Safety record in brief:8 NTSB events (substantial damage at worst, latest Aug 2000)3 ADs may apply
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The pilot's selection of unsuitable terrain for landing. A factor in the accident was a hidden obstruction, and soft terrain.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC00LA099)
the pilot's inadequate compensation for wind conditions, and his failure to maintain directional control of the airplane, which resulted in a ground swerve and damage to the airplane. A factor relating to the accident was: the crosswind condition.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC97LA131)
The pilot's excessive application of the brakes during the landing roll.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC96LA114)
A FAILURE OF THE PILOT TO MAINTAIN ADEQUATE DISTANCE FROM THE TERRAIN (SNOW BANK). FLAT LIGHTING AND LOW CONTRAST CONDITIONS WERE FACTORS IN THE ACCIDENT.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC95LA003)
FUEL EXHAUSTION AS A RESULT OF THE PILOT IN COMMAND'S NOT REFUELING. A FACTOR IN THE ACCIDENT WAS THE OPERATOR/MANAGEMENT INADEQUATE FLIGHT FOLLOWING AND OPERATIONAL CONTROL OVER THE FLIGHT.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC93LA147)
THE FAILURE OF THE NO. TWO CYLINDER CONNECTING ROD DUE TO A SLIPPED (SPUN) MAIN CRANKSHAFT BEARING WHICH BLOCKED OFF THE OIL HOLE TO THE CONNECTING ROD. A FACTOR IN THE ACCIDENT WAS THE UNSUITABLE TERRAIN ON WHICH TO PERFORM A FORCED LANDING.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC93LA016)
THE IMPROPER USE OF THE FLT CONTROLS BY THE SECOND PILOT DURING LANDING ROLL. FACTORS RELATING TO THE MISHAP WERE THE ROUGH/UNEVEN SNOW COVERED TERRAIN.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC92LA067)
ACFT BOUNCED SEVERAL TIMES DURING LANDING. THE PILOT COLLAPSED SHORTLY AFTER GETTING OUT OF THE AIRPLANE. BLOOD SAMPLES, TAKEN FROM THE PILOT THREE HOURS AFTER LANDING, CONTAINED 22.1% CARBON MONOXIDE. THE LEFT ENGINE MUFFLER OVERBOARD TUBE WAS BROKEN LOOSE FROM THE MUFFLER, WHERE THE TWO ARE WELDED, ALLOWING EXHAUST GAS TO ENTER THE COCKPIT THROUGH THE HEATER SYSTEM. THE OVERBOARD TUBE HAD A…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC89IA019)
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 (A185F) |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (A185F) |
| 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.
No Service Difficulty Reports found for this airframe since 1995.