What was found
DURING INSPECTION, FOUND CORROSION WAS FOUND ON STRINGER 36R FRAME 58+14. REPAIRED THE STRINGER IAW SRM 53-00-13, PARA 4.A FIG 201, SHEET 2 AND DWG E53470330.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND CORROSION WAS FOUND ON STRINGER 36R FRAME 58+14. REPAIRED THE STRINGER IAW SRM 53-00-13, PARA 4.A FIG 201, SHEET 2 AND DWG E53470330.