AD 2016-19-15
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; REIMS AVIATION S.A. Airplanes |
Unsafe Condition
Cracks found in the horizontal stabilizer rear attach structure and the vertical fin rear spar attach structure.
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Required Actions
Inspect the horizontal stabilizer rear attach structure and the vertical fin rear spar attach structure for cracks and oversized bolt holes using eddy-current non-destructive test (NDT) inspections. Make all necessary repairs and replacements as required.
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Compliance Time
Within 50 flight hours after the effective date of this AD.
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Affected Aircraft
REIMS AVIATION S.A. Model F406 airplanes, serial numbers F406-0001 through F406-0098, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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