As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DEFECT SECTION 43 FUSELAGE SKIN GOUGED FROM BS414 TO BS438 AT S-20R. RESOLUTION: DAMAGE WAS TRIMMED OUT FROM BS414 TO BS438 AT STRINGER 20R. STRINGER 20R WAS FOUND CRAKCED ATHE THE AFT THREE FASTENER HOLES WHICH WAS TRIMMED AND REPAIRED. A REPLACEMENT STRINGER WAS ORDERED AND RECEIVED FOR PERMANENT REPAIR.