OK, anyone have anything definitive on whether or not the Stab Trim Cutouts were re-egnaged?
https://abcnews.go.com/International/damaged-sensor-ethiopian-airlines-737-max-triggered-fatal/story?id=62139860
Two aviation sources familiar with the probe told ABC News that the Ethiopian Airlines flight suffered a damaged angle-of-attack sensor upon takeoff from a bird or foreign object, triggering erroneous data and the activation an anti-stall system -- called MCAS -- sending the pitch of the plane downward and ultimately crashing into the ground.
According to the sources, the pilots did not try to electronically pull the nose of the plane up before following Boeing's emergency procedures of disengaging power to the horizontal stabilizer on the rear of the aircraft. One source told ABC News they manually attempted to bring the nose of the plane back up by using the trim wheel. Soon after, the pilots restored power to the horizontal stabilizer.
With power restored, the MCAS was re-engaged, the sources said, and the pilots were unable to regain control before the crash.
I am loathe to trust a source like CBS but I have seen this on BBC and a few others. The Prelim doesn't seem to mention this unless I missed it.
The other thing is the thrust. From the Prelim: "During takeoff roll, the engines stabilized at about 94% N1, which matched the N1 Reference recorded on the DFDR. From this point for most of the flight, the N1 Reference remained about 94% and the throttles did not move."
Strange, no? No where in the Prelim did I see any definitive statement about use of A/T. Usually autothrotttles would be engaged on takeoff. If engaged, they would surely have gone to idle when the aircraft approached VMO, right? In fact, would have retarded approaching whatever speed was in the flight guidance, like 250 below 10K or whatever was programmed. Funny there's no mention of this. Were the power levers set manually at 94% for takeoff and just left there? Enquiring minds want to know.