What was found
DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR WEB NEXT TO FUSELAGE BETWEEN FRAMES 69 AND 70. REPLACED SUPPORT ANGLE AND WEB PER SRM 51-42-11, ARM 51-44-11, AND AIRBUS DRAWING D534-74180.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR WEB NEXT TO FUSELAGE BETWEEN FRAMES 69 AND 70. REPLACED SUPPORT ANGLE AND WEB PER SRM 51-42-11, ARM 51-44-11, AND AIRBUS DRAWING D534-74180.