Safety record in brief:3 NTSB accidents (substantial damage at worst, latest May 2017)2 ADs may apply
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The pilot’s use of excessive speed during a right turn from the runway to the taxiway, which resulted in a loss of directional control.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for GAA17CA290)
The pilot's failure to maintain directional control during the landing, which led to a ground loop and a resultant overload failure of the right main landing gear attach points.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX98LA074)
PRIOR TO TAKEOFF THE PILOT OBSERVED AN ASYMMETRICAL DEFLECTION OF THE RUDDER/BRAKE PEDALS. UPON LANDING HE EXECUTED A RIGHT TURN TO DEPART THE RUNWAY. THE PILOT STATED THAT HE WAS UNABLE TO STOP THE RIGHT TURN AND THE AIRCRAFT GROUND LOOPED DAMAGING THE LEFT WING AND LANDING GEAR. THE PLT STATED AFTER THE ACC THAT THE LEFT BRAKE, PART #0341005-65, WAS WORN BEYOND ALLOWABLE TOLERANCES AS…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX87LA154)
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 (190)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 (190) |
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.