As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INITIAL CLIMB THE ENGINE 1 INDICATES LOW OIL QUANTITY, SHOWING 3 IN TOTAL . WORK PERFORMED IAW AMM 79-00-00-200-802-F00 AND OIL LEAK WAS IDENTIFIED ON OIL NOZZLE PLUG. CONSIDERING THE FINDING WORKS PERFORMED IAW AMM 70-30-01-910-802-F00: REPLAEMENT OF PACKING O-RINGS FROM "TGB OIL NOZZLE". IN ADITTION ENGINE #1 RUN UP WAS PERFORMED IAW AMM 71-00-00-700-823-F00. NO LEAKS WERE FOUND AFTER CORRECTIVE MEASURES