As I said this mindless yanking back of the control column to maintain this rate of rotation at any cost is completely unnecessary. Rather than maintaining the rate of rotation at 3 degree per second through the whole manoeuvre, simply reduce the rate while the the attitude is passing through 10 - 12 degrees. It will only increase the time taken to reach the take-off attitude by a second or two. Big deal. It will also prevent a tail scrape.
So Boeing got it wrong eh? What ever happened to just doing it the way the manufacturer tells us how to do it?