What was found
FUSELAGE SKIN DAMAGED, RIGHT SIDE, BETWEEN BS 617 & 636, STRINGERS 20R & 21R. INSTALLED CLASS III REPAIR IAW SRM 53-04-3, FIG 8, SHEET 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DAMAGED, RIGHT SIDE, BETWEEN BS 617 & 636, STRINGERS 20R & 21R. INSTALLED CLASS III REPAIR IAW SRM 53-04-3, FIG 8, SHEET 5.