| Decrease in a forward c.g. location, higher altitude and due to the slip stream from a propeller on an engine located forward of the wing |
| Increase during turn, increased mass and forward c.g. location |
| Increase with increased load factor, more flaps but will not increase due to the bank angle in a turn |
| Increase with increased load factor, icing conditions and an aft c.g. location |
EN 