This N-number isn't registered right now. Below is its last known registration, canceled Apr 16, 2015.
Safety record in brief:1 NTSB accident (substantial damage, Oct 1994)4 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 DECISION TO DEPART AN AIRPORT AND CONTINUE FLIGHT WITH A KNOWN DEFICIENCIES IN EQUIPMENT. CONTRIBUTING TO THE ACCIDENT WAS THE FAILURE OF COMPANY MAINTENANCE PERSONNEL TO ADJUST THE DOWN LOCK MECHANISM PRIOR TO FLIGHT.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA95LA012)
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.
PILOT HAD A COMPLETE ELEC FAILURE AFTER TAKEOFF & RETURNED SAFELY.
From FAA Service Difficulty Reports; matched by N-number and serial number.ALTERNATOR FAILED AFTER 30 DAYS AND 54 HOURS TIS. (ELECTROSYSTEMS OVH UNIT).
From FAA Service Difficulty Reports; matched by N-number and serial number.