diff --git a/A320-200-IAE (changed CG).xml b/A320-200-IAE (before rewriting aerodynamics channel).xml
similarity index 93%
rename from A320-200-IAE (changed CG).xml
rename to A320-200-IAE (before rewriting aerodynamics channel).xml
index b1c32e1b..c58a33ee 100644
--- a/A320-200-IAE (changed CG).xml	
+++ b/A320-200-IAE (before rewriting aerodynamics channel).xml	
@@ -30,7 +30,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 		<z> -25.2091 </z>
 	</location -->
 	<location name="AERORP" unit="IN">
-		<x> 650.00 </x>
+		<x> 680.00 </x>
 		<y> 0 </y>
 		<z> 0.00 </z>
 	</location>
@@ -75,8 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
 	<iyz unit="SLUG*FT2">         0 </iyz>
 	<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
 
-	<!-- 	#### PB: That makes no sense, the wohle aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
-		Also: The z-axis is -41.73 unches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
+	<!-- 	#### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
+		Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
 	-->
 	<!-- location name="CG" unit="IN">
 		<! - -x> 642.122 </x- - >
@@ -85,104 +85,82 @@ YAW MOI_________3950000______23089847_______24848934
 		<z> -41.7398 </z>
 	</location -->
 	<location name="CG" unit="IN">
-		<x> 650.00 </x>
+		<x> 655.00 </x>
 		<y> 0 </y>
 		<z> 0.00 </z>
 	</location>
 
-	<pointmass name="Crew">
-		<weight unit="LBS">400</weight> <!-- MAX: 600lbs-->
+	<pointmass name="Cockpit Crew">
+		<weight unit="LBS">400</weight> <!-- MAX: 400lbs, two pilots-->
 		<location name="POINTMASS" unit="IN">
 			<x>200</x>
 			<y>0</y>
 			<z>0</z>
 		</location>
 	</pointmass>
-	<pointmass name="PAX">
-		<weight unit="LBS">19750</weight> <!-- MAX: 39500 lbs ** looks too heavy. maybe low it and give a long cilinder shape. need to do some maths-->
-		<form shape="cylinder">
-			<radius unit="M"> 2.13 </radius>
-			<length unit="M"> 24.44 </length>
-		</form>
+	<pointmass name="Cabin Crew">
+		<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
 		<location name="POINTMASS" unit="IN">
-			<x>705</x>
+			<x>696</x>
 			<y>0</y>
 			<z>0</z>
 		</location>
 	</pointmass>
-
-<!-- NEW Pointmasses Start Weights for good CG -->
-	<pointmass name="Fwd Cargo">
-		<weight unit="LBS">3750</weight> <!-- #REF-3 page 19, MAX 3402 kilograms = 7500.12616 lbs -->
-		<form shape="cylinder">
-			<radius unit="M"> 1.24 </radius>
-			<length unit="M"> 4.95 </length>
-		</form> 
-		<location name="POINTMASS" unit="IN"> 
-			<!-- #REF-1 page 88+98,
-			x= (door form nose(8.16m))-(door with(1.816m)/2)+(Cargo compartment lenght(4.953m)/2)
-			x= 9.7285 meters = 383.011811 in
-			-->
-			<x>383.01</x>
-			<y>0</y>
-			<z>-59.05</z> <!-- Aprox lower deck 1.5 meters = 59.0551181 in -->
-		</location>
-	</pointmass>
-
-	<pointmass name="Aft Cargo">
-		<weight unit="LBS">0</weight> <!-- #REF-3 page 19, MAX 4536 kilograms = 10000.1682 lbs -->
-		<form shape="cylinder">
-			<radius unit="M"> 1.24 </radius>
-			<length unit="M"> 6.6 </length>
-		</form> 
