diff --git a/ACJ-IAE-set.xml b/ACJ-IAE-set.xml
new file mode 100644
index 00000000..514228a2
--- /dev/null
+++ b/ACJ-IAE-set.xml
@@ -0,0 +1,91 @@
+<?xml version="1.0" encoding="UTF-8" ?>
+
+<PropertyList include="A320-main.xml">
+
+	<sim>
+	
+		<sound>
+			<path>Aircraft/A320Family/Sounds/v2500-sound.xml</path>
+		</sound>
+	
+		<description>Airbus Corperate Jet (IAE V2500)</description>
+		<status>Flyable</status>
+		<flight-model>jsb</flight-model>
+		<aero>ACJ-IAE</aero>
+		<model>
+			<path>Aircraft/A320Family/Models/A319-200-IAE.xml</path>
+			<livery>
+				<file>USAirwaysStar</file>
+			</livery>
+		</model>
+		
+		<view>
+			<name>Pilot View</name>
+			<internal archive="y">true</internal>
+			<config>
+				<x-offset-m archive="y">-0.45</x-offset-m>
+				<y-offset-m archive="y">2.25</y-offset-m>
+				<z-offset-m archive="y">-12.10</z-offset-m>
+				<pitch-offset-deg archive="y">-12.0</pitch-offset-deg>
+				<default-field-of-view-deg type="double">60</default-field-of-view-deg>
+			</config>
+		</view>
+		<view n="103">
+			<name>Copilot View</name>
+			<type>lookfrom</type>
+			<internal archive="y">true</internal>
+			<config>
+				<from-model type="bool">true</from-model>
+				<x-offset-m archive="y">0.45</x-offset-m>
+				<y-offset-m archive="y">2.30</y-offset-m>
+				<z-offset-m archive="y">-12.00</z-offset-m>
+				<pitch-offset-deg archive="y">-12.0</pitch-offset-deg>
+				<default-field-of-view-deg type="double">60</default-field-of-view-deg>
+			</config>
+		</view>
+		<view n="104">
+			<name>Overhead Panel View</name>
+			<type>lookfrom</type>
+			<internal archive="y">true</internal>
+			<config>
+				<from-model type="bool">true</from-model>
+				<x-offset-m archive="y">0</x-offset-m>
+				<y-offset-m archive="y">2.3635023</y-offset-m>
+				<z-offset-m archive="y">-12.1</z-offset-m>
+				<pitch-offset-deg archive="y">40</pitch-offset-deg>
+				<default-field-of-view-deg type="double">85</default-field-of-view-deg>
+			</config>
+		</view>
+
+		<menubar>
+			<default>
+				<menu n="100">
+					<label>Airbus ACJ</label>
+				</menu>
+			</default>
+		</menubar>
+	</sim>
+	
+	<nasal>
+		<A320>
+			<file>Aircraft/A320Family/Nasal/engines.nas</file>
+			<file>Aircraft/A320Family/Nasal/electrical.nas</file>
+			<file>Aircraft/A320Family/Nasal/v-speeds.nas</file>
+			<file>Aircraft/A320Family/Nasal/tyresmoke.nas</file>
+			<file>Aircraft/A320Family/Nasal/systems.nas</file>
+			<file>Aircraft/A320Family/Nasal/acjlivery.nas</file>
+			<file>Aircraft/A320Family/Models/Instruments/ND/ND.nas</file>
+            <file>Aircraft/A320Family/Nasal/gpws.nas</file>
+            <file>Aircraft/A320Family/Nasal/efis.nas</file>
+			<file>Aircraft/A320Family/Nasal/PFD_FMA.nas</file>
+			<file>Aircraft/A320Family/Nasal/fctl.nas</file>
+		</A320>
+		<itaf>
+			<file>Aircraft/A320Family/Nasal/it-autoflight.nas</file>
+		</itaf>
+		<thrust>
+			<file>Aircraft/A320Family/Nasal/thrust.nas</file>
+		</thrust>
+	</nasal>
+
+</PropertyList>
diff --git a/ACJ-IAE.xml b/ACJ-IAE.xml
new file mode 100644
index 00000000..435c557f
--- /dev/null
+++ b/ACJ-IAE.xml
@@ -0,0 +1,1331 @@
+<?xml version="1.0"?>
+<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
+<fdm_config name="A320family" version="2.0" release="BETA"
+xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
+xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
+
+<fileheader>
+	<author> Bicyus (Jon Ortuondo) </author>
+	<email> bicyus@gmail.com </email>
