If the stabilizer leading edge moves up and the rudder tab moves right, what are you trying to trim towards?

When the stabilizer leading edge moves up, it indicates an adjustment meant to increase the angle of attack, which contributes to a nose-up attitude. This adjustment helps counteract a tendency for the aircraft to descend or pitch downward.

Simultaneously, if the rudder tab moves to the right, it suggests that there's a need for right yaw correction. This is often done to counteract adverse yaw effects or to maintain coordinated flight when the aircraft is banking or experiencing a side slip.

Thus, when both the stabilizer leading edge is adjusted upwards and the rudder tab is moved to the right, the intended outcome is to trim the aircraft for a more nose-down attitude while also correcting for right yaw. This effectively allows the aircraft to maintain a more level flight path with adjustments that provide the desired stability and control, particularly if there were previously any tendencies for nose-up or leftward drift.

In this context, the appropriate trim adjustment aligns with leaning towards more nose down and more nose left, balancing the effects of both trim adjustments for optimal flight performance.