diff --git a/Aircraft-yasim/a10cl-yasim.xml b/Aircraft-yasim/a10cl-yasim.xml
index 256df1f1b..96d4902f0 100644
--- a/Aircraft-yasim/a10cl-yasim.xml
+++ b/Aircraft-yasim/a10cl-yasim.xml
@@ -8,16 +8,17 @@
 <airplane mass="37700">
 
 <!-- Approach configuration -->
-<approach speed="110" aoa="14">
+<approach speed="110" aoa="8">
   <control-setting axis="/controls/throttle[0]" value="0.5"/>
+  <control-setting axis="/controls/throttle[1]" value="0.5"/>
   <control-setting axis="/controls/flaps" value="1.0"/>
-  <control-setting axis="/controls/spoilers" value="1.0"/>
   <control-setting axis="/controls/gear-down" value="1"/>
 </approach>
 
 <!-- Cruise configuration -->
-<cruise speed="380" alt="35000">
-  <control-setting axis="/controls/throttle[0]" value="0.8"/>
+<cruise speed="398" alt="1200">
+  <control-setting axis="/controls/throttle[0]" value="1.0"/>
+  <control-setting axis="/controls/throttle[1]" value="1.0"/>
   <control-setting axis="/controls/flaps" value="0.0"/>
   <control-setting axis="/controls/gear-down" value="0"/>
 </cruise>
@@ -37,7 +38,7 @@
 
 <wing x="-8.8" y="0.5" z="-0.5" taper="0.6" incidence="-1.0"
       length="8.3" chord="3.1" sweep="0.0" dihedral="3.0" camber="0.006">
-  <stall aoa="17" width="3" peak="1.3"/>
+  <stall aoa="17" width="6" peak="1.3"/>
   <flap0 start="0.04" end="0.51" lift="1.5" drag="1.2"/>
   <flap1 start="0.54" end="0.86" lift="1.3" drag="1.2"/>
   <spoiler start="0.54" end="0.86" lift="0.1" drag="20.0"/>
@@ -62,27 +63,27 @@
 
 </wing>
 
-<hstab x="-15.5" y="0.4" z="0.4" taper="0.0" effectiveness="1.2"
-       length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0.0">
+<hstab x="-15.5" y="0.4" z="0.4" taper="0.0" effectiveness="3"
+       length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0">
   <stall aoa="18" width="5" peak="1.5"/>
-  <flap0 start="0" end="1" lift="1.6" drag="1.2"/>
+  <flap0 start="0" end="1" lift="1.5" drag="1.2"/>
   <control-input axis="/controls/elevator" control="FLAP0"/>
   <control-input axis="/controls/elevator-trim" control="FLAP0"/>
   <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
 </hstab>
 
-<vstab x="-15.0" y="2.5" z="-0.9" taper="0.7"
+<vstab x="-15.0" y="2.5" z="-0.9" taper="0.7" effectiveness="2"
        length="2.8" chord="2.0" sweep="0.0">
   <stall aoa="16" width="5" peak="1.5"/>
-  <flap0 start="0" end="1" lift="1.15" drag="1.3"/>
+  <flap0 start="0" end="1" lift="1.3" drag="1.3"/>
   <control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
   <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
 </vstab>
 
-<vstab x="-15.0" y="-2.5" z="-0.9" taper="0.7"
+<vstab x="-15.0" y="-2.5" z="-0.9" taper="0.7" effectiveness="2"
        length="2.8" chord="2.0" sweep="0.0">
   <stall aoa="16" width="5" peak="1.5"/>
-  <flap0 start="0" end="1" lift="1.15" drag="1.3"/>
+  <flap0 start="0" end="1" lift="1.3" drag="1.3"/>
   <control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
   <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
 </vstab>
@@ -102,7 +103,7 @@
 
 <!-- Undercarriage -->
 <!-- nose -->
-<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.8">
+<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.7">
   <control-input axis="/controls/rudder" control="STEER" square="true"/>
   <control-input axis="/controls/gear-down" control="EXTEND"/>
   <control-speed control="EXTEND" transition-time="7"/>
@@ -133,9 +134,8 @@
 </gear>
 
 <!-- Ballast -->
-<ballast x="-3.5" y="0" z="1.0" mass="1200"/> <!-- C/pit + Pilot -->
+<ballast x="-3.5" y="0" z="1.0" mass="2000"/> <!-- Armored cockpit -->
 <ballast x="-4.0" y="0" z="-1.0" mass="4000"/> <!-- Gun -->
 <ballast x="-5.0" y="0" z="0.0" mass="1000"/> <!-- avionics -->
-<ballast x="-7.0" y="0" z="-0.8" mass="2500"/> <!-- trim ballast -->
 
