Originally Posted by
vilas
Strictly this is only applicable to direct law because alternate in pitch is same as normal law. However since the speed is below VLS the ability to hold the flight path may be not that great. At two places need to hold down with thrust increase and while slat are extending. After that when speed is out of VLS a gentle but continuous pitch up till established in climb and trend arrow in control enables you perform the manoeuvre without a hiccup.
Thank you Vilas, you are correct, again
BoeingDriver99, re: THS position, that makes sense why it has a pitch up tendency as the IAS increases with the thrust increase.
I’m still learning👍