Safety record in brief:1 NTSB accident (substantial damage, Oct 1991)5 ADs may apply2 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
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 RECOVERY FROM A BOUNCED LANDING. FACTORS WERE THE PILOT'S EXCESSIVE AIRSPEED AND IMPROPER FLARE TECHNIQUE.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW92GA011)
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 (T210R) |
| 2012-10-04 | Wings | Jun 5, 2012 | Airframe (T210R)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 (T210R) |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (T210R)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. |
| 98-20-33 | Cessna Aircraft Company Model T210R Airplanes | Nov 17, 1998 | Airframe (T210R) |
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.
PERFORMED A POST PAINT STRIP INSPECTION AND FOUND A VERY LARGE QTY OF UNIVERSAL HEAD RIVETS HAD BEEN SANDED DOWN.
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND LARGE OIL LEAK AT NR 4 CYLINDER ROCKER COVER DURING FIRST GROUND RUN OF THIS ENGINE FROM CONTINENTAL. FOUND NR 4 UPPER RT MOUNT MACHINED INCORRECTLY. THIS IS A CONTINENTAL REBUILT ENGINE.
From FAA Service Difficulty Reports; matched by N-number and serial number.