What was found
A SYSTEM HYDRAULIC QUANTITY DECREASED DURING FLIGHT TO 54%. ALL A SYSTEM HYDRAULIC FLIGHT CONTROLS REMAINED NORMAL. R & R THE A/P ACTUATOR PRESSURE LINE PACKING IN THE ELEVATOR SERVO IAW AMM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A SYSTEM HYDRAULIC QUANTITY DECREASED DURING FLIGHT TO 54%. ALL A SYSTEM HYDRAULIC FLIGHT CONTROLS REMAINED NORMAL. R & R THE A/P ACTUATOR PRESSURE LINE PACKING IN THE ELEVATOR SERVO IAW AMM.