EASA Regulations for Airbus A380-841

57 airworthiness directives and regulations affecting Airbus A380-841.

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New ADs and bulletins for Airbus A380-841, summarized like the ones below, every Monday.

EASA PAD 26-125

Oct 15, 2026

Pneumatic – Pylon / Wing Interface Bleed Duct and Fuel Pipe – Inspection / Modification / Replacement

EASA Airworthiness Directive 26-125 is a proposed directive addressing inspection, modification, and replacement of the pneumatic pylon/wing interface bleed duct and fuel pipe on Airbus A380-841, A380-842, and A380-861 aeroplanes. It targets specific bleed-air duct assemblies identified by part numbers related to the four wing-to-engine pylon interfaces. The directive aims to mitigate risks associated with bleed-air duct detachments and potential fuel leaks that could lead to fire hazards.

Proposed AD
  • Airbus A380841842861

EASA AD 2026-0154

Jul 31, 2026

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

EASA Airworthiness Directive 2026-0154 is an amendment concerning the Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 1, Safe Life Airworthiness Limitations Items, requiring compliance with the latest Airbus A380 ALS Revision 14. This directive ensures continued airworthiness by mandating replacement of life-limited parts and maintenance program revisions.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2026-0155

Jul 31, 2026

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

EASA Airworthiness Directive 2026-0155 is an amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with the updated Airworthiness Limitations Section Part 2, Damage Tolerant Airworthiness Limitation Items (DT-ALI) Revision 12 to ensure continued airworthiness. This directive updates maintenance requirements and intervals for these aircraft models.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2026-0156

Jul 31, 2026

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3, Certification Maintenance Requirements – Amendment

EASA Airworthiness Directive 2026-0156 is an amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with the updated Airbus A380 Airworthiness Limitations Section Part 3, Certification Maintenance Requirements Revision 08 to ensure continued airworthiness. This directive applies to all manufacturer serial numbers of the affected Airbus A380 models.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2026-0157

Jul 31, 2026

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

EASA Airworthiness Directive 2026-0157 is an amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 4, System Equipment Maintenance Requirements, requiring compliance with Airbus A380 ALS Part 4, SEMR Revision 17. This directive ensures mandatory maintenance tasks and life limits are followed to maintain continued airworthiness.

Airworthiness Directive
  • Airbus A380841842861

EASA PAD 26-078

Jun 29, 2026

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

EASA Airworthiness Directive PAD No. 26-078 is a proposed amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 2, specifically the Damage Tolerant Airworthiness Limitation Items (DT-ALI), to Revision 12. This directive ensures continued airworthiness by mandating compliance with the latest maintenance tasks and intervals.

Proposed AD
  • Airbus A380841842861

EASA PAD 26-079

Jun 29, 2026

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3, Certification Maintenance Requirements – Amendment

EASA Airworthiness Directive 26-079 is a proposed amendment addressing the Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 3, Certification Maintenance Requirements, specifically Revision 08 of the Airbus A380 ALS. This directive mandates compliance with new and/or more restrictive maintenance tasks to ensure continued airworthiness of these aircraft models.

Proposed AD
  • Airbus A380841842861

EASA PAD 26-080

Jun 29, 2026

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

EASA Airworthiness Directive PAD No. 26-080 is a proposed amendment concerning the Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 4, System Equipment Maintenance Requirements (SEMR) to Revision 17. This directive mandates compliance with new and more restrictive maintenance tasks and life limits to ensure continued airworthiness.

Proposed AD
  • Airbus A380841842861

EASA AD 2024-0191

Oct 10, 2024

Wings — Wing Front and Rear Spars — Inspection

EASA Airworthiness Directive 2024-0191 is an airworthiness directive addressing inspection requirements for the wing front and rear spars of Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates special detailed inspections of specific wing spar areas to detect cracks that could compromise structural integrity. This directive applies to all manufacturer serial numbers of these Airbus A380 models.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2024-0163

Aug 20, 2024

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

EASA Airworthiness Directive 2024-0163 is an airworthiness directive issued by EASA affecting all Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with updated safe life airworthiness limitations as specified in Airbus A380 Airworthiness Limitations Section Part 1, Safe Life Airworthiness Limitations Items, Variation 12.1. This directive ensures the continued airworthiness of these aircraft by enforcing new and more restrictive maintenance limitations.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2024-0141

