What was found
(CAN)ON CLIMB #1 SYSTEM HYDRAULIC FLUID QUANTITY INDICATED LOSS OF FLUID. AIRCRAFT RETURNED TO BLOCKS. ALTERNATE GEAR LOWERING USED. EMERGENCY SERVICES CALLED OUT. LEAK CAUSED BY CHECK VALVE NOT SEATED PRO PERLY ON REFILL PANEL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN)ON CLIMB #1 SYSTEM HYDRAULIC FLUID QUANTITY INDICATED LOSS OF FLUID. AIRCRAFT RETURNED TO BLOCKS. ALTERNATE GEAR LOWERING USED. EMERGENCY SERVICES CALLED OUT. LEAK CAUSED BY CHECK VALVE NOT SEATED PRO PERLY ON REFILL PANEL.