What was found
(CAN)DURING WALKAROUND HYDRAULIC FLUID NOTED DRIPPING FROM #1 NACELLE. SYSTEM PRESSURIZED AND FLUID FOUND DRIPPING FROM END OF HYDRAULIC LINE AT ANTI SKID CONTROL VALVE. CRACK NEAR FLARE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN)DURING WALKAROUND HYDRAULIC FLUID NOTED DRIPPING FROM #1 NACELLE. SYSTEM PRESSURIZED AND FLUID FOUND DRIPPING FROM END OF HYDRAULIC LINE AT ANTI SKID CONTROL VALVE. CRACK NEAR FLARE.