How are pilots expected to disable a malfunctioning MCAS in an emergency, and balance manually by trial and error the aerodynamic extravagances of the angle of attack of such unbalanced aircraft in the middle of procedures?
The user of the parent comment is remarking about time.
The aircraft can be certified without MCAS?
By what I read, MCAS is there for to avoid entering into an aerodynamic stall when the aircraft is approaching a high angle of attack, due it's using larger motors for what classical 737 was designed for. It's balancing an unbalanced aircraft using software to repeatedly adjust the horizontal stabilizer.
It is not my field, but I'm not even sure if it should be called to trim, it sounds like a euphemism for what's going on.
The user of the parent comment is remarking about time.
The aircraft can be certified without MCAS?
By what I read, MCAS is there for to avoid entering into an aerodynamic stall when the aircraft is approaching a high angle of attack, due it's using larger motors for what classical 737 was designed for. It's balancing an unbalanced aircraft using software to repeatedly adjust the horizontal stabilizer.
It is not my field, but I'm not even sure if it should be called to trim, it sounds like a euphemism for what's going on.