As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERNAL FUSELAGE SKIN DENTED BS 660-680 BETWEEN S25 - 26L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REMOVED DAMAGE IAW SRM 53-00-01 FIG 201 REPAIR 7. NO CRACKS FOUND AROUND DAMAGED AREA, FABRICATED REPAIR PARTS IAW SRM 53-00-01 REPAIR 7 FIG 201 P 201 STEPS 4-10, PG 203 TABLE II. INSTALLED ALL REPAIR PARTS IAW SRM 53-00-01 FIG 201 REPAIR 7 AND DWG 143N3691. MAJOR REPAIR.