The Ethiopian aircraft impacted at an exceptionally high speed. The natural pilot inclination with a descent close to the ground is to add power, with the notion that excess power over trimmed speed equates to climb performance (and yes, there is a pitching moment associated with a power increase). However, increasing power in a dive, particularly with nose-down trim and increasing nose-down trim, increases airspeed and with the increase in airspeed, even if pitch trim does not change, will result in a stronger nose down tendency.
I have used this example before; I took an interview ride with the owner of a small back country operation, in a Cessna 207. The ride was simple; takeoff with full nose-up trim, fly a truncated (200') left traffic pattern, and land. Run trim full nose down, takeoff, fly a 200' right pattern, and land. His point? Keep it slow, and the trim is manageable. What he looked for was an applicant that understood that relationship.
I don't advocate that practice, but the point of the demonstration is that even in an unusual situation involving control difficulty (CG near or past limits, trim runaway, etc), there's more to consider and more available to the pilot than raw thrust or trim; a fundamental understanding of the control relationship shows that running the airplane to a high speed (eg, max power to 600+ knots until impact) may not be the best control tactic when the controls are heavy and the airplane is getting hard to muscle around.
Many years ago in Wyoming, a crew in a C-119 Boxcar had a runaway propeller, which they were unable to feather. The crew went through a series of oscillations; the propeller would overspeed, causing a great deal of drag. The engine was still running; adding thrust caused the overspeed, reducing thrust slowed the airplane, and prevented the overspeed. What the crew did not grasp was that the overspeed was largely due to higher airspeed; if the crew had slowed the aircraft, they could have used partial power on the engine. Instead, they went through a series of oscillations and eventually put the aircraft down in the high desert. The relationship between airspeed and control issues can't be overemphasized. If the speed keeps increasing and the control difficulty gets worse, perhaps speed increase (and the factors that are contributing to it) are not the best course of action.
If indeed one has cut off power to the elevator trim due to unwanted movement, restoring that power may not be in one's best interest.
Quote:
MCAS exists for design certification purposes within a specific set of conditions in terms of automation, angle of attack, and aircraft configuration. Pitching moment due to thrust increase or reduction occurs regardless, but the pitch moment due to thrust change may be the more minor issue compared to other players in this case.Originally Posted by pacnw77
Pretty sure that reducing thrust in the Max would increase NOSE DOWN pitch -- for the same reason that MCAS exists in the first place.