What was found
AT SCHEDULED INSPECTION DISCOVERED SKIN CORROSION AT FS 438.250, STRINGER WL 13R. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW MFG STRUCTURAL REPAIR MANUAL 51-70-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT SCHEDULED INSPECTION DISCOVERED SKIN CORROSION AT FS 438.250, STRINGER WL 13R. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW MFG STRUCTURAL REPAIR MANUAL 51-70-06.