Comment Re:MCAS Purpose (Score 5, Informative) 131
Do you have an explanation as to why they tied the electric override to autopilot/mcas? This seems to be the root cause, the pilots simply couldn't overcome the forces to trim manually. And for whatever reason the MAX ties electric control to auto/mcas. Previous 737s didn't do this and as the physical labeling on the controls reflect this change it was obviously done for a reason.
I'm not entirely sure what you mean by this. The stab trim motor uses electric power to spin the wheel and move the stab trim. The autopilot and a couple other stability systems move that wheel frequently throughout the flight on all 737s. Aside from using the handles on the wheel and manually spinning it, there is no other way to move the stabilizer. MCAS is just an additional system on the Max that has an input into the stab trim motor. As it was originally designed, when MCAS activates, it moves the stab trim a certain number of units nose down and will stop. If the pilot then uses the switches on the yoke to move the stab trim the other way, in other words, trimming back to nose-up, the software governing MCAS resets its initial index to the point that it originally moved the trim to. Let's say MCAS activates when the trim is currently set at 6 units. It activates, spinning the wheel nose down to 3 units. The pilot uses the switches on the yoke to spin the trim back to 6 units. MCAS still senses a stall, so a couple seconds after the pilot releases the yoke switches, MCAS activates again. But this time, its little brain is now set to consider 3 units as its starting point, so it spins the wheel back to 3 units and then goes beyond, and now gets all the way to the stops. Why Boeing programmed it this way, you'd have to ask them. I've read that the software update removes this index-resetting so it won't be as likely to wind up trimming the nose fully nose down. Depending on the airspeed, the airplane can be flown like this, but it's really difficult. You'd have the yoke all the way back just to maintain altitude, and it would take a lot of strength to do it. Because of the aerodynamic force you're putting on the stabilizer like this, it would be very difficult, if not impossible, to use the handle on the trim wheel to manually spin that wheel back to nose up. Assuming you have enough altitude to play with, the proper thing to do, once you've disabled the electric trim motor, is accept a little altitude loss, relax the back-pressure on the yoke and let the nose fall, control the airspeed so you don't get too much aerodynamic force on the stabilizer, and now you'd be able to manually spin the wheel with the handle. You might have to do two or three up and down maneuvers like this to get the stab trim spun back to nose-up enough to really regain complete control over the airplane. This would be the case on any 737, including the Max, regardless of what system put the airplane into that full-nose-down trim.