Spit/109 sea level speed comparisons in 1.08 beta patch

[Crumpp]

Lift limit is a new term to me

Lift limit is the aerodynamic limits of the wing. Propeller aircraft are called power producers and are aerodynamically limited at the stall point.

The lift line is the stall line.

load doesn't impact lift

Load does impact lift.....

Thrust Limit is also a new term to me

It is the thrust limited portion of our envelope. Here the aerodynamics of the wing are not the limiting factor but rather how much excess thrust the aircraft can produce.

[Glider]

Originally Posted by Crumpp

Load does impact lift.

I think you will find that load increases the lift required in a certain situation and if I remember correctly roughly doubles at 60 degree bank