AD 2009-11-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A310 Series Airplanes |
Unsafe Condition
Fatigue cracks and corrosion around and under the chafing plates of the wing root, which could result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform an initial inspection to detect discrepancies around and under the chafing plates of the wing root, using Airbus Service Bulletin A310-53-2069, Revision 06, or earlier revisions. If any discrepancy is found, accomplish corrective actions such as removal of corrosion, corrosion protection, high frequency eddy current inspection, or x-ray inspection. Repeat inspections at intervals specified in the applicable service bulletin.
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Compliance Time
Within 4 years since date of manufacture, or within 12 months after June 3, 1998, whichever occurs later.
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Affected Aircraft
Airbus Model A310 series airplanes, certificated in any category, on which Airbus Modifications 8888 and 8889 have not been accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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