This N-number isn't registered right now. Below is its last known registration, canceled Oct 13, 2016.
Safety record in brief:1 NTSB accident (substantial damage, Sep 2010)3 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 loss of engine power due to fuel exhaustion as a result of the pilot’s inadequate fuel planning.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN10LA573)
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 |
|---|---|---|---|
| 2009-10-09 R2 | Rudder Control System | Sep 12, 2011 | Airframe (152)Certain serial numbers: 150F 15061533–15064532; 150G 15064533–15064969; 150G 15064971–15067198; 150H 15067199–15069308; 150H 649; 150J 15069309–15071128; …. Only with: FA150L S/N FA1500121-FA1500261 and FA150M S/N FA1500262-FA1500336 only when equipped with FKA150-2311 and FKA150-2316. |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (152) |
| 2008-22-18 | Cessna Aircraft Company 150 Series Airplanes | Dec 9, 2008 | Airframe (152)Only with: BRS-150 Parachute System with serial number 50001 through 50006 installed via STC SA64CH. |
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.
ON ANNUAL INSPECTION FOUND LEFT VERTICAL FIN ATTACH POINT OUTBOARD EAR BROKEN OFF. ALSO FOUND A STEEL TAPERED SHIM (.018 TO .065) UNDER THE RIGHT THREE OF THE FOUR AFT FIN ATTACH FITTING BOLTS. TECH SUPPORT FOUND NO REF TO ANY SUCH PART. REMOVED SHIM AND REPLACED FIN ATTACH FITTING WITH SERVICABLE…
From FAA Service Difficulty Reports; matched by N-number and serial number.