Originally Posted by
grizzled
During that time, the power lever angle increased from 41% to 44%.
...
One second after the “click” sound, the aircraft was at the initiation of its last turn at 368 feet AGL, the high-pressure turbine speed (Nh) of both engines increased from 73% to 77%.
This is where I'm a bit confused: Why do the engines remain feathered, when higher thrust is commanded again?
Or is it just that it takes more time than it took for the energy of the aircraft to dissipate?