Regarding AH's comments above.
I understand the slats on the blue system, but with the flap lever in position 3 and assuming there is some residual hydraulic pressure to the flaps, does the system also require electrical power to lower the flaps and would the AC and DC ESS busses provide this supply?
As the pictures show, the flaps are clearly (partially) extended. Was this the result of remaining in a take off configuration, or extended subsequently ?