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EASA Regulations for Airbus A350

224 airworthiness directives and regulations affecting Airbus A350.

EASA AD 2026-0018

Wings — Main Landing Gear Trunnion Block Fuse Pins and Retaining Pins — Inspection

EASA Airworthiness Directive 2026-0018 is an official directive addressing Airbus A350-941 aeroplanes with specific manufacturer serial numbers. It mandates inspection of the main landing gear trunnion block fuse pins and retaining pins due to a serialization non-conformity issue. The directive ensures the traceability and continued airworthiness of these critical landing gear components.

Airworthiness Directive

Airbus A350

EASA PAD 26-009

Landing Gear — Main Landing Gear Bogie Pivot Pin and Bushes — Inspection

EASA Airworthiness Directive 26-009 is a proposed directive addressing the inspection of main landing gear bogie pivot pins and bushes on Airbus A350-941 aeroplanes. It mandates repetitive detailed inspections to detect damage caused by frictional heating and potential cracking. The directive applies to all manufacturer serial numbers of the Airbus A350-941 and aims to prevent main landing gear collapse.

Airbus A350

EASA AD 2025-0247R1

Fuselage — Forward and Aft Cargo Door Piano Hinges — Inspection

EASA Airworthiness Directive 2025-0247R1 is an updated regulatory requirement for Airbus A350-941 and A350-1041 aeroplanes concerning the inspection of forward and aft cargo door piano hinges. This directive mandates repetitive inspections of specific piano hinges and related structures to detect cracks, damage, or sheared fasteners that could compromise the structural integrity of the aircraft fuselage. The directive applies to all manufacturer serial numbers of the affected Airbus A350 models.

Airworthiness Directive

Airbus A350

EASA AD 2025-0272

Airborne Auxiliary Power — Air Intake Flap Hinge — Inspection; Master Minimum Equipment List — Amendment

EASA Airworthiness Directive 2025-0272 is issued for Airbus A350-941 and A350-1041 aeroplanes addressing inspection requirements for the Auxiliary Power Unit (APU) air intake flap hinge. The directive also mandates an amendment to the Airbus A350 Master Minimum Equipment List (MMEL) to mitigate risks associated with APU air intake flap detachment. This AD applies to affected APU air intake assemblies with specific part numbers installed on these aircraft.

Airworthiness Directive

Airbus A350

EASA AD 2021-0291R2

Doors — Passenger Door Stop Screw — Inspection

EASA Airworthiness Directive 2021-0291R2 is an updated safety directive addressing inspection requirements for passenger door stop screws on Airbus A350-941 and A350-1041 aeroplanes. It mandates repetitive general visual inspections of the door stop screws to detect missing or damaged screw heads, which could compromise the aircraft's structural integrity. The directive applies to all serial numbers except those with specific Airbus modifications that optimize the door stop screw design.

Airworthiness Directive

Airbus A350

EASA AD 2025-0259

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

EASA Airworthiness Directive 2025-0259 is issued for Airbus A350-941 and A350-1041 aeroplanes equipped with any Trent XWB engines, focusing on the replacement of the Trent XWB Engine Bleed Air Supply System T-Duct with part number RR03-11011-001. This directive addresses a potential unsafe condition caused by manufacturing non-conformance that may lead to cracking and air leakage in the T-Duct, risking uncontained engine failure or uncontrolled engine fire. The AD mandates replacement of affected parts and restricts installation of certain parts on specific engine models.

Airworthiness Directive

Airbus A350

EASA AD 2025-0238

[Correction] Electrical Power — Ram Air Turbine — Replacement

EASA Airworthiness Directive 2025-0238 is a corrective directive addressing the replacement of the Ram Air Turbine (RAT) module on Airbus A350-941 and A350-1041 aeroplanes. It targets RAT modules identified by Part Number 1713586A that have been deployed and retracted in flight, due to corrosion issues affecting electrical power generation. This directive applies to all manufacturer serial numbers of the specified Airbus A350 models.

Airworthiness Directive

Airbus A350

EASA AD 2025-0244

Doors — Passenger / Crew Door Girt Bar Fitting Assemblies — Inspection

The document titled 'Doors — Passenger / Crew Door Girt Bar Fitting Assemblies — Inspection' is an airworthiness directive applicable to AIRBUS S.A.S. A350 aircraft. It addresses the inspection requirements for the passenger and crew door girt bar fitting assemblies to ensure their continued airworthiness and safety. The directive provides guidance on inspection procedures specific to these door components on the Airbus A350 model.

Airworthiness Directive

Airbus A350

EASA AD 2025-0197R1

Flight Controls — Primary Flight Control System — Modification

EASA Airworthiness Directive 2025-0197R1 is a regulatory update addressing the primary flight control system modification for Airbus A350-941 and A350-1041 aeroplanes. It focuses on the replacement and modification of Rudder and Elevator Flight Control Remote Modules (FCRMs) contaminated by hydraulic fluid and mandates the installation of updated Flight Control and Guidance System software standards. This directive ensures continued airworthiness by mitigating risks of flight control surface runaway due to hydraulic contamination.

Airworthiness Directive

Airbus A350

EASA AD 2025-0209

Wings — Centre Wing Box and Belly Fairing Fasteners — Modification

EASA Airworthiness Directive 2025-0209 is an airworthiness directive applicable to Airbus A350-941 aeroplanes with manufacturer serial numbers 0005 through 0047. It addresses issues related to the centre wing box and belly fairing fasteners, specifically those fasteners with Part Number EN6115 code B. The directive mandates modifications to ensure structural integrity and compliance with safety standards.

