What was found
DURING C-CHECK INSPECTION, LEVEL 2 CORORSION WAS NOTED ON FUSELAGE FRAME 219.8, AT WL 220.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, LEVEL 2 CORORSION WAS NOTED ON FUSELAGE FRAME 219.8, AT WL 220.