AD 92-27-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 650 | Airworthiness Directives; CESSNA Model 650 Series Airplanes |
Unsafe Condition
Potential loss of elevator control due to insufficient material wall thickness or cracking in the inboard attach fittings of the left-hand and right-hand elevator torque tubes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect inboard attach fittings of the elevator torque tubes for material wall thickness and cracking per Cessna Alert Service Letter A650-27-30. Depending on findings, either no further action, replace fittings within 150 flight hours if thickness is 0.040-0.044 inches, or replace with part number 6234132-8 prior to further flight if thickness is below 0.040 inches or cracking is found.
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Compliance Time
Within 25 hours time-in-service after the effective date of this AD for the initial inspection. Subsequent actions may require compliance within 150 flight hours or prior to further flight depending on inspection results.
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Affected Aircraft
Cessna Model 650 series airplanes with serial numbers -0001 thru -0219, inclusive, and -7001 thru -7013, inclusive, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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