What was found
DURING C4 CHECK FUSELAGE SECTION 45" CORROSION DAMAGE TO BULKHEAD WEB- UPPER FRAME STA 1065 S11R, S12R. REPAIR WAS PERFORMED WITH EWO 767-53-119.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C4 CHECK FUSELAGE SECTION 45" CORROSION DAMAGE TO BULKHEAD WEB- UPPER FRAME STA 1065 S11R, S12R. REPAIR WAS PERFORMED WITH EWO 767-53-119.