-		<location name="POINTMASS" unit="IN"> 
-			<!-- #REF-1 page 88+98,
-			x= (door form nose(22.69m))-(door with(1.816m)/2)
-			x= 21.78200 meters = 857.559055 in
-			-->
-			<x>857.55</x>
-			<y>0</y>
-			<z>-59.05</z> <!-- Aprox lower deck 1.5 meters = 59.0551181 in -->
-		</location>
-	</pointmass>
-	<pointmass name="Rear Bulk Cargo">
-		<weight unit="LBS">0</weight> <!-- #REF-3 page 19, MAX 1497 kilograms = 3300.32006 lbs -->
-		<form shape="cylinder">
-			<radius unit="M"> 1.24 </radius>
-			<length unit="M"> 2 </length>
-		</form> 
-		<location name="POINTMASS" unit="IN"> 
-			<!-- #REF-1 page 88+102,
-			x= (door form nose(22.69m))+(door with(1.816m)/2)+( Dist. between rear doors(2.19))+(Aprox to compartment center (2m))
-			x= 27.78800 meters = 1 094.01575 in
-			-->
-			<x>1094</x>
-			<y>0</y>
-			<z>-39.37</z> <!-- Aprox bulk lower deck 1 meter = 39.3700787 in -->
-		</location>
-	</pointmass>
-	<pointmass name="Engine1">
-		<weight unit="LBS">5248</weight>
-		<form shape="cylinder">
-			<radius unit="M"> 1.31 </radius>
-			<length unit="M"> 5 </length>
-		</form>
+	<pointmass name="PAX 0A (60 seats)">
+		<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
 		<location name="POINTMASS" unit="IN">
-			<x>589.735</x>	
-			<y>-226.575</y>
-			<z>-45.567</z>
+			<x>450.1711</x>
+			<y>0</y>
+			<z>0</z>
 		</location>
 	</pointmass>
-	<pointmass name="Engine2">
-		<weight unit="LBS">5248</weight>
-		<form shape="cylinder">
-			<radius unit="M"> 1.31 </radius>
-			<length unit="M"> 5 </length>
-		</form>
+	<pointmass name="PAX 0B (60 seats)">
+		<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
 		<location name="POINTMASS" unit="IN">
-			<x>589.735</x>	
-			<y>226.575</y>
-			<z>-45.567</z>
+			<x>739.5669</x>
+			<y>0</y>
+			<z>0</z>
+		</location>
+	</pointmass>
+	<pointmass name="PAX 0C (54 seats)">
+		<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
+		<location name="POINTMASS" unit="IN">
+			<x>1093.2729</x>
+			<y>0</y>
+			<z>0</z>
+		</location>
+	</pointmass>
+	<pointmass name="Cargo Hold 1">
+		<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
+		<location name="POINTMASS" unit="IN">
+			<x>383.4792</x>
+			<y>0</y>
+			<z>-29.5</z>	<!-- 1.5m and now half of it for the center point of the load -->
+		</location>
+	</pointmass>
+	<!-- Cargo Hold 2 doesn't exist, that is the center tank -->
+	<pointmass name="Cargo Hold 3">
+		<weight unit="LBS">2000</weight> <!-- MAX: 5384.414lbs -->
+		<location name="POINTMASS" unit="IN">
+			<x>849.1324</x>
+			<y>0</y>
+			<z>-29.5</z>
+		</location>
+	</pointmass>
+	<pointmass name="Cargo Hold 4">
+		<weight unit="LBS">1500</weight> <!-- MAX: 4651.754lbs -->
+		<location name="POINTMASS" unit="IN">
+			<x>931.0653</x>
+			<y>0</y>
+			<z>-29.5</z>
+		</location>
+	</pointmass>
+	<pointmass name="Cargo Hold 5">
+		<weight unit="LBS">2000</weight> <!-- MAX: 3300.320lbs -->
+		<location name="POINTMASS" unit="IN">
+			<x>1068.2634</x>
+			<y>0</y>
+			<z>0</z>	<!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
 		</location>
 	</pointmass>
 