Airworthiness Directive

Airbus A350

EASA AD 2025-0210

Wings — Centre Wing Box Fasteners — Replacement

EASA Airworthiness Directive 2025-0210 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes with specific manufacturer serial numbers. The directive addresses the replacement of centre wing box fasteners and the application of additional head nut cap protection to ensure continued airworthiness.

Airworthiness Directive

Airbus A350

EASA AD 2025-0203

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 4 — System Equipment Maintenance Requirements — Amendment

EASA Airworthiness Directive 2025-0203 is an amendment addressing the Airbus A350-941 and A350-1041 aeroplanes. It updates the Airworthiness Limitations Section Part 4 related to System Equipment Maintenance Requirements to ensure continued airworthiness. This directive applies to all manufacturer serial numbers of the affected Airbus A350 models.

Airworthiness Directive

Airbus A350

EASA AD 2025-0204

Time Limits / Maintenance Checks — Damage Tolerant Airworthiness Limitation Items — ALS Part 2 — Amendment

EASA Airworthiness Directive 2025-0204 is an amendment addressing the Airbus A350-941 and A350-1041 aeroplanes. It updates the Damage Tolerant Airworthiness Limitation Items in the Airbus A350 Airworthiness Limitations Section (ALS) Part 2, Revision 11, to ensure continued airworthiness through revised maintenance tasks and intervals. This directive applies to all manufacturer serial numbers of the specified Airbus A350 models.

Airworthiness Directive

Airbus A350

EASA AD 2025-0192

Doors – Passenger / Crew Door Girt Bar Fitting Assemblies – Inspection

EASA Airworthiness Directive 2025-0192 is issued for Airbus A350-941 and A350-1041 aeroplanes, addressing a safety issue with passenger and crew door girt bar fitting assemblies. The directive mandates inspection and corrective actions to ensure proper function of the girt bar fittings, which are critical for emergency door slide deployment. This AD applies to all manufacturer serial numbers of the specified Airbus A350 models.

Airworthiness DirectiveSuperseded

Airbus A350

EASA AD 2025-0183

Engine Fuel and Control — Hydro-Mechanical Unit — Replacement / Life Limitation

The document titled 'Engine Fuel and Control — Hydro-Mechanical Unit — Replacement / Life Limitation' applies to the AIRBUS S.A.S. A350 aircraft. It addresses requirements related to the replacement and life limitation of the hydro-mechanical unit within the engine fuel and control system. This ensures continued airworthiness and safe operation of the affected aircraft.

Airworthiness Directive

Airbus A350

EASA AD 2024-0058R2-CN

CANCELLED: Pneumatic — Precooler Exchanger — Inspection

EASA Airworthiness Directive Cancellation Notice 2024-0058R2-CN cancels the previous directive 2024-0058R2 concerning the inspection of the pneumatic precooler exchanger on Airbus A350-941 and A350-1041 aeroplanes. The affected part is the pre-cooler exchanger with Part Number 67200000-02. This cancellation follows further investigation that confirmed the safety risk initially addressed is no longer considered an unsafe condition.

Airworthiness Directive

Airbus A350

EASA AD 2025-0181

Integrated Modular Avionics — Core Processing Input and Output Module — Replacement

EASA Airworthiness Directive 2025-0181 is an airworthiness directive addressing Airbus A350-941 and A350-1041 aeroplanes. It mandates the replacement of certain Core Processing Input and Output Modules J (CPIOM-J) due to a manufacturing quality issue identified by the part manufacturer, Thales. The directive applies to specific serial numbers of CPIOM-J parts installed on these aircraft.

Airworthiness Directive

Airbus A350

EASA AD 2025-0180

Equipment / Furnishings — Slide Upper Latches — Inspection

The document titled Equipment / Furnishings — Slide Upper Latches — Inspection is an airworthiness directive applicable to AIRBUS S.A.S. A350 aircraft. It addresses the inspection requirements for the upper latches of evacuation slides installed on these aircraft to ensure their proper function and safety.

Airworthiness Directive

Airbus A350

EASA AD 2025-0152

Flight Controls — Primary Flight Control Actuators — Replacement

EASA Airworthiness Directive 2025-0152 is an airworthiness directive addressing Airbus A350-941 and A350-1041 aeroplanes. It mandates the replacement of certain primary flight control actuators, including servo controls, electrical backup hydraulic actuators (EBHA), and electro-hydrostatic actuators (EHA), that were exposed to mechanical overloads during production. The directive aims to ensure continued safe operation of these aircraft by removing affected parts from service.

Airworthiness Directive

Airbus A350

EASA AD 2025-0139

Hydraulic Power — Engine Driven Pump — Software Update / Modification; Aircraft Flight Manual — Abnormal and Emergency Procedures — Amendment

EASA Airworthiness Directive 2025-0139 is an update applicable to Airbus A350-941 and A350-1041 aeroplanes, excluding those with Airbus modification 116830 embodied in production. It addresses hydraulic engine driven pump failures by requiring software updates to the hydraulic monitoring and control application and amendments to the Aircraft Flight Manual's abnormal and emergency procedures. This directive ensures continued airworthiness and safety compliance for affected Airbus A350 models.

Airworthiness Directive

Airbus A350