diff --git a/src/main/config/config.c b/src/main/config/config.c
index d476a6ed7d..efc8865ebb 100755
--- a/src/main/config/config.c
+++ b/src/main/config/config.c
@@ -133,7 +133,7 @@ static uint32_t activeFeaturesLatch = 0;
 static uint8_t currentControlRateProfileIndex = 0;
 controlRateConfig_t *currentControlRateProfile;
 
-static const uint8_t EEPROM_CONF_VERSION = 114;
+static const uint8_t EEPROM_CONF_VERSION = 115;
 
 static void resetAccelerometerTrims(flightDynamicsTrims_t *accelerometerTrims)
 {
@@ -148,13 +148,13 @@ static void resetPidProfile(pidProfile_t *pidProfile)
 
     pidProfile->P8[ROLL] = 40;
     pidProfile->I8[ROLL] = 30;
-    pidProfile->D8[ROLL] = 18;
+    pidProfile->D8[ROLL] = 23;
     pidProfile->P8[PITCH] = 40;
     pidProfile->I8[PITCH] = 30;
-    pidProfile->D8[PITCH] = 18;
+    pidProfile->D8[PITCH] = 23;
     pidProfile->P8[YAW] = 100;
     pidProfile->I8[YAW] = 50;
-    pidProfile->D8[YAW] = 10;
+    pidProfile->D8[YAW] = 12;
     pidProfile->P8[PIDALT] = 50;
     pidProfile->I8[PIDALT] = 0;
     pidProfile->D8[PIDALT] = 0;
diff --git a/src/main/flight/pid.c b/src/main/flight/pid.c
index 48986f5fdf..a85a95bcbe 100644
--- a/src/main/flight/pid.c
+++ b/src/main/flight/pid.c
@@ -318,7 +318,7 @@ static void pidRewrite(pidProfile_t *pidProfile, controlRateConfig_t *controlRat
             delta = filterApplyPt1(delta, &DTermState[axis], pidProfile->dterm_cut_hz, dT);
         }
 
-        DTerm = (delta * 3 * pidProfile->D8[axis] * PIDweight[axis] / 100) >> 8; // Multiplied by 3 to match old scaling
+        DTerm = (delta * 2 * pidProfile->D8[axis] * PIDweight[axis] / 100) >> 8; // Multiplied by 2 to approximately match old scaling
 
         // -----calculate total PID output
         axisPID[axis] = PTerm + ITerm + DTerm;