Manufacturer
Piaggio Aviation
Number
EASA 2024-0006
Model(s)
P.180
Published Date
Effective Date
Summary
Requires repetitive high-frequency eddy current inspections of the lower skin external reinforcement doublers on the main wain and any necessary corrective actions. Prompted by reported occurrences of corrosion and cracks found around the head of attaching fasteners during scheduled maintenance. An investigation determined that stress corrosion may develop on these fasteners. If not detected and corrected, this condition could reduce the structural integrity of the main wing.
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