+	<filecreationdate> 2012-02-15 </filecreationdate>
+	<version> 0.99 </version>
+	<description> Airbus ACJ with IAE V2500 Engines </description>
+	<note> Revised and fixed by Peter Brendt (jwocky) and Joshua Davidson (it0uchpods). Fork from the A320-Family aircraft project (Thanks to all authors) </note>
+	<limitation></limitation>
+</fileheader>
+
+<metrics>
+	<wingarea  unit="FT2"> 1319.79 </wingarea>
+	<wingspan  unit="FT" >  111.26 </wingspan>
+	<wing_incidence>          1.03 </wing_incidence>
+	<chord     unit="FT" >   13.76 </chord>
+	<htailarea unit="FT2">  334.24 </htailarea>
+	<htailarm  unit="FT" >   57.88 </htailarm>
+	<vtailarea unit="FT2">  248.79 </vtailarea>
+	<vtailarm  unit="FT" >   57.33 </vtailarm>
+
+	<!-- location name="AERORP" unit="IN">
+		<x> 642.122 </x>
+		<y> 0 </y>
+		<z> -25.2091 </z>
+	</location -->
+	<location name="AERORP" unit="IN">
+		<x> 680.00 </x>
+		<y> 0 </y>
+		<z> 0.00 </z>
+	</location>
+
+	<location name="EYEPOINT" unit="IN">
+		<x> 80 </x>
+		<y> -30 </y>
+		<z> 70 </z>
+	</location>
+
+	<location name="VRP" unit="IN">
+		<x> 661.1 </x>
+		<y> 0 </y>
+		<z> -37 </z>
+	</location>
+
+</metrics>
+
+<mass_balance>
+	<ixx unit="SLUG*FT2">    611903 </ixx>
+	<iyy unit="SLUG*FT2">   1735389 </iyy>
+	<izz unit="SLUG*FT2">   2301293 </izz> 
+<!--
+___________________A320_________A330__________A340
+BOW_____________178000________270000________283925
+SPAN______________144___________198___________209
+LENGTH____________153___________209___________209
+ROLL MOI_________1725000______5727777_______10613448
+PITCH MOI________2550000______19040141_______13904249
+YAW MOI_________3950000______23089847_______24848934
+
+	<ixx unit="SLUG*FT2">   2262183 </ixx>
+	<iyy unit="SLUG*FT2">   3172439 </iyy>
+	<izz unit="SLUG*FT2">   3337024 </izz>
+
+	<ixx unit="SLUG*FT2">1725000</ixx>
+	<iyy unit="SLUG*FT2">2550000</iyy>
+	<izz unit="SLUG*FT2">3950000</izz> -->
+
+	<ixy unit="SLUG*FT2">         0 </ixy>
+	<ixz unit="SLUG*FT2">         0 </ixz>
+	<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 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- - >
+		<x> 650.122 </x><! - - At zero load of fuel and cargo/pax the CG goes to 642 - - >
+		<y> 0 </y>
+		<z> -41.7398 </z>
+	</location -->
+	<location name="CG" unit="IN">
+		<x> 642.00 </x>
+		<y> 0 </y>
+		<z> 0.00 </z>
+	</location>
+
+	<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="Cabin Crew">
+		<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
+		<location name="POINTMASS" unit="IN">
+			<x>696</x>
+			<y>0</y>
+			<z>0</z>
+		</location>
+	</pointmass>
+	<pointmass name="PAX 0A (60 seats)">
+		<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
+		<location name="POINTMASS" unit="IN">
+			<x>470.1711</x>
+			<y>0</y>
+			<z>0</z>
+		</location>
+	</pointmass>
+	<pointmass name="PAX 0B (60 seats)">
+		<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
+		<location name="POINTMASS" unit="IN">
+			<x>809.5669</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>1163.2729</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>
+
+
+</mass_balance>
+
+<ground_reactions>
+	<!-- REF-1 page 165 + 271  -->
+	<contact type="BOGEY" name="NOSE_LG">
+		<location unit="IN">
+			<x> 197.6772 </x>
+			<y> 0 </y>
+			<z> -137.9617 </z> 
+		</location>
+		<static_friction> 0.8 </static_friction>
+		<dynamic_friction> 0.5 </dynamic_friction>
+		<rolling_friction> 0.02 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
