving human interventions related to flight deck design, operating procedures, training, or combinations thereof. It applies specifically to commercial air transport operators of large aeroplanes certified under CS 25, JAR 25, or FAR 25 standards. The bulletin provides guidance on mandatory and recommended reporting of safety-relevant events detected during flight operations and simulator training to the design approval holder to support safety analysis.

Safety Information Bulletin