What was found
CORROSION ON THE CENTER WING REAR SPAR WEB, AT FUSELAGE STATION 955.10, RIGHT BODY BUTT LINE 75, JUST BELOW THE UPPER CHORD. THE WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON THE CENTER WING REAR SPAR WEB, AT FUSELAGE STATION 955.10, RIGHT BODY BUTT LINE 75, JUST BELOW THE UPPER CHORD. THE WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.