EASA Regulations & Airworthiness Directives

Browse 130 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 787114Show all...
Filtered by: Airbus A350-941Clear filter

EASA PAD 26-122

Oct 9, 2026

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

EASA Airworthiness Directive 26-122 is a proposed amendment affecting Airbus A350-941 and A350-1041 aeroplanes. It updates the Damage Tolerant Airworthiness Limitation Items in the Airbus A350 Airworthiness Limitations Section Part 2, Revision 12, introducing new and more restrictive maintenance tasks. This directive ensures continued airworthiness by mandating compliance with updated maintenance requirements.

Proposed AD
  • Airbus A3501041941

EASA PAD 26-120

Oct 6, 2026

Electrical Power – Emergency Electrical Network Management Unit – Modification / Re-Identification

EASA Airworthiness Directive PAD No. 26-120 is a proposed directive addressing the Emergency Electrical Network Management Unit (EENMU) on Airbus A350-941 and A350-1041 aeroplanes. It targets specific EENMU part numbers that may have incorrect firmware logic affecting the electrical power distribution system. The directive applies to all manufacturer serial numbers except those with Airbus modification 120968 incorporated during production.

Proposed AD
  • Airbus A3501041941

EASA PAD 26-110

Sep 18, 2026

Stabilizers – Trimmable Horizontal Stabilizer Centre Joint Pivot Fitting – Inspections

EASA Airworthiness Directive Proposal PAD No. 26-110 addresses inspections of the trimmable horizontal stabilizer centre joint pivot fitting on Airbus A350-941 and A350-1041 aeroplanes. The directive targets potential structural integrity issues in the horizontal tail plane rear support fitting joint due to cracked sealant, rotated fasteners, and migrated bushes. It applies to all manufacturer serial numbers of these Airbus A350 models.

Proposed AD
  • Airbus A3509411041

EASA AD 2026-0177

Sep 14, 2026

Indicating / Recording Systems – Integrated Control Panels – Inspection

EASA Airworthiness Directive 2026-0177 is an airworthiness directive addressing Airbus A350-941 and A350-1041 aeroplanes equipped with Fire Integrated Control Panels (ICP) Part Number 727-7206-03. The directive mandates inspection of these integrated control panels to detect potential internal damage that could cause an in-flight engine shutdown. It applies to all manufacturer serial numbers of the affected aircraft models.

Airworthiness Directive
  • Airbus A3509411041

EASA AD 2026-0163

Aug 12, 2026

Navigation – GLU-2100 Global Navigation Satellite System Clock Oscillator – Operational Limitation

EASA Airworthiness Directive 2026-0163 is an operational limitation directive affecting Airbus A350-941 and A350-1041 aeroplanes. It addresses issues with the GLU-2100 Global Navigation Satellite System Clock Oscillator, specifically certain units with untested oscillators that may cause erroneous position information. The directive prohibits operation and installation of affected GLU-2100 units unless modified according to Collins Aerospace instructions.

Airworthiness Directive
  • Airbus A3509411041

EASA PAD 26-087

Jul 21, 2026

Indicating / Recording Systems – Integrated Control Panels – Inspection

EASA Airworthiness Directive PAD No. 26-087 is a proposed directive addressing inspection requirements for fire integrated control panels (ICP) on Airbus A350-941 and A350-1041 aeroplanes. The directive focuses on the ICP Functional Item Number 245VM with Part Number 727-7206-03, which may suffer internal damage leading to in-flight engine shutdown. This directive applies to all manufacturer serial numbers of the affected aircraft models.

Proposed AD
  • Airbus A3509411041

EASA PAD 26-085

Jul 15, 2026

Navigation – GLU-2100 Global Navigation Satellite System Clock Oscillator – Operational Limitation

EASA Airworthiness Directive PAD No. 26-085 is a proposed directive addressing an operational limitation for the GLU-2100 Global Navigation Satellite System Clock Oscillator installed on Airbus A350-941 and A350-1041 aeroplanes. It identifies certain affected GLU-2100 units with specific part and serial numbers that may cause erroneous aircraft position information without warning. The directive applies to all manufacturer serial numbers of these aircraft models.

Proposed AD
  • Airbus A3509411041

EASA AD 2026-0122

Jun 26, 2026

Flight Controls – Droop Nose Geared Rotary Actuator Ring – Inspection / Replacement

EASA Airworthiness Directive 2026-0122 is an airworthiness directive applicable to Airbus A350-941 and A350-1041 aeroplanes. It addresses inspection and replacement requirements for the droop nose geared rotary actuator ring, specifically part number 4776A0000-03, due to identified corrosion issues. The directive mandates inspection and corrective actions to ensure continued safe operation of the affected flight control components.

Airworthiness Directive
  • Airbus A3509411041

EASA AD 2023-0176R1

Mar 6, 2026

Fuselage — Cargo Compartment Panels Sealing Tape — Inspection

EASA Airworthiness Directive 2023-0176R1 is a regulatory update addressing inspection requirements for sealing tape on cargo compartment panels of Airbus A350-941 and A350-1041 aeroplanes, excluding those with Airbus modification 120495. It mandates repetitive detailed inspections of sealing tapes installed in both longitudinal and transversal directions in cargo compartments to ensure fire extinguishing system effectiveness. The directive applies to all manufacturer serial numbers except those modified in production.

