ATR42 - Pitch/Power Couple?

[ATR Newby]

Can anyone please tell me how the pitch/power couple is arranged on the ATR42?

I am curious due to it's high-wing & high-mounted engine design:-

Which way does it pitch when power is applied & conversely, when power is reduced?

Is it the same as, or the opposite to, a low-mounted engine design such as your typical Boeing?

Thanks...