AD 2005-23-08
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 A300 F4-605R and A300 C4-605R Variant F Airplanes |
Unsafe Condition
Reports of cracks found before the inspection thresholds in the existing AD and cracks found in nearby areas not inspected by the existing AD. 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
Repetitive inspections to detect cracks of certain attachment holes, installation of new fasteners, follow-on inspections or repair if necessary, and modification of the angle fittings of fuselage frame FR47. Revision of certain inspection thresholds and intervals. Addition of inspections to detect cracks of additional attachment holes.
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 B4-601, B4-603, B4-620, and B4-622 airplanes; Model A300 B4-605R and B4-622R airplanes; Model A300 F4-605R airplanes; and Model A300 C4-605R Variant F airplanes; certificated in any category; except airplanes on which Airbus Modification 12171 or 12249 has been accomplished or on which Airbus Service Bulletin A300-57-6069 has been accomplished.
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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