As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RHW I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. RT AFT I/B FLAP O/B HINGE PIVOT I/B BORE CORROSION HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. ORIGINAL THK 1.2555" FINAL 1.2555" MAXIMIUM ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-5750-106570. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.