What was found
DURING INSPECTION, FOUND CORROSION ON SUPPORT ANGLE IN AFT. FUSELAGE UNDERFLOOR LOCATED AT FRAME 66 STRINGER 25R. REPLACED THE SUPPORT ANGLE IAW SRM 51-72-11 AND DWG D53480062.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND CORROSION ON SUPPORT ANGLE IN AFT. FUSELAGE UNDERFLOOR LOCATED AT FRAME 66 STRINGER 25R. REPLACED THE SUPPORT ANGLE IAW SRM 51-72-11 AND DWG D53480062.