AD Amdt-39-10933
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300-600 | Airworthiness Directives; Airbus Model A300-600 Series Airplanes |
Unsafe Condition
Cracks in the angle fitting at frame 40 of the center wing box, which could result in the failure of the center wing box and reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a detailed visual, eddy current, or liquid penetrant inspection to detect cracking in the angle fitting of frame 40 (both left and right), with the nut removed. Repeat inspections at specified intervals until the modification is completed. Modify the angle fitting at frame 40 in accordance with Airbus Service Bulletin A300-57-6053, Revision 1, dated October 31, 1995. If cracks are found, take corrective actions as specified in Airbus Service Bulletin A300-57-6052, Revision 1, dated July 22, 1996.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 1,500 flight cycles after the effective date of this AD, or prior to the accumulation of the threshold specified in Table 1, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300-600 series airplanes on which Airbus Modification 10453 has not been installed, certificated in any category.
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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