This N-number isn't registered right now. Below is its last known registration, canceled Nov 15, 2019.
Safety record in brief:1 NTSB accident (substantial damage, Jun 2012)2 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 ensure that the landing gear was down and locked before landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN12LA387)
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 |
|---|---|---|---|
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (R182) |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (R182)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.
A NEW LIGHT WEIGHT STARTER WAS INSTALLED WHEN THE EXISTING STARTER FAILED. THE STARTER CONTACTOR WELDS ITSELF TOGETHER AFTER ABOUT 15 STARTS. 2 NEW MFG CONTACTORS WERE INSTALLED AND HAD THE SAME RESULTS. A HEAVY DUTY CONTACTOR HAS BEEN INSTALLED IAW MFG SERVICE BULLETIN. THE SUSPICION IS THAT THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.OIL COOLER TO ENGINE HOSE RUPTURED APPROXIMATELY 6 INCHES FROM FITTING. SUSPECT SOME KIND OF ACID PENETRATED THE HOSE IN ONE SPOT APPROXIMATELY 3 INCHES TO 3.50 INCHES AND DETERIORATED THE METAL AWAY. HOSE LINING FAILED ON A REAL HOT DAY AND PUMPED ALL THE OIL OVERBOARD CAUSING ENGINE TO SEIZE.
From FAA Service Difficulty Reports; matched by N-number and serial number.