@@ -430,6 +408,7 @@ YAW MOI_________3950000______23089847_______24848934
 </ground_reactions>
 
 <propulsion>
+
 	<engine file="v2527_a5">
 	<location unit="IN">
 		<x> 589.735 </x>
@@ -457,6 +436,7 @@ YAW MOI_________3950000______23089847_______24848934
 		</orient>
 	</thruster>
 	</engine>
+
 	<engine file="v2527_a5">
 	<location unit="IN">
 		<x> 589.735 </x>
@@ -488,7 +468,7 @@ YAW MOI_________3950000______23089847_______24848934
 
 	<tank type="FUEL">    <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
 		<location unit="IN">
-			<x> 788.4322 </x>
+			<x> 783.0709 </x>
 			<y> -574.4148 </y>
 			<z> 3.1080 </z>
 		</location>
@@ -501,11 +481,11 @@ YAW MOI_________3950000______23089847_______24848934
 	</tank>
 	<tank type="FUEL">    <!-- Left Tank (Outer) 1 -->
 		<location unit="IN">
-			<x> 737.4190 </x>
+			<x> 739.5669 </x>
 			<y> -457.4259 </y>
 			<z> -8.0898 </z>
 		</location>
-		<capacity unit="LBS"> 1548.8 </capacity><!-- need review -->
+		<capacity unit="LBS"> 1520.00 </capacity><!-- need review -->
 		<contents unit="LBS"> 154.88 </contents>
 		<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
 		<priority>2</priority>
@@ -514,12 +494,12 @@ YAW MOI_________3950000______23089847_______24848934
 	</tank>
 	<tank type="FUEL">    <!-- Left Tank (Inner) 2 -->
 		<location unit="IN">
-			<x> 630.6588 </x>
+			<x> 652.5591 </x>
 			<y> -236.2992 </y>
 			<z> -33.9470 </z>
 		</location>
-		<capacity unit="LBS"> 12186.9 </capacity><!-- need review -->
-		<contents unit="LBS"> 2437.38 </contents>
+		<capacity unit="LBS"> 11982 </capacity><!-- need review -->
+		<contents unit="LBS"> 11982 </contents>
 		<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
 		<priority>3</priority>
 		<type>JET-A1</type>
@@ -527,12 +507,12 @@ YAW MOI_________3950000______23089847_______24848934
 	</tank>
 	<tank type="FUEL">    <!-- Center Tank 3 -->
 		<location unit="IN">
-			<x> 580.9955 </x>
+			<x> 522.0473 </x>
 			<y> 0 </y>
 			<z> -47.0 </z>
 		</location>
-		<capacity unit="LBS"> 14520 </capacity><!-- need review -->
-		<contents unit="LBS"> 0 </contents>
+		<capacity unit="LBS"> 14281 </capacity><!-- need review -->
+		<contents unit="LBS"> 7260 </contents>
 		<standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
 		<priority>1</priority>
 		<type>JET-A1</type>
@@ -540,24 +520,24 @@ YAW MOI_________3950000______23089847_______24848934
 	</tank>
 	<tank type="FUEL">    <!-- Right Tank (Inner) 4 -->
 		<location unit="IN">
-			<x> 630.6588 </x>
+			<x> 652.5591 </x>
 			<y> 236.2992 </y>
 			<z> -33.9470 </z>
 		</location>
-		<capacity unit="LBS"> 12186.9 </capacity><!-- need review -->
-		<contents unit="LBS"> 2437.38 </contents>
-		<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+		<capacity unit="LBS"> 11982 </capacity><!-- need review -->
+		<contents unit="LBS"> 11982 </contents>
+		<standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
 		<priority>3</priority>
 		<type>JET-A1</type>
 		<temperature>50</temperature>
 	</tank>
 	<tank type="FUEL">    <!-- Right Tank (Outer) 5 -->
 		<location unit="IN">
-			<x> 737.4190 </x>
+			<x> 739.5669 </x>
 			<y> 457.4259 </y>
 			<z> -8.0898 </z>
 		</location>
-		<capacity unit="LBS"> 1548.8 </capacity><!-- need review -->
+		<capacity unit="LBS"> 1520 </capacity><!-- need review -->
 		<contents unit="LBS"> 154.88 </contents>
 		<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
 		<priority>2</priority>
@@ -566,7 +546,7 @@ YAW MOI_________3950000______23089847_______24848934
 	</tank>
 	<tank type="FUEL">    <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
 		<location unit="IN">
-			<x> 788.4322 </x>
+			<x> 783.0709 </x>
 			<y> 574.4148 </y>
 			<z> 3.1080 </z>
 		</location>
diff --git a/A320-200-IAE.xml b/A320-200-IAE.xml
index a10194e3..b4a32069 100644
--- a/A320-200-IAE.xml
+++ b/A320-200-IAE.xml
@@ -526,7 +526,7 @@ YAW MOI_________3950000______23089847_______24848934
 		</location>
 		<capacity unit="LBS"> 11982 </capacity><!-- need review -->
 		<contents unit="LBS"> 11982 </contents>
-		<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+		<standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
 		<priority>3</priority>
 		<type>JET-A1</type>
 		<temperature>50</temperature>
@@ -802,7 +802,9 @@ YAW MOI_________3950000______23089847_______24848934
    </aerosurface_scale>
 
 	</channel>
+
 	<channel name="Flaps">
+
 	<kinematic name="Flaps Control">
 		<input>fcs/flap-cmd-norm</input>
 		<traverse>
@@ -830,7 +832,9 @@ YAW MOI_________3950000______23089847_______24848934
 		</range>
 		<output>fcs/flap-pos-norm</output>
 	</aerosurface_scale>
+
 	</channel>
+
 	<channel name="Landing Gear">
 	<kinematic name="Gear Control">
 		<input>gear/gear-cmd-norm</input>
@@ -914,679 +918,347 @@ YAW MOI_________3950000______23089847_______24848934
 </flight_control>
 
 
-<aerodynamics>
-	<function name="aero/function/kCDge">
-		<description>Change_in_drag_due_to_ground_effect</description>
-		<product>
-			<table>
-				<independentVar>aero/h_b-mac-ft</independentVar>
-				<tableData>
-					0.0000	0.4800
-					0.1000	0.5150
-					0.1500	0.6290
-					0.2000	0.7090
-					0.3000	0.8150
-					0.4000	0.8820
-					0.5000	0.9280
-					0.6000	0.9620
-					0.7000	0.9880
-					0.8000	1.0000
-					0.9000	1.0000
-					1.0000	1.0000
-					1.1000	1.0000
-				</tableData>
-			</table>
-		</product>
-	</function>
-	<function name="aero/function/kCLge">
-		<description>Change_in_lift_due_to_ground_effect</description>
-		<product>
-			<table>
-				<independentVar>aero/h_b-mac-ft</independentVar>
-				<tableData>
-					0.0000	1.2030
-					0.1000	1.1270
-					0.1500	1.0900
-					0.2000	1.0730
-					0.3000	1.0460
-					0.4000	1.0550
-					0.5000	1.0190
-					0.6000	1.0130
-					0.7000	1.0080
-					0.8000	1.0060
-					0.9000	1.0030
-					1.0000	1.0020
-					1.1000	1.0000
-				</tableData>
-			</table>
-		</product>
-	</function>
+	<aerodynamics>
 
-	<axis name="LIFT">
-		<function name="aero/force/Lift_gain">
-			<description>Drag_at_zero_lift</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<value>0.30</value>
-			</product>
-		</function>
+		<axis name="LIFT">
 
