diff --git a/src/modules/fw_att_control/FixedwingAttitudeControl.cpp b/src/modules/fw_att_control/FixedwingAttitudeControl.cpp
index 7de353c8f9..be4aaf9b23 100644
--- a/src/modules/fw_att_control/FixedwingAttitudeControl.cpp
+++ b/src/modules/fw_att_control/FixedwingAttitudeControl.cpp
@@ -92,7 +92,7 @@ FixedwingAttitudeControl::vehicle_manual_poll(const float yaw_body)
 		// Always copy the new manual setpoint, even if it wasn't updated, to fill the actuators with valid values
 		if (_manual_control_setpoint_sub.copy(&_manual_control_setpoint)) {
 
-			if (!_vcontrol_mode.flag_control_climb_rate_enabled & _vcontrol_mode.flag_control_attitude_enabled) {
+			if (!_vcontrol_mode.flag_control_climb_rate_enabled && _vcontrol_mode.flag_control_attitude_enabled) {
 
 				// STABILIZED mode generate the attitude setpoint from manual user inputs
 
@@ -479,4 +479,4 @@ fw_att_control is the fixed wing attitude controller.
 extern "C" __EXPORT int fw_att_control_main(int argc, char *argv[])
 {
 	return FixedwingAttitudeControl::main(argc, argv);
-}
+}
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