What was found
STRINGER TIE HARDWARE AT FR -18.25, STR 31P IS CORRODED. REMOVED HARDWARE IAW AMM 20-10-01-430-801, REV 40. INSTALLED NEW HARDWARE IAW AMM 20-10-01-430-801, REV 40.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRINGER TIE HARDWARE AT FR -18.25, STR 31P IS CORRODED. REMOVED HARDWARE IAW AMM 20-10-01-430-801, REV 40. INSTALLED NEW HARDWARE IAW AMM 20-10-01-430-801, REV 40.