AD 2014-25-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-211 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracking at the splice plate of the frame (FR) 47 butt joint crossing area found during full-scale fatigue testing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive inspections for cracking of both sides of the splice plate of the FR 47 butt joint crossing area. Take corrective action if necessary. An optional modification is available to terminate repetitive inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in the AD.
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Affected Aircraft
Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes, all serial numbers, except those with Modification 31012 embodied in production.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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