AD 2009-10-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A380-841 | Airworthiness Directives; Airbus Model A380-841, -842, and -861 Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A380-841, -842, and -861 Airplanes |
Unsafe Condition
Cracks were found on the Movable Flap Track Fairing number 6 (MFTF<sub>6</sub>) at the pivot attachment support-ring and U-frame in the attachment area to aft-kinematic. Delamination was also observed within the monolithic Carbon Fibre Reinforced Plastic (CFRP) structure around the pivot support-ring. This could lead to in-flight loss of the MFTF<sub>6</sub>, potentially resulting in injuries to persons on the ground.
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Required Actions
Inspect the MFTF<sub>6</sub> using a special detailed inspection (ultrasonic and high-frequency eddy current) to detect cracks and delamination. Replace the MFTF<sub>6</sub> if cracks or delamination are found.
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Compliance Time
Within 12 months of the effective date
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Affected Aircraft
Airbus Model A380-841, -842, and -861 airplanes, all serial numbers.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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