What was found
INSPECTION OF THE FUSELAGE FITTING LT SIDE FOUND HOLE-C CRACKED FRAME 47. REPAIRED IAW EA6-5710-T0331014 P1. MAJOR REPAIR IAW GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION OF THE FUSELAGE FITTING LT SIDE FOUND HOLE-C CRACKED FRAME 47. REPAIRED IAW EA6-5710-T0331014 P1. MAJOR REPAIR IAW GMM 6-2-100.