As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT HAND OUTBOARD FLAP INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE CORRODED (INBOARD SUPPORT). REMOVED CORROSION IAW DACCMM 57-52-02. ETCHED AND PEENED IAW DACCMM PERCENT &-52-02 AND 20-11-02. FABBED BUSHING IAW DACCMM 57-52-02 AND EA8-5750-81472. CAD PLATED BUSHING IAW QQ-P- 416TC AT BY OUTSIDE VENDOR PO NR 460364, THEN INSTALLED IAW DACCMM 57-52-02 FINAL HONED BUSHING TO A BORE OF .8752 IAW DACCMM 57-52-02 USING TOOL TWS8725 DATE 6-18-05.