AD Amdt-39-10655
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
Unsafe Condition
Fatigue cracking of the bottom flanges of the longitudinal floor beams at frame 43 and fatigue cracking of the fastener holes in the longitudinal floor beams could result in reduced structural integrity of the airplane.
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Required Actions
Conduct repetitive inspections for fatigue cracking of the bottom flanges of the longitudinal floor beams at frame 43 and repair if necessary. Perform a one-time inspection for fatigue cracking of the fastener holes in the longitudinal floor beams and modify the floor beams as terminating action for the repetitive inspections.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A320 series airplanes with certain configurations requiring the mandatory continuing airworthiness information from a foreign civil airworthiness authority.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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