Back to OT.
This is a few questions I have;
Do we know how far from required stall caracteristics the aircraft is without the MCAS?
How serious is this deficiency in (pre) stall characteristics?
How much redundancy, based on the seriousness of the deficiency, will be required by the revised MCAS?
Based on the very old and limited FCC/sensor package/system layout on the 737Max, how much redundancy can feasibly be built into a revised MCAS system?
Last edited by SteinarN; 15th Mar 2019 at 19:48.