As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ONE EACH CRACK INDICATION WAS FOUND AT THE LT J HOLE OF THE FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 & 26 IAW AB6 NTM 51-10-01 PART 1. REWORKED THE HOLE & INSTALLED BUSHING IAW EA 6-5310-T0311900. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.