diff --git a/Aircraft-yasim/a10cl-yasim.xml b/Aircraft-yasim/a10cl-yasim.xml
index e517b7220..256df1f1b 100644
--- a/Aircraft-yasim/a10cl-yasim.xml
+++ b/Aircraft-yasim/a10cl-yasim.xml
@@ -37,7 +37,7 @@
 
 <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="14" width="3" peak="1.3"/>
+  <stall aoa="17" width="3" 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"/>
@@ -64,7 +64,7 @@
 
 <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">
-  <stall aoa="20" width="5" peak="1.5"/>
+  <stall aoa="18" width="5" peak="1.5"/>
   <flap0 start="0" end="1" lift="1.6" drag="1.2"/>
   <control-input axis="/controls/elevator" control="FLAP0"/>
   <control-input axis="/controls/elevator-trim" control="FLAP0"/>
@@ -102,7 +102,7 @@
 
 <!-- Undercarriage -->
 <!-- nose -->
-<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.7">
+<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.8">
   <control-input axis="/controls/rudder" control="STEER" square="true"/>
   <control-input axis="/controls/gear-down" control="EXTEND"/>
   <control-speed control="EXTEND" transition-time="7"/>
@@ -133,7 +133,7 @@
 </gear>
 
 <!-- Ballast -->
-<ballast x="-3.5" y="0" z="1.0" mass="800"/> <!-- C/pit + Pilot -->
+<ballast x="-3.5" y="0" z="1.0" mass="1200"/> <!-- 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 -->
diff --git a/Aircraft-yasim/a10wl-yasim.xml b/Aircraft-yasim/a10wl-yasim.xml
index 9cde51d6a..fc411310e 100644
--- a/Aircraft-yasim/a10wl-yasim.xml
+++ b/Aircraft-yasim/a10wl-yasim.xml
@@ -37,7 +37,7 @@
 
 <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="14" width="3" peak="1.3"/>
+  <stall aoa="17" width="3" 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"/>
@@ -64,7 +64,7 @@
 
 <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">
-  <stall aoa="20" width="5" peak="1.5"/>
+  <stall aoa="18" width="5" peak="1.5"/>
   <flap0 start="0" end="1" lift="1.6" drag="1.2"/>
   <control-input axis="/controls/elevator" control="FLAP0"/>
   <control-input axis="/controls/elevator-trim" control="FLAP0"/>
@@ -102,7 +102,7 @@
 
 <!-- Undercarriage -->
 <!-- nose -->
-<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.7">
+<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.8">
   <control-input axis="/controls/rudder" control="STEER" square="true"/>
   <control-input axis="/controls/gear-down" control="EXTEND"/>
   <control-speed control="EXTEND" transition-time="7"/>
@@ -133,7 +133,7 @@
 </gear>
 
 <!-- Ballast -->
-<ballast x="-3.5" y="0" z="1.0" mass="800"/> <!-- C/pit + Pilot -->
+<ballast x="-3.5" y="0" z="1.0" mass="1200"/> <!-- 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 -->
@@ -141,81 +141,81 @@
 <!-- Weapons load -->
 
 <!-- AGM65 x 16 objects and ballast (Left to Right) -->
-<!-- Positioned in line with the aircraft CG (x) - y and z locs approximate -->
+<!-- Positioned just ahead of the aircraft CG (x) - y and z locs approximate -->
 
 <!-- Left Wing Outer AGM65 -->
 <fuselage ax="-7.65" ay="4.71" az="-0.47" bx="-10.15" by="4.71" bz="-0.35" width="0.35"/>
-<ballast x="-8.6" y="4.71" z="-0.41" mass="485"/>
+<ballast x="-8.9" y="4.71" z="-0.41" mass="485"/>
 
 <!-- Left Wing Mid Cluster Outer AGM65 -->
 <fuselage ax="-7.65" ay="3.89" az="-0.53" bx="-10.15" by="3.89" bz="-0.41" width="0.35"/>
-<ballast x="-8.6" y="3.89" z="-0.47" mass="485"/>
+<ballast x="-8.9" y="3.89" z="-0.47" mass="485"/>
 
 <!-- Left Wing Mid Cluster Mid AGM65 -->
 <fuselage ax="-7.65" ay="3.59" az="-0.96" bx="-10.15" by="3.59" bz="-0.84" width="0.35"/>
-<ballast x="-8.6" y="3.89" z="-0.90" mass="485"/>
+<ballast x="-8.9" y="3.89" z="-0.90" mass="485"/>
 
 <!-- Left Wing Mid Cluster Inner AGM65 -->
 <fuselage ax="-7.65" ay="3.21" az="-0.59" bx="-10.15" by="3.21" bz="-0.47" width="0.35"/>
-<ballast x="-8.6" y="3.21" z="-0.53" mass="485"/>
+<ballast x="-8.9" y="3.21" z="-0.53" mass="485"/>
 
 <!-- Left Wing Inner Cluster Outer AGM65 -->
 <fuselage ax="-7.65" ay="1.97" az="-0.65" bx="-10.15" by="1.97" bz="-0.53" width="0.35"/>
-<ballast x="-8.6" y="1.97" z="-0.59" mass="485"/>
+<ballast x="-8.9" y="1.97" z="-0.59" mass="485"/>
 
