diff --git a/Aircraft/A320-jsbsim-set.xml b/Aircraft/A320-jsbsim-set.xml
new file mode 100755
index 000000000..e794e4e42
--- /dev/null
+++ b/Aircraft/A320-jsbsim-set.xml
@@ -0,0 +1,93 @@
+<?xml version="1.0"?>
+<PropertyList>
+ <sim>
+
+  <description>Airbus A320-200</description>
+
+  <flight-model>jsb</flight-model>
+  <aero>A320</aero>
+  <fuel-fraction>0.5</fuel-fraction>
+
+  <systems>
+   <electrical>
+    <path>Aircraft/Generic/generic-electrical.xml</path>
+   </electrical>
+  </systems> 
+  
+  <sound>
+   <audible>true</audible>
+   <path>Aircraft/A320/A320-sound.xml</path>
+  </sound>
+<!--
+  <panel>
+   <path>Aircraft/737/Panels/737-trans-mini-panel.xml</path>
+   <visibility>true</visibility>
+  </panel>
+-->
+  <hud>
+   <path>Huds/Custom/default.xml</path>
+   <visibility>true</visibility>
+  </hud>
+  
+  <model>
+   <path>Aircraft/A320/Models/a320-fb.xml</path>
+  </model>
+
+  <view>
+   <internal archive="y">true</internal>
+   <config>
+     <!-- x/y/z == right/up/back -->
+     <x-offset-m archive="y">-0.6</x-offset-m>
+     <y-offset-m archive="y">3.26</y-offset-m>
+     <z-offset-m archive="y">-16.16</z-offset-m>
+     <pitch-offset-deg archive="y">-11.0</pitch-offset-deg>
+   </config>
+  </view>
+  <view n="1">
+   <config>
+     <!-- big plane, so extend chase view offset a bit -->
+     <z-offset-m type="double" archive="y">-45.0</z-offset-m>
+   </config>
+  </view>
+  <view n="4">
+   <config>
+     <!-- big plane, so extend chase view offset a bit -->
+     <z-offset-m type="double" archive="y">-45.0</z-offset-m>
+   </config>
+  </view>
+<!--
+  <current-view>
+     <pitch-offset-deg archive="y">-11.0</pitch-offset-deg>
+  </current-view>
+-->
+ </sim>
+ 
+ <consumables>
+  <fuel>
+   <tank n="0">
+    <level-gal_us archive="y">1500</level-gal_us>
+   </tank>
+   <tank n="1">
+    <level-gal_us archive="y">1500</level-gal_us>
+   </tank>
+  </fuel>
+ </consumables>
+
+ <autopilot>
+   <config>
+     <min-climb-speed-kt type="float">150.0</min-climb-speed-kt>
+     <best-climb-speed-kt type="float">300.0</best-climb-speed-kt>
+     <target-climb-rate-fpm type="float">2000.0</target-climb-rate-fpm>
+     <target-descent-rate-fpm type="float">1500.0</target-descent-rate-fpm>
+     <elevator-adj-factor type="float">3500.0</elevator-adj-factor>
+     <integral-contribution type="float">0.01</integral-contribution>
+     <zero-pitch-throttle type="float">0.0001</zero-pitch-throttle>
+     <zero-pitch-trim-full-throttle type="float">0.0001</zero-pitch-trim-full-throttle>
+     <max-roll-deg type="float">30</max-roll-deg>
+     <max-aileron type="float">1.0</max-aileron>
+   </config>
+ </autopilot>
+
+</PropertyList>
+
+
diff --git a/Engine/CFM56_5_sim.xml b/Engine/CFM56_5_sim.xml
new file mode 100755
index 000000000..f71a340c9
--- /dev/null
+++ b/Engine/CFM56_5_sim.xml
@@ -0,0 +1,107 @@
+<?xml version="1.0"?>
+
+<!-- CFM56-5 turbofan engine model
+     Version 1.0, 4 Jun 2003, David Culp, davidculp2@attbi.com
+-->
+
+<FG_SIMTURBINE NAME="CFM56_5">
+  <!--
+     MAXMILTHRUST  max static thrust at S.L. (installed), lbf
+     BYPASSRATIO   bypass ratio
+     TSFC          thrust-specific fuel consumption (lbm/hr/lbf)
+     ATSFC         augmented TSFC (lbm/hr/lbf)
+     IDLEN1        idle percent rpm of fan spool
+     IDLEN2        idle percent rpm of inner spool
+     MAXN1         N1 at 100% throttle
