From 3b71d1337ec371eff7b038a624f868dce654bf35 Mon Sep 17 00:00:00 2001
From: Joshua Davidson <joshuadavidson2000@gmail.com>
Date: Fri, 20 Oct 2017 14:05:58 -0400
Subject: [PATCH] A32X: Cleanup

---
 A318-100-CFM.xml      |  4 +--
 A319-100-CFM.xml      |  4 +--
 A319-100-IAE.xml      |  4 +--
 A320-100-CFM.xml      |  4 +--
 A321-200-CFM.xml      |  4 +--
 A321-200-IAE.xml      |  4 +--
 A321neo-CFM.xml       |  4 +--
 A321neo-PW.xml        |  4 +--
 Engines/cfm56_5a1.xml | 59 -------------------------------------------
 Engines/cfm56_5b3.xml | 59 -------------------------------------------
 Engines/cfm56_5b6.xml | 59 -------------------------------------------
 Engines/cfm56_5b9.xml | 59 -------------------------------------------
 Engines/leap1a32.xml  | 59 -------------------------------------------
 Engines/pw1133g.xml   | 59 -------------------------------------------
 Engines/v2522_a5.xml  | 59 -------------------------------------------
 Engines/v2533_a5.xml  | 59 -------------------------------------------
 revision.txt          |  2 +-
 17 files changed, 17 insertions(+), 489 deletions(-)
 delete mode 100644 Engines/cfm56_5a1.xml
 delete mode 100644 Engines/cfm56_5b3.xml
 delete mode 100644 Engines/cfm56_5b6.xml
 delete mode 100644 Engines/cfm56_5b9.xml
 delete mode 100644 Engines/leap1a32.xml
 delete mode 100644 Engines/pw1133g.xml
 delete mode 100644 Engines/v2522_a5.xml
 delete mode 100644 Engines/v2533_a5.xml

diff --git a/A318-100-CFM.xml b/A318-100-CFM.xml
index 226263ca..c68df8ee 100644
--- a/A318-100-CFM.xml
+++ b/A318-100-CFM.xml
@@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 	</ground_reactions>
 
 	<propulsion>
-		<engine file="cfm56_5b9">
+		<engine file="cfm56_5b4">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> -5.755 </y>
@@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 			</thruster>
 		</engine>
 
-		<engine file="cfm56_5b9">
+		<engine file="cfm56_5b4">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> 5.755 </y>
diff --git a/A319-100-CFM.xml b/A319-100-CFM.xml
index 54482609..c68df8ee 100644
--- a/A319-100-CFM.xml
+++ b/A319-100-CFM.xml
@@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 	</ground_reactions>
 
 	<propulsion>
-		<engine file="cfm56_5b6">
+		<engine file="cfm56_5b4">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> -5.755 </y>
@@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 			</thruster>
 		</engine>
 
-		<engine file="cfm56_5b6">
+		<engine file="cfm56_5b4">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> 5.755 </y>
diff --git a/A319-100-IAE.xml b/A319-100-IAE.xml
index e9ae7ceb..03df8631 100644
--- a/A319-100-IAE.xml
+++ b/A319-100-IAE.xml
@@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 	</ground_reactions>
 
 	<propulsion>
-		<engine file="v2522_a5">
+		<engine file="v2527_a5">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> -5.755 </y>
@@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 			</thruster>
 		</engine>
 
-		<engine file="v2522_a5">
+		<engine file="v2527_a5">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> 5.755 </y>
diff --git a/A320-100-CFM.xml b/A320-100-CFM.xml
index c2991ad4..0cc12ac7 100644
--- a/A320-100-CFM.xml
+++ b/A320-100-CFM.xml
@@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 	</ground_reactions>
 
 	<propulsion>
-		<engine file="cfm56_5a1">
+		<engine file="cfm56_5a4">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> -5.755 </y>
@@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 			</thruster>
 		</engine>
 
