AD 2000-07-22
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300-600 | Airworthiness Directives; Airbus Model A300-600 Series Airplanes |
Unsafe Condition
Fatigue cracking of the doubler angle and discrepancies of the fasteners that connect the doubler angle and the bottom panel of the center wing box, 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 for cracking of the doubler angle and discrepancies of the fasteners connecting the doubler angle and the bottom panel of the center wing box. Perform corrective actions, if necessary, including crack stopping, rotating probe inspection, and eventual modification of the doubler angle as specified in Airbus Service Bulletin A300-53-6110, Revision 01.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in Airbus Service Bulletin A300-53-6110, Revision 01, or as extended under paragraph (f) of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300-600 series 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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