AD Amdt-39-14628
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A321-100 | Airworthiness Directives; Airbus Model A321-100 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 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 for fatigue cracking. Repair, if necessary. Optional terminating action is provided for the repetitive inspections, which includes additional inspections of three mounting holes and revised inspection thresholds.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the applicable compliance times specified in the referenced AD 2006-04-11, as revised.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A321-100 Series airplanes, specifically A321-111, -112, and -131, with all manufacturer serial numbers (MSN), except MSN 364 and 385.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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