As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) AIRCRAFT AILERONS BINDING, MUST OVER CORRECT TO MOVE AILERONS, TO MUCH FORCE NEEDED. AILERON CONTROL SYSTEM ADJUSTMENT/TEST DONE IAW AMM 27-12-00. FUSELAGE AND WING CABLE TENSIONS FOUND TO BE HIGH, ADJUSTED AS PER FIG 201 SHEETS 344. 2. REPLACED RT AILERON ASSEMBLY IAW AMM 27-12-11. REPLACED BUSHINGS OUTBOARD HINGE BEARING FITTING IAW AMM 20-19-02 PAGE 2. (TC NR 20090112012)