-		<!--function name="aero/coefficient/CLalpha">
-			<description>Lift_due_to_alpha</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<table>
-				<independentVar lookup="row">aero/alpha-rad</independentVar>
-				<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
-				<tableData>
-					0.0000	1.0000	9.0000	10.0000	40.0000
-				-0.0900	-0.2200	-0.2200	-0.1200	-0.1200	0.3200
-				0.0000	0.2500	0.2500	0.3500	0.3500	0.7500
-				0.0900	0.7300	0.7300	0.8300	0.8300	1.2300
-				0.1000	0.8300	0.8300	0.9300	0.9300	1.3300
-				0.1200	0.9200	0.9200	1.0200	1.0200	1.4200
-				0.1400	1.0200	1.0200	1.1200	1.1200	1.5200
-				0.1600	1.0800	1.0800	1.1800	1.1800	1.5800
-				0.1700	1.1300	1.1300	1.2300	1.2300	1.6300
-				0.1900	1.1900	1.1900	1.2900	1.2900	1.6900
-				0.2100	1.2500	1.2500	1.3500	1.3500	1.7700
-				0.2400	1.3500	1.3700	1.4700	1.4800	1.9300
-				0.2600	1.4400	1.4700	1.5700	1.6200	2.1200
-				0.2800	1.4700	1.5100	1.6100	1.7800	2.4000
-				0.3000	1.5000	1.5600	1.6600	1.9000	2.3000
-				0.3200	1.4700	1.6100	1.6000	1.7000	2.0300
-				0.3400	1.3500	1.5000	1.4100	1.5000	1.5300
-				0.3600	1.1500	1.2000	1.2000	1.2000	1.2000
-				</tableData>
-			</table>
-			</product>
-		</function-->
-
-		<function name="aero/force/Lift_alpha">
-			<description>Lift_due_to_alpha</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>aero/function/kCLge</property>
-			<table>
-				<independentVar lookup="row">aero/alpha-rad</independentVar>
-				<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
-				<tableData>
-					0.0000	1.0000	9.0000	10.0000	40.0000
-				-0.0900	-0.2200	-0.2200	-0.1200	-0.1200	0.2500
-				0.0000	0.2500	0.2500	0.3500	0.3500	0.7500
-				0.0900	0.7300	0.7300	0.8300	0.8300	1.2300
-				0.1000	0.8300	0.8300	0.9300	0.9300	1.3300
-				0.1200	0.9200	0.9200	1.0200	1.0200	1.4200
-				0.1400	1.0200	1.0200	1.1200	1.1200	1.5200
-				0.1600	1.0800	1.0800	1.1800	1.1800	1.5800
-				0.1700	1.1300	1.1300	1.2300	1.2300	1.6300
-				0.1900	1.1900	1.1900	1.2900	1.2900	1.6900
-				0.2100	1.2500	1.2500	1.3500	1.3500	1.7700
-				0.2400	1.3500	1.3700	1.4700	1.4800	1.9300
-				0.2600	1.4400	1.4700	1.5700	1.6200	2.1200
-				0.2800	1.4700	1.5100	1.6100	1.7800	2.4000
-				0.3000	1.5000	1.5600	1.6600	1.9000	2.3000
-				0.3200	1.4700	1.6100	1.6000	1.7000	2.0300
-				0.3400	1.3500	1.5000	1.4100	1.5000	1.5300
-				0.3600	1.1500	1.2000	1.2000	1.2000	1.2000
-				</tableData>
-			</table>
-			</product>
-		</function>
-		<!--function name="aero/coefficient/CLDe">
-			<description>Lift_due_to_Elevator_Deflection</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>fcs/elevator-pos-rad</property>
-			<value>0.1930</value>
-			</product>
-		</function>-->
-		<function name="aero/force/Lift_elevator">
-			<description>Lift due to Elevator Deflection</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>fcs/elevator-pos-rad</property>
-				<value>0.1930</value>
-			</product>
-		</function>
-
-
-
-		<function name="aero/force/Lift_speedbrake">
-			<description>Delta Lift due to speedbrake</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>fcs/speedbrake-pos-norm</property>
-				<value>-0.15</value>
-			</product>
-		</function>
-
-
-  </axis>
-
-  <axis name="DRAG">
-
-		<function name="aero/force/Drag_zero_lift">
-			<description>Drag_at_zero_lift</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<value>0.016</value>
-			</product>
-		</function>
-<!--function name="aero/coefficient/CDalpha">
-			<description>Drag_due_to_alpha</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<table>
-				<independentVar lookup="row">aero/alpha-rad</independentVar>
-				<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
-				<tableData>
-					0.0000	1.0000	25.0000	40.0000
-				-0.0873	0.0041	0.0000	0.0005	0.0014
-				-0.0698	0.0013	0.0004	0.0025	0.0041
-				-0.0524	0.0001	0.0023	0.0059	0.0084
-				-0.0349	0.0003	0.0057	0.0108	0.0141
-				-0.0175	0.0020	0.0105	0.0172	0.0212
-				0.0000	0.0052	0.0168	0.0251	0.0399
-				0.0175	0.0099	0.0248	0.0346	0.0502
-				0.0349	0.0162	0.0342	0.0457	0.0621
-				0.0524	0.0240	0.0452	0.0583	0.0755
-				0.0698	0.0334	0.0577	0.0724	0.0904
-				0.0873	0.0442	0.0718	0.0881	0.1068
-				0.1047	0.0566	0.0874	0.1053	0.1248
-				0.1222	0.0706	0.1045	0.1240	0.1443
-				0.1396	0.0860	0.1232	0.1442	0.1654
-				0.1571	0.0962	0.1353	0.1573	0.1790
-				0.1745	0.1069	0.1479	0.1708	0.1930
-				0.1920	0.1180	0.1610	0.1849	0.2075
-				0.2094	0.1298	0.1746	0.1995	0.2226
-				0.2269	0.1424	0.1892	0.2151	0.2386
-				0.2443	0.1565	0.2054	0.2323	0.2564
