Originally Posted by
Maninthebar
My question was not to do with either accident but the circumstances for which MCAS was designed to work. Its implementation suggests that Boeing did not believe that the Pitch and Power mantra would be insufficient support to air crews if they reached "certain corners of the envelope"
Given that original mcas has it's own issues, an airspeed unreliable condition in takeoff configuration (as the cases under discussion) need to be handled with Pitch & Power until causes identified, no major changes in configuration and speed, will most likely end up in a return to dep rwy. (valid for FBW and conventional flight control system, sounds all over the cockpit increasing distraction and workload).