diff --git a/A320-main.xml b/A320-main.xml
index 10df1aaf..064983bb 100644
--- a/A320-main.xml
+++ b/A320-main.xml
@@ -388,29 +388,6 @@
 	<it-autoflight>
 		<config>
 			<altitude-dial-mode>0</altitude-dial-mode>
-			<roll>
-				<gain>-0.1</gain>
-				<min>-0.4</min>
-				<max>0.4</max>
-			</roll>
-			<pitch>
-				<gain>0.15</gain>
-				<min>-0.3</min>
-				<max>0.3</max>
-			</pitch>
-			<cmd>
-				<roll-kp>-0.9</roll-kp>
-				<roll-scale>1.4</roll-scale>
-				<vorloc>-2.8</vorloc>
-				<vs>0.01</vs>
-			</cmd>
-			<autoland>
-				<kp-pitch>0.035</kp-pitch>
-				<kp-rudder>-0.05</kp-rudder>
-			</autoland>
-			<rollout>
-				<kp-rudder>-0.02</kp-rudder>
-			</rollout>
 		</config>
 		<output>
 			<ap1>0</ap1>
diff --git a/Systems/fmgc-pitch.xml b/Systems/fmgc-pitch.xml
index f7dcdfb3..dee7a344 100644
--- a/Systems/fmgc-pitch.xml
+++ b/Systems/fmgc-pitch.xml
@@ -469,7 +469,6 @@
 		</enable>
 		<input>
 			<property>/it-autoflight/internal/vert-speed-fpm</property>
-			<scale>0.16667</scale>
 		</input>
 		<reference>
 			<condition>
@@ -491,7 +490,6 @@
 				</or>
 			</condition>
 			<property>/it-autoflight/internal/target-fpm</property>
-			<scale>0.16667</scale>
 		</reference>
 		<reference>
 			<condition>
@@ -501,7 +499,6 @@
 				</equals>
 			</condition>
 			<property>/it-autoflight/internal/vs</property>
-			<scale>0.16667</scale>
 		</reference>
 		<reference>
 			<condition>
@@ -527,7 +524,6 @@
 				</or>
 			</condition>
 			<property>/it-autoflight/internal/target-fpm-b</property>
-			<scale>0.16667</scale>
 		</reference>
 		<reference>
 			<condition>
@@ -537,7 +533,6 @@
 				</equals>
 			</condition>
 			<property>/it-autoflight/internal/target-fpm-c</property>
-			<scale>0.16667</scale>
 		</reference>
 		<reference>
 			<condition>
@@ -547,7 +542,6 @@
 				</equals>
 			</condition>
 			<property>/it-autoflight/internal/target-fpm-d</property>
-			<scale>0.16667</scale>
 		</reference>
 		<reference>
 			<condition>
@@ -557,7 +551,6 @@
 				</equals>
 			</condition>
 			<property>/it-autoflight/internal/nav1-rate-of-climb-fpm</property>
-			<scale>0.16667</scale>
 		</reference>
 		<output>
 			<property>/it-autoflight/internal/target-pitch-deg</property>
@@ -570,7 +563,7 @@
 						<value>6</value>
 					</not-equals>
 				</condition>
-				<property>/it-autoflight/config/cmd/vs</property>
+				<value>0.0017</value>
 			</Kp>
 			<Kp>
 				<condition>
@@ -579,7 +572,7 @@
 						<value>6</value>
 					</equals>
 				</condition>
-				<property>/it-autoflight/config/autoland/kp-pitch</property>
+				<value>0.0055</value>
 			</Kp>
 			<Ti>3.0</Ti>
 			<Td>0.0001</Td>
@@ -663,9 +656,7 @@
 		<name>System Command: Pitch Rate</name>
 		<debug>false</debug>
 		<type>gain</type>
-		<gain>
-			<property>/it-autoflight/config/pitch/gain</property>
-		</gain>
+		<gain>0.15</gain>
 		<enable>
 			<condition>
 				<or>
@@ -689,12 +680,8 @@
 		<output>
