AD 2015-26-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-211 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking of the lower surface panel on the wing center box, which could result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the lower surface panel on the wing center box for fatigue cracking, repair if necessary, and modify the lower surface panel on the wing center box as terminating action for repetitive inspections. Reduce compliance times for repetitive inspections and require an additional repair for certain airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within reduced thresholds and intervals as specified in the AD.
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Affected Aircraft
Airbus Model A320-211, -212, and -231 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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