yep .. very good info ...
so a couple of questions.
The fault on RA # 1 was apparently noted on several occasions prior to the accident flight, I am not aware as to whether it was written up or not ( and I am not going back onto the other thread to find out ! )
IF it were written up, what is the engineering procedure and the operator procedure from the MEL ?
My guess is that the CB for RA#1 would be pulled and collared ?
TR