Originally Posted by
Callsign Kilo
Someone mentioned that the MCAS provides 10 secs of trim input when activated. Can that be correct/verified? 10 secs of trim input is massive on the 737. The stabiliser is a powerful secondary flight control and has known limitations - for example Boeing are explicit about overuse of stabiliser trim
during the approach to stall recovery. Positioning the stabiliser in such a sense can severely reduce elevator authority - was this not the contributing factor in the FlyDubai 738 crash in Rostov? Two separate variants, one without MCAS, but with the same concerns relating to pitch authority?
MCAS trims 0.27 units per second - up to 2.5 units in 10 second cycle