EASA AD 2020-0162
SUPERSEDED BY EASA AD 2020-0286
Summary
EASA Airworthiness Directive 2020-0162 is an airworthiness directive issued for Airbus A380-841, A380-842, and A380-861 aeroplanes. It addresses a safety issue involving the bleed duct and fuel pipe at the pylon/wing interface, where a bracket weld failure could cause contact between these components. The directive mandates inspection and corrective actions to prevent potential fire hazards.
What Changed
This directive introduces a one-time inspection requirement of the affected bleed duct and fuel pipe area on Airbus A380 aircraft. It requires operators to inspect within 50 flight cycles or 400 flight hours and to perform corrective actions if discrepancies are found. Additionally, it mandates reporting inspection results to Airbus.
Why It Matters
This airworthiness directive is critical for aviation professionals because it addresses a potential ignition source caused by mechanical failure that could lead to uncontrolled fire. Compliance ensures continued airworthiness and safety of Airbus A380 fleets. Maintenance and compliance teams must prioritize inspections to avoid operational disruptions and regulatory penalties.
What To Do
Operators of Airbus A380-841, A380-842, and A380-861 must perform a one-time inspection of the bleed duct and fuel pipe at the pylon/wing interface within 50 flight cycles or 400 flight hours from 4 August 2020. Any discrepancies found must be corrected before the next flight. Inspection results, including no findings, must be reported to Airbus within 30 days after inspection.
Your fleet's weekly compliance brief
AI-summarized regulatory changes, compliance deadlines, and action items — filtered to your aircraft, every Monday.
AI-generated summary from official EASA source document. Always verify against the original.