-		<engine file="cfm56_5a1">
+		<engine file="cfm56_5a4">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> 5.755 </y>
diff --git a/A321-200-CFM.xml b/A321-200-CFM.xml
index 90f669d6..c68df8ee 100644
--- a/A321-200-CFM.xml
+++ b/A321-200-CFM.xml
@@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 	</ground_reactions>
 
 	<propulsion>
-		<engine file="cfm56_5b3">
+		<engine file="cfm56_5b4">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> -5.755 </y>
@@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 			</thruster>
 		</engine>
 
-		<engine file="cfm56_5b3">
+		<engine file="cfm56_5b4">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> 5.755 </y>
diff --git a/A321-200-IAE.xml b/A321-200-IAE.xml
index 21f41271..03df8631 100644
--- a/A321-200-IAE.xml
+++ b/A321-200-IAE.xml
@@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 	</ground_reactions>
 
 	<propulsion>
-		<engine file="v2533_a5">
+		<engine file="v2527_a5">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> -5.755 </y>
@@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 			</thruster>
 		</engine>
 
-		<engine file="v2533_a5">
+		<engine file="v2527_a5">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> 5.755 </y>
diff --git a/A321neo-CFM.xml b/A321neo-CFM.xml
index 557211e2..e9917700 100644
--- a/A321neo-CFM.xml
+++ b/A321neo-CFM.xml
@@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 	</ground_reactions>
 
 	<propulsion>
-		<engine file="leap1a32">
+		<engine file="leap1a26">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> -5.755 </y>
@@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 			</thruster>
 		</engine>
 
-		<engine file="leap1a32">
+		<engine file="leap1a26">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> 5.755 </y>
diff --git a/A321neo-PW.xml b/A321neo-PW.xml
index 1f777642..eddbe032 100644
--- a/A321neo-PW.xml
+++ b/A321neo-PW.xml
@@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 	</ground_reactions>
 
 	<propulsion>
-		<engine file="pw1133g">
+		<engine file="pw1127g">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> -5.755 </y>
@@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
 			</thruster>
 		</engine>
 
