As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE EXTERIOR SKIN RT SIDE AT BS 1530, BETWEEN STRINGER 27 - 28, THERE IS A DEEP BLEND. DEEP BLEND FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 116 & REPAIR CARRIED OUT IAW SRM 53-00-01 FIG 201 REPAIR 16 REV 116. THIS IS CAT B REPAIR. INSPECTION THRESHOLD 16,000 FC FROM TIME OF REPAIR REQUIRED LFEC REPEAT INSPECTION AT 3,000 FC. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.