|
|
SiteMap
|
You are here: home->com_plt->H302->2.5.2.2.6.A.1
5226
If the airplane attitude remains in a new position after the elevator control is pressed forward and released, the airplane displays
| | A) neutral longitudinal dynamic stability. |
| * | B) neutral longitudinal static stability. |
| | C) positive longitudinal static stability. |
|
|
|
|
