Safety record in brief:1 NTSB accident (substantial damage, Aug 2025)2 ADs may apply1 service difficulty report
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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.
Failure of the left main landing gear due to the loss of the protective paint coating and a change in the local surface finish from impermissible grinding, which resulted in fatigue cracking.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA25LA295)
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 |
|---|---|---|---|
| 2004-21-08 R1 | Aileron Control System | May 9, 2013 | Airframe (195B)Only with: Equipped with at least one P/N 0322709 or P/N 0322709-1 inboard aileron hinge bracket. |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (195B) |
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.
AIRCRAFT LH MAIN SPRING STRUT SHEARED AT THE FUSELAGE ATTACH POINT. THE SERIAL NUMBER OF THE FAILED STRUT IS 6L85, RETURNED TO SERVICE IN 2017. VISUAL INSPECTION OF THE SPRING STRUT SHOWS THAT THE CRACK HAD BEEN THERE FOR A LONG TIME, EVIDENCED BY IRON OXIDE ACROSS THE SEPARATED MATING SURFACES.…
From FAA Service Difficulty Reports; matched by N-number and serial number.