What was found
(CAN) IN NR 2 ENGINE NACELLE, FLIGHT VALVE SPOILER DUMP VALVE HYDRAULIC LINE LEAKING THROUGH PIN HOLES AT BEND RADIUS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) IN NR 2 ENGINE NACELLE, FLIGHT VALVE SPOILER DUMP VALVE HYDRAULIC LINE LEAKING THROUGH PIN HOLES AT BEND RADIUS.