While the video's conclusions match with my model of the world, the testing methods don't accurately model the dynamics of a real system. It might be a relevant test, it might not be. I'm not going to take it as proof that I'm right.
My own Bearhawk happened to have about 3 degrees per side toe in when I bought it. It was a docile machine so I saw no need to mess with it. Then one day I had a gear leg fail on a benign landing. The field repair to get it out of the field and back home resulted in 15 degrees toe in on the repaired side. At that level, the 31" ABW wheels were trying to buckle underneath the aircraft as they attempted to drive toward each other. The plan had been to do a high speed taxi test before flying. Taxiing was so awful that I decided I'd be happier in the air and took off. I landed on a section of gravel back home to maximize scrub and minimize bite. The asymmetric toe resulted in a sideways crabbing behavior that was excruciatingly painful to experience for this long time taildragger pilot (learned to fly in a J-3, first solo on 16th B-day) who was strongly conditioned to keep the nose pointed in the direction of travel. Outside of that problem, the landing was uneventful. The Bearhawk (at least the larger ones) have properties that would present challenges for a C-172 pilot who hasn't had appropriate additional training, directional manners is not a problem with them.
My point? If 18 degrees of total toe in with the track 6 degrees off straight can be flown, I don't think that symmetric toe anywhere within a few degrees of straight is going to result in bad manners.