EASA AD 2024-0061
Wings — Flaps — Flap Support Structure — Inspection
Summary
EASA Airworthiness Directive 2024-0061 is an airworthiness directive issued by EASA concerning Airbus A350-1041 aeroplanes with specific manufacturer serial numbers. It mandates inspections of the flap support structures to detect corrosion and surface protection deficiencies that could compromise structural integrity. This directive applies to left-hand and right-hand flap support structures 1 through 4 on affected aircraft.
What Changed
This new airworthiness directive introduces a requirement for a one-time detailed inspection and subsequent repetitive inspections of the flap support structures on certain Airbus A350-1041 aircraft. It also requires corrective actions if corrosion or surface protection deficiencies are found, including restoration of anti-corrosion protection and contacting Airbus for further instructions if necessary.
Why It Matters
This directive is critical for aviation professionals because it addresses a potential safety risk due to production quality issues that could lead to corrosion and possible in-flight detachment of flap assemblies. Operators and maintenance organizations must comply to ensure continued airworthiness and avoid reduced aircraft control. Compliance with this AD helps prevent structural failures and enhances flight safety.
What To Do
Operators of affected Airbus A350-1041 aircraft must perform a one-time detailed inspection of specified flap support structure locations within 78 months of the aircraft's manufacture date. Following this, repetitive inspections must be conducted every 36 months. Any corrosion or deficiencies found must be corrected before the next flight, including restoring anti-corrosion protection or following Airbus-approved repair instructions.
AI-generated summary from official EASA source document. Always verify against the original.