This N-number isn't registered right now. Below is its last known registration, canceled Aug 14, 2002.
Safety record in brief:1 NTSB accident (destroyed damage, Aug 1999)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 failure to maintain sufficient airspeed during final approach to landing, resulting in an inadvertent stall. A factor was the high density altitude.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DEN99FA137)
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 |
|---|---|---|---|
| 2020-03-16 | Fuselage Main, Structure | Mar 9, 2020 | Airframe (T210M) |
| 2012-10-04 | Wings | Jun 5, 2012 | Airframe (T210M)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 (T210M) |
| 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 (T210M)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. |
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.
ONE BENT BLADE AND ONE BLADE SEPARATED AT HALF ITS LENGTH. PART FAILED ON FINAL APPROACH TO LANDING. COMPRESSOR SHAFT AND TURBINE SHAFT BENT. NO KNOWN REASON FOR COMPRESSOR BLADE TO HAVE SEPARATED, OR FOR SHAFT TO HAVE BENT, NO EVIDENCE OF FOREIGN OBJECTS BEING INJESTED INTO TURBOCHARGER.
From FAA Service Difficulty Reports; matched by N-number and serial number.BOLT ATTACHING ALTERNATOR ADJUSTING BRACKET TO ENGINE FAILED. THIS ALLOWED THE ALTERNATOR TO MOVE UNTIL ELECTRICAL TERMINAL CONTACTED A GROUND CAUSING A DIRECT SHORT. THE BOLT WAS A NON-STANDARD BOLT OF UNKNOWN ORIGIN. UNAPPROVED PART.
From FAA Service Difficulty Reports; matched by N-number and serial number.