+		<max_steer unit="DEG"> 70 </max_steer> <!-- REF-1 page 133 -->
+		<brake_group> NONE </brake_group>
+		<retractable>1</retractable>
+	</contact>
+	<contact type="BOGEY" name="LEFT_MLG">
+		<location unit="IN">
+			<!--<x> 699.9243 </x>-->
+			<x> 695.3149 </x>
+			<y> -149.4094 </y>
+			<z> -150.4824 </z>
+		</location>
+<!-- 		<static_friction> 0.5 </static_friction>  WHAT??? less static than dinamyc friction?-->
+		<static_friction> 0.8 </static_friction>
+		<dynamic_friction> 0.5 </dynamic_friction>
+		<rolling_friction> 0.02 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> LEFT </brake_group>
+		<retractable>1</retractable>
+	</contact>
+	<contact type="BOGEY" name="RIGHT_MLG">
+		<location unit="IN">
+			<!-- <x> 697.3425 </x> It should be right left simetric
+			<x> 699.9243 </x> -->
+			<x> 695.3149 </x>
+			<y> 149.4094 </y>
+			<z> -150.4824 </z>
+		</location>
+<!-- 		<static_friction> 0.5 </static_friction>  WHAT??? less static than dinamyc friction?-->
+		<static_friction> 0.8 </static_friction>
+		<dynamic_friction> 0.5 </dynamic_friction>
+		<rolling_friction> 0.02 </rolling_friction>
+		<!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
+		<spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> RIGHT </brake_group>
+		<retractable>1</retractable>
+	</contact>
+
+	<contact type="STRUCTURE" name="NOSE_1">
+		<location unit="IN">
+			<x> 37.7953 </x>
+			<y> 0 </y>
+			<z> -38.1374 </z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 0.4 </dynamic_friction>
+		<rolling_friction> 0.4 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+	<contact type="STRUCTURE" name="NOSE_2">
+		<location unit="IN">
+			<x> 128.1102 </x>
+			<y> 0 </y>
+			<z> -55.0271 </z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 0.4 </dynamic_friction>
+		<rolling_friction> 0.4 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+	<contact type="STRUCTURE" name="CENTER_1">
+		<location unit="IN">
+			<x> 274.0157 </x>
+			<y> 0 </y>
+			<z> -60.0665 </z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 0.4 </dynamic_friction>
+		<rolling_friction> 0.4 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+	<contact type="STRUCTURE" name="CENTER_2">
+		<location unit="IN">
+			<x> 930 </x>
+			<y> 0 </y>
+			<z> -60.0665 </z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 0.4 </dynamic_friction>
+		<rolling_friction> 0.4 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+
+	<contact type="STRUCTURE" name="ENG_1">
+		<location unit="IN">
+			<x>589.735</x>	
+			<y>-226.575</y>
+			<z>-95.567</z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 0.4 </dynamic_friction>
+		<rolling_friction> 0.4 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+	<contact type="STRUCTURE" name="ENG_2">
+		<location unit="IN">
+			<x>589.735</x>	
+			<y>226.575</y>
+			<z>-95.567</z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 0.5 </dynamic_friction>
+		<rolling_friction> 0.4 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+
+
+	<contact type="STRUCTURE" name="TAIL_1">
+		<location unit="IN">
+			<x> 1097.9921 </x>
+			<y> 0 </y>
+			<z> -44.7722 </z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 0.4 </dynamic_friction>
+		<rolling_friction> 0.4 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+	<contact type="STRUCTURE" name="TAIL_2">
+		<location unit="IN">
+			<x> 1225 </x>
+			<y> 0 </y>
+			<z> -18.8067 </z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 0.4 </dynamic_friction>
