Full Go-Around Thrust Perferfomance
Hi, I've got a question I can't find an answer to.
B737NG FCOM says: A/T (if armed) engages in GA and advances thrust toward the reduced go–around N1 to produce 1000 to 2000 fpm rate of climb...With the second push of either TO/GA switch (if A/T engaged and after A/T reaches reduced go–around thrust):
• the A/T advances to the full go–around N1 limit"
The FCOM does not say what kind of performance the full go-around N1 limit should give, for eg at max landing weight, what kind of rate of climb should we expect?