What was found
STRINGER 24S CORRODED FROM FS 136 TO X232. DERIVETED STRINGER 24S FROM FS 116 TO FS 232 IAW SRM 51-42-05. DRILLED & INSTALLED NEW STRINGER 24S BETWEEN FS 116 AND FS 232 IAW SRM 51-42-05, 51-40-15, 51-25-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRINGER 24S CORRODED FROM FS 136 TO X232. DERIVETED STRINGER 24S FROM FS 116 TO FS 232 IAW SRM 51-42-05. DRILLED & INSTALLED NEW STRINGER 24S BETWEEN FS 116 AND FS 232 IAW SRM 51-42-05, 51-40-15, 51-25-10.