+		<rolling_friction> 0.4 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+	<contact type="STRUCTURE" name="TAIL_3">
+		<location unit="IN">
+			<x> 1341.6142 </x>
+			<y> 0 </y>
+			<z> -10.2599 </z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 0.4 </dynamic_friction>
+		<rolling_friction> 0.4 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+	<contact type="STRUCTURE" name="TAIL_4">
+		<location unit="IN">
+			<x> 1469.0945 </x>
+			<y> 0 </y>
+			<z> 47.4138 </z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 1 </dynamic_friction>
+		<rolling_friction> 1 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+	<contact type="STRUCTURE" name="WING_TIP_1">
+		<location unit="IN">
+			<x> 838.8898 </x>
+			<y> -667.5197 </y>
+			<z> 35.7926 </z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 0.4 </dynamic_friction>
+		<rolling_friction> 0.4 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+	<contact type="STRUCTURE" name="WING_TIP_2">
+		<location unit="IN">
+			<x> 838.8898 </x>
+			<y> 667.5197 </y>
+			<z> 35.7926 </z>
+		</location>
+		<static_friction> 1.0 </static_friction>
+		<dynamic_friction> 1 </dynamic_friction>
+		<rolling_friction> 1 </rolling_friction>
+		<spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+		<damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+		<max_steer unit="DEG"> 0.0 </max_steer>
+		<brake_group> NONE </brake_group>
+		<retractable>0</retractable>
+	</contact>
+</ground_reactions>
+
+<propulsion>
+
+	<engine file="v2527_a5">
+	<location unit="IN">
+		<x> 620.0683 </x>
+		<y> -226.575 </y>
+		<z> -45.567 </z>
+	</location>
+	<orient unit="DEG">
+		<roll> 0.0 </roll>
+		<pitch> 2.2 </pitch>
+		<yaw> 1 </yaw>
+	</orient>
+	<feed>3</feed>
+	<feed>1</feed>
+	<feed>2</feed>
+	<thruster file="direct">
+		<location unit="IN">
+		<x> 655.4820 </x>
+		<y> -226.575 </y>
+		<z> 0.000 </z>
+		</location>
+		<orient unit="DEG">
+		<roll> 0.0 </roll>
+		<pitch> 2.2 </pitch>
+		<yaw> 1 </yaw>
+		</orient>
+	</thruster>
+	</engine>
+
+	<engine file="v2527_a5">
+	<location unit="IN">
+		<x> 620.00683 </x>
+		<y> 226.575 </y>
+		<z> -45.567 </z>
+	</location>
+	<orient unit="DEG">
+		<roll> 0.0 </roll>
+		<pitch> 2.2 </pitch>
+		<yaw> -1 </yaw>
+	</orient>
+	<feed>3</feed>
+	<feed>5</feed>
+	<feed>4</feed>
+	<thruster file="direct">
+		<location unit="IN">
+		<x> 655.4820 </x>
+		<y> 226.575 </y>
+		<z> 0.000 </z>
+		</location>
+		<orient unit="DEG">
+		<roll> 0.0 </roll>
+		<pitch> 2.2 </pitch>
+		<yaw> -1 </yaw>
+		</orient>
+	</thruster>
+	</engine>
+
+
+	<tank type="FUEL">    <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
+		<location unit="IN">
+			<x> 783.0709 </x>
+			<y> -574.4148 </y>
+			<z> 3.1080 </z>
+		</location>
+		<capacity unit="LBS"> 150 </capacity><!-- need review -->
+		<contents unit="LBS"> 0 </contents>
+		
+		<priority>4</priority>
+		<type>JET-A1</type>
+		<temperature>50</temperature>
+	</tank>
+	<tank type="FUEL">    <!-- Left Tank (Outer) 1 -->
+		<location unit="IN">
+			<x> 739.5669 </x>
+			<y> -457.4259 </y>
+			<z> -8.0898 </z>
+		</location>
+		<capacity unit="LBS"> 1520.00 </capacity><!-- need review -->
+		<contents unit="LBS"> 0 </contents>
+		<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+		<priority>2</priority>
+		<type>JET-A1</type>
+		<temperature>50</temperature>
+	</tank>
+	<tank type="FUEL">    <!-- Left Tank (Inner) 2 -->
+		<location unit="IN">
+			<x> 652.5591 </x>
+			<y> -236.2992 </y>
+			<z> -33.9470 </z>
