In the hypothetical vertical crush down hypothesis (not actually supported by empirical observation of the video data IMO) impact of the top ductile steel-frame block into the bigger/stronger bottom ductile steel-frame block IMO should result in some deceleration of the smaller/weaker top. The "engine of the movement" of the top block down is the distortion of space called "gravity", created by the mass of the planet existing in space and the standing start acceleration on offer for the top block, from gravity, is about 32ft/s/s at around sea level.
This weird video aircraft business is about a horizontal impact of a moving vehicle into a stationary steel-frame building. The aircraft was said to be moving at a final impact velocity considerably higher than the standing start acceleration on offer to the top block through gravity of course. Nevertheless, I suggest that when an aircraft impacts and penetrates a ductile steel frame building, it should start to decelerate and disintegrate (just as I would expect the falling top block to decelerate on impact).
Now the "nose" of the aircraft is the front end of the aircraft, I hope we can agree. When the helicopter video was examined in a frame by frame manner by the "Nose Out" theorists, it was found that the "image of the nose" of the UA175 object did not decelerate during the apparent passage of the "aircraft" whilst it was hypothetically inside WTC2. If the UA175 aircraft image was therefore a computer generated image (CGI) of an aircraft (not a video of the genuine impacting material object aircraft) then the "nose out" event reappeared at precisely the correct moment in time and in precisely the correct shape for it to be the "undamaged nose". The very soft nose of a then evidently video fraudulent CGI aircraft, that did not apparently decelerate or suffer any damage from impacting and penetrating and transiting the interior of the tower. The "nose" did not accelerate whilst "inside the tower" but neither did it decelerate.
Therefore, if you wish to postulate that an engine transited the interior of the tower and the "nose out" is not the "nose" but the engine, then the "engine" (if a genuine material object) self-evidently must have exited the tower a little too soon. The engines being located under the wings further back down the aircraft than the nose. The fade to black was carried out perhaps just in time to avoid the embarrassment of not only the nose getting through the building unscathed but the wings, engines and possibly even the tail doing the same thing
(major FUBAR). This of course also means that if a genuine aircraft hit the tower in the video and the "nose out" artefact was a genuine engine instead, then the engine must have accelerated inside the tower instead of decelerating (as I would expect). For this reason I cannot accept your proposition "as any sane person might conclude, the engine did not accelerate while in the building, but just didn't decelerate as much as the other parts" as having much merit.
Here is a list of strangely different UA175 impact speeds issued from official bodies that were presumably calculated using various different bits of official video footage of the WTC2 strike:
Massachusetts Institute of Technology - 503 mph / 436 knots / M0.653
British Royal Air Force - 575 mph / 500 knots / M0.750
Federal Aviation Administration - 586 mph / 510 knots / M0.765
National Institute of Standards and Technology - 546 mph / 475 knots / M0.714
Federal Emergency Management Agency - 590 mph / 514 knots / M0.771
http://web.mit.edu/civenv/wtc/PDFfiles/Chapter III Aircraft speed.pdf
Eduardo Kausel, MIT – "the above data indicates that the terrorists flew towards the WTC close to the ground at nearly the full cruising speed of the planes, which is about 900 km/h (560 mph) at a normal altitude of 10km (33,000 feet). It is surprising that the inexperienced pilots that the terrorists were could still steer the planes at those speeds and hit their target head on. Also, considering that the air at low altitudes is much denser than that at normal cruising height, the pilots greatly exceeded Vne ("Velocity Never Exceed")
and thereby risked disintegration of the aircraft by air friction."
Ahem, cough, cough!