 			<property>/it-autoflight/internal/elevator-cmd</property> <!-- Inputs to the FBW Pitch Rate -->
 		</output>
-		<min>
-			<property>/it-autoflight/config/pitch/min</property>
-		</min>
-		<max>
-			<property>/it-autoflight/config/pitch/max</property>
-		</max>
+		<min>-0.3</min>
+		<max>0.3</max>
 	</filter>
 
 </PropertyList>
diff --git a/Systems/fmgc-roll-yaw.xml b/Systems/fmgc-roll-yaw.xml
index fdd3a12c..a3245236 100644
--- a/Systems/fmgc-roll-yaw.xml
+++ b/Systems/fmgc-roll-yaw.xml
@@ -13,7 +13,7 @@
  <!-- =============================================================== -->
  <!-- Lateral  Modes                                                  -->
  <!-- =============================================================== -->
- 
+
 	<pi-simple-controller>
 		<name>ROLL CONTROLLER: HDG/LNAV</name>
 		<debug>false</debug>
@@ -53,9 +53,6 @@
 		</enable>
 		<input>
 			<property>/it-autoflight/internal/heading-error-deg</property>
-			<scale>
-				<property>/it-autoflight/config/cmd/roll-scale</property>
-			</scale>
 		</input>
 		<reference>
 			<value>0</value>
@@ -64,10 +61,8 @@
 			<property>/it-autoflight/internal/target-roll-deg</property>
 		</output>
 		<config>
-			<Kp>
-				<property>/it-autoflight/config/cmd/roll-kp</property>
-			</Kp>
-			<Ki>0.0</Ki>
+			<Kp>-1.3</Kp>
+			<Ki>-0.000001</Ki>
 			<min>
 				<property>/it-autoflight/internal/bank-limit</property>
 				<scale>-1</scale>
@@ -134,9 +129,7 @@
 			<property>/it-autoflight/internal/target-roll-deg</property>
 		</output>
 		<config>
-			<Kp>
-				<property>/it-autoflight/config/cmd/vorloc</property>
-			</Kp>
+			<Kp>-2.8</Kp>
 			<Ki>-0.0001</Ki>
 			<min>
 				<property>/it-autoflight/internal/bank-limit</property>
@@ -203,9 +196,7 @@
 		<name>System Command: Roll Rate</name>
 		<debug>false</debug>
 		<type>gain</type>
-		<gain>
-			<property>/it-autoflight/config/roll/gain</property>
-		</gain>
+		<gain>-0.1</gain>
 		<enable>
 			<condition>
 				<or>
@@ -256,12 +247,8 @@
 		<output>
 			<property>/it-autoflight/internal/aileron-cmd</property> <!-- Inputs to the FBW Roll Rate -->
 		</output>   	
-		<min>
-			<property>/it-autoflight/config/roll/min</property>
-		</min>
-		<max>
-			<property>/it-autoflight/config/roll/max</property>
-		</max>
+		<min>-0.4</min>
+		<max>0.4</max>
 	</filter>
 	
  <!-- =============================================================== -->
@@ -300,7 +287,7 @@
 						</equals>
 					</and>
 				</condition>
-				<property>/it-autoflight/config/autoland/kp-rudder</property>
+				<value>-0.05</value>
 			</Kp>
 			<Kp>
 				<condition>
@@ -315,7 +302,7 @@
 						</equals>
 					</or>
 				</condition>
-				<property>/it-autoflight/config/rollout/kp-rudder</property>
+				<value>-0.02</value>
 			</Kp>
 			<Ki>0</Ki>
 		</config>
diff --git a/revision.txt b/revision.txt
index 56ac2041..b1f0448f 100644
--- a/revision.txt
+++ b/revision.txt
@@ -1 +1 @@
-4073
\ No newline at end of file
+4074
\ No newline at end of file