As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING DEGRADED HYDRAULIC POWER CHECK, THE PTU INDICATION WAS NOT FUCTIONING PROPERLY WHEN THE NR 2 ENGINE PUMP WAS OFF. ACFT GROUNDED. RESEATED THE CONNECTOR ON THE NR 2 ENGINE HYD PUMP. PERFORMED AN OPS TEST OF THE PTU WITH ENGINE PUMPS IAW AMM 29-23-00-710-004-A. FUNCTIONAL TESTED GOOD.