diff --git a/msg/versioned/AirspeedValidated.msg b/msg/versioned/AirspeedValidated.msg
index c9d9eb2a61..4e44d3e9e2 100644
--- a/msg/versioned/AirspeedValidated.msg
+++ b/msg/versioned/AirspeedValidated.msg
@@ -18,10 +18,10 @@ int8 SOURCE_GROUND_MINUS_WIND = 0  # Ground speed minus wind
 int8 SOURCE_SENSOR_1 = 1           # Sensor 1
 int8 SOURCE_SENSOR_2 = 2           # Sensor 2
 int8 SOURCE_SENSOR_3 = 3           # Sensor 3
-int8 SOURCE_SYNTHETIC = 4          # Synthetic airspeed 
+int8 SOURCE_SYNTHETIC = 4          # Synthetic airspeed
 
 float32 calibrated_ground_minus_wind_m_s  # [m/s] [@invalid NaN] CAS calculated from groundspeed - windspeed, where windspeed is estimated based on a zero-sideslip assumption
-float32 calibraded_airspeed_synth_m_s     # [m/s] [@invalid NaN] Synthetic airspeed
-float32 airspeed_derivative_filtered      # [m/s^2] Filtered indicated airspeed derivative 
-float32 throttle_filtered                 # [-] Filtered fixed-wing throttle 
-float32 pitch_filtered                    # [rad] Filtered pitch 
+float32 calibrated_airspeed_synth_m_s     # [m/s] [@invalid NaN] Synthetic airspeed
+float32 airspeed_derivative_filtered      # [m/s^2] Filtered indicated airspeed derivative
+float32 throttle_filtered                 # [-] Filtered fixed-wing throttle
+float32 pitch_filtered                    # [rad] Filtered pitch
diff --git a/src/modules/airspeed_selector/airspeed_selector_main.cpp b/src/modules/airspeed_selector/airspeed_selector_main.cpp
index 07d5fc66b3..d51875a6e0 100644
--- a/src/modules/airspeed_selector/airspeed_selector_main.cpp
+++ b/src/modules/airspeed_selector/airspeed_selector_main.cpp
@@ -742,7 +742,7 @@ void AirspeedModule::select_airspeed_and_publish()
 	airspeed_validated_s airspeed_validated = {};
 	airspeed_validated.timestamp = _time_now_usec;
 	airspeed_validated.calibrated_ground_minus_wind_m_s = NAN;
-	airspeed_validated.calibraded_airspeed_synth_m_s = NAN;
+	airspeed_validated.calibrated_airspeed_synth_m_s = NAN;
 	airspeed_validated.indicated_airspeed_m_s = NAN;
 	airspeed_validated.calibrated_airspeed_m_s = NAN;
 	airspeed_validated.true_airspeed_m_s = NAN;
@@ -764,7 +764,7 @@ void AirspeedModule::select_airspeed_and_publish()
 		airspeed_validated.calibrated_airspeed_m_s = _ground_minus_wind_CAS;
 		airspeed_validated.true_airspeed_m_s = _ground_minus_wind_TAS;
 		airspeed_validated.calibrated_ground_minus_wind_m_s = _ground_minus_wind_CAS;
-		airspeed_validated.calibraded_airspeed_synth_m_s = get_synthetic_airspeed(airspeed_validated.throttle_filtered);
+		airspeed_validated.calibrated_airspeed_synth_m_s = get_synthetic_airspeed(airspeed_validated.throttle_filtered);
 
 		break;
 
@@ -774,7 +774,7 @@ void AirspeedModule::select_airspeed_and_publish()
 			float synthetic_airspeed = get_synthetic_airspeed(airspeed_validated.throttle_filtered);
 			airspeed_validated.calibrated_airspeed_m_s = synthetic_airspeed;
 			airspeed_validated.indicated_airspeed_m_s = synthetic_airspeed;
-			airspeed_validated.calibraded_airspeed_synth_m_s = synthetic_airspeed;
+			airspeed_validated.calibrated_airspeed_synth_m_s = synthetic_airspeed;
 			airspeed_validated.true_airspeed_m_s =
 				calc_true_from_calibrated_airspeed(synthetic_airspeed, _vehicle_air_data.rho);
 			break;
@@ -785,7 +785,7 @@ void AirspeedModule::select_airspeed_and_publish()
 		airspeed_validated.calibrated_airspeed_m_s = _airspeed_validator[valid_airspeed_index - 1].get_CAS();
 		airspeed_validated.true_airspeed_m_s = _airspeed_validator[valid_airspeed_index - 1].get_TAS();
 		airspeed_validated.calibrated_ground_minus_wind_m_s = _ground_minus_wind_CAS;
-		airspeed_validated.calibraded_airspeed_synth_m_s = get_synthetic_airspeed(airspeed_validated.throttle_filtered);
+		airspeed_validated.calibrated_airspeed_synth_m_s = get_synthetic_airspeed(airspeed_validated.throttle_filtered);
 		break;
 	}