diff --git a/src/lib/npfg/DirectionalGuidance.cpp b/src/lib/npfg/DirectionalGuidance.cpp
index 4c19c82366..72a06568d9 100644
--- a/src/lib/npfg/DirectionalGuidance.cpp
+++ b/src/lib/npfg/DirectionalGuidance.cpp
@@ -71,7 +71,6 @@ DirectionalGuidance::guideToPath(const Vector2f &curr_pos_local, const Vector2f
 	// must be called before trackErrorBound() as it updates time_const_
 	adapted_period_ = adaptPeriod(ground_speed, airspeed, wind_speed, track_error,
 				      path_curvature, wind_vel, unit_path_tangent, feas_on_track_);
-	//const float p_gain = pGain(adapted_period, damping_);
 	_time_const = timeConst(adapted_period_, damping_);
 
 	// track error bound is dynamic depending on ground speed
diff --git a/src/modules/fw_lateral_longitudinal_control/FwLateralLongitudinalControl.cpp b/src/modules/fw_lateral_longitudinal_control/FwLateralLongitudinalControl.cpp
index ec904ad19c..b1857dc622 100644
--- a/src/modules/fw_lateral_longitudinal_control/FwLateralLongitudinalControl.cpp
+++ b/src/modules/fw_lateral_longitudinal_control/FwLateralLongitudinalControl.cpp
@@ -317,8 +317,6 @@ FwLateralLongitudinalControl::tecs_update_pitch_throttle(const float control_int
 	/* No underspeed protection in landing mode */
 	_tecs.set_detect_underspeed_enabled(!disable_underspeed_detection);
 
-	//updateTECSAltitudeTimeConstant(is_low_height, control_interval);
-
 	// HOTFIX: the airspeed rate estimate using acceleration in body-forward direction has shown to lead to high biases
 	// when flying tight turns. It's in this case much safer to just set the estimated airspeed rate to 0.
 	const float airspeed_rate_estimate = 0.f;