Jul 16, 2024

Wings – Main Landing Gear Attachment – Inspection

EASA Airworthiness Directive 2024-0141 is issued for Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates repetitive inspections of the main landing gear attachment rib 9 fittings on both left-hand and right-hand wings to detect cracks and sealant condition. This directive addresses potential structural integrity risks due to corrosion and cracking in these critical components.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2024-0099

May 6, 2024

Equipment / Furnishings – Fuselage / Belly Fairing Mounted Emergency Evacuation Escape Slides – Replacement

EASA Airworthiness Directive 2024-0099 is an airworthiness directive issued for Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses issues with fuselage and belly fairing mounted emergency evacuation escape slides, specifically those with certain part numbers and serial numbers that have shown seam failures during proof pressure testing after overhaul. The directive mandates replacement and inspection requirements to ensure the continued airworthiness of these emergency slides.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2023-0198

Nov 16, 2023

Wings – Wing Front and Rear Spars – Inspection

EASA Airworthiness Directive 2023-0198 is issued for Airbus A380-841, A380-842, and A380-861 aeroplanes to mandate inspections of wing front and rear spars due to reported cracks. The directive applies to all manufacturer serial numbers and focuses on specific wing spar areas to ensure structural integrity. It requires special detailed inspections using ultrasonic testing methods following Airbus service bulletins and alert operator transmissions.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2023-0124

Jun 16, 2023

Landing Gear – Body Landing Gear Rear Axle – Replacement

EASA Airworthiness Directive 2023-0124 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses the replacement of certain right-hand and left-hand body landing gear rear axles identified as affected due to corrosion and potential failure risks. The directive mandates inspections and replacement of these parts to ensure continued safe operation of the aircraft.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2023-0067

Mar 24, 2023

Fuselage — Butt Strap Skin Panels — Inspection / Repair

EASA Airworthiness Directive 2023-0067 is an airworthiness directive issued by EASA concerning Airbus A380-841 and A380-861 aeroplanes with specific manufacturer serial numbers. It addresses inspection and repair requirements for the butt strap skin panels at the orbital junction of Frame 22 and Stringer 33 on the left-hand side of the fuselage. The directive mandates inspections and corrective actions to ensure structural integrity of the affected area.

Airworthiness Directive
  • Airbus A380841861

EASA AD 2023-0034

Feb 8, 2023

Fuselage — Frame 80 Fairing Outboard End Fitting Assemblies — Inspection

EASA Airworthiness Directive 2023-0034 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates inspections of the fuselage belly fairing outboard end fitting assemblies at frame 80 to detect potential cracks that could compromise structural integrity. The directive references Airbus Service Bulletin A380-53-8212 for inspection procedures.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2023-0031

Feb 8, 2023

Landing Gear – Body Landing Gear Rear Axle – Replacement

EASA Airworthiness Directive 2023-0031 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses the replacement of certain right-hand and left-hand body landing gear rear axles identified as affected due to corrosion and potential failure risks. The directive mandates inspections and replacement of these parts to ensure continued airworthiness and safety.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2023-0024

Jan 26, 2023

Fuselage – Frame 99 to 104 Shear Tie and Mouse Holes – Inspection

EASA Airworthiness Directive 2023-0024 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates inspections of the fuselage frame 99 to 104 shear ties and mouse holes as specified in the Airbus A380 Airworthiness Limitations Section Part 2 Damage Tolerant Airworthiness Limitation Items Revision 10 Variation 10.1. This directive ensures continued airworthiness by requiring updated maintenance tasks for these aircraft models.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2022-0262

Dec 21, 2022

Wings – Front and Rear Spars – Inspection

EASA Airworthiness Directive 2022-0262 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aircraft. It mandates inspections of specific wing spars, including the outer rear spar, outer inner front spar, and outer front spar, to detect cracks that could compromise wing structural integrity. This directive updates previous inspection requirements and applies to all manufacturer serial numbers of the Airbus A380.

Airworthiness DirectiveSuperseded
  • Airbus A380841842861

EASA AD 2022-0238

Dec 5, 2022

Doors — Slide Management System Triple Reed Contact Switch — Replacement

EASA Airworthiness Directive 2022-0238 is an airworthiness directive affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses corrosion issues found on the triple reed contact switches (TRCS) used in the doors and slide management system. The directive mandates inspections and replacement of affected Diehl Aerospace GmbH TRCS parts to ensure proper door functionality and evacuation capability.

Airworthiness Directive
  • Airbus A380841842861