Critcal engine during T/o run
Hello people,
How do you explain which engine is Critical for a Twin Engine Propeller aircraft during a T/o run on the ground.
I am aware of the factors (assymentric etc.) that determine a critical engine when the aircraft is in air. But since assymetric factor does not occur during a T/o run I am really confused as to what factor determines a critical engine during T/o run.
Thnak you,
fly