Exactly. In fact, there are two problems:
- 1: the switch is in the middle (stand bye position); the electro-pump gives hyd power when batt is on (engine not running)
-2: as long as the switch is in backword (stop), even if engine running, the elevon (flight control) stay in down position as if there's no hyd power but in this case HYD1 and HYD2 give this power....
In reality, if you forgot to posit the switch in the middle pilot will have a sonor and light alarm and the aircraft will not have an emergency hyd to the circuit n°2 and if you keep this switch on stop, main HYD POWER (circuits 1&2) will be delivered.
I think french pilots of 2/5 squadron will say the same thing...