-				0.2618	0.1727	0.2240	0.2521	0.2767
-				0.2793	0.1782	0.2302	0.2587	0.2835
-				0.2967	0.1716	0.2227	0.2507	0.2753
-				0.3142	0.1618	0.2115	0.2388	0.2631
-				0.3316	0.1475	0.1951	0.2214	0.2451
-				0.3491	0.1097	0.1512	0.1744	0.1966
-				</tableData>
-			</table>
-			</product>
-		</function-->
-		<function name="aero/force/Drag_alpha">
-			<description>Drag_due_to_alpha</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<table>
-				<independentVar lookup="row">aero/alpha-rad</independentVar>
-				<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
-				<tableData>
-					0.0000	1.0000	25.0000	40.0000
-				-0.0873	0.0041	0.0000	0.0005	0.0014
-				-0.0698	0.0013	0.0004	0.0025	0.0041
-				-0.0524	0.0001	0.0023	0.0059	0.0084
-				-0.0349	0.0003	0.0057	0.0108	0.0141
-				-0.0175	0.0020	0.0105	0.0172	0.0212
-				0.0000	0.0052	0.0168	0.0251	0.0399
-				0.0175	0.0099	0.0248	0.0346	0.0502
-				0.0349	0.0162	0.0342	0.0457	0.0621
-				0.0524	0.0240	0.0452	0.0583	0.0755
-				0.0698	0.0334	0.0577	0.0724	0.0904
-				0.0873	0.0442	0.0718	0.0881	0.1068
-				0.1047	0.0566	0.0874	0.1053	0.1248
-				0.1222	0.0706	0.1045	0.1240	0.1443
-				0.1396	0.0860	0.1232	0.1442	0.1654
-				0.1571	0.0962	0.1353	0.1573	0.1790
-				0.1745	0.1069	0.1479	0.1708	0.1930
-				0.1920	0.1180	0.1610	0.1849	0.2075
-				0.2094	0.1298	0.1746	0.1995	0.2226
-				0.2269	0.1424	0.1892	0.2151	0.2386
-				0.2443	0.1565	0.2054	0.2323	0.2564
-				0.2618	0.1727	0.2240	0.2521	0.2767
-				0.2793	0.1782	0.2302	0.2587	0.2835
-				0.2967	0.1716	0.2227	0.2507	0.2753
-				0.3142	0.1618	0.2115	0.2388	0.2631
-				0.3316	0.1475	0.1951	0.2214	0.2451
-				0.3491	0.1097	0.1512	0.1744	0.1966
-				</tableData>
-			</table>
-			</product>
-		</function>
-
-   
-		<!--function name="aero/coefficient/CDde">
-			<description>Drag_due_to_elevator_Deflection</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>fcs/mag-elevator-pos-rad</property>
-				<value>0.0500</value>
-			</product>
-		</function-->
-		<function name="aero/force/Drag_elevator">
-			<description>Drag due to Elevator Deflection</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<abs><property>fcs/elevator-pos-norm</property></abs>
-				<value>0.055</value>
-			</product>
-		</function>
-
-
-		<!--function name="aero/coefficient/CDbeta">
-			<description>Drag_due_to_sideslip</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>aero/mag-beta-rad</property>
-			<value>0.2000</value>
-			</product>
-		</function-->
-		<function name="aero/force/Drag_beta">
-			<description>Drag_due_to_sideslip</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>aero/mag-beta-rad</property>
-				<value>0.2000</value>
-			</product>
-		</function>
-
-
-		<!--function name="aero/coefficient/CDgear">
-			<description>Drag_due_to_landing_gear</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>gear/gear-pos-norm</property>
-			<value>0.0400</value>
-			</product>
-		</function-->
-		<function name="aero/force/Drag_gear">
-			<description>Drag due to gear</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>gear/gear-pos-norm</property>
-				<value>0.04</value>
-			</product>
-		</function>
-
-		<!--function name="aero/coefficient/CDspeedbrake">
-			<description>Drag_due_to_speedbrake</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>fcs/speedbrake-pos-norm</property>
-			<value>0.0400</value>
-			</product>
-		</function-->
-		<function name="aero/force/Drag_speedbrake">
-			<description>Drag due to speedbrakes</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>fcs/speedbrake-pos-norm</property>
-				<value>0.04</value>
-			</product>
-		</function>
-
-		<!--function name="aero/coefficient/CDo">
-			<description>Drag_at_zero_lift</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<value>0.016</value>
-			</product>
-		</function-->
-
-		<function name="aero/force/Drag_mach">
-			<description>Drag due to mach</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<table>
-					<independentVar lookup="row">velocities/mach</independentVar>
+			<function name="aero/force/Lift_alpha">
+				<description>Lift due to alpha</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<table>
+						<independentVar lookup="row">aero/alpha-rad</independentVar>
 						<tableData>
-						0.00      0.000
-						0.79      0.000
-						1.10      0.023
-						1.80      0.015
+							-0.20 -0.880
+							 0.00  0.500
+							 0.23  1.500
+							 0.60  0.900
 						</tableData>
-				</table>
-			</product>
-		</function>
+					</table>
+				</product>
+			</function>
 
