Originally Posted by
vilas
In B+Y fail both ailerons are available and since aircraft is in normal law roll control is automatic. So it may not need any speed addition for roll control. Even after gear down since in normal law Pitch control remains automatic but should need some addition for better control.
Yeah, sorry, didn't realise that both Ailerons would be operative (albeit on single actuator mode).
So then... THS will operate solely off the G Hyd. Sys. , correct?
Oh, and sorry for the questions, but any clue why the Rudder has all 3 systems working on it (G+Y+B)? Is it cause it's a vital part of the Manual Reversion??