AD 2018-11-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310-203 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
The outer wing lower junction is subject to widespread fatigue damage (WFD) at the level of the first fasteners row, close to Rib 1 between Frame (FR) 40 and FR 47.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the fastener holes at rib 1, stiffeners 1 to 14, on both outer wings between FR 40 and FR 47 by cold-working, including related investigative actions and applicable corrective actions.
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Compliance Time
Before further flight
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Affected Aircraft
All Airbus Model A310-203, -221, -222, -304, -322, -324, and -325 airplanes.
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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