+		</location>
+		<capacity unit="LBS"> 11982 </capacity><!-- need review -->
+		<contents unit="LBS"> 3000 </contents>
+		<standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+		<priority>3</priority>
+		<type>JET-A1</type>
+		<temperature>50</temperature>
+	</tank>
+	<tank type="FUEL">    <!-- Center Tank 3 -->
+		<location unit="IN">
+			<x> 522.0473 </x>
+			<y> 0 </y>
+			<z> -47.0 </z>
+		</location>
+		<capacity unit="LBS"> 14281 </capacity><!-- need review -->
+		<contents unit="LBS"> 3000 </contents>
+		<standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
+		<priority>1</priority>
+		<type>JET-A1</type>
+		<temperature>50</temperature>
+	</tank>
+	<tank type="FUEL">    <!-- Right Tank (Inner) 4 -->
+		<location unit="IN">
+			<x> 652.5591 </x>
+			<y> 236.2992 </y>
+			<z> -33.9470 </z>
+		</location>
+		<capacity unit="LBS"> 11982 </capacity><!-- need review -->
+		<contents unit="LBS"> 3000 </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> 739.5669 </x>
+			<y> 457.4259 </y>
+			<z> -8.0898 </z>
+		</location>
+		<capacity unit="LBS"> 1520 </capacity><!-- need review -->
+		<contents unit="LBS"> 0 </contents>
+		<standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+		<priority>2</priority>
+		<type>JET-A1</type>
+		<temperature>50</temperature>
+	</tank>
+	<tank type="FUEL">    <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
+		<location unit="IN">
+			<x> 783.0709 </x>
+			<y> 574.4148 </y>
+			<z> 3.1080 </z>
+		</location>
+		<capacity unit="LBS"> 150 </capacity><!-- need review -->
+		<contents unit="LBS"> 0 </contents>
+		<priority>4</priority>
+		<type>JET-A1</type>
+		<temperature>50</temperature>
+	</tank>
+</propulsion>
+
+<system file="pushback" />
+<!--system file="a320-fuel" /-->
+<system file="glass-effect1"/>
+
+<flight_control name="FCS: A320">
+	<channel name="Pitch">
+	<summer name="Pitch Trim Sum">
+		<input>/controls/flight/elevator</input>
+		<input>/controls/flight/elevator-trim</input>
+		<clipto>
+		<min>-1</min>
+		<max>1</max>
+		</clipto>
+	</summer>
+
+	<aerosurface_scale name="Elevator Control">
+		<input>fcs/pitch-trim-sum</input>
+		<gain>0.025</gain>
+		<range>
+		<min>-10</min>
+		<max>10</max>
+		</range>
+		<output>fcs/elevator-pos-rad</output>
+	</aerosurface_scale>
+
+	<aerosurface_scale name="Elevator position normalized">
+		<input>fcs/elevator-pos-deg</input>
+		<domain>
+		<min>-10</min>
+		<max>10</max>
+		</domain>
+		<range>
+		<min>-1</min>
+		<max>1</max>
+		</range>
+		<output>fcs/elevator-pos-norm</output>
+	</aerosurface_scale>
+	</channel>
+	<channel name="Roll">
+	<summer name="Roll Trim Sum">
+		<input>/controls/flight/aileron</input>
+		<input>/controls/flight/aileron-trim</input>
+		<clipto>
+		<min>-1</min>
+		<max>1</max>
+		</clipto>
+	</summer>
+
+	<aerosurface_scale name="Left Aileron Control">
+		<input>fcs/roll-trim-sum</input>
+		<gain>0.02</gain>
+		<range>
+		<min>-15</min>
+		<max>15</max>
+		</range>
+		<output>fcs/left-aileron-pos-rad</output>
+	</aerosurface_scale>
+
+	<aerosurface_scale name="Right Aileron Control">
+		<input>-fcs/roll-trim-sum</input>
+		<gain>0.02</gain>
+		<range>
+		<min>-15</min>
+		<max>15</max>
+		</range>
+		<output>fcs/right-aileron-pos-rad</output>
+	</aerosurface_scale>
+
+	<aerosurface_scale name="Left Aileron position normalized">
+		<input>fcs/left-aileron-pos-deg</input>
+		<domain>
+		<min>-15</min>
+		<max>15</max>
+		</domain>
+		<range>
+		<min>-1</min>
+		<max>1</max>
