AD Amdt-39-10928
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A321-111 | Airworthiness Directives; Airbus Model A321-111, -112, and -131 Series Airplanes |
Unsafe Condition
Fatigue cracking in the area surrounding certain attachment holes of the forward pintle fittings of the main landing gear (MLG) and the actuating cylinder anchorage fittings on the inner rear spar, 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 for fatigue cracking in the specified areas of the forward pintle fittings of the main landing gear (MLG) and the actuating cylinder anchorage fittings on the inner rear spar. Repair any detected cracking as necessary. Optional terminating action is provided for the repetitive inspections.
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Compliance Time
Not specified in the provided text.
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Affected Aircraft
Airbus Model A321-111, -112, and -131 series 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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