Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Sep 2020)2 ADs may apply
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The fatigue fracture failure of the left main landing gear U-bolt during landing, which resulted in the collapse and separation of the left main landing gear spring.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC20LA098)
THE AIR TAXI PILOT LANDED LONG AND WAS UNABLE TO STOP THE AIRCRAFT BEFORE IT RAN OFF THE RUNWAY AND CAME TO REST IN A DITCH. A 30-40 KT GUSTY CROSSWIND AND TURBULENCE EXISTED AT THE TIME. THE PILOT STATED THAT DURING THE LANDING ROLL, HE DISCOVERED THAT THE LEFT BRAKE WAS INOPERATIVE AND SUBSEQUENT EXAMINATION FOUND THE COTTER PIN MISSING FROM THE LEFT RUDDER/BRAKE PEDAL. THIS HAD ALLOWED THE…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC89LA018)
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 |
|---|---|---|---|
| 2020-21-22 | Fuselage; 55, Stabilizers | Dec 7, 2020 | Airframe (182C) |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (182C) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
No Service Difficulty Reports found for this airframe since 1995.