AD 2017-11-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-211 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracks in the fastener holes of the former junction of the aft fuselage, specifically at frame (FR) 68 between stringers 4 and 5, which could propagate and reduce structural integrity.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitive inspections of the fastener holes at the former junction of the aft fuselage, specifically at frame (FR) 68 between stringers 4 and 5. Depending on findings, accomplishment of applicable repair solutions, including cold working of fastener and tooling holes as per Airbus Service Bulletin A320-53-1090. Rotating probe inspection and eddy current inspection of cold expanded holes as part of repair actions.
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Compliance Time
Within revised inspection compliance times, as specified in the AD.
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Affected Aircraft
Airbus Model A320-211, -212, and -231 airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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