What was found
AT LOWER FUSELAGE STRUCTURE, CORROSION ON FRAME 88 BTW STRINGERS 27-29R. THE FRAME WAS REPLACED IAW SRM 51-43-03 AND 51-41-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT LOWER FUSELAGE STRUCTURE, CORROSION ON FRAME 88 BTW STRINGERS 27-29R. THE FRAME WAS REPLACED IAW SRM 51-43-03 AND 51-41-01.