Safety record in brief:2 NTSB accidents (substantial damage at worst, latest May 2018)5 ADs may apply1 service difficulty report
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Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The pilot’s improper landing flare, which resulted in a long landing and a runway excursion.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for GAA18CA271)
the pilot's improper planning/decision and inaccurate fuel consumption calculations, which resulted in an inadequate supply of fuel, fuel exhaustion, and a subsequent forced landing at night. Darkness was a related factor.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW97LA064)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2023-02-17 | Fuselage Main, Structure | Mar 20, 2023 | Airframe (P210N) |
| 2012-10-04 | Wings | Jun 5, 2012 | Airframe (P210N)Certain serial numbers: 210G 21058819–21058936; T210G T210-0198–T210-0307; 210H 21058937–21059061; T210H T210-0308–T210-0392; 210J 21059062–21059199; T210J 21058140; … |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (P210N) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (TSIO-520 SER)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
| 98-05-14 R1 | Cessna Aircraft Company Models T210N, P210N, and P210R Airplanes | Sep 22, 1998 | Airframe (P210N)Certain serial numbers: T210N 21063641–21064897; P210N P21000386–P21000834 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
ELEVATOR TRIM BECAME FROZEN IN-FLIGHT AND WAS NOT ABLE TO OPERATE TRIM WHEEL IN BELOW FREEZING TEMPERATURE. AFTER ENTERING SHOP, TRIM WHEEL WAS FREE, BUT STICKY. FOUND TRIM ACTUATOR CRACKED AND DIRTY. SUBMITTER STATED ACTUATOR MAY NOT HAVE BEEN SERVICED PROPERLY AND MAY HAVE IMPROPER GREASE.
From FAA Service Difficulty Reports; matched by N-number and serial number.