-  </axis>
+			<function name="aero/force/Lift_flap">
+				<description>Delta Lift due to flaps</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>fcs/flap-pos-deg</property>
+					<value> 0.03500 </value>
+				</product>
+			</function>
 
-  <axis name="SIDE">
-		<!-- function name="aero/coefficient/CYb">
-			<description>Side_force_due_to_beta</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<table>
-				<independentVar>aero/beta-rad</independentVar>
-				<tableData>
-				-0.3500	0.5000
-				0.0000	0.0000
-				0.3500	-0.5000
-				</tableData>
-			</table>
-			</product>
-		</function -->
-		<function name="aero/force/Side_beta">
-			<description>Side force due to beta</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>aero/beta-rad</property>
-				<value>-1</value>
-			</product>
-		</function>
+			<function name="aero/force/Lift_speedbrake">
+				<description>Delta Lift due to speedbrake</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>fcs/speedbrake-pos-norm</property>
+					<value>-0.1</value>
+				</product>
+			</function>
 
-  </axis>
+			<function name="aero/force/Lift_elevator">
+				<description>Lift due to Elevator Deflection</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>fcs/elevator-pos-rad</property>
+					<value>0.15</value>
+				</product>
+			</function>
 
-  <axis name="ROLL">
-		<!--function name="aero/coefficient/Clb">
-			<description>Roll_moment_due_to_beta</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/bw-ft</property>
-			<table>
-				<independentVar>aero/beta-rad</independentVar>
-				<tableData>
-				-0.3500	0.0100
-				0.0000	0.0000
-				0.3500	-0.0100
-				</tableData>
-			</table>
-			</product>
-		</function-->
-		<function name="aero/moment/Roll_beta">
-			<description>Roll moment due to beta</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>metrics/bw-ft</property>
-				<property>aero/beta-rad</property>
-				<value>-0.1</value>
-			</product>
-		</function>
+		</axis>
 
+		<axis name="DRAG">
 
-		<!--function name="aero/coefficient/Clp">
-			<description>Roll_moment_due_to_roll_rate_(roll_damping)</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/bw-ft</property>
-			<property>aero/bi2vel</property>
-			<property>velocities/p-aero-rad_sec</property>
-			<value>-0.5000</value>
-			</product>
-		</function-->
+			<function name="aero/force/Drag_basic">
+				<description>Drag at zero lift</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<table>
+						<independentVar lookup="row">aero/alpha-rad</independentVar>
+						<tableData>
+							-1.57    1.500
+							-0.26    0.026
+							 0.00    0.020
+							 0.26    0.026
+							 1.57    1.500
+						</tableData>
+					</table>
+				</product>
+			</function>
 
-		<function name="aero/moment/Roll_damp">
-			<description>Roll moment due to roll rate</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>metrics/bw-ft</property>
-				<property>aero/bi2vel</property>
-				<property>velocities/p-aero-rad_sec</property>
-				<value>-0.4</value>
-			</product>
-		</function>
+			<function name="aero/force/Drag_induced">
+				<description>Induced drag</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>aero/cl-squared</property>
+					<value>0.043</value>
+				</product>
+			</function>
 
+			<function name="aero/force/Drag_mach">
+				<description>Drag due to mach</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<table>
+						<independentVar lookup="row">velocities/mach</independentVar>
+						<tableData>
+							 0.00      0.000
+							 0.79      0.000
+							 1.10      0.023
+							 1.80      0.015
+						</tableData>
+					</table>
+				</product>
+			</function>
 
-		<!--function name="aero/coefficient/Clr">
-			<description>Roll_moment_due_to_yaw_rate</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/bw-ft</property>
-			<property>aero/bi2vel</property>
-			<property>velocities/r-aero-rad_sec</property>
-			<value>0.0050</value>
-			</product>
-		</function-->
-		<function name="aero/moment/Roll_yaw">
-			<description>Roll moment due to yaw rate</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>metrics/bw-ft</property>
-				<property>aero/bi2vel</property>
-				<property>velocities/r-aero-rad_sec</property>
-				<value>0.005</value>
-			</product>
-		</function>
+			<function name="aero/force/Drag_flap">
+				<description>Drag due to flaps</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>fcs/flap-pos-deg</property>
+					<value> 0.00197 </value>
+				</product>
+			</function>
 
+			<function name="aero/force/Drag_gear">
+				<description>Drag due to gear</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>gear/gear-pos-norm</property>
+					<value>0.025</value>
+				</product>
+			</function>
 
-		<!--function name="aero/coefficient/Clda">
-			<description>Roll_moment_due_to_aileron</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/bw-ft</property>
-			<property>fcs/left-aileron-pos-rad</property>
-			<!- value>0.2000</value -> <!- Excesive roll !!! ->
+			<function name="aero/force/Drag_speedbrake">
+				<description>Drag due to speedbrakes</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>fcs/speedbrake-pos-norm</property>
+					<value>0.02</value>
+				</product>
+			</function>
 
