AD 2013-17-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A318-112 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
A fastener, which connects the cargo door keel beam foot to the circumferential butt-strap and the section 13-14 lower shell panel, was not installed on airplanes during production.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect forward fuselage frame 24, stringer 39, right hand, to determine if the fastener is missing. Measure the hole dimensions of the five holes surrounding the missing fastener if necessary. Perform related investigative and corrective actions if necessary, including a rototest inspection for cracking and repairing holes or fasteners as needed.
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Compliance Time
Within 50 flight hours after the effective date of this AD.
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Affected Aircraft
Airbus Model A318-112, A319-111, A319-112, A319-115, A319-132, and A319-133 airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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