From eb3cf81cedb4c89b050c89fff247f78c7cc109dd Mon Sep 17 00:00:00 2001
From: Joshua Davidson <joshuadavidson2000@gmail.com>
Date: Tue, 8 Nov 2016 23:07:44 -0500
Subject: [PATCH] update infos

---
 A319-200-IAE-set.xml                          |    1 +
 ...before rewriting aerodynamics channel).xml | 1605 -----------------
 A320-200-IAE-set.xml                          |    1 +
 A320-main.xml                                 |    1 -
 A321-200-IAE-set.xml                          |    1 +
 README.md                                     |    2 +-
 6 files changed, 4 insertions(+), 1607 deletions(-)
 delete mode 100644 A320-200-IAE (before rewriting aerodynamics channel).xml

diff --git a/A319-200-IAE-set.xml b/A319-200-IAE-set.xml
index 27374cc3..314e54f7 100644
--- a/A319-200-IAE-set.xml
+++ b/A319-200-IAE-set.xml
@@ -9,6 +9,7 @@
 		</sound>
 	
 		<description>NOT READY: Airbus A319 (IAE V2500)</description>
+		<status>Not Flyable</status>
 		<flight-model>jsb</flight-model>
 		<aero>A319-200-IAE</aero>
 		<model>
diff --git a/A320-200-IAE (before rewriting aerodynamics channel).xml b/A320-200-IAE (before rewriting aerodynamics channel).xml
deleted file mode 100644
index c58a33ee..00000000
--- a/A320-200-IAE (before rewriting aerodynamics channel).xml	
+++ /dev/null
@@ -1,1605 +0,0 @@
-<?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 A320-200 with IAE V2500 Engines </description>
-	<note> 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> 655.00 </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>450.1711</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>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>
-
-
-</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> 589.735 </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> 589.735 </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>
-	</thruster>
-	</engine>
-
-	<engine file="v2527_a5">
-	<location unit="IN">
-		<x> 589.735 </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> 589.735 </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>
-	</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"> 328.13 </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"> 154.88 </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"> 11982 </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"> 7260 </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"> 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> 739.5669 </x>
-			<y> 457.4259 </y>
-			<z> -8.0898 </z>
-		</location>
-		<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>
-		<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"> 328.13 </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>fcs/flap-cmd-norm</input>
-		<traverse>
-		<setting>
-			<position>0</position>
-			<time>0</time>
-		</setting>
-		<setting>
-			<position>40</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>40</max>
-		</domain>
-		<range>
-		<min>0</min>
-		<max>1</max>
-		</range>
-		<output>fcs/flap-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>
-	<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>
-
-	<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>
-
-		<!--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>
-						<tableData>
-						0.00      0.000
-						0.79      0.000
-						1.10      0.023
-						1.80      0.015
-						</tableData>
-				</table>
-			</product>
-		</function>
-
-  </axis>
-
-  <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>
-
-  </axis>
-
-  <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>
-
-
-		<!--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/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/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/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 !!! ->
-
-			<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/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>
-
-	</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>
-
-	<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>
-
-    <!--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/A320-200-IAE-set.xml b/A320-200-IAE-set.xml
index 0ea645bb..fc35f484 100644
--- a/A320-200-IAE-set.xml
+++ b/A320-200-IAE-set.xml
@@ -9,6 +9,7 @@
 		</sound>
 	
 		<description>Airbus A320 (IAE V2500)</description>
+		<status>Flyable</status>
 		<flight-model>jsb</flight-model>
 		<aero>A320-200-IAE</aero>
 		<model>
diff --git a/A320-main.xml b/A320-main.xml
index 8b35a7ec..85285e59 100644
--- a/A320-main.xml
+++ b/A320-main.xml
@@ -5,7 +5,6 @@
 	<sim>
 		
 		<author>Joshua Davidson (it0uchpods/411)</author>
-		<status>beta</status>
 
 		<model>
 			<pushback>
diff --git a/A321-200-IAE-set.xml b/A321-200-IAE-set.xml
index a3d6056d..0d6fb51b 100644
--- a/A321-200-IAE-set.xml
+++ b/A321-200-IAE-set.xml
@@ -9,6 +9,7 @@
 		</sound>
 	
 		<description>NOT READY: Airbus A321 (IAE V2500)</description>
+		<status>Not Flyable</status>
 		<flight-model>jsb</flight-model>
 		<aero>A321-200-IAE</aero>
 		<model>
diff --git a/README.md b/README.md
index 4bb28428..5cd03153 100644
--- a/README.md
+++ b/README.md
@@ -1,2 +1,2 @@
 # A320Family
-Airbus A320 Family for FlightGear. NOT FLYABLE YET!!! Only A319-200/A320-200/A321-200 with IAE engines for now, more models coming later, once the aircraft is flyable.
\ No newline at end of file
+Airbus A320 Family for FlightGear. A320-200 Flyable! A319-200/A321-200 Flyable soon! Note: Flaps indicator still missing from ECAM, coming soon!
\ No newline at end of file