What was found
LOSS OF NR 2 HYD FLUID IN FLIGHT. PRESSURE AT ZERO FOR MORE THAN 20 MINUTES. NR 1 HYD QUANITY DROPPED TO ZERO WHEN PARK BRAKE APPLIED. ACFT WAS BEING POSITION FOR REMOVAL OF OTBD ROLL SPOILER AND ENGINE DRIVEN PUMP.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOSS OF NR 2 HYD FLUID IN FLIGHT. PRESSURE AT ZERO FOR MORE THAN 20 MINUTES. NR 1 HYD QUANITY DROPPED TO ZERO WHEN PARK BRAKE APPLIED. ACFT WAS BEING POSITION FOR REMOVAL OF OTBD ROLL SPOILER AND ENGINE DRIVEN PUMP.