AD 2017-05-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A318-112 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Aluminum alloy with inadequate heat treatment was delivered and used on several structural parts, which could result in reduced structural integrity of the airplane following fatigue load.
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Required Actions
Conduct a one-time eddy current conductivity measurement of certain cabin, cargo compartment, and frame structural parts to determine if aluminum alloy with inadequate heat treatment was used. Replace any affected parts with serviceable parts if necessary.
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Compliance Time
Within 12 months of the effective date (April 17, 2017).
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Affected Aircraft
Airbus Model A318-112 airplanes, A319-111, -112, -115, -132, and -133 airplanes, A320-214, -232, and -233 airplanes, and A321-211, -212, -213, -231, and -232 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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