AD 2012-25-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-2C | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracking of the frame (FR) 40 forward fitting, which could result in a deterioration of the structural integrity of the frame.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform repetitive detailed visual inspections of the forward fitting at FR 40 without nut removal. Conduct a one-time eddy current or liquid penetrant inspection of the forward fitting at FR 40 with nut removal, and repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in the AD, unless the actions have already been done.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 B4-2C, B4-103, B4-203, B4-601, B4-603, B4-605R, B4-620, B4-622, and B4-622R airplanes, all serial numbers, modified preventively in service as specified in Airbus Service Bulletin A300-53-0297 or A300-57-6053.
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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