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Kayoh@190
I don't know if airliners are routinely assigned a block altitude to climb and descend at their discretion. Without a block altitude, going 100 or 200 feet or more above cruising altitude would be a big problem with ATC. Second, I believe airliners travel much closer to the critical Mach number. Any overspeed in the descent could lead to a dangerous Mach stall.
We don't use block altitudes (well, not typically), although being a hundred feet high won't necessarily cause a problem. There are a number of things that should be cleared up with your understanding of critical mach and how we operate near it, but that's kind of a long response that's better suited for someone less lazy than me. The bottom line is that I could replicate jsstevens' test in my airliner without any trouble.
I'm guessing the reason you don't see it with an airliner is that we usually climb at a speed that is pretty close to what we use for cruise. Before I transition to mach, it's actually the exact same speed. After I transition, it's within about .02 mach, and sometimes even the same if I'm at a lighter weight. Point is, the acceleration that jsstevens is measuring is usually only a few seconds long, if there is one at all.