-			<table>
-				<independentVar lookup="row">velocities/mach</independentVar>
-					<tableData>
-						0.0    0.100
-						2.0    0.033
-					</tableData>
-			</table>
-			</product>
-		</function-->
-		<function name="aero/moment/Roll_aileron">
-			<description>Roll moment due to aileron</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>metrics/bw-ft</property>
-				<property>fcs/left-aileron-pos-rad</property>
-				<table>
-					<independentVar lookup="row">velocities/mach</independentVar>
-					<tableData>
-					<!--	0.0    0.100  -->
-						0.0    0.080
-						2.0    0.033
-					</tableData>
-				</table>
-			</product>
-		</function>
+			<function name="aero/force/Drag_beta">
+				<description>Drag due to sideslip</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<table>
+						<independentVar lookup="row">aero/beta-rad</independentVar>
+						<tableData>
+							-1.57    1.230
+							-0.26    0.050
+							 0.00    0.000
+							 0.26    0.050
+							 1.57    1.230
+						</tableData>
+					</table>
+				</product>
+			</function>
 
-		<!--function name="aero/coefficient/Cldr">
-			<description>Roll_moment_due_to_rudder</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/bw-ft</property>
-			<property>fcs/rudder-pos-rad</property>
-			<value>0.0050</value>
-			</product>
-		</function-->
-		<function name="aero/moment/Roll_rudder">
-			<description>Roll moment due to rudder</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>metrics/bw-ft</property>
-				<property>fcs/rudder-pos-rad</property>
-				<value>0.005</value>
-			</product>
-		</function>
+			<function name="aero/force/Drag_elevator">
+				<description>Drag due to Elevator Deflection</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<abs><property>fcs/elevator-pos-norm</property></abs>
+					<value>0.04</value>
+				</product>
+			</function>
 
-	</axis>
+		</axis>
 
-	<axis name="PITCH">
-		<function name="aero/moment/Pitch_zero_alpha_and_flaps">
-			<description>Pitching_moment_at_zero_alpha</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>metrics/cbarw-ft</property>
-				<table>
-					<independentVar>fcs/flap-pos-deg</independentVar>
-					<tableData>
-					0.0000	0.0000
-					40.0000	-0.1000
-					</tableData>
-				</table>
-			</product>
-		</function>
-		<function name="aero/moment/Pitch_alpha">
-			<description>Pitch_moment_due_to_alpha</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/cbarw-ft</property>
-			<property>aero/alpha-rad</property>
-			<!-- value>-4.0000</value> -->
-			<value>-0.8</value>
-			</product>
-		</function>
-		<function name="aero/moment/Pitch_elevator">
-			<description>Pitch_moment_due_to_elevator_Deflection</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/cbarw-ft</property>
-			<property>fcs/elevator-pos-rad</property>
-			<!-- <value>-1.5000</value>  Excesive Pitch -->
-			<table>
-				<independentVar lookup="row">velocities/mach</independentVar>
-				<tableData>
-				<!--	0.0     -1.200 -->
-					0.0     -1.000
-					2.0     -0.300
-				</tableData>
-			</table>
-			</product>
-		</function>
-		<function name="aero/moment/Pitch_damp">
-			<description>Pitch_moment_due_to_pitch_rate</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/cbarw-ft</property>
-			<property>aero/ci2vel</property>
-			<property>velocities/q-aero-rad_sec</property>
-			<!--value>-10.0000</value-->
-			<value>-10</value>
-			</product>
-		</function>
-		<function name="aero/moment/Pitch_alpha_rate">
-			<description>Pitch_moment_due_to_alpha_rate</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/cbarw-ft</property>
-			<property>aero/ci2vel</property>
-			<property>aero/alphadot-rad_sec</property>
-			<!--value>-12.0000</value-->
-			<value>-12</value>
-			</product>
-		</function>
+		<axis name="SIDE">
 
-	</axis>
+			<function name="aero/force/Side_beta">
+				<description>Side force due to beta</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>aero/beta-rad</property>
+					<value>-1</value>
+				</product>
+			</function>
 
-	<axis name="YAW">
-		<!--function name="aero/coefficient/Cnr">
-			<description>Yaw_moment_due_to_yaw_rate</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/bw-ft</property>
-			<property>aero/bi2vel</property>
-			<property>velocities/r-aero-rad_sec</property>
-			<value>-0.0400</value>
-			</product>
-		</function-->
-		<function name="aero/moment/Yaw_damp">
-			<description>Yaw moment due to yaw rate</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>metrics/bw-ft</property>
-				<property>aero/bi2vel</property>
-				<property>velocities/r-aero-rad_sec</property>
-				<value>-0.15</value>
-			</product>
-		</function>
-		<!--function name="aero/coefficient/Cnb">
-			<description>Yaw_moment_due_to_beta</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/bw-ft</property>
-			<property>aero/beta-rad</property>
-			<value>0.2000</value>
-			</product>
-		</function-->
-		<function name="aero/moment/Yaw_beta">
-			<description>Yaw moment due to beta</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>metrics/bw-ft</property>
-				<property>aero/beta-rad</property>
-				<value>0.12</value>
-			</product>
-		</function>
-		<!--function name="aero/coefficient/Cndr">
-			<description>Yaw_moment_due_to_rudder</description>
-			<product>
-			<property>aero/qbar-psf</property>
-			<property>metrics/Sw-sqft</property>
-			<property>metrics/bw-ft</property>
-			<property>fcs/rudder-pos-rad</property>
-			<!- <value>-0.5000</value> Excesive Yaw->
-			<value>-0.3</value>
-			</product>
-		</function-->
-		<function name="aero/moment/Yaw_rudder">
-			<description>Yaw moment due to rudder</description>
-			<product>
-				<property>aero/qbar-psf</property>
-				<property>metrics/Sw-sqft</property>
-				<property>metrics/bw-ft</property>
-				<property>fcs/rudder-pos-rad</property>
-				<!--value>-0.2</value-->
-				<value>-0.15</value>
-			</product>
-		</function>
+		</axis>
 
