As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT IDG LEAKING 25 DROPS PER MIN RUNNING. ON SHUTDOWN THERE IS A STEADY STREAM OF OIL UNTIL SHAFT CAVITY EMPTIES. REMOVED RT IDG. CIRCUIT BREAKER 'R IDG DISC' PULLED AT LOCATION 'J2' ON P210 PANEL. REPLACED THE NR 2 ENGINE IDG. ALSO REPLACED THE IDG DRIVE SEAL. SYSTEM CKS NORMAL AFTER ENGINE RUN.