What was found
DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON FUSELAGE FRAME 227.8 FROM WL 208 TO WL 225.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON FUSELAGE FRAME 227.8 FROM WL 208 TO WL 225.