AD 2001-16-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330 | Airworthiness Directives; Airbus Model A330 Series Airplanes |
Unsafe Condition
Fatigue cracking of the fuselage longitudinal buttstrap, which could result in reduced structural integrity of the fuselage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect fastener holes of certain fuselage joints for cracks using a roto-test inspection. If cracks are detected, perform a high frequency eddy current (HFEC) inspection and repair as necessary. Reinforce the fuselage structure between frames 31 and 37.1.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A330 series airplanes, as specified in the referenced service bulletin.
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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