As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AND WEAR IN THE HINGE BOLT BORE OF THE OUTBOARD FLAP IDLER HINGE ON THE RH WING. ER/A 541841-14 ISSUED FOR REPAIR. THIS IS THE LOG PAGE THAT TRACKS THE DTA REQUIREMENTS FOR ER/A 541841-14. DTA MUST BE ACCOMPLISHED WITHIN 24 MONTHS. ENGINEERING PURPOSES ONLY. ASSOCIATED ER/A 00-541841 ADDED FOR AC 9524. ** REDEFERRED LOG TO QC, ESTAB MONITOR INSPECTION; ** ER/A 541841-14 REV A IS CURRENT. DTA RESTRICTION MODIFIED FROM 365 DAYS TO 60,000 CYCLES. DTI STAGE III RESTRICTION. (LP #2246647)