Tcas ra at aircraft service ceiling
Hi folks
I was wondering if someone can point me in the direction where to find some documentation regarding an RA at the aircraft service ceiling.
I know that the climb can be inhibited in response to discrete indications if the aircraft climb performance prevents it to climb at at least 1500fpm - likewise at its service ceiling.
Any more inputs - in the specific regarding tcas 2 version 7.0 - where to find official data and if the tcas that a specific airframe is mounting has such inhibition?
Many thanks.