As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE IN SERVICE, A CRACK WAS FOUND ON FUSELAGE LONGERON 2R BETWEEN BS 1458-1475. ACCOMPLISHED A SPLICE REPAIR AND INSTALLED A 0.160" THICK STRAP. INSTALLED REPAIR IAW PROCESS STANDARD 900-5-1 NR 04. COMPLIED WITH ER/A 510485-14, REV "O".