diff --git a/docs/Settings.md b/docs/Settings.md
index 508108e97ee..0ec4bd8a69b 100644
--- a/docs/Settings.md
+++ b/docs/Settings.md
@@ -5672,19 +5672,9 @@ See tpa_rate.
 
 ---
 
-### tpa_on_yaw
-
-Throttle PID attenuation also reduces influence on YAW for multi-rotor, Should be set to ON for tilting rotors.
-
-| Default | Min | Max |
-| --- | --- | --- |
-| OFF | OFF | ON |
-
----
-
 ### tpa_rate
 
-Throttle PID attenuation reduces influence of PDFF on ROLL and PITCH of multi-rotor, PIDFF on ROLL,PITCH,YAW OF fixed_wing as throttle increases. For every 1% throttle after the TPA breakpoint, P is reduced by the TPA rate.
+Throttle PID attenuation reduces influence of P on ROLL and PITCH as throttle increases. For every 1% throttle after the TPA breakpoint, P is reduced by the TPA rate.
 
 | Default | Min | Max |
 | --- | --- | --- |