+		</range>
+		<output>fcs/left-aileron-pos-norm</output>
+	</aerosurface_scale>
+
+	<aerosurface_scale name="Right Aileron position normalized">
+		<input>fcs/right-aileron-pos-deg</input>
+		<domain>
+		<min>-15</min>
+		<max>15</max>
+		</domain>
+		<range>
+		<min>-1</min>
+		<max>1</max>
+		</range>
+		<output>fcs/right-aileron-pos-norm</output>
+	</aerosurface_scale>
+	</channel>
+	<channel name="Throttle">
+	<pure_gain name="fcs/throttle1">
+		<input>/controls/engines/engine[0]/throttle-fdm</input>
+		<gain>1</gain>
+		<output>fcs/throttle-cmd-norm</output>
+		<output>fcs/throttle-pos-norm</output>
+	</pure_gain>
+	<pure_gain name="fcs/throttle2">
+		<input>/controls/engines/engine[1]/throttle-fdm</input>
+		<gain>1</gain>
+		<output>fcs/throttle-cmd-norm[1]</output>
+		<output>fcs/throttle-pos-norm[1]</output>
+	</pure_gain>
+	</channel>
+	<channel name="Yaw">
+	<!-- Testing on Ground steering Rudder bug
+	<pure_gain name="Yaw Damper Rate">
+		<input>velocities/r-rad_sec</input>
+		<gain>2</gain>
+	</pure_gain>
+
+	<pure_gain name="Yaw Damper Beta">
+		<input>aero/beta-rad</input>
+		<gain>-5</gain>
+	</pure_gain>
+
+	<summer name="Yaw Trim Sum">
+		<input>fcs/rudder-cmd-norm</input>
+		<input>fcs/yaw-trim-cmd-norm</input>
+		<clipto>
+		<min>-1</min>
+		<max>1</max>
+		</clipto>
+	</summer>
+
+	<summer name="Rudder Sum">
+		<input>fcs/yaw-trim-sum</input>
+		<input>fcs/yaw-damper-rate</input>
+		<input>fcs/yaw-damper-beta</input>
+		<clipto>
+		<min>-1</min>
+		<max>1</max>
+		</clipto>
+	</summer>
+
+	<aerosurface_scale name="Rudder Control">
+		<input>fcs/rudder-sum</input>
+		<gain>0.01745</gain>
+		<range>
+		<min>-25</min>
+		<max>25</max>
+		</range>
+		<output>fcs/rudder-pos-rad</output>
+	</aerosurface_scale>
+
+	<aerosurface_scale name="Rudder position normalized">
+		<input>fcs/rudder-pos-deg</input>
+		<domain>
+		<min>-25</min>
+		<max>25</max>
+		</domain>
+		<range>
+		<min>-1</min>
+		<max>1</max>
+		</range>
+		<output>fcs/rudder-pos-norm</output>
+	</aerosurface_scale> -->
+   <summer name="Rudder Command Sum">
+      <input>fcs/rudder-cmd-norm</input>
+      <input>fcs/yaw-trim-cmd-norm</input>
+      <clipto>
+        <min> -0.35 </min>
+        <max>  0.35 </max>
+      </clipto>
+   </summer>
+
+   <scheduled_gain name="Yaw Damper Rate">
+      <input>velocities/r-aero-rad_sec</input>
+      <table>
+        <independentVar lookup="row">velocities/ve-kts</independentVar>
+         <tableData>
+            30     0.00
+            60     2.00
+         </tableData>
+      </table>
+   </scheduled_gain>
+
+   <scheduled_gain name="Yaw Damper Beta">
+      <input>aero/beta-rad</input>
+      <table>
+        <independentVar lookup="row">velocities/ve-kts</independentVar>
+        <tableData>
+           30     0.00
+           60     0.00
+        </tableData>
+      </table>
+   </scheduled_gain>
+
+   <summer name="Yaw Damper Sum">
+      <input>fcs/yaw-damper-beta</input>
+      <input>fcs/yaw-damper-rate</input>
+      <clipto>
+        <min> -0.1 </min>
+        <max>  0.1 </max>
+      </clipto>
+   </summer>
+
+   <scheduled_gain name="Yaw Damper Final">
+      <input>fcs/yaw-damper-sum</input>
+      <table>
+        <independentVar lookup="row">velocities/ve-kts</independentVar>
+        <tableData>
+           30         0.0
+           31         1.0
+        </tableData>
+      </table>
+   </scheduled_gain>
+
+   <summer name="Rudder Sum">
+      <input>fcs/rudder-command-sum</input>