 </airplane>
diff --git a/Aircraft-yasim/a10fl-yasim.xml b/Aircraft-yasim/a10fl-yasim.xml
new file mode 100755
index 000000000..73331a774
--- /dev/null
+++ b/Aircraft-yasim/a10fl-yasim.xml
@@ -0,0 +1,153 @@
+<!--  A10 yasim config.  This is a hack and not an authentic
+      representation of the aircraft.  Having said that, the
+      numbers, where I could find them, roughly match those of
+      the original aircraft.
+      Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
+-->
+
+<airplane mass="37700">
+
+<!-- Approach configuration -->
+<approach speed="110" aoa="8">
+  <control-setting axis="/controls/throttle[0]" value="0.5"/>
+  <control-setting axis="/controls/throttle[1]" value="0.5"/>
+  <control-setting axis="/controls/flaps" value="1.0"/>
+  <control-setting axis="/controls/gear-down" value="1"/>
+</approach>
+
+<!-- Cruise configuration -->
+<cruise speed="398" alt="1200">
+  <control-setting axis="/controls/throttle[0]" value="1.0"/>
+  <control-setting axis="/controls/throttle[1]" value="1.0"/>
+  <control-setting axis="/controls/flaps" value="0.0"/>
+  <control-setting axis="/controls/gear-down" value="0"/>
+</cruise>
+
+<cockpit x="4.5" y="0.0" z="1.2"/>
+
+<fuselage ax="8" ay="0" az="0" bx="-8.26" by="0" bz="0"
+          width="1.4"/>
+
+<!-- Left Engine -->
+<fuselage ax="-2" ay="1.50" az="1" bx="-5.5" by="1.50" bz="0.8"
+          width="1.5"/>
+
+<!-- Right Engine -->
+<fuselage ax="-2" ay="-1.50" az="1" bx="-5.5" by="-1.50" bz="0.8"
+          width="1.5"/>
+
+<wing x="-0.8" y="0.5" z="-0.5" taper="0.6" incidence="-1.0"
+      length="8.3" chord="3.1" sweep="0.0" dihedral="3.0" camber="0.006">
+  <stall aoa="17" width="6" peak="1.3"/>
+  <flap0 start="0.04" end="0.51" lift="1.5" drag="1.2"/>
+  <flap1 start="0.54" end="0.86" lift="1.3" drag="1.2"/>
+  <spoiler start="0.54" end="0.86" lift="0.1" drag="20.0"/>
+
+  <control-input axis="/controls/flaps" control="FLAP0"/>
+  <control-input axis="/controls/aileron" control="FLAP1" split="true"/>
+  <control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/>
+  <control-input axis="/controls/spoilers" control="SPOILER"/>
+
+  <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
+  <control-output control="FLAP1" side="left"
+      prop="/surface-positions/left-aileron-pos-norm"/>
+  <control-output control="FLAP1" side="right"
+      prop="/surface-positions/right-aileron-pos-norm"/>
+  <control-output control="SPOILER" side="left"
+		  prop="/surface-positions/left-spoiler-pos-norm"/>
+  <control-output control="SPOILER" side="right"
+		  prop="/surface-positions/right-spoiler-pos-norm"/>
+
+  <control-speed control="FLAP0" transition-time="5"/>
+  <control-speed control="SPOILER" transition-time="0.5"/>
+
+</wing>
+
+<hstab x="-7.5" y="0.4" z="0.4" taper="0.0" effectiveness="3"
+       length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0">
+  <stall aoa="18" width="5" peak="1.5"/>
+  <flap0 start="0" end="1" lift="1.5" drag="1.2"/>
+  <control-input axis="/controls/elevator" control="FLAP0"/>
+  <control-input axis="/controls/elevator-trim" control="FLAP0"/>
+  <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
+</hstab>
+
+<vstab x="-7.0" y="2.5" z="-0.9" taper="0.7" effectiveness="2"
+       length="2.8" chord="2.0" sweep="0.0">
+  <stall aoa="16" width="5" peak="1.5"/>
+  <flap0 start="0" end="1" lift="1.3" drag="1.3"/>
+  <control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
+  <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
+</vstab>
+
+<vstab x="-7.0" y="-2.5" z="-0.9" taper="0.7" effectiveness="2"
+       length="2.8" chord="2.0" sweep="0.0">
+  <stall aoa="16" width="5" peak="1.5"/>
+  <flap0 start="0" end="1" lift="1.3" drag="1.3"/>
+  <control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
+  <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
+</vstab>
+
+<!-- Engines and tanks -->
+<jet x="-3.8" y="-1.5" z="1.0" mass="1000" thrust="9065">
+  <control-input axis="/controls/throttle[0]" control="THROTTLE"/>
+</jet>
+
+<jet x="-3.8" y="1.5" z="1.0" mass="1000" thrust="9065">
+  <control-input axis="/controls/throttle[1]" control="THROTTLE"/>
+</jet>
+
+<tank x="-0.5" y="-1.5" z="0.0" jet="true" capacity="2000"/>
+<tank x="-0.5" y="1.5" z="0.0" jet="true" capacity="2000"/>
+<tank x="-0.5" y="0" z="0.0" jet="true" capacity="6700"/>
+<!-- Ferry Tanks -->
+<tank x="-0.5" y="1.29" z="-0.7" jet="true" capacity="4032"/>
+<tank x="-0.5" y="0" z="-0.7" jet="true" capacity="4032"/>
+<tank x="-0.5" y="-1.29" z="-0.7" jet="true" capacity="4032"/>
+
+<!-- Undercarriage -->
+<!-- nose -->
+<gear x="5.1" y="0.4" z="-2.8" retract-time="7" compression="0.7">
+  <control-input axis="/controls/rudder" control="STEER" square="true"/>
+  <control-input axis="/controls/gear-down" control="EXTEND"/>
+  <control-speed control="EXTEND" transition-time="7"/>
+  <control-output control="EXTEND" prop="/gear/gear/position-norm"/>
+</gear>
+
+<!-- left main -->
+<gear x="-1.0" y="2.5" z="-2.8" retract-time="7" compression="0.6">
+  <control-input axis="/controls/brakes[0]" control="BRAKE"/>
+  <control-input axis="/controls/gear-down" control="EXTEND"/>
+  <control-speed control="EXTEND" transition-time="7"/>
+  <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
+</gear>
+
+<!-- right main -->
+<gear x="-1.0" y="-2.5" z="-2.8" retract-time="7" compression="0.6">
+  <control-input axis="/controls/brakes[1]" control="BRAKE"/>
+  <control-input axis="/controls/gear-down" control="EXTEND"/>
+  <control-speed control="EXTEND" transition-time="7"/>
+  <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
+</gear>
+
+<!-- Canopy -->
+<gear x="5.4" y="0.0" z="1.4" retract-time="7" compression="0.6">
+  <control-input axis="/controls/parking-brake" control="EXTEND"/>
+  <control-speed control="EXTEND" transition-time="5"/>
+  <control-output control="EXTEND" prop="/canopy/position-norm"/>
+</gear>
+
+<!-- Ballast -->
+<ballast x="4.5" y="0" z="1.0" mass="2000"/> <!-- Armored cockpit -->
+<ballast x="4.0" y="0" z="-1.0" mass="4000"/> <!-- Gun -->
+<ballast x="3.0" y="0" z="0.0" mass="1000"/> <!-- avionics -->
+
+<!-- Ferry Tanks -->
+<fuselage ax="1.1" ay="0.0" az="-1.2" bx="-2.9" by="0.0" bz="-1.2"
+          width="0.8"/>
+<fuselage ax="1.1" ay="1.29" az="-1.2" bx="-2.9" by="1.29" bz="-1.2"
+          width="0.8"/>
+<fuselage ax="1.1" ay="-1.29" az="-1.2" bx="-2.9" by="-1.29" bz="-1.2"
+          width="0.8"/>
+
+</airplane>
diff --git a/Aircraft-yasim/a10wl-yasim.xml b/Aircraft-yasim/a10wl-yasim.xml
index fc411310e..0d7738a24 100644
--- a/Aircraft-yasim/a10wl-yasim.xml
+++ b/Aircraft-yasim/a10wl-yasim.xml
@@ -8,16 +8,17 @@
 <airplane mass="45860">
 
