As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON SUPPORT ANGLE AT THE AFT LEFT CORNER OF THE INNER KEEL BEAM AREA ACCESSED THRU PANEL 139FZ. REMOVED CORROSION ON SUPPORT ANGLE WITHIN ALLOWABLE DAMAGE LIMITS OF SRM 53-50-12 FIGURE 101 DETAIL II AND TALE I. REMOVED .010 OF MATERIAL, ORIGINAL THICKNESS .160. TREATED AND PRIMED AREA IN ACCORDANCE WITH AMM 51-21-04, 51-21-10. AIRCRAFT WAS GROUNDED.