AD 2001-23-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes; Correction |
Unsafe Condition
Cracks in the canted rib upper cap in the center wing carry-through area.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the canted rib upper cap for cracks. Repair cracks or modify the area depending on the extent of the cracks. Modify the canted rib upper cap at a specified time period as a terminating action for repetitive inspections.
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
Reims Aviation S.A. Model F406 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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