This N-number isn't registered right now. Below is its last known registration, canceled May 30, 2018.
Safety record in brief:1 NTSB accident (substantial damage, Jun 2011)1 AD 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 fatigue failure of the left main landing gear due to inadequate maintenance inspection that did not detect and correct corrosion pitting.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA11LA357)
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 (182F) |
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.
LEFT MAIN GEAR SPRING BROKE ON TAXI TO TAKEOFF. CRACK WAS LOCATED INSIDE THE SADDLE AREA WHICH PREVENTED ABILITY TO SEE CRACK THROUGH THE ACCESS PANNELS. THE ONLY WAY TO INSPECT THIS SPRING STRUT IS TO REMOVE THE GEAR STRUT FROM THE ACFT AND VISUALLY OR NDT AREA.
From FAA Service Difficulty Reports; matched by N-number and serial number.