diff --git a/Aircraft-yasim/tsr2-yasim.xml b/Aircraft-yasim/tsr2-yasim.xml
index eff4a26d2..da61099f5 100755
--- a/Aircraft-yasim/tsr2-yasim.xml
+++ b/Aircraft-yasim/tsr2-yasim.xml
@@ -23,9 +23,9 @@
 
 <!-- Cruise configuration -->
 <!-- <cruise speed="500" alt="35000"> -->
- <cruise speed="850" alt="35000"> -->
-  <control-setting axis="/controls/throttle[0]" value="0.95"/>
-  <control-setting axis="/controls/throttle[1]" value="0.95"/>
+ <cruise speed="550" alt="35000"> -->
+  <control-setting axis="/controls/throttle[0]" value="0.5"/>
+  <control-setting axis="/controls/throttle[1]" value="0.5"/>
   <control-setting axis="/controls/flaps" value="0.0"/>
   <control-setting axis="/controls/gear-down" value="0"/>
  </cruise>
@@ -88,7 +88,7 @@
  </gear>
 
 <!-- left main -->
- <gear x="-4.0" y="1.19" z="-2.0" retract-time="7" compression="0.8">
+ <gear x="-4.0" y="2.5" z="-2.0" retract-time="7" compression="0.8">
   <control-input axis="/controls/brakes[0]" control="BRAKE"/>
   <control-input axis="/controls/gear-down" control="EXTEND"/>
   <control-speed control="EXTEND" transition-time="7"/>
@@ -96,7 +96,7 @@
  </gear>
 
 <!-- right main -->
- <gear x="-4.0" y="-1.19" z="-2.0" retract-time="7" compression="0.8">
+ <gear x="-4.0" y="-2.5" z="-2.0" retract-time="7" compression="0.8">
   <control-input axis="/controls/brakes[1]" control="BRAKE"/>
   <control-input axis="/controls/gear-down" control="EXTEND"/>
   <control-speed control="EXTEND" transition-time="7"/>
@@ -110,19 +110,19 @@
   <control-output control="EXTEND" prop="/canopy/position-norm"/>
  </gear>
 
- <jet x="-8.0" y="-1.0" z=".44" mass="4000" thrust="16600" afterburner="30600">
+ <jet x="-8.0" y="-1.0" z="0.4" mass="4000" thrust="16600" afterburner="30600">
 <!-- <jet x="-22.0" y="-1.0" z=".44" mass="4000" thrust="30600"> -->
   <control-input axis="/controls/throttle[0]" control="THROTTLE"/>
   <control-input axis="/controls/afterburner[0]" control="REHEAT"/>
  </jet>
 
- <jet x="-8.0" y="1.0" z=".44" mass="4000" thrust="16600" afterburner="30600">
+ <jet x="-8.0" y="1.0" z="0.4" mass="4000" thrust="16600" afterburner="30600">
 <!-- <jet x="-22.0" y="1.0" z=".44" mass="4000" thrust="30600"> -->
   <control-input axis="/controls/throttle[1]" control="THROTTLE"/>
   <control-input axis="/controls/afterburner[1]" control="REHEAT"/>
  </jet>
 
- <tank x="-2.0" y="0.0" z="1.0" jet="true" capacity="13000"/>
+ <tank x="-2.0" y="0.0" z="0.5" jet="true" capacity="13000"/>
  <tank x="-3.0" y="2.5" z="1.7" jet="true" capacity="11000"/>
  <tank x="-3.0" y="-2.5" z="1.7" jet="true" capacity="11000"/>
 
diff --git a/Aircraft/tsr2-yasim-set.xml b/Aircraft/tsr2-yasim-set.xml
index 8a4f9e145..9d3ab8baa 100755
--- a/Aircraft/tsr2-yasim-set.xml
+++ b/Aircraft/tsr2-yasim-set.xml
@@ -19,10 +19,10 @@ BAC TSR2 simulation config.
   </sound>
 
   <panel>
-   <path>Aircraft/c310/c310-vfr-panel.xml</path>
+   <path>Aircraft/tsr2/tsr2-vfr-panel.xml</path>
   </panel>
   <panel_2>
-   <path>Aircraft/c310/c310-mini-panel.xml</path>
+   <path>Aircraft/tsr2/tsr2-mini-panel.xml</path>
   </panel_2>
 
   <hud>
@@ -57,15 +57,15 @@ BAC TSR2 simulation config.
      <target-climb-rate-fpm type="float">12000.0</target-climb-rate-fpm>
      <target-descent-rate-fpm type="float">8000.0</target-descent-rate-fpm>
 
-     <elevator-adj-factor type="float">400.0</elevator-adj-factor>
+     <elevator-adj-factor type="float">800.0</elevator-adj-factor>
 
      <integral-contribution type="float">0.005</integral-contribution>
 
-     <max-aileron type="float">0.3</max-aileron>
+     <max-aileron type="float">0.5</max-aileron>
      <max-roll-deg type="float">60.0</max-roll-deg>
 
-     <roll-out-deg type="float">8.0</roll-out-deg>
-     <roll-out-smooth-deg type="float">8.0</roll-out-smooth-deg>
+     <roll-out-deg type="float">4.0</roll-out-deg>
+     <roll-out-smooth-deg type="float">20.0</roll-out-smooth-deg>
 
      <zero-pitch-throttle type="float">0.5</zero-pitch-throttle>
      <zero-pitch-trim-full-throttle type="float">0.001</zero-pitch-trim-full-throttle>