What was found
DURING C-CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LT NR 1 SKIN PANEL BETWEEN RIBS 1 AND 2 AT THE FRONT SPAR. CORROSION REMOVAL EXCEEDED SRM LIMITS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LT NR 1 SKIN PANEL BETWEEN RIBS 1 AND 2 AT THE FRONT SPAR. CORROSION REMOVAL EXCEEDED SRM LIMITS.