As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERNAL FUSELAGE SKIN HAS TWO DEEP SCRATCHES AT BS 437 ABOVE STRINGER 47L. AFTER BLENDING, THE SKIN THICKNESS WAS OUT OF LIMITS IAW SRM 53-00-01. REMOVED DAMAGE, MANUFACTURED DOUBLER & FILLERS & INSTALLED REPAIR IAW SRM 53-00-01 REPAIR 6. ALL FASTENER HOLES WERE NOT ZERO TIMED DUE TO EDGE MARGIN CONCERNS.