As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
1EA CRACK INDICATION WAS FOUND AT L/H SIDE HOLE 166 ON THE INTERNAL ANGLE ON FR47. (DEPTH LENGTH 16MM) ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENER HOLE REPAIRS (RH AND LH SIDES) I.A.W. EA NO: T6-5710-114908 C P5 (SEQ NO: 000896) AND A300-600 SRM 51-40-00-001 P. 138.