Matt Barrow wrote:

Ahem...
for an aircraft of ANY size, a 10 degree crab is required by an 18 kt
crosswind, for every 100 kts of approach sppeed.

This may be a little misleading. The

-- crab angle decreases with increasing TAS for a given crosswind strength.

This may suggest that the

-- crab angle increases with increasing TAS.

Yes indeed. Thanks for pointing that out.

Unless I'm missing something, it sounds like he contradicted himself or left
something out.

You're missing that "this" refers to the post he's referring.