| Real | CL_Basic | | basic lift coefficient |
| Real | dCL_Flap | | change in lift coefficient due to flaps |
| Real | dCL_Elevator | | change in lift coefficient due to elevator |
| Real | dCL_PitchRate | | change in lift coefficient due to pitch rate |
| Real | dCL_AlphaDot | | change in lift coefficient due to aoa rate |
| Real | CD_Basic | | basic drag coefficient |
| Real | dCD_Flap | | change in drag coefficient due to flaps |
| Real | dCD_Elevator | | change in drag coefficient due to elevator |
| Real | dCY_Beta | | change in side force coefficient due to side slip angle |
| Real | dCY_RollRate | | change in side force coefficient due to roll rate |
| Real | dCl_Aileron | | change in roll moment coefficient due to aileron |
| Real | dCl_Beta | | change in roll moment coefficient due to side slip angle |
| Real | dCl_RollRate | | change in roll moment coefficient due to roll rate |
| Real | dCl_YawRate | | change in roll moment coefficient due to yaw rate |
| Real | Cm_Basic | | |
| Real | dCm_Flap | | change in pitch moment coefficient due to flaps |
| Real | dCm_Elevator | | change in pitch moment coefficient due to elevator |
| Real | dCm_PitchRate | | change in pitch moment coefficient due to pitch rate |
| Real | dCm_AlphaDot | | change in pitch moment coefficient due to aoa rate |
| Real | dCn_Aileron | | change in yaw moment coefficient due to aileron |
| Real | dCn_Rudder | | change in yaw moment coefficient due to rudder |
| Real | dCn_Beta | | change in yaw moment coefficient due to side slip angle |
| Real | dCn_RollRate | | change in yaw moment coefficient due to roll rate |
| Real | dCn_YawRate | | change in yaw moment coefficient due to yaw rate |