What was found
PREVIOUS REPAIR OF FUSELAGE SKIN BETWEEN BS 120 TO 133 AND LONGERONS 24RT TO 25RT. WAS FOUND REPAIRED SRM 53-04, FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PREVIOUS REPAIR OF FUSELAGE SKIN BETWEEN BS 120 TO 133 AND LONGERONS 24RT TO 25RT. WAS FOUND REPAIRED SRM 53-04, FIG 2.