|
|
SiteMap
|
You are here: home->com_plt->H110->5.5.6.3.4.A.1
5634
The CG of an aircraft can be determined by which of the following methods?
| | A) Multiplying total arms by total weight. |
| | B) Dividing total arms by total moments. |
| * | C) Dividing total moments by total weight. |
|
|
|
|
