AD 2002-11-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-600 and A300 B4-600R | Airworthiness Directives; Airbus Model A300 B4-600 and A300 B4-600R Series Airplanes, and Model A300 F4-605R Airplanes |
Unsafe Condition
Fatigue cracking of the forward fitting of fuselage frame FR47, which could result in reduced structural integrity of the frame.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive inspections to detect cracks of certain attachment holes, install new fasteners, perform follow-on inspections or repairs if necessary, and modify the angle fittings of frame FR47.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the specified compliance intervals outlined in the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 B4-600, A300 B4-600R, and A300 F4-600R series airplanes (A300-600).
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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