As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BODY STATION 1640 FUSELAGE FRAME WEB AT STRINGER S-14 AT LH. CRACK INDICATION NOTED FOR BOTTOM INBOARD HOLE COMPLIED WITH EA# F-5310-T0359452 P1. FUSELAGE-MAINFRAME-CRACK INDICATION AT STA 1640 FUSELAGE FRAME WEB, S-14L AT LOWER INBOARD HOLE LOCTION- TEMPORARY FREEZE PLUG REPAIR. CAT "C" MAJOR REPAIR