+      <input>fcs/yaw-damper-final</input>
+      <clipto>
+        <min> -1 </min>
+        <max>  1 </max>
+      </clipto>
+   </summer>
+
+   <aerosurface_scale name="Rudder Control">
+      <input>fcs/rudder-sum</input>
+      <range>
+        <min> -0.35 </min>
+        <max>  0.35 </max>
+      </range>
+      <output>fcs/rudder-pos-rad</output>
+   </aerosurface_scale>
+
+   <aerosurface_scale name="rudder normalization">
+      <input>fcs/rudder-pos-rad</input>
+      <domain>
+        <min> -0.35 </min>
+        <max>  0.35 </max>
+      </domain>
+      <range>
+        <min> -1 </min>
+        <max>  1 </max>
+      </range>
+      <output>fcs/rudder-pos-norm</output>
+   </aerosurface_scale>
+
+	</channel>
+
+		<channel name="Flaps">
+
+		<kinematic name="Flaps Control">
+			<input>/controls/flight/flaps</input>
+			<traverse>
+			<setting>
+				<position>0</position>
+				<time>0</time>
+			</setting>
+			<setting>
+				<position>35</position>
+				<time>40</time>
+			</setting>
+			</traverse>
+			<output>fcs/flap-pos-deg</output>
+		</kinematic>
+
+		<aerosurface_scale name="Flap position normalized">
+			<input>fcs/flap-pos-deg</input>
+			<domain>
+				<min>0</min>
+				<max>35</max>
+			</domain>
+			<range>
+				<min>0</min>
+				<max>1</max>
+			</range>
+			<output>fcs/flap-pos-norm</output>
+		</aerosurface_scale>
+
+	</channel>
+
+	<channel name="Slats">
+
+		<kinematic name="Slats Control">
+			<input>/controls/flight/slats</input>
+			<traverse>
+			<setting>
+				<position>0</position>
+				<time>0</time>
+			</setting>
+			<setting>
+				<position>27</position>
+				<time>40</time>
+			</setting>
+			</traverse>
+			<output>fcs/slat-pos-deg</output>
+		</kinematic>
+
+		<aerosurface_scale name="Slat position normalized">
+			<input>fcs/slat-pos-deg</input>
+			<domain>
+			<min>0</min>
+			<max>27</max>
+			</domain>
+			<range>
+			<min>0</min>
+			<max>1</max>
+			</range>
+			<output>fcs/slat-pos-norm</output>
+		</aerosurface_scale>
+
+	</channel>
+
+	<channel name="Landing Gear">
+
+		<kinematic name="Gear Control">
+			<input>gear/gear-cmd-norm</input>
+			<traverse>
+			<setting>
+				<position>0</position>
+				<time>0</time>
+			</setting>
+			<setting>
+				<position>1</position>
+				<time>10</time>
+			</setting>
+			</traverse>
+			<output>gear/gear-pos-norm</output>
+		</kinematic>
+	</channel>
+
+	<channel name="Speedbrake">
+		<kinematic name="Speedbrake">
+			<input>fcs/speedbrake-cmd-norm</input>
+			<traverse>
+			<setting>
+				<position>0</position>
+				<time>0</time>
+			</setting>
+			<setting>
+				<position>1</position>
+				<time>2</time>
+			</setting>
+			</traverse>
+			<output>fcs/speedbrake-pos-norm</output>
+		</kinematic>
+	</channel>
+    
+	<channel name="Tiller">
+		
+		<switch name="/controls/gear/tiller-disabled">
+			<default value="0"/>
+			<test logic="AND" value="1">
+				/controls/gear/tiller-enabled == 0
+			</test>
+		</switch>
+        
+        <fcs_function name="Nose Wheel Steering 0">
+            <function name="fcs/steer-nose-deg[0]">
+                <description>Steering command for nose gear</description>
+                <sum>
+                    <product>
+                        <table>
+                            <independentVar lookup="row">/controls/gear/tiller-cmd-norm</independentVar>
+                            <independentVar lookup="column">/controls/flight/rudder</independentVar>
+                            <tableData>
