As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN HAS NUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT AT BS 540 -560. DAMAGE REMOVED & FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 109 AND REPAIRED IAW EA F-5330-T0302746. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.