 <!-- Left Wing Inner Cluster Mid AGM65 -->
 <fuselage ax="-7.65" ay="1.63" az="-1.05" bx="-10.15" by="1.63" bz="-0.93" width="0.35"/>
-<ballast x="-8.6" y="1.63" z="-0.99" mass="485"/>
+<ballast x="-8.9" y="1.63" z="-0.99" mass="485"/>
 
 <!-- Left Wing Inner Cluster Inner AGM65 -->
 <fuselage ax="-7.65" ay="1.29" az="-0.65" bx="-10.15" by="1.29" bz="-0.53" width="0.35"/>
-<ballast x="-8.6" y="1.29" z="-0.59" mass="485"/>
+<ballast x="-8.9" y="1.29" z="-0.59" mass="485"/>
 
 <!-- Left Fuselage AGM65 -->
 <fuselage ax="-7.65" ay="0.53" az="-0.70" bx="-10.15" by="0.53" bz="-0.58" width="0.35"/>
-<ballast x="-8.6" y="0.53" z="-0.64" mass="485"/>
+<ballast x="-8.9" y="0.53" z="-0.64" mass="485"/>
 
 <!-- Right Wing Outer AGM65 -->
 <fuselage ax="-7.65" ay="-4.71" az="-0.47" bx="-10.15" by="-4.71" bz="-0.35" width="0.35"/>
-<ballast x="-8.6" y="-4.71" z="-0.41" mass="485"/>
+<ballast x="-8.9" y="-4.71" z="-0.41" mass="485"/>
 
 <!-- Right Wing Mid Cluster Outer AGM65 -->
 <fuselage ax="-7.65" ay="-3.89" az="-0.53" bx="-10.15" by="-3.89" bz="-0.41" width="0.35"/>
-<ballast x="-8.6" y="-3.89" z="-0.47" mass="485"/>
+<ballast x="-8.9" y="-3.89" z="-0.47" mass="485"/>
 
 <!-- Right Wing Mid Cluster Mid AGM65 -->
 <fuselage ax="-7.65" ay="-3.59" az="-0.96" bx="-10.15" by="-3.59" bz="-0.84" width="0.35"/>
-<ballast x="-8.6" y="-3.89" z="-0.90" mass="485"/>
+<ballast x="-8.9" y="-3.89" z="-0.90" mass="485"/>
 
 <!-- Right Wing Mid Cluster Inner AGM65 -->
 <fuselage ax="-7.65" ay="-3.21" az="-0.59" bx="-10.15" by="-3.21" bz="-0.47" width="0.35"/>
-<ballast x="-8.6" y="-3.21" z="-0.53" mass="485"/>
+<ballast x="-8.9" y="-3.21" z="-0.53" mass="485"/>
 
 <!-- Right Wing Inner Cluster Outer AGM65 -->
 <fuselage ax="-7.65" ay="-1.97" az="-0.65" bx="-10.15" by="-1.97" bz="-0.53" width="0.35"/>
-<ballast x="-8.6" y="-1.97" z="-0.59" mass="485"/>
+<ballast x="-8.9" y="-1.97" z="-0.59" mass="485"/>
 
 <!-- Right Wing Inner Cluster Mid AGM65 -->
 <fuselage ax="-7.65" ay="-1.63" az="-1.05" bx="-10.15" by="-1.63" bz="-0.93" width="0.35"/>
-<ballast x="-8.6" y="-1.63" z="-0.99" mass="485"/>
+<ballast x="-8.9" y="-1.63" z="-0.99" mass="485"/>
 
 <!-- Right Wing Inner Cluster Inner AGM65 -->
 <fuselage ax="-7.65" ay="-1.29" az="-0.65" bx="-10.15" by="-1.29" bz="-0.53" width="0.35"/>
-<ballast x="-8.6" y="-1.29" z="-0.59" mass="485"/>
+<ballast x="-8.9" y="-1.29" z="-0.59" mass="485"/>
 
 <!-- Right Fuselage AGM65 -->
 <fuselage ax="-7.65" ay="-0.53" az="-0.70" bx="-10.15" by="-0.53" bz="-0.58" width="0.35"/>
-<ballast x="-8.6" y="-0.53" z="-0.64" mass="485"/>
+<ballast x="-8.9" y="-0.53" z="-0.64" mass="485"/>
 
 <!-- AIM9 x 2 objects and ballast (guessed) - (Left to Right) -->
 <!-- Positioned ahead of the aircraft CG (x) - y and z locs approximate -->
 
 <!-- Left Wing AIM9 -->
 <fuselage ax="-6.9" ay="5.76" az="-0.27" bx="-9.9" by="5.76" bz="-0.15" width="0.13"/>
-<ballast x="-7.9" y="5.76" z="-0.21" mass="200"/>
+<ballast x="-8.9" y="5.76" z="-0.21" mass="200"/>
 
 <!-- Right Wing AIM9 -->
 <fuselage ax="-6.9" ay="-5.76" az="-0.27" bx="-9.9" by="-5.76" bz="-0.15" width="0.13"/>
-<ballast x="-7.9" y="-5.76" z="-0.21" mass="200"/>
+<ballast x="-8.9" y="-5.76" z="-0.21" mass="200"/>
 
 </airplane>