diff --git a/src/modules/vtol_att_control/standard.cpp b/src/modules/vtol_att_control/standard.cpp
index 3ae02ae227..0f90b1667c 100644
--- a/src/modules/vtol_att_control/standard.cpp
+++ b/src/modules/vtol_att_control/standard.cpp
@@ -498,7 +498,7 @@ void Standard::fill_actuator_outputs()
 
 		// pitch
 		_actuators_out_1->control[actuator_controls_s::INDEX_PITCH] =
-			_actuators_fw_in->control[actuator_controls_s::INDEX_PITCH] + _params->fw_pitch_trim;
+			_actuators_fw_in->control[actuator_controls_s::INDEX_PITCH];
 		// yaw
 		_actuators_out_1->control[actuator_controls_s::INDEX_YAW] =
 			_actuators_fw_in->control[actuator_controls_s::INDEX_YAW];
@@ -510,7 +510,7 @@ void Standard::fill_actuator_outputs()
 		if (_params->elevons_mc_lock) {
 			// zero outputs when inactive
 			_actuators_out_1->control[actuator_controls_s::INDEX_ROLL] = 0.0f;
-			_actuators_out_1->control[actuator_controls_s::INDEX_PITCH] = _params->fw_pitch_trim;
+			_actuators_out_1->control[actuator_controls_s::INDEX_PITCH] = 0.0f;
 			_actuators_out_1->control[actuator_controls_s::INDEX_YAW] = 0.0f;
 			_actuators_out_1->control[actuator_controls_s::INDEX_AIRBRAKES] = 0.0f;
 
@@ -521,7 +521,7 @@ void Standard::fill_actuator_outputs()
 
 			// pitch
 			_actuators_out_1->control[actuator_controls_s::INDEX_PITCH] =
-				_actuators_fw_in->control[actuator_controls_s::INDEX_PITCH] + _params->fw_pitch_trim;
+				_actuators_fw_in->control[actuator_controls_s::INDEX_PITCH];
 
 			_actuators_out_1->control[actuator_controls_s::INDEX_YAW] = 0.0f;
 			_actuators_out_1->control[actuator_controls_s::INDEX_AIRBRAKES] = 0.0f;