What was found
DURING C-INSPECTION, FOUND UPPER RUDDER HINGE BRACKET CORRODED AT THE RIGHT AND LEFT ATTACH BOLTS. REPLACED RUDDER HINGE BRACKET IAW DC9 MAINTANCE MANUAL CHAPTERS 55-50-0 AND 20-16-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-INSPECTION, FOUND UPPER RUDDER HINGE BRACKET CORRODED AT THE RIGHT AND LEFT ATTACH BOLTS. REPLACED RUDDER HINGE BRACKET IAW DC9 MAINTANCE MANUAL CHAPTERS 55-50-0 AND 20-16-0.