What was found
UPPER FUSELAGE SKIN HAS CORROSION BS 1005 - BS 1016, STRINGER 3L TO 3R. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE IN LIMITS IAW SRM 53-00-01-1A-1 TREATED AND PRIME IAW SRM 51-20-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER FUSELAGE SKIN HAS CORROSION BS 1005 - BS 1016, STRINGER 3L TO 3R. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE IN LIMITS IAW SRM 53-00-01-1A-1 TREATED AND PRIME IAW SRM 51-20-01.