diff --git a/modules/aerodyn/src/AirfoilInfo.f90 b/modules/aerodyn/src/AirfoilInfo.f90
index cc96479a3a..80fc2939c6 100644
--- a/modules/aerodyn/src/AirfoilInfo.f90
+++ b/modules/aerodyn/src/AirfoilInfo.f90
@@ -1043,10 +1043,12 @@ SUBROUTINE CalculateUACoeffs(CalcDefaults,p,ColCl,ColCd,ColCm,ColUAf,UA_f_cn)
                         fullySeparate = p%Coefs(Row,ColCl) / 2.0_ReKi                      ! Eq. 61
                      end if
                   
+                     p%Coefs(Row,col_fs) = fullySeparate
+
                   end if
                
                   p%Coefs(Row,ColUAf) = f_st
-                  p%Coefs(Row,col_fs) = fullySeparate
+
                end do
                
                ! Compute variables to help x3 state with +/-180-degree wrap-around issues