diff --git a/src/modules/fw_att_control/FixedwingAttitudeControl.cpp b/src/modules/fw_att_control/FixedwingAttitudeControl.cpp
index 676bfc1f1d..e4e64aed48 100644
--- a/src/modules/fw_att_control/FixedwingAttitudeControl.cpp
+++ b/src/modules/fw_att_control/FixedwingAttitudeControl.cpp
@@ -447,7 +447,6 @@ void FixedwingAttitudeControl::Run()
 			control_input.airspeed_min = _param_fw_airspd_stall.get();
 			control_input.airspeed_max = _param_fw_airspd_max.get();
 			control_input.airspeed = airspeed;
-			control_input.scaler = _airspeed_scaling;
 			control_input.lock_integrator = lock_integrator;
 
 			if (wheel_control) {
diff --git a/src/modules/fw_att_control/ecl_controller.h b/src/modules/fw_att_control/ecl_controller.h
index 10f525952f..cb383ccb09 100644
--- a/src/modules/fw_att_control/ecl_controller.h
+++ b/src/modules/fw_att_control/ecl_controller.h
@@ -67,7 +67,6 @@ struct ECL_ControlData {
 	float airspeed_min;
 	float airspeed_max;
 	float airspeed;
-	float scaler;
 	float groundspeed;
 	float groundspeed_scaler;
 	bool lock_integrator;