This N-number isn't registered right now. Below is its last known registration, canceled Jun 10, 2014.
Safety record in brief:1 NTSB accident (substantial damage, Dec 2013)4 ADs may apply3 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.
A total loss of engine power due to the fatigue failure of the No. 4 connecting rod. Contributing to the accident was a likely loss of lubrication for reasons that could not be determined during a postaccident engine examination.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA14LA076)
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 (210N) |
| 2012-10-04 | Wings | Jun 5, 2012 | Airframe (210N)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 (210N) |
| 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.
CRACKED AT BARREL AND HEAD. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.INSPECTED ACTUATORS FOR CRACKS. FOUND CRACKS, REMOVED FROM SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.INSPECTED ACTUATORS FOR CRACKS. FOUND CRACKS, REMOVED FROM SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.