-		<engine file="pw1133g">
+		<engine file="pw1127g">
 			<location unit="M">
 				<x> 14.3962788 </x>
 				<y> 5.755 </y>
diff --git a/Engines/cfm56_5a1.xml b/Engines/cfm56_5a1.xml
deleted file mode 100644
index 12ec5680..00000000
--- a/Engines/cfm56_5a1.xml
+++ /dev/null
@@ -1,59 +0,0 @@
-<?xml version="1.0"?>
-
-<!--
-#########################################
-# Copyright (c) it0uchpods Design Group #
-#########################################
--->
-
-<turbine_engine name="CFM56_5A1">
-
-	<milthrust>     27000 </milthrust>
-	<bypassratio>     8.1 </bypassratio>
-	<tsfc>            0.5 </tsfc>
-	<bleed>          0.03 </bleed>
-	<idlen1>         19.7 </idlen1>
-	<idlen2>         61.2 </idlen2>
-	<n1spinup>        0.2 </n1spinup>
-	<n2spinup>        2.0 </n2spinup>
-	<maxn1>         103.8 </maxn1>
-	<maxn2>          99.6 </maxn2>
-	<augmented>         0 </augmented>
-	<injected>          0 </injected>
-
-	<function name="IdleThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			    -10000   0       10000   20000   30000   40000   50000
-			0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467
-			0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
-			0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
-			0.6  0.0     0.0     0.0     0.0     0.0276  0.0718  0.1073
-			0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900
-			1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800
-			</tableData>
-		</table>
-	</function>
-
-	<function name="MilThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			     -10000   0       10000   20000   30000   40000   50000
-			0.0   1.2600  1.0000  0.7400  0.5440  0.3720  0.2410  0.0000
-			0.2   1.1710  0.9740  0.6970  0.5160  0.3650  0.2310  0.0000
-			0.4   1.1500  0.9570  0.6920  0.5260  0.3670  0.2230  0.0000
-			0.6   1.1810  0.9410  0.7210  0.5460  0.3380  0.1880  0.0000
-			0.8   1.2290  1.0200  0.7820  0.5370  0.2840  0.1450  0.0000
-			0.9   1.2580  1.0200  0.7820  0.5020  0.2510  0.0650  0.0000
-			1.0   1.1810  0.9510  0.7210  0.4210  0.1540  0.0150  0.0000
-			1.2   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			1.4   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			</tableData>
-		</table>
-	</function>
-	
-</turbine_engine>
diff --git a/Engines/cfm56_5b3.xml b/Engines/cfm56_5b3.xml
deleted file mode 100644
index 89709acc..00000000
--- a/Engines/cfm56_5b3.xml
+++ /dev/null
@@ -1,59 +0,0 @@
-<?xml version="1.0"?>
-
-<!--
-#########################################
-# Copyright (c) it0uchpods Design Group #
-#########################################
--->
-
-<turbine_engine name="CFM56_5B3">
-
-	<milthrust>     27000 </milthrust>
-	<bypassratio>     8.1 </bypassratio>
-	<tsfc>            0.5 </tsfc>
-	<bleed>          0.03 </bleed>
-	<idlen1>         19.7 </idlen1>
-	<idlen2>         61.2 </idlen2>
-	<n1spinup>        0.2 </n1spinup>
-	<n2spinup>        2.0 </n2spinup>
-	<maxn1>         103.8 </maxn1>
-	<maxn2>          99.6 </maxn2>
-	<augmented>         0 </augmented>
-	<injected>          0 </injected>
-
-	<function name="IdleThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			    -10000   0       10000   20000   30000   40000   50000
-			0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467
-			0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
-			0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
-			0.6  0.0     0.0     0.0     0.0     0.0276  0.0718  0.1073
-			0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900
-			1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800
-			</tableData>
-		</table>
-	</function>
-
-	<function name="MilThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			     -10000   0       10000   20000   30000   40000   50000
-			0.0   1.2600  1.0000  0.7400  0.5440  0.3720  0.2410  0.0000
-			0.2   1.1710  0.9740  0.6970  0.5160  0.3650  0.2310  0.0000
-			0.4   1.1500  0.9570  0.6920  0.5260  0.3670  0.2230  0.0000
-			0.6   1.1810  0.9410  0.7210  0.5460  0.3380  0.1880  0.0000
-			0.8   1.2290  1.0200  0.7820  0.5370  0.2840  0.1450  0.0000
-			0.9   1.2580  1.0200  0.7820  0.5020  0.2510  0.0650  0.0000
-			1.0   1.1810  0.9510  0.7210  0.4210  0.1540  0.0150  0.0000
-			1.2   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			1.4   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			</tableData>
-		</table>
-	</function>
