AD Amdt-39-10997
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-301 | Airworthiness Directives; Airbus Model A330-301, -321, -322, - 341, -342, and A340-211, -212, -213, -311, -312, and -313 Series Airplanes |
Unsafe Condition
Fatigue cracking of the inner flange of the rear fuselage frame FR73A, between beams 5 and 6, which could result in reduced structural integrity of the fuselage.
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Required Actions
Conduct repetitive high-frequency eddy current (HFEC) inspections to detect cracking of the inner flange of the rear fuselage frame FR73A. Perform corrective actions if cracking is detected. Optional terminating action is provided for the repetitive inspections.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A330-301, -321, -322, -341, -342, and A340-211, -212, -213, -311, -312, and -313 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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