AD 2001-06-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-601 | Airworthiness Directives; Airbus Model A300 B4-601, A300 B4-603, A300 B4-620, A300 B4-605R, A300 B4-622R, and A300 F4-605R Airplanes |
Unsafe Condition
Cracking in the area surrounding the frame feet attachment holes between fuselage frames (FR) 41 and FR46, which could result in rupture of the frame foot and reduced structural integrity of the airplane.
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Required Actions
Perform repetitive high frequency eddy current (HFEC) or rototest inspections to detect cracking in the specified area. Install new fasteners for certain airplanes if no cracking is detected. Take follow-on corrective actions if necessary.
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Compliance Time
Within the applicable grace period or before reaching the specified flight-cycle or flight-hour threshold, whichever occurs first.
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Affected Aircraft
Airbus Model A300 B4-601, A300 B4-603, A300 B4-620, A300 B4-605R, A300 B4-622R, and A300 F4-605R airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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