What was found
STRINGER CLIP S25S IS CORRODED AT BS 236. REMOVED STRINGER CLIP AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-03-00-01, 51-42-05-02-01 REV 12. INSTALLED NEW STRINGER CLIP SRM 51-42-05-02-01 REV 12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRINGER CLIP S25S IS CORRODED AT BS 236. REMOVED STRINGER CLIP AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-03-00-01, 51-42-05-02-01 REV 12. INSTALLED NEW STRINGER CLIP SRM 51-42-05-02-01 REV 12.