What was found
DURING INSPECTION, FOUND CORROSION ON FUSELAGE INTERNAL STRUCTURE AT STRINGER 28L FRAME 67. REPAIRED IAW SRM 51-72-11 AND DWG D53480019.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND CORROSION ON FUSELAGE INTERNAL STRUCTURE AT STRINGER 28L FRAME 67. REPAIRED IAW SRM 51-72-11 AND DWG D53480019.