The article "Boeing’s MCAS on the 737 Max may not have been needed at all" (The Air Current, January 10, 2021) quotes a Boeing e-mail about the 737 MAX that says (emphasis mine),
I can't comment on last time either stalled an NG.
Flaps up engineering data for straight, turning, idle & FAR power show the MAX worse than the NG in two areas ...
Greater pitchup ("harder" than the NG)
Less stickforce per gThe shape of the pitching moment curve as the airplane approaches stall is similar to NG. However the MAX extends to higher alpha, and when it does stall, it breaks more abruptly (pitchup) than NG. This effectively makes the pilots push on column, reducing forces, and resulting in an Elevator Feel Shift than [that? —cjs] is ineffective. Meaning the stick forces are light to none, resulting in unacceptable stall id.
What is "FAR power" in this context?