This N-number isn't registered right now. Below is its last known registration, canceled Apr 16, 2013.
Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Apr 1997)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.
The pilot's failure to obtain the proper touchdown point during an emergency landing resulting in an overrun and subsequent nose over. A factor in the accident was a reported partial loss of engine power for undetermined reasons.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA97LA118)
THE ACFT WAS FOUR MILES FROM THE ARPT ON AN ILS APCH WHEN AN ENG FAILURE WAS EXPERIENCED. THE ACFT WAS DAMAGED DURING THE FORCED LANDING ON A FROZEN LAKE. POST ACCIDENT ENG TEARDOWN REVEALED THE ENG FAILURE ORIGINATED FROM MOVEMENT OF THE #2 MAIN BEARING. THIS RESULTED IN A BENDING OVERLOAD OF THE CRANKSHAFT AND EVENTUAL SEPARATION OF THE CRANKSHAFT AT THE #3 CHEEK.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI86LA091)
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 (210M) |
| 2012-10-04 | Wings | Jun 5, 2012 | Airframe (210M)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 (210M) |
| 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.
DURING A DISASSEMBLY INSPECTION OF PROPELLER LINK, THE BLADE ACTUATING ON THE NR 2 BLADE WAS BROKEN AT THE .4375 INCH BLADE BUTT ATTACH POINT AND THE CHROME PLATING ON THE BLADE PITCH FITTING WAS DETERIORATED AND SHOWED EXTENSIVE PITTING. SUSPECT POSSIBLE FAILURE TO REPLACE OR REWORK COMPONENTS…
From FAA Service Difficulty Reports; matched by N-number and serial number.