Airplane Description DA 62 AFM
The operating mode for the retraction of the landing gear is shown in the next figure. While
energizing the right hydraulic valve, the fluid flow in the hydraulic system is started due
to different piston areas of the landing gear cylinders, although the pressure on both sides
of the system is equal.
While the landing gear is retracted, both valves are energized and excess hydraulic fluid
on one side is drained into the tank. This configuration of the system is shown in the
following figure.
Page 7 - 16 Rev. 0 11-Jan-2019 Doc. No. 11.01.05-E
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