Automated trim/stability augmentation has been part of the computer system since the 737 Classic, and has always had full manual reversion. MCAS was just another trigger algorithm for the same basic software and hardware, and all the manual reversion systems were still in place.Thermalator wrote: Sun Nov 10, 2019 5:24 pmg....then Boeing decided to break that tradition/philosphy with MCAS & screwed the pooch bigtime.
From a pilots point of view, the only difference was that a failure of the other automated trim systems would result in continuous runaway trim, while some MCAS failure modes would result in an intermittent runaway trim.
(Oops - one other functional change - MCAS bypasses the column cutout - which is quite important from a pilots point of view, as in some existing trim runaway situation, any significant column movement would stop the trim too.)