-    <!--function name="aero/moment/Yaw_aileron">
-       <description>Adverse yaw</description>
-       <product>
-           <property>aero/qbar-psf</property>
-           <property>metrics/Sw-sqft</property>
-           <property>metrics/bw-ft</property>
-           <property>fcs/left-aileron-pos-rad</property>
-           <value>0</value>
-       </product>
-    </function-->
+		<axis name="ROLL">
 
+			<function name="aero/moment/Roll_beta">
+				<description>Roll moment due to beta</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/bw-ft</property>
+					<property>aero/beta-rad</property>
+					<value>-0.1</value>
+				</product>
+			</function>
 
+			<function name="aero/moment/Roll_damp">
+				<description>Roll moment due to roll rate</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/bw-ft</property>
+					<property>aero/bi2vel</property>
+					<property>velocities/p-aero-rad_sec</property>
+					<value>-0.4</value>
+				</product>
+			</function>
 
-	</axis>
+			<function name="aero/moment/Roll_yaw">
+				<description>Roll moment due to yaw rate</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/bw-ft</property>
+					<property>aero/bi2vel</property>
+					<property>velocities/r-aero-rad_sec</property>
+					<value>0.15</value>
+				</product>
+			</function>
 
-</aerodynamics>
+			<function name="aero/moment/Roll_aileron">
+				<description>Roll moment due to aileron</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/bw-ft</property>
+					<property>fcs/left-aileron-pos-rad</property>
+					<value>0.1</value>
+				</product>
+			</function>
+
+			<function name="aero/moment/Roll_rudder">
+				<description>Roll moment due to rudder</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/bw-ft</property>
+					<property>fcs/rudder-pos-rad</property>
+					<value>0.01</value>
+				</product>
+			</function>
+
+		</axis>
+
+		<axis name="PITCH">
+
+			<function name="aero/moment/Pitch_alpha">
+				<description>Pitch moment due to alpha</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/cbarw-ft</property>
+					<property>aero/alpha-rad</property>
+					<value>-0.6</value>
+				</product>
+			</function>
+
+			<function name="aero/moment/Pitch_elevator">
+				<description>Pitch moment due to elevator</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/cbarw-ft</property>
+					<property>fcs/elevator-pos-rad</property>
+					<table>
+						<independentVar lookup="row">velocities/mach</independentVar>
+						<tableData>
+							0.0     -1.200
+							2.0     -0.300
+						</tableData>
+					</table>
+				</product>
+			</function>
+
+			<function name="aero/moment/Pitch_damp">
+				<description>Pitch moment due to pitch rate</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/cbarw-ft</property>
+					<property>aero/ci2vel</property>
+					<property>velocities/q-aero-rad_sec</property>
+					<value>-17</value>
+				</product>
+			</function>
+
+			<function name="aero/moment/Pitch_alphadot">
+				<description>Pitch moment due to alpha rate</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/cbarw-ft</property>
+					<property>aero/ci2vel</property>
+					<property>aero/alphadot-rad_sec</property>
+					<value>-6</value>
+				</product>
+			</function>
+
+		</axis>
+
+		<axis name="YAW">
+
+			<function name="aero/moment/Yaw_beta">
+				<description>Yaw moment due to beta</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/bw-ft</property>
+					<property>aero/beta-rad</property>
+					<value>0.12</value>
+				</product>
+			</function>
+
+			<function name="aero/moment/Yaw_damp">
+				<description>Yaw moment due to yaw rate</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/bw-ft</property>
+					<property>aero/bi2vel</property>
+					<property>velocities/r-aero-rad_sec</property>
+					<value>-0.15</value>
+				</product>
+			</function>
+
+			<function name="aero/moment/Yaw_rudder">
+				<description>Yaw moment due to rudder</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/bw-ft</property>
+					<property>fcs/rudder-pos-rad</property>
+					<value>-0.1</value>
+				</product>
+			</function>
+
+			<function name="aero/moment/Yaw_aileron">
+				<description>Adverse yaw</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>metrics/bw-ft</property>
+					<property>fcs/left-aileron-pos-rad</property>
+					<value>0</value>
+				</product>
+			</function>
+
+		</axis>
+
+	</aerodynamics>
 
 	<external_reactions>
 		<force name="pushback" frame="BODY">