Severe CAVOK : Apparently there is a history of the filterelement with the particular O-ring attached, which can
Quote:
collapse and migrate into the landing gear hydraulic system.
A review of the aircraft’s hydraulic system concluded that the rogue O-Ring could not have traveled from the SSV to its final location in the right main landing gear retraction/extension actuator restrictor valve.
From the latter half of
http://www.hcl.dk/graphics/Synkron-L...K_03112007.pdf
Not a bad read, I think it was the butler in the kitchen with a candle stick, but I'm happy to wait for the final report to find out