diff --git a/aviary/subsystems/aerodynamics/flops_based/test/test_tabular_aero_group.py b/aviary/subsystems/aerodynamics/flops_based/test/test_tabular_aero_group.py
index 1fb1e5845..e02ae2985 100644
--- a/aviary/subsystems/aerodynamics/flops_based/test/test_tabular_aero_group.py
+++ b/aviary/subsystems/aerodynamics/flops_based/test/test_tabular_aero_group.py
@@ -271,7 +271,7 @@ def test_parameters(self):
 
         assert_near_equal(
             prob.get_val("traj.cruise.rhs_all.drag", units='lbf')[0],
-            9896.0,
+            9907.0,
             1.0e-3
         )