What was found
AFTER DEPARTURE, THE A-SYSTEM HYDRAULIC QUANTITY DECREASED TO .25 GALLONS AND STABILIZED. FOUND RETURN LINE FOR THE NR 13 SPOILER ACTUATOR LEAKING AT THE B-NUT, TIGHTENED B-NUT AT ACTUATOR. RAN HYDRAULIC PUMPS AND NO LEAKS WERE NOTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER DEPARTURE, THE A-SYSTEM HYDRAULIC QUANTITY DECREASED TO .25 GALLONS AND STABILIZED. FOUND RETURN LINE FOR THE NR 13 SPOILER ACTUATOR LEAKING AT THE B-NUT, TIGHTENED B-NUT AT ACTUATOR. RAN HYDRAULIC PUMPS AND NO LEAKS WERE NOTED.