This N-number isn't registered right now. Below is its last known registration, canceled Jan 31, 2020.
Safety record in brief:1 NTSB accident (substantial damage, Oct 2018)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 failure of the left main landing gear due to fatigue cracking of a bolt that initiated at a corrosion pit, which formed in the absence of a required protective cadmium coating.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR19LA020)
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 (182G) |
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 ACCIDENT INVESTIGATION OF N3267S, THE FORWARD OUTBOARD ATTACH BOLT P/N NAS147-34 HAD A PREEXISTING CRACK AT THE BEGINNING OF THE THREADS FROM THE SHAFT WITH THE PRESENCE OF CORROSION. THIS LEAD TO AN INSTANTANEOUS FAIL OF THE BOLT UPON LANDING AND SPRING GEAR SEPARATION. AIRCRAFT EQUIPPED…
From FAA Service Difficulty Reports; matched by N-number and serial number.