+     MAXN2         N2 at 100% throttle
+     AUGMENTED     =1 if augmentation installed, else =0
+     INJECTED      =1 if water injection installed, else =0  
+
+     TABLE(0)      idle thrust vs. altitude and mach
+     TABLE(1)      maximum un-augmented thrust vs. altitude and mach
+     TABLE(2)      augmented thrust multiplier vs. altitude and mach
+     TABLE(3)      water-injection multiplier vs. altitude and mach
+  -->
+
+  MAXMILTHRUST 25000
+  BYPASSRATIO  5.9
+  TSFC         0.657
+  ATSFC        0.0
+  IDLEN1       30.0
+  IDLEN2       60.0
+  MAXN1        100.0
+  MAXN2        100.0
+  AUGMENTED    0
+  INJECTED     0
+
+
+  <TABLE NAME="IdleThrust" TYPE="TABLE">
+    Idle_power_thrust_factor
+    6
+    6
+    velocities/mach-norm
+    position/h-sl-ft
+    none
+                0   10000   20000   30000   40000  50000
+    0.0    0.0836  0.0528  0.0694  0.0899  0.1183  0.1467
+    0.2    0.0501  0.0335  0.0544  0.0797  0.1049  0.1341
+    0.4    0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
+    0.6   -0.0804 -0.0560 -0.0237  0.0276  0.0718  0.1073
+    0.8   -0.2129 -0.1498 -0.1025 -0.0195  0.0473  0.0868
+    1.0   -0.2839 -0.1104 -0.0469 -0.0270 -0.0158  0.0552
+  </TABLE>
+
+  <TABLE NAME="MilThrust" TYPE="TABLE">
+    Effects_of_altitude_and_mach_on_thrust
+    7
+    6
+    velocities/mach-norm
+    position/h-sl-ft
+    none
+               0    10000   20000     30000    40000    50000
+    0.0   1.0000   0.7216   0.4890   0.3115   0.1932   0.1104
+    0.2   1.0000   0.7216   0.4979   0.3186   0.1948   0.1104
+    0.4   0.9945   0.7344   0.5213   0.3383   0.2050   0.1230
+    0.6   0.9968   0.7759   0.5591   0.3675   0.2240   0.1309
+    0.8   0.9771   0.8025   0.6112   0.4196   0.2563   0.1522
+    0.9   0.9300   0.7900   0.6000   0.3900   0.2300   0.1300
+    1.0   0.5000   0.5000   0.4000   0.2000   0.1500   0.0900
+  </TABLE>
+
+  <TABLE NAME="AugThrust" TYPE="TABLE">
+    Augmented_thrust_factor
+    8
+    6
+    velocities/mach-norm
+    position/h-sl-ft
+    none
+                0    10000   20000     30000    40000    50000
+    0.0    1.4146   1.4146   1.4146   1.4146   1.4146   1.4146
+    0.2    1.4146   1.4146   1.4146   1.4146   1.4146   1.4146
+    0.4    1.4146   1.4146   1.4146   1.4146   1.4146   1.4146
+    0.6    1.4146   1.4146   1.4146   1.4146   1.4146   1.4146
+    0.8    1.4146   1.4146   1.4146   1.4146   1.4146   1.4146
+    1.0    1.4146   1.4146   1.4146   1.4146   1.4146   1.4146
+    1.2    1.4146   1.4146   1.4146   1.4146   1.4146   1.4146
+    1.4    1.4146   1.4146   1.4146   1.4146   1.4146   1.4146
+  </TABLE>
+
+  <TABLE NAME="WaterFactor" TYPE="TABLE">
+    Water_Injection_factor
+    8
+    6
+    velocities/mach-norm
+    position/h-sl-ft
+    none
+                0    10000   20000     30000    40000    50000
+    0.0    1.2000   1.2000   1.2000   1.2000   1.2000   1.2000
+    0.2    1.2000   1.2000   1.2000   1.2000   1.2000   1.2000
+    0.4    1.2000   1.2000   1.2000   1.2000   1.2000   1.2000
+    0.6    1.2000   1.2000   1.2000   1.2000   1.2000   1.2000
+    0.8    1.2000   1.2000   1.2000   1.2000   1.2000   1.2000
+    1.0    1.2000   1.2000   1.2000   1.2000   1.2000   1.2000
+    1.2    1.2000   1.2000   1.2000   1.2000   1.2000   1.2000
+    1.4    1.2000   1.2000   1.2000   1.2000   1.2000   1.2000
+  </TABLE>
+
+</FG_SIMTURBINE>