AD 2016-01-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-2C | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracking of the splice fitting at fuselage frame (FR) 47 between stringers 24 and 26 (left- and right-hand sides), which could result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the splice fitting at fuselage frame (FR) 47 between stringers 24 and 26 for cracking using High Frequency Eddy Current (HFEC) rotating probe inspections. Perform corrective actions if necessary. Update the inspection compliance time and intervals as specified in the AD.
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Compliance Time
Within the new thresholds and intervals introduced with Airbus Service Bulletin A300-53-6123 Revision 06.
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Affected Aircraft
Airbus Model A300 B4-2C, B4-103, B4-203, B4-600, B4-600R, F4-600R series, and C4-605R Variant F 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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