What was found
UPON REMOVAL OF UPPER FUSELAGE VHF ANTENNA LIGHT CORROSION FOUND ON SKIN. CORROSION REMOVED, SKIN REMAINING THICKNESS CHECKED TO PRODUCTION DWG. NDT HFEC CHECKS CARRIED OUT. REMOVED MATERIAL WITHIN SRM LIMITS MAXIMUM 0.003" 6"X1".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON REMOVAL OF UPPER FUSELAGE VHF ANTENNA LIGHT CORROSION FOUND ON SKIN. CORROSION REMOVED, SKIN REMAINING THICKNESS CHECKED TO PRODUCTION DWG. NDT HFEC CHECKS CARRIED OUT. REMOVED MATERIAL WITHIN SRM LIMITS MAXIMUM 0.003" 6"X1".