What was found
INTERNAL FUSELAGE SKIN HAD CORROSION UNDER THE STANDOFF, AFT OF FRAME 31, BETWEEN STRINGERS 10R-11R. REPAIRED SRAS ES-531/16.9972, ISSUE B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERNAL FUSELAGE SKIN HAD CORROSION UNDER THE STANDOFF, AFT OF FRAME 31, BETWEEN STRINGERS 10R-11R. REPAIRED SRAS ES-531/16.9972, ISSUE B.