SR20-G2-Pitch Trim System

Would anyone be able to help with the followings please:

The earlier SR20 G2 made use of a pitch trim motor for both autopilot and the manual trim system.

The pitch trim motor at the back of the aircraft is connected to an “ACTUATION ARM” which is then connected to a Rod end.

My question is has anyone got any access to a reference manual that can specify how tight or loose the nut and bolt that keep the “actuation arm” and the “rod end” should be and also how much free play within the “Rod End” is allowed.

part no for: actuation arm is: 14910-001 and Rod end: 11314-003.