Boeing has a maneuver to correct this, but it involves descending to reduce aerodynamic forces on the stabilizer, adjusting trim, regaining altitude, and rinse and repeat until you're back in trim.
Personally, I wouldn't want to be a passenger on a 737 without electric trim and go through that maneuver, but it's better than crashing. Basically, the 737 should be considered too old an airframe to allow for non-type-rating-changing modifications (i.e. fly-by-wire stab trim, etc).
The engines are wider than the old ones. They are also much further forward, in order to avoid being low enough to hit the pavement. (part of the engine is higher up than the underside of the wing) These differences mean that the engines can act somewhat like canards, generating lift near the front of the aircraft. The engines themselves, even when not powered, generate lift.
The lift increases as the nose rises. This means that raising the nose becomes easier the more the pilot raises the nose, which is a hazardous way for controls to operate.
If MCAS is disabled, then the airplane will fly very differently from the 737s that everyone with an existing 737 flight rating is used to.
So the plane can fly, but it'll feel different.
And that sure does seem like a problem to get back safely to the ground.
If it disables due to faulty sensors and the pilots are told it is disabled, most flights won't have to do anything different at that point. The plane will handle just like it normally does.
If there are flights that are supposed to have maneuvers that would trigger MCAS, pilots are going to need to be trained to avoid those maneuvers when MCAS is disabled.
Also, in events that 'rarely happen' one of which is approaching a stall (according to the FAA's report), is it safe to disable the system in the actual scenario when encountered? It doesn't seem so. I can't see how both "Need this system for extremely rare scenario" and "Disabling this system because scenario is extremely rare is okay" can both be true.
The benevolent interpretation is:
a) the plane being in a situation where the system is required is rare, but frequent enough that the risk wouldn't be acceptable without MCAS.
b) MCAS breaking is rare, but frequent enough that we can't allow it to fly the plane into the ground when it does (as has been demonstrated).
c) Both things happening at the same time is so exceedingly rare that a crater is an acceptable outcome, just like we accept that all engines simultaneously failing at the same time during take-off will likely result in a crash.
(compare: https://commons.wikimedia.org/wiki/File:FAA_8040.4B_Risk_mat...)
That said, I hope EASA takes a very close look instead of blindly trusting the FAA again...
> MCAS breaking is rare
This is the part I'm not particularly inclined to agree with. The scenario is no longer breaking, it's breaking OR disabling. There are a host of new conditions that will result in MCAS being disabled according to the report. Some of these conditions disable MCAS for the remainder of the flight, and the way that I read the scenarios, it's certainly possible for these conditions to stack together.
Reading the report gives the impression that the FAA is completely incompetent. They didn't specify any rate of failure or disabling of MCAS, and the 'failure scenarios' that are proposed to be carried out in the near future are lacking in exposing these disabled scenarios.
Also, the FAA stated in the report that the plane handles similar to the 737 NG when STS is disabled; however, the MCAS automation disables MCAS and STS. There is no information about the rate at which STS has been disabled in flights in NGs, and no comparison on how disabling STS during the 'near stall' portion of a 'rare event' behaves in those planes.
They wrote this long-winded document that's almost entirely devoid of meaningful factual detail. It reads like a Boeing PR piece if I've ever seen one.
My understanding is that the MCAS or something equivalent is necessary on the 737 MAX because the engines sit lower than they really should and the forward propulsion creates torque that raises the nose of the plane. Something needs to counteract that force.
If the MCAS is disabled, is the pilot able to trim the airplane manually similar to how MCAS works? Or will they have to just kinda hold the nose down with the main steering controls?