+                                -1   0   1
+                                -1 -70 -70 -70
+                                0  -7   0   7
+                                1  70  70  70
+                            </tableData>
+                        </table>
+                        <property>/controls/gear/tiller-enabled</property>
+                    </product>
+                    <product>
+                        <product>
+                            <property>/controls/flight/rudder</property>
+                            <value>70</value>
+                        </product>
+                        <property>/controls/gear/tiller-disabled</property>
+                    </product>
+                </sum>
+            </function>
+        </fcs_function>
+        
+        <!-- simulate rotational friction -->
+        <actuator name="Gear Nose Actuator">
+            <input>fcs/steer-nose-deg[0]</input>
+            <rate_limit>70</rate_limit>
+            <output>fcs/steer-pos-deg[0]</output>
+        </actuator>
+        
+    </channel>
+
+    
+</flight_control>
+
+
+	<aerodynamics>
+
+		<axis name="LIFT">
+
+			<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>
+							-0.20 -0.780
+							 0.00  0.345
+							 0.23  1.100
+							 0.60  0.700
+						</tableData>
+					</table>
+				</product>
+			</function>
+
+			<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> 0.00700 </value>
+				</product>
+			</function>
+
+			<function name="aero/force/Lift_slats">
+				<description>Delta Lift due to slats</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>fcs/slat-pos-deg</property>
+					<value> 0.02000 </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>
+
+			<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>
+
+		<axis name="DRAG">
+
+			<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    1.300
+							-0.26    0.021
+							 0.00    0.012
+							 0.26    0.021
+							 1.57    1.300
+						</tableData>
+					</table>
+				</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>0.041</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/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> 0.00120 </value>
+				</product>
+			</function>
+
+			<function name="aero/force/Drag_slats">
+				<description>Drag due to slats</description>
+				<product>
+					<property>aero/qbar-psf</property>
+					<property>metrics/Sw-sqft</property>
+					<property>fcs/flap-pos-deg</property>
+					<value> 0.00120 </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>0.020</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>0.02</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>
+					<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/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>0.045</value>
+				</product>
+			</function>
+
+		</axis>
+
+		<axis name="SIDE">
+
+			<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>
+
+		<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>
+
+			<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>
+
+			<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">
+			<location unit="IN">
+				<x>294</x>
+				<y>0</y>
+				<z>-149</z>
+			</location>
+			<direction>
+				<x>1</x>
+				<y>0</y>
+				<z>0</z>
+			</direction>
+		</force>
+	</external_reactions>
+</fdm_config>
diff --git a/Nasal/hydraulics.nas b/Nasal/hydraulics.notes
similarity index 100%
rename from Nasal/hydraulics.nas
rename to Nasal/hydraulics.notes