EASA AD 26-087
Indicating / Recording Systems – Integrated Control Panels – Inspection
Summary
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.
What Changed
This new proposed airworthiness directive introduces a one-time general visual inspection of the affected fire ICP parts to detect internal damage caused by mechanical shocks. It requires replacement of any damaged parts found and mandates reporting inspection results to Airbus. Additionally, it sets installation conditions for these parts to ensure only serviceable units are installed after the effective date.
Why It Matters
This directive is critical for aviation professionals because undetected damage to the fire ICP can cause unintended engine shutdowns during flight, posing safety risks. Operators and maintenance teams must comply to prevent potential in-flight engine failures and ensure continued airworthiness. The directive also supports ongoing safety investigations and helps maintain regulatory compliance.
What To Do
Operators of Airbus A350-941 and A350-1041 aeroplanes with affected ICP parts installed must perform a general visual inspection within 24 months of the directive's effective date. If damage is found, the affected part must be replaced within 6 months of inspection but no later than 24 months after the effective date. Inspection results must be reported to Airbus within 30 days after inspection or the effective date, whichever is later. Installation of affected parts is only allowed if they pass inspection per Airbus instructions.
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