I believe we may be confusing the issue. I adjusted the tail push rod length so that at neutral (tail servo arm at 90° to the tail pushrod) the bell crank is at 90° to the boom. As you mentioned, this yields a built-in pitch (about 5°) against the main rotor torque. I maxed out the right rudder command (against the main rotor torque, CW) to the mechanical extreme. However, an equal VBar tail throw (96/96) for the left rudder command (with the main torque, CCW) leaves about 5mm of tail shaft untraveled.
I read a thread some time ago on either the BeastX or the VBar forum discussing tail blade pitch and blade stall. The numbers I remember are approximately 30° tail blade pitch against main rotor torque (CW, right rudder command) and 15° pitch with the main rotor torque (CCW, left rudder command), and to not worry about not using all the tail shaft travel. I believe VBar/VStabi even mentions that too much tail travel (tail blade pitch) can reduce tail authority.
I understand that Synergy recommends using all the mechanical tail travel on the torque tube helicopters, but the information from the different forums is conflicting.