 <!-- Approach configuration -->
-<approach speed="110" aoa="14">
+<approach speed="110" aoa="8">
   <control-setting axis="/controls/throttle[0]" value="0.5"/>
+  <control-setting axis="/controls/throttle[1]" value="0.5"/>
   <control-setting axis="/controls/flaps" value="1.0"/>
-  <control-setting axis="/controls/spoilers" value="1.0"/>
   <control-setting axis="/controls/gear-down" value="1"/>
 </approach>
 
 <!-- Cruise configuration -->
-<cruise speed="380" alt="35000">
-  <control-setting axis="/controls/throttle[0]" value="0.8"/>
+<cruise speed="398" alt="1200">
+  <control-setting axis="/controls/throttle[0]" value="1.0"/>
+  <control-setting axis="/controls/throttle[1]" value="1.0"/>
   <control-setting axis="/controls/flaps" value="0.0"/>
   <control-setting axis="/controls/gear-down" value="0"/>
 </cruise>
@@ -37,7 +38,7 @@
 
 <wing x="-8.8" y="0.5" z="-0.5" taper="0.6" incidence="-1.0"
       length="8.3" chord="3.1" sweep="0.0" dihedral="3.0" camber="0.006">
-  <stall aoa="17" width="3" peak="1.3"/>
+  <stall aoa="17" width="6" peak="1.3"/>
   <flap0 start="0.04" end="0.51" lift="1.5" drag="1.2"/>
   <flap1 start="0.54" end="0.86" lift="1.3" drag="1.2"/>
   <spoiler start="0.54" end="0.86" lift="0.1" drag="20.0"/>
@@ -62,27 +63,27 @@
 
