This N-number isn't registered right now. Below is its last known registration, canceled Jul 28, 2010.
Safety record in brief:1 NTSB accident (substantial damage, Oct 2003)4 ADs may apply1 service difficulty report
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.
Loss of engine power due to crankshaft counterweight failure.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL04TA012)
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 (210L) |
| 2012-10-04 | Wings | Jun 5, 2012 | Airframe (210L)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 (210L) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO 520 SERIES)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. |
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.
CRACKS HAVE BEEN FOUND ON THE REAR STABILIZER SPAR. SUSPECT CRACKS ARE CAUSED BY IMPROPER USE OF A RIVET SQUEEZER DURING FACTORY INSTALLATION. SUBMITTER STATED THESE CRACKS AND TOOLING MARKS HAVE BEEN FOUND ON 4 OTHER ASSEMBLIES. CRACKS RANGE IN SIZE FROM .25 INCH TO .50 INCH LONG, AND ARE FOUND…
From FAA Service Difficulty Reports; matched by N-number and serial number.