AD 2006-16-19
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; B-N Group Ltd. BN-2, BN-2A, BN-2B, BN-2T, and BN-2T-4R Series (All Individual Models Included in Type Certificate Data Sheet (TCDS) A17EU, Revision 16, Dated December 9, 2002) Airplanes |
Unsafe Condition
Corrosion of the interior surface of the elevator system final drive control rod could result in failure or collapse of the rod, leading to loss of control or jamming of the elevator system.
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Required Actions
Inspect the internal surface of the elevator system final drive control rod within 50 hours time-in-service or one month after the effective date, whichever occurs first. If corrosion is found, replace the elevator control rod before further flight. Repeat the inspection at intervals not to exceed 12 months.
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Compliance Time
Within 50 hours time-in-service or one month after the effective date, whichever occurs first.
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Affected Aircraft
All BN-2, BN-2A, BN-2B, BN-2T, and BN-2T-4R Series airplanes included in Type Certificate Data Sheet (TCDS) A17EU, Revision 16, dated December 9, 2002, certificated in any U.S. category.
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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