diff --git a/Models/A320neo-CFM.xml b/Models/A320neo-CFM.xml
index 8be7aae8..12df5cc4 100644
--- a/Models/A320neo-CFM.xml
+++ b/Models/A320neo-CFM.xml
@@ -79,7 +79,7 @@
 
 	<model>
 		<name>Horizontal Stabilizer</name>
-		<path>Aircraft/A320Family/Models/Fuselages/A320/hstab.xml</path>
+		<path>Aircraft/A320Family/Models/Fuselages/A320neo/hstab.xml</path>
 		<offsets>
 			<x-m>34.1512207</x-m>
 			<pitch-deg>0.0</pitch-deg>
@@ -88,7 +88,7 @@
 
 	<model>
 		<name>Vertical Stabilizer</name>
-		<path>Aircraft/A320Family/Models/Fuselages/A320/vstab.xml</path>
+		<path>Aircraft/A320Family/Models/Fuselages/A320neo/vstab.xml</path>
 		<offsets>
 			<x-m>32.2535728</x-m>
 		</offsets>
diff --git a/Models/A321neo-CFM.xml b/Models/A321neo-CFM.xml
index d0f94da4..d1d46405 100644
--- a/Models/A321neo-CFM.xml
+++ b/Models/A321neo-CFM.xml
@@ -78,7 +78,7 @@
 
 	<model>
 		<name>Horizontal Stabilizer</name>
-		<path>Aircraft/A320Family/Models/Fuselages/A321/hstab.xml</path>
+		<path>Aircraft/A320Family/Models/Fuselages/A321neo/hstab.xml</path>
 		<offsets>
 			<x-m>36.8212207</x-m>
 			<pitch-deg>0.0</pitch-deg>
@@ -87,7 +87,7 @@
 
 	<model>
 		<name>Vertical Stabilizer</name>
-		<path>Aircraft/A320Family/Models/Fuselages/A321/vstab.xml</path>
+		<path>Aircraft/A320Family/Models/Fuselages/A321neo/vstab.xml</path>
 		<offsets>
 			<x-m>34.9235728</x-m>
 		</offsets>
diff --git a/Systems/a319-aerodynamics.xml b/Systems/a319-aerodynamics.xml
index 318d7b8a..b30bbd88 100644
--- a/Systems/a319-aerodynamics.xml
+++ b/Systems/a319-aerodynamics.xml
@@ -82,11 +82,11 @@
 				<table>
 					<independentVar lookup="row">aero/alpha-rad</independentVar>
 					<tableData>
-						-1.57    1.260
-						-0.26    0.018
+						-1.57    1.275
+						-0.26    0.025
 						 0.00    0.008
-						 0.26    0.017
-						 1.57    1.320
+						 0.26    0.019
+						 1.57    1.322
 					</tableData>
 				</table>
 			</product>
@@ -111,8 +111,7 @@
 					<independentVar lookup="row">velocities/mach</independentVar>
 					<tableData>
 						 0.00      0.000
-						 0.79      0.000
-						 1.10      0.023
+						 1.10      0.018
 						 1.80      0.015
 					</tableData>
 				</table>
@@ -125,7 +124,7 @@
 				<property>aero/qbar-psf</property>
 				<property>metrics/Sw-sqft</property>
 				<property>fcs/flap-pos-deg</property>
-				<value> 0.00080 </value>
+				<value> 0.00110 </value>
 			</product>
 		</function>
 
@@ -155,7 +154,7 @@
 				<property>aero/qbar-psf</property>
 				<property>metrics/Sw-sqft</property>
 				<property>fcs/speedbrake-pos-norm</property>
-				<value>0.035</value>
+				<value>0.025</value>
 			</product>
 		</function>
 
diff --git a/Systems/a320-aerodynamics.xml b/Systems/a320-aerodynamics.xml
index 318d7b8a..b30bbd88 100644
--- a/Systems/a320-aerodynamics.xml
+++ b/Systems/a320-aerodynamics.xml
@@ -82,11 +82,11 @@
 				<table>
 					<independentVar lookup="row">aero/alpha-rad</independentVar>
 					<tableData>
-						-1.57    1.260
-						-0.26    0.018
+						-1.57    1.275
+						-0.26    0.025
 						 0.00    0.008
-						 0.26    0.017
-						 1.57    1.320
+						 0.26    0.019
+						 1.57    1.322
 					</tableData>
 				</table>
 			</product>
@@ -111,8 +111,7 @@
 					<independentVar lookup="row">velocities/mach</independentVar>
 					<tableData>
 						 0.00      0.000
-						 0.79      0.000
-						 1.10      0.023
+						 1.10      0.018
 						 1.80      0.015
 					</tableData>
 				</table>
@@ -125,7 +124,7 @@
 				<property>aero/qbar-psf</property>
 				<property>metrics/Sw-sqft</property>
 				<property>fcs/flap-pos-deg</property>
-				<value> 0.00080 </value>
+				<value> 0.00110 </value>
 			</product>
 		</function>
 
@@ -155,7 +154,7 @@
 				<property>aero/qbar-psf</property>
 				<property>metrics/Sw-sqft</property>
 				<property>fcs/speedbrake-pos-norm</property>
-				<value>0.035</value>
+				<value>0.025</value>
 			</product>
 		</function>
 
diff --git a/Systems/a321-aerodynamics.xml b/Systems/a321-aerodynamics.xml
index 318d7b8a..b30bbd88 100644
--- a/Systems/a321-aerodynamics.xml
+++ b/Systems/a321-aerodynamics.xml
@@ -82,11 +82,11 @@
 				<table>
 					<independentVar lookup="row">aero/alpha-rad</independentVar>
 					<tableData>
-						-1.57    1.260
-						-0.26    0.018
+						-1.57    1.275
+						-0.26    0.025
 						 0.00    0.008
-						 0.26    0.017
-						 1.57    1.320
+						 0.26    0.019
+						 1.57    1.322
 					</tableData>
 				</table>
 			</product>
@@ -111,8 +111,7 @@
 					<independentVar lookup="row">velocities/mach</independentVar>
 					<tableData>
 						 0.00      0.000
-						 0.79      0.000
-						 1.10      0.023
+						 1.10      0.018
 						 1.80      0.015
 					</tableData>
 				</table>
@@ -125,7 +124,7 @@
 				<property>aero/qbar-psf</property>
 				<property>metrics/Sw-sqft</property>
 				<property>fcs/flap-pos-deg</property>
-				<value> 0.00080 </value>
+				<value> 0.00110 </value>
 			</product>
 		</function>
 
@@ -155,7 +154,7 @@
 				<property>aero/qbar-psf</property>
 				<property>metrics/Sw-sqft</property>
 				<property>fcs/speedbrake-pos-norm</property>
-				<value>0.035</value>
+				<value>0.025</value>
 			</product>
 		</function>