As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 'B-3' CHECK PER HB5301, FOUND .125 INCH VERTICAL CRACK FROM RIVET HOLE AT AFT FUSELAGE EXTERIOR SKIN RT SIDE AT FS848, WL170, LBL68. REPAIRED INNER RIB IAW SMP583 FIG. 53-50-10. EXTERIOR SKIN REPAIRED IAW SMP583 FIG. 51-140-12. N/R 2053.