Safety record in brief:3 NTSB accidents (destroyed damage at worst, latest Jun 2013)6 ADs may apply2 service difficulty reports
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The pilot's decision to land on a wet grass airstrip, which resulted in a main landing gear collapse after a collision with rough terrain.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR13CA271)
the fatigue failure of the crankshaft due to improper overhaul procedures. Factors include a soft area in the field where the forced landing took place.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA00LA173)
THE PILOT EXPERIENCED ENGINE POWER FAILURE DUE TO FUEL EXHAUSTION FOR UNKNOWN REASONS SINCE ABOUT 30 GALLONS OF FUEL SHOULD HAVE BEEN ON BOARD WHEN THE CRASH OCCURRED. THE PILOT WAS VECTORED TOWARD THE NEAREST AIRPORT BUT WAS UNABLE TO REACH IT AND CRASHED INTO A ROUGH AND ROCKY TREE-COVERED HILLSIDE ABOUT ONE-HALF MILE SHORT OF THE APPROACH END OF THE INTENDED RUNWAY. AN OPERATIONAL CHECK OF…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW85FA257)
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 (T210N) |
| 2012-10-04 | Wings | Jun 5, 2012 | Airframe (T210N)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 (T210N) |
| 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. |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (T210N)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 98-05-14 R1 | Cessna Aircraft Company Models T210N, P210N, and P210R Airplanes | Sep 22, 1998 | Airframe (T210N)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.
POWER LOSS AFTER TAKEOFF RESULTING IN RETURN TO AIRPORT. FUEL FLOW WAS REPORTED HIGH AND MANIFOLD PRESSURE NORMAL. SUSPECTED PARTIALLY PLUGGED FUEL INJECTOR NOZZLE.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED LOUD BANG ON CLIMBOUT. RETURNED WITHOUT INCIDENT TO FIELD. UPON EXAMINATION FOUND NR 4 CYLINDER HEAD SEPARATED FROM CYLINDER AT 5TH COOLING FIN ON HEAD. ENGINE TSO AND CYLINDER TSN 817.6 HRS. LAST COMPRESSION CHECK WAS AT 100 HR INSPECTION 19.2 HRS PRIOR WITH COMPRESSION 69/80.
From FAA Service Difficulty Reports; matched by N-number and serial number.