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EASA Regulations & Airworthiness Directives

Browse 218 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320286 Airbus A321285 Airbus A319253 Airbus A350222 Airbus A330220 Airbus A318189 Airbus A380182 Boeing 737175 Airbus A340141 Airbus A350-941132 Airbus BD-500 (A220 Series)123 Airbus Helicopters AS 332119 Airbus Helicopters EC 225116 Airbus Helicopters SA 330116 Boeing 787114 Show all...

Filtered by: Airbus A350Clear filter

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

Superseded by EASA AD 2025-0244

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 Directive

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 DirectiveSuperseded

Airbus A350

EASA AD 2025-0150

Landing Gear — Main Landing Gear Brake Rod Centre Pin and Nut — Inspection

EASA Airworthiness Directive 2025-0150 is an airworthiness directive addressing the inspection of the main landing gear brake rod centre pin and nut sub-assemblies on Airbus A350-941 aeroplanes with specific manufacturer serial numbers. The directive mandates inspections to detect corrosion and potential detachment risks of these parts, which could affect the extension of the main landing gear. It applies to multiple groups of affected aircraft and references Airbus Alert Operators Transmission A32P034-24 Revision 01 for inspection procedures.

Airworthiness Directive

Airbus A350

EASA AD 2025-0138

Oxygen — Chemical Oxygen Generators — Replacement

EASA Airworthiness Directive 2025-0138 is an airworthiness directive issued by EASA affecting Airbus A350-941 and A350-1041 aeroplanes. It addresses the replacement of certain chemical oxygen generators installed in these aircraft due to issues with the clamp holding the oxygen generator in place. The directive applies to all manufacturer serial numbers of the specified Airbus A350 models.

Airworthiness Directive

Airbus A350

EASA AD 2025-0129

Superseded by EASA AD 2025-0197

EASA Airworthiness Directive 2025-0129 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes. It addresses the replacement of Flight Control Remote Modules (FCRM) that have been exposed to hydraulic fluid contamination, which could lead to loss of control of flight control surfaces such as rudder and elevator. The directive applies to all manufacturer serial numbers of these aircraft models and references Airbus Alert Operators Transmission A27P021-25.

Airworthiness DirectiveSuperseded

Airbus A350

EASA AD 2025-0089

[Correction] Equipment / Furnishings — Forward of Door 4 Galleys Lower Attachment Studs — Inspection / Replacement

[Correction] Equipment / Furnishings — Forward of Door 4 Galleys Lower Attachment Studs — Inspection / Replacement is a document concerning the Airbus A350 aircraft. It addresses inspection and replacement procedures for the lower attachment studs located forward of Door 4 galleys. The document aims to ensure continued airworthiness and safety of these specific equipment components on the Airbus A350.

Airbus A350

EASA AD 2025-0120

Cabin Systems — Antenna Adapter Plate — Inspection

EASA Airworthiness Directive 2025-0120 is an airworthiness directive addressing inspection requirements for the antenna adapter plate and related parts installed on Airbus A319, A320, A321, A330, A350, and A380 aircraft models. The directive mandates repetitive general visual inspections of affected broadband antenna adapter plates to detect corrosion and cracks that could compromise aircraft safety. It applies to all manufacturer serial numbers of the specified Airbus models.

Airworthiness Directive

Airbus A319
Airbus A320
Airbus A321
Airbus A330
Airbus A350
Airbus A380

EASA AD 2025-0117

Fuselage — Bracket Supporting Flap Shaft Catcher — Inspection

EASA Airworthiness Directive 2025-0117 is an airworthiness directive addressing the Airbus A350-1041 aeroplanes with specific manufacturer serial numbers. It mandates inspection of the fuselage bracket supporting the flap shaft catcher to detect incorrect installation that could cause misalignment and potential flap surface detachment. The directive applies to affected left-hand and right-hand side brackets identified by part numbers V5393528020000 and V5393528020100.

Airworthiness Directive

Airbus A350