AD 85-11-07 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | P210N | Airworthiness Directives; Cessna Model P210N, P210R and T210R Airplanes |
| aircraft | Cessna Aircraft Company | P210R | Airworthiness Directives; Cessna Model P210N, P210R and T210R Airplanes |
| aircraft | Cessna Aircraft Company | T210R | Airworthiness Directives; Cessna Model P210N, P210R and T210R Airplanes |
Unsafe Condition
Separation of the turbocharger oil reservoir outlet fitting and subsequent rapid loss of engine lubricating oil.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the turbocharger oil reservoir outlet fitting for cracks using a strong light. If no cracks are found, reinspect every 25 hours time-in-service or replace the reservoir with specified Cessna parts. If cracks are detected, replace the reservoir immediately with the appropriate Cessna part number and follow installation procedures.
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Compliance Time
Prior to further flight
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Affected Aircraft
Cessna Model P210N (serial numbers P21000001 through P21000855), P210R (serial numbers P21000001 through P21000855), and T210R (serial numbers 21064898 through 21064929) airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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