What was found
CHECK FOUND FUSELAGE STRINGER CORRODED AT STA 740-STA 760 S25L. MADE THE REPAIR PARTS PER SRM 53-00-03 REPAIR 2 FIG 201, WET INSTALLED THE REPAIR PARTS PER SRM51-40-02. MAJOR REPAIR IAW GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CHECK FOUND FUSELAGE STRINGER CORRODED AT STA 740-STA 760 S25L. MADE THE REPAIR PARTS PER SRM 53-00-03 REPAIR 2 FIG 201, WET INSTALLED THE REPAIR PARTS PER SRM51-40-02. MAJOR REPAIR IAW GMM 6-2-100.