-	
-</turbine_engine>
diff --git a/Engines/cfm56_5b6.xml b/Engines/cfm56_5b6.xml
deleted file mode 100644
index d7e00b42..00000000
--- a/Engines/cfm56_5b6.xml
+++ /dev/null
@@ -1,59 +0,0 @@
-<?xml version="1.0"?>
-
-<!--
-#########################################
-# Copyright (c) it0uchpods Design Group #
-#########################################
--->
-
-<turbine_engine name="CFM56_5B6">
-
-	<milthrust>     27000 </milthrust>
-	<bypassratio>     8.1 </bypassratio>
-	<tsfc>            0.5 </tsfc>
-	<bleed>          0.03 </bleed>
-	<idlen1>         19.7 </idlen1>
-	<idlen2>         61.2 </idlen2>
-	<n1spinup>        0.2 </n1spinup>
-	<n2spinup>        2.0 </n2spinup>
-	<maxn1>         103.8 </maxn1>
-	<maxn2>          99.6 </maxn2>
-	<augmented>         0 </augmented>
-	<injected>          0 </injected>
-
-	<function name="IdleThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			    -10000   0       10000   20000   30000   40000   50000
-			0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467
-			0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
-			0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
-			0.6  0.0     0.0     0.0     0.0     0.0276  0.0718  0.1073
-			0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900
-			1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800
-			</tableData>
-		</table>
-	</function>
-
-	<function name="MilThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			     -10000   0       10000   20000   30000   40000   50000
-			0.0   1.2600  1.0000  0.7400  0.5440  0.3720  0.2410  0.0000
-			0.2   1.1710  0.9740  0.6970  0.5160  0.3650  0.2310  0.0000
-			0.4   1.1500  0.9570  0.6920  0.5260  0.3670  0.2230  0.0000
-			0.6   1.1810  0.9410  0.7210  0.5460  0.3380  0.1880  0.0000
-			0.8   1.2290  1.0200  0.7820  0.5370  0.2840  0.1450  0.0000
-			0.9   1.2580  1.0200  0.7820  0.5020  0.2510  0.0650  0.0000
-			1.0   1.1810  0.9510  0.7210  0.4210  0.1540  0.0150  0.0000
-			1.2   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			1.4   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			</tableData>
-		</table>
-	</function>
-	
-</turbine_engine>
diff --git a/Engines/cfm56_5b9.xml b/Engines/cfm56_5b9.xml
deleted file mode 100644
index 21f5c507..00000000
--- a/Engines/cfm56_5b9.xml
+++ /dev/null
@@ -1,59 +0,0 @@
-<?xml version="1.0"?>
-
-<!--
-#########################################
-# Copyright (c) it0uchpods Design Group #
-#########################################
--->
-
-<turbine_engine name="CFM56_5B9">
-
-	<milthrust>     27000 </milthrust>
-	<bypassratio>     8.1 </bypassratio>
-	<tsfc>            0.5 </tsfc>
-	<bleed>          0.03 </bleed>
-	<idlen1>         19.7 </idlen1>
-	<idlen2>         61.2 </idlen2>
-	<n1spinup>        0.2 </n1spinup>
-	<n2spinup>        2.0 </n2spinup>
-	<maxn1>         103.8 </maxn1>
-	<maxn2>          99.6 </maxn2>
-	<augmented>         0 </augmented>
-	<injected>          0 </injected>
-
-	<function name="IdleThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			    -10000   0       10000   20000   30000   40000   50000
-			0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467
-			0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
-			0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
-			0.6  0.0     0.0     0.0     0.0     0.0276  0.0718  0.1073
-			0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900
-			1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800
-			</tableData>
-		</table>
-	</function>
-
-	<function name="MilThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			     -10000   0       10000   20000   30000   40000   50000
-			0.0   1.2600  1.0000  0.7400  0.5440  0.3720  0.2410  0.0000
-			0.2   1.1710  0.9740  0.6970  0.5160  0.3650  0.2310  0.0000
-			0.4   1.1500  0.9570  0.6920  0.5260  0.3670  0.2230  0.0000
-			0.6   1.1810  0.9410  0.7210  0.5460  0.3380  0.1880  0.0000
-			0.8   1.2290  1.0200  0.7820  0.5370  0.2840  0.1450  0.0000
-			0.9   1.2580  1.0200  0.7820  0.5020  0.2510  0.0650  0.0000
-			1.0   1.1810  0.9510  0.7210  0.4210  0.1540  0.0150  0.0000
-			1.2   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			1.4   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			</tableData>
-		</table>
-	</function>
-	
-</turbine_engine>
diff --git a/Engines/leap1a32.xml b/Engines/leap1a32.xml
deleted file mode 100644
