L & L1 good to go
EC225 no good and now L2 no good.
Pretty hard story to sell if you ask me!
Are the SUS Bars and Gearbox's that much different between lets say an L1 and an L2? I would think not.
Is it because an L2 and 225 are heavier?
Is it just Risk tolerance?
Is there a "b Omega" issue they are not talking about?
Is it because of the Articulated Head design?
Explain why if Airbus suspect a Sus Bar failure would the L and L1 be allowed to fly and the L2 and 225 not?