As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE PYLON UPPER LINK FORWARD ATTACH POINT IS CORRODED. REMOVED NR 1 PYLON UPPER LINK AND REPLACED BUSHINGS IN THE FWD ATTACH POINT IAW AMM 51-54-03 AND SOPM 20-50-03. PNEUMATIC DUCT REMOVED FOR ACCESS AND REINSTALLED IAW AMM 36-13-01.