Airworthiness Directive
  • Airbus A3509411041

EASA AD 2024-0189

Oct 1, 2024

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 1 — Safe Life Airworthiness Limitations Items — Amendment

EASA Airworthiness Directive 2024-0189 is an amendment addressing the Safe Life Airworthiness Limitations Items for Airbus A350-941 and A350-1041 aeroplanes. It updates the Airbus A350 Airworthiness Limitations Section Part 1 to Revision 08, Issue 2, ensuring mandatory compliance with new and more restrictive maintenance limits. This directive applies to all manufacturer serial numbers of the affected Airbus A350 models.

Airworthiness Directive
  • Airbus A3509411041

EASA AD 2024-0188

Sep 27, 2024

Landing Gear – Nose Landing Gear Shock Absorber – Functional Check

EASA Airworthiness Directive 2024-0188 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes. It addresses potential mechanical noise and structural issues related to the nose landing gear shock absorber, specifically parts with Part Numbers 6406Axxxx and 4816Axxxx. The directive mandates repetitive functional steering checks to detect and correct increased friction and possible corrosion that could lead to nose landing gear failure.

Airworthiness DirectiveSuperseded
  • Airbus A3509411041

EASA AD 2024-0186

Sep 24, 2024

Oxygen — Crew Oxygen Cylinder Assembly — Inspection / Replacement

EASA Airworthiness Directive 2024-0186 is an airworthiness directive addressing oxygen crew cylinder assemblies on Airbus A350-941 and A350-1041 aeroplanes. It mandates inspection and replacement of specific oxygen cylinder assemblies with part numbers 4441227-058-000 and 4441227-058-001 due to a design defect causing loss of retention of the regulator inlet filter retainer. The directive applies to all manufacturer serial numbers of these aircraft models.

Airworthiness Directive
  • Airbus A3509411041

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 2024-0161

Aug 19, 2024

Wings — Centre Wing Box Fasteners — Replacement

EASA Airworthiness Directive 2024-0161 is issued for Airbus A350-941 and A350-1041 aeroplanes with specific manufacturer serial numbers. It mandates the replacement of centre wing box fasteners and the application of additional head nut cap protection at the front and rear spar areas. This directive ensures continued airworthiness by addressing a potential unsafe condition related to fastener rotation and clamping loss.

Airworthiness Directive
  • Airbus A3509411041

EASA AD 2024-0156

Aug 13, 2024

Landing Gear — Main Landing Gear Bogie Beam Axle — Replacement

EASA Airworthiness Directive 2024-0156 is an airworthiness directive addressing the replacement of the main landing gear bogie beam axle on Airbus A350-941 aeroplanes. It specifically targets affected parts with Part Number 55-3575047-00 and certain serial numbers due to identified anodic burns that reduce fatigue life. The directive mandates replacement of these parts to prevent potential structural failure of the main landing gear.

Airworthiness Directive
  • Airbus A350941

EASA AD 2024-0155

Aug 13, 2024

Wings — RIB 1 corner fitting and Upper / Lower Wing Skin Cover Edge Glow Sealant — Inspection / Modification

EASA Airworthiness Directive 2024-0155 is an airworthiness directive issued for Airbus A350-941 and A350-1041 aeroplanes. It addresses inspection and modification requirements related to the RIB 1 corner fitting and upper/lower wing skin cover edge glow sealant to ensure proper lightning strike protection on the wing tanks. This directive applies to specific manufacturer serial numbers as defined by Airbus service bulletins.

Airworthiness Directive
  • Airbus A3509411041

EASA AD 2024-0129

Jul 5, 2024

Fuselage – Forward Cargo Door Piano Hinges – Inspection

EASA Airworthiness Directive 2024-0129 is issued for Airbus A350-941 and A350-1041 aeroplanes, addressing inspection requirements for the forward cargo door piano hinges 2 and 3. The directive applies to specific manufacturer serial numbers and aims to ensure continued airworthiness by detecting potential cracking and damage in these parts. This directive updates previous requirements to enhance safety related to the forward cargo door structure.

Airworthiness DirectiveSuperseded
  • Airbus A3509411041

EASA AD 2024-0098

May 2, 2024

Fuselage – Forward Cargo Door Piano Hinges – Inspection

EASA Airworthiness Directive 2024-0098 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 and A350-1041 aeroplanes. It mandates inspection of the forward cargo door piano hinges 2 and 3 due to potential cracking risks. This directive applies to specific manufacturer serial numbers and aims to ensure continued structural integrity of the affected aircraft.

Airworthiness DirectiveSuperseded
  • Airbus A3509411041

EASA AD 2024-0060R1

Apr 16, 2024

Nacelles / Pylons – Air Intake Cowl – Inspection

EASA Airworthiness Directive 2024-0060R1 is an updated safety directive affecting Airbus A350-941 and A350-1041 aeroplanes. It mandates inspection of specific engine air inlet cowls with certain part numbers due to potential elongation of locating holes in the Nacelle Anti-Icing forward bulkheads. This condition could reduce anti-icing performance and risk loss of control of the aircraft.

Airworthiness DirectiveSuperseded
  • Airbus A3509411041

EASA AD 2024-0078

Mar 20, 2024

Equipment / Furnishings — AFT Galley Complex Lower Attachment Studs — Inspection / Replacement

EASA Airworthiness Directive 2024-0078 is issued for Airbus A350-941 and A350-1041 aeroplanes, addressing inspection and replacement of the aft galley complex lower attachment studs. The directive targets specific part numbers of lower attachment studs that secure the aft galley complex to the aircraft structure. It mandates inspections and replacement to ensure continued airworthiness and safety.

Airworthiness Directive
  • Airbus A3509411041