AD 2016-01-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking of the front spar vertical stringers on the wings and the horizontal floor beam on frame 36, which could result in reduced structural integrity of the airframe.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive high frequency eddy current (HFEC) inspections for cracking of the radius of the front spar vertical stringers and the horizontal floor beam on frame 36. Perform a rototest inspection for cracking of the fastener holes of the front spar vertical stringers on frame 36. Repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 months of the effective date (February 25, 2016).
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Affected Aircraft
Airbus Model A320 series airplanes with manufacturer serial numbers 0080 to 0155 inclusive, and all airplanes with serial numbers 0156 and higher.
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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