As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND 2ND FROM THE BOTTOM IN WEB, WHERE STIFFENER ATTACHES AT STA. 246 LBL 24 HOLE DAMAGED, DAMAGE REMOVAL AT LBL 24 HOLE IS CURRENTLY 0.359" IN WEB MADE OF 0.025 7075-T6 WEB ATTACHES TO ANGLE ON FWD SIDE PN #141T5814-136. REPAIRED PER E.A.#:H-5310-T0381485 TITLED: FUSELAGE - MAINFRAME - WEB DAMAGE FLOOR BEAM STA 246.0, LBL 25 - GOUGE DAMAGE TO A FASTENER HOLE - SPLICE REPAIR. "MAJOR REPAIR"