Safety record in brief:1 NTSB accident (substantial damage, Aug 2015)6 ADs may apply1 service difficulty report
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The pilot’s improper landing flare, which resulted in a hard landing and separation of the left main landing gear wheel from its strut.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA15LA372)
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 |
|---|---|---|---|
| 2023-05-16 | Reciprocating Engine Power Section | Mar 15, 2023 | Engine (IO-520-D) |
| 2022-04-04 | Reciprocating Engine Oil System | Mar 29, 2022 | Engine (IO-520-D)Only with: F&M Enterprises, Inc. or Stratus Tool Technologies, LLC oil filter adapter installed per STC SE8409SW, SE09356SC, or SE10348SC. |
| 2020-21-22 | Fuselage; 55, Stabilizers | Dec 7, 2020 | Airframe (A185F) |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (A185F) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO-520-D)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 98-23-02 | Cessna Aircraft Company 180 and 185 Series Airplanes | Dec 22, 1998 | Airframe (A185F)Only with: Airglas Engineering Company (AECI) Model LW3600-180 or LW3600-180A fixed penetration wheel skis installed per STC SA213AL. |
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.
AFTER LANDING, DURING THE LANDING ROLL THE LT MAIN GEAR WHEEL COLLAPSED. RESULTING IN DAMAGE TO THE LT WING AND LT SIDE OF FUSELAGE. DURING THE INSPECTION OF THE WHEEL ASSEMBLY, IT WAS OBSERVED THAT 2 OF THE LT GEAR WHEEL ATTACH BOLTS WHICH HAD SHEARED OFF, SHOWED SIGNS OF INTERNAL CORROSION.
From FAA Service Difficulty Reports; matched by N-number and serial number.