Nearly every claim in this post is factually wrong. This person apparently knows nearly nothing about aircraft flying characteristics, other than buzzwords.
I am a degreed aerospace engineer working in flight test for over 30 years and I have tested large commercial/passenger-class aircraft, including deliberately-induced Dutch rolls for test purposes. I have sat in the cockpit behind pilots executing these Dutch roll maneuvers intentionally. I personally joined a flight test team that had a crash a few years before, due to a Dutch roll event during flight test in the early 1990s. I also edited the US Naval Test Pilot School handbook FTM-103 "Fixed-Wing Stability and Control Theory and Flight Test Techniques" in 2019-2021. So I'm working with definitive expertise acknowledged in my field.
Some facts.
1) The proper term is "Dutch roll", uppercase, not lowercase, just like "American flag" not "american flag."
2) Dutch roll has absolutely NOTHING to do with the wings alternately stalling. Zero. Nada. Its cause is more subtle and would take a few pages to explain; go look up section 5.2.2.3 of the USNTPS FTM-103 flight test manual (which I edited) if you want the math. A wing stall MIGHT occur AS A RESULT of Dutch roll if you cause such a very large Dutch roll at a very low speed, but I've never seen that happen in hundreds of flight test events, some of which were done with me in the airplane. And even if the wing DOES stall, it's not a big deal most of the time; I've also done many stall tests. We're careful and we know what will happen, but most stalls are immediately recoverable (because all airplanes are carefully designed to recover quickly and gracefully from an inadvertent stall).
3) There is no "triplet" input to "get out of" Dutch roll. It is a natural oscillatory motion and will persist until a "yaw damper" is engaged to counter it automatically; it's almost impossible to manually damp out because it will simply recur naturally. Even if you put in a complicated input to damp it out, it'll start again just due to small gusts. No pilot wants to spend all their time fighting Dutch roll; that's why aircraft have yaw damping systems.
4) Dutch roll absolutely CAN shear off the vertical tail if it becomes large enough. Look up the crash of American Airlines AA587 in 2001. And I personally worked on a program that crashed a Navy S-3B test airplane in 1991 from Dutch roll testing when the vertical tail failed due to bad test technique (deliberately overdriving the Dutch roll mode beyond the limits of the vertical tail strength, due to miscalculation of the tail strength limits). I personally have on my desk the control stick that was recovered by wreckage divers from the bottom of the Chesapeake Bay to remind me of that failure. That crash still informs Navy flight testing practices today.
5) But in normal operation with a properly-functioning control system and absent extreme pilot inputs, Dutch roll will never become large enough to cause a failure; all aircraft are designed with sufficient stability to not reach this point without a control system input (either deliberate or due to a hardover rudder input). It is, however often a nuisance residual motion which can be annoying or nauseating.
6) Dutch rolls not exactly a "very slow" oscillation. Slow, but not VERY slow. In most large aircraft, its period is about 5-6 seconds per cycle. Smaller aircraft have faster oscillations, maybe 2-3 seconds. It's easy to observe, and quite annoying.
See my root-level post here with more information about Dutch roll in general, and the actual issues in this event.