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 RIGHT SIDE FR54 STGR44 FASTENER HOLE. ACCOMPLISHED THE WORK BY REAMING THE HOLE THIS IS CATE.B REPAIR I.A.W EA NO:6-5330- T0369235 P1, SEQ NO:000909, TITLE:FUSELAGE-PLATES & SKINS-RH JUNCTION BETWEEN LATERAL SKIN PANEL AND STRINGER S-44R AT FR54 ECCENTRIC BUSHING REPAIR-ALI 531582- 01-1A & A300-600 SRM 51-40-21-001, PARA.7, PAGE.24-50