diff --git a/Systems/a320-aerodynamics.xml b/Systems/a320-aerodynamics.xml
index 36ae4f45..e0fb3535 100644
--- a/Systems/a320-aerodynamics.xml
+++ b/Systems/a320-aerodynamics.xml
@@ -28,7 +28,7 @@
 						-0.64 -1.0312
 						-0.25 -0.9379
 						 0.00  0.1494
-						 0.25  1.6072
+						 0.25  1.6272
 						 0.60  1.0305
 						 0.88  0.6415
 						 1.05  0.2294
@@ -46,7 +46,7 @@
 				<property>metrics/Sw-sqft</property>
 				<property>velocities/q-aero-rad_sec</property>
 				<property>aero/ci2vel</property>
-				<value>6.5404</value>
+				<value>6.9404</value>
 			</product>
 		</function>
 		
@@ -100,10 +100,10 @@
 					<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
 					<tableData>
 						0.000  0.0000
-						0.290  0.0648
-						0.596  0.1017
-						0.645  0.2404
-						1.000  0.3066
+						0.290  0.0948
+						0.596  0.1617
+						0.645  0.2704
+						1.000  0.3466
 					</tableData>
 				</table>
 			</product>
@@ -118,9 +118,9 @@
 					<independentVar lookup="row">fcs/slat-pos-norm</independentVar>
 					<tableData>
 						0.000  0.0000
-						0.666  0.1734
-						0.814  0.2509
-						1.000  0.3113
+						0.666  0.2334
+						0.814  0.2809
+						1.000  0.3323
 					</tableData>
 				</table>
 			</product>
@@ -611,7 +611,7 @@
 				<property>metrics/Sw-sqft</property>
 				<property>metrics/bw-ft</property>
 				<toradians><property>hydraulics/rudder/final-deg</property></toradians>
-				<value>0.053</value>
+				<value>0.067</value>
 			</product>
 		</function>
 	
diff --git a/revision.txt b/revision.txt
index d757c6b8..032fb5c3 100644
--- a/revision.txt
+++ b/revision.txt
@@ -1 +1 @@
-4654
\ No newline at end of file
+4655
\ No newline at end of file