 </wing>
 
-<hstab x="-15.5" y="0.4" z="0.4" taper="0.0" effectiveness="1.2"
-       length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0.0">
+<hstab x="-15.5" y="0.4" z="0.4" taper="0.0" effectiveness="3"
+       length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0">
   <stall aoa="18" width="5" peak="1.5"/>
-  <flap0 start="0" end="1" lift="1.6" drag="1.2"/>
+  <flap0 start="0" end="1" lift="1.5" drag="1.2"/>
   <control-input axis="/controls/elevator" control="FLAP0"/>
   <control-input axis="/controls/elevator-trim" control="FLAP0"/>
   <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
 </hstab>
 
-<vstab x="-15.0" y="2.5" z="-0.9" taper="0.7"
+<vstab x="-15.0" y="2.5" z="-0.9" taper="0.7" effectiveness="2"
        length="2.8" chord="2.0" sweep="0.0">
   <stall aoa="16" width="5" peak="1.5"/>
-  <flap0 start="0" end="1" lift="1.15" drag="1.3"/>
+  <flap0 start="0" end="1" lift="1.3" drag="1.3"/>
   <control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
   <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
 </vstab>
 
-<vstab x="-15.0" y="-2.5" z="-0.9" taper="0.7"
+<vstab x="-15.0" y="-2.5" z="-0.9" taper="0.7" effectiveness="2"
        length="2.8" chord="2.0" sweep="0.0">
   <stall aoa="16" width="5" peak="1.5"/>
-  <flap0 start="0" end="1" lift="1.15" drag="1.3"/>
+  <flap0 start="0" end="1" lift="1.3" drag="1.3"/>
   <control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
   <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
 </vstab>
@@ -133,10 +134,9 @@
 </gear>
 
 <!-- Ballast -->
-<ballast x="-3.5" y="0" z="1.0" mass="1200"/> <!-- C/pit + Pilot -->
+<ballast x="-3.5" y="0" z="1.0" mass="2000"/> <!-- C/pit + Pilot -->
 <ballast x="-4.0" y="0" z="-1.0" mass="4000"/> <!-- Gun -->
 <ballast x="-5.0" y="0" z="0.0" mass="1000"/> <!-- avionics -->
-<ballast x="-7.0" y="0" z="-0.8" mass="2500"/> <!-- trim ballast -->
 
 <!-- Weapons load -->
 
diff --git a/Aircraft/a10cl-yasim-set.xml b/Aircraft/a10cl-yasim-set.xml
index 12bd2ca53..376158501 100644
--- a/Aircraft/a10cl-yasim-set.xml
+++ b/Aircraft/a10cl-yasim-set.xml
@@ -19,10 +19,10 @@ Fairchild A10 (Clean) )simulation config.
   </sound>
 
   <panel>
-   <path>Aircraft/c310/c310-vfr-panel.xml</path>
+   <path>Aircraft/a10/a10-vfr-panel.xml</path>
   </panel>
   <panel_2>
-   <path>Aircraft/c310/c310-mini-panel.xml</path>
+   <path>Aircraft/a10/a10-mini-panel.xml</path>
   </panel_2>
 
   <hud>
@@ -36,7 +36,7 @@ Fairchild A10 (Clean) )simulation config.
 
   <view n="1">
    <config>
-     <z-offset-m type="double" archive="y">-70.0</z-offset-m>
+     <z-offset-m type="double" archive="y">-50.0</z-offset-m>
    </config>
 
   </view>
diff --git a/Aircraft/a10wl-yasim-set.xml b/Aircraft/a10wl-yasim-set.xml
index 4ed1ba855..0e6bee0cf 100644
--- a/Aircraft/a10wl-yasim-set.xml
+++ b/Aircraft/a10wl-yasim-set.xml
@@ -19,10 +19,10 @@ Fairchild A10 (Weapon load) simulation config.
   </sound>
 
   <panel>
-   <path>Aircraft/c310/c310-vfr-panel.xml</path>
+   <path>Aircraft/a10/a10-vfr-panel.xml</path>
   </panel>
   <panel_2>
-   <path>Aircraft/c310/c310-mini-panel.xml</path>
+   <path>Aircraft/a10/a10-mini-panel.xml</path>
   </panel_2>
 
   <hud>
@@ -36,7 +36,7 @@ Fairchild A10 (Weapon load) simulation config.
 
   <view n="1">
    <config>
-     <z-offset-m type="double" archive="y">-70.0</z-offset-m>
+     <z-offset-m type="double" archive="y">-50.0</z-offset-m>
    </config>
 
   </view>