EASA Regulations & Airworthiness Directives

Browse 181 EASA regulations with AI-powered summaries.

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EASA AD US-2026-20-12

Oct 12, 2026

Turbine - High-Pressure Turbine Interstage Seal - Replacement

The Federal Register document titled 'Turbine - High-Pressure Turbine Interstage Seal - Replacement' is a final rule airworthiness directive (AD 2026-20-12) issued by the FAA affecting Engine Alliance Model GP7270, GP7272, and GP7277 engines. It addresses an unsafe condition related to uncontained failure of the high-pressure turbine interstage seal, which was reported during an aborted takeoff on an Airbus A380 equipped with these engines. The AD mandates removal and replacement of certain high-cycle HPT interstage seals to prevent potential engine fire and aircraft damage.

Airworthiness Directive
  • Engine Alliance GP7200
  • Engine Alliance GP7270
  • Engine Alliance GP7272
  • Engine Alliance GP7277
  • Airbus A380

EASA PAD 26-118

Sep 29, 2026

Fire Protection – Fire-extinguishing Pipes – Replacement

EASA Airworthiness Directive Proposal 26-118 addresses a safety issue on Airbus A380-861 aeroplanes equipped with EA GP7200 engines. It concerns the replacement of fire-extinguishing pipes, specifically part number L2621011100200, located in the core zone of each engine pylon. The directive aims to improve fire protection by mandating the installation of redesigned fire-extinguishing pipes.

Proposed AD
  • Airbus A380

EASA AD 2026-0181

Sep 18, 2026

Power Plant – Air Intake Cowl – Nacelle Anti-ice Duct Female Socket – Inspection

EASA Airworthiness Directive 2026-0181 is an airworthiness directive addressing the inspection of the air intake cowl nacelle anti-ice duct female socket on Airbus A380-861 aeroplanes equipped with SAFRAN engine nacelles. It mandates repetitive inspections to detect wear and damage in the affected nacelle anti-ice systems to prevent structural failures. The directive applies to all manufacturer serial numbers of the Airbus A380-861.

Airworthiness Directive
  • Airbus A380

EASA AD 2016-0193R2

Aug 13, 2026

Engine – Low Pressure Turbine Exhaust Case and Support Assembly (Tail Bearing Housing) – Inspection / Replacement

EASA Airworthiness Directive 2016-0193R2 is an updated regulation addressing inspection and replacement requirements for the low pressure turbine exhaust case and support assembly (Tail Bearing Housing) of Rolls-Royce RB211 Trent 900 engines, commonly installed on Airbus A380 aircraft. This directive mandates inspections to detect cracks or damage in specific TBH components and outlines corrective actions and optional terminating modifications to ensure continued airworthiness.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900
  • Airbus A380

EASA AD 2026-0164

Aug 13, 2026

Time Limits / Maintenance Checks – Engine Time Limits Manual – Amendment

EASA Airworthiness Directive 2026-0164 is an amendment addressing the time limits and maintenance checks for Rolls-Royce Deutschland RB211 Trent 900 engines, specifically models RB211 Trent 970-84, 972-84, and 972E-84, commonly installed on Airbus A380 aircraft. This directive updates the Airworthiness Limitations Section (ALS) in the Rolls-Royce Time Limits Manual to ensure mandatory inspections and life limits are correctly applied. It mandates compliance with the revised maintenance tasks and life limits to maintain engine airworthiness.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900
  • Airbus A380

EASA PAD 26-092

Aug 3, 2026

Power Plant – Air Intake Cowl – Nacelle Anti-ice Duct Female Socket – Inspection

EASA Airworthiness Directive PAD No. 26-092 is a proposed directive addressing inspection requirements for the air intake cowl nacelle anti-ice duct female socket on Airbus A380-861 aeroplanes equipped with SAFRAN engine nacelles. It targets potential structural failures caused by excessive wear in the female socket of the anti-ice duct. The directive applies to all manufacturer serial numbers of the Airbus A380 and references specific Airbus and SAFRAN service bulletins for inspection procedures.

Proposed AD
  • Airbus A380

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 26-084

Jul 13, 2026

Time Limits / Maintenance Checks – Engine Time Limits Manual – Amendment

EASA Airworthiness Directive PAD No. 26-084 is a proposed amendment concerning the time limits and maintenance checks for Rolls-Royce Deutschland Ltd & Co KG RB211 Trent 900 engines, specifically models RB211 Trent 970-84, 972-84, and 972E-84, commonly installed on Airbus A380 aircraft. This directive updates the Airworthiness Limitations Section (ALS) within the Rolls-Royce Time Limits Manual Revision 70 to ensure continued airworthiness of these engines. It mandates compliance with new and more restrictive maintenance tasks and life limits to address potential unsafe conditions.

Proposed AD
  • Rolls-Royce Deutschland Ltd & Co Kg RB211 TRENT 900
  • Airbus A380

EASA PAD 26-077

Jun 29, 2026

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

EASA Airworthiness Directive PAD No. 26-077 is a proposed amendment affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It updates the Airworthiness Limitations Section Part 1, Safe Life Airworthiness Limitations Items, introducing new and more restrictive maintenance limitations. This directive ensures continued airworthiness by mandating compliance with the latest Airbus A380 ALS revision 14.

Proposed AD
  • Airbus A380

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 2026-0119-E

Jun 22, 2026

Wings – Wing Mid Spars – Inspection

EASA Airworthiness Directive 2026-0119-E is an emergency directive addressing inspection requirements for the wing mid spars on Airbus A380-841, A380-842, and A380-861 aeroplanes with specific manufacturer serial numbers. It mandates special detailed inspections to detect cracks that could compromise wing structural integrity. The directive applies to certain serial numbers grouped into two categories with different compliance times.

Airworthiness Directive
  • Airbus A380

EASA AD 2026-0030

Feb 26, 2026

Wings — Movable Flap Track Fairings 2 and 5 / Forward Attachments — Inspection

EASA Airworthiness Directive 2026-0030 is issued for Airbus A380-841, A380-842, and A380-861 aeroplanes concerning the movable flap track fairings 2 and 5 forward attachments. It mandates inspections to detect potential structural issues caused by unexpected aerodynamic loads on these parts. The directive applies to all serial numbers except those with specific Airbus modifications or service bulletins already incorporated.

Airworthiness Directive
  • Airbus A380

EASA AD 2025-0270

Dec 2, 2025

Wings — Leading Edge Devices / Slats and Droop Noses — Identification

EASA Airworthiness Directive 2025-0270 is an airworthiness directive issued by EASA affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses identification and verification of wing leading edge devices including slats and droop noses to ensure correct part numbers are installed. This directive applies to all manufacturer serial numbers of the Airbus A380 models mentioned.

Airworthiness Directive
  • Airbus A380