As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RHW O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION HAND CLEANED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG. 621-622. ORIGINAL THK 1.151" FINAL 1.151" MAX. ALLOWABLE THK 1.150". BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-04 IAW REFERENCE E.A.1-5754-90387. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.