What was found
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOBEAM CORROSION AROUND CLIP NUT HOLES AT BS 344 LBL 7, 10, 12 AND BL 0, ON FWD AND AFT FLANGES. REPLACED T-CAP PER BOEING SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOBEAM CORROSION AROUND CLIP NUT HOLES AT BS 344 LBL 7, 10, 12 AND BL 0, ON FWD AND AFT FLANGES. REPLACED T-CAP PER BOEING SRM.