index fa13eff2..00000000
--- a/Engines/leap1a32.xml
+++ /dev/null
@@ -1,59 +0,0 @@
-<?xml version="1.0"?>
-
-<!--
-#########################################
-# Copyright (c) it0uchpods Design Group #
-#########################################
--->
-
-<turbine_engine name="LEAP1A32">
-
-	<milthrust>     27000 </milthrust>
-	<bypassratio>     8.1 </bypassratio>
-	<tsfc>            0.5 </tsfc>
-	<bleed>          0.03 </bleed>
-	<idlen1>         19.7 </idlen1>
-	<idlen2>         61.2 </idlen2>
-	<n1spinup>        0.2 </n1spinup>
-	<n2spinup>        2.0 </n2spinup>
-	<maxn1>         103.8 </maxn1>
-	<maxn2>          99.6 </maxn2>
-	<augmented>         0 </augmented>
-	<injected>          0 </injected>
-
-	<function name="IdleThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			    -10000   0       10000   20000   30000   40000   50000
-			0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467
-			0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
-			0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
-			0.6  0.0     0.0     0.0     0.0     0.0276  0.0718  0.1073
-			0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900
-			1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800
-			</tableData>
-		</table>
-	</function>
-
-	<function name="MilThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			     -10000   0       10000   20000   30000   40000   50000
-			0.0   1.2600  1.0000  0.7400  0.5440  0.3720  0.2410  0.0000
-			0.2   1.1710  0.9740  0.6970  0.5160  0.3650  0.2310  0.0000
-			0.4   1.1500  0.9570  0.6920  0.5260  0.3670  0.2230  0.0000
-			0.6   1.1810  0.9410  0.7210  0.5460  0.3380  0.1880  0.0000
-			0.8   1.2290  1.0200  0.7820  0.5370  0.2840  0.1450  0.0000
-			0.9   1.2580  1.0200  0.7820  0.5020  0.2510  0.0650  0.0000
-			1.0   1.1810  0.9510  0.7210  0.4210  0.1540  0.0150  0.0000
-			1.2   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			1.4   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			</tableData>
-		</table>
-	</function>
-	
-</turbine_engine>
diff --git a/Engines/pw1133g.xml b/Engines/pw1133g.xml
deleted file mode 100644
index 2d5d340f..00000000
--- a/Engines/pw1133g.xml
+++ /dev/null
@@ -1,59 +0,0 @@
-<?xml version="1.0"?>
-
-<!--
-#########################################
-# Copyright (c) it0uchpods Design Group #
-#########################################
--->
-
-<turbine_engine name="PW1133G">
-
-	<milthrust>     26345 </milthrust>
-	<bypassratio>     8.1 </bypassratio>
-	<tsfc>            0.5 </tsfc>
-	<bleed>          0.03 </bleed>
-	<idlen1>         19.7 </idlen1>
-	<idlen2>         61.2 </idlen2>
-	<n1spinup>        0.2 </n1spinup>
-	<n2spinup>        2.0 </n2spinup>
-	<maxn1>         103.8 </maxn1>
-	<maxn2>          99.6 </maxn2>
-	<augmented>         0 </augmented>
-	<injected>          0 </injected>
-
-	<function name="IdleThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			    -10000   0       10000   20000   30000   40000   50000
-			0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467
-			0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
-			0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
-			0.6  0.0     0.0     0.0     0.0     0.0276  0.0718  0.1073
-			0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900
-			1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800
-			</tableData>
-		</table>
-	</function>
-
-	<function name="MilThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			     -10000   0       10000   20000   30000   40000   50000
-			0.0   1.2600  1.0000  0.7400  0.5440  0.3720  0.2410  0.0000
-			0.2   1.1710  0.9740  0.6970  0.5160  0.3650  0.2310  0.0000
-			0.4   1.1500  0.9570  0.6920  0.5260  0.3670  0.2230  0.0000
-			0.6   1.1810  0.9410  0.7210  0.5460  0.3380  0.1880  0.0000
-			0.8   1.2290  1.0200  0.7820  0.5370  0.2840  0.1450  0.0000
-			0.9   1.2580  1.0200  0.7820  0.5020  0.2510  0.0650  0.0000
-			1.0   1.1810  0.9510  0.7210  0.4210  0.1540  0.0150  0.0000
-			1.2   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			1.4   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			</tableData>
-		</table>
-	</function>
-	
-</turbine_engine>
diff --git a/Engines/v2522_a5.xml b/Engines/v2522_a5.xml
deleted file mode 100644
index e2241b9b..00000000
--- a/Engines/v2522_a5.xml
+++ /dev/null
@@ -1,59 +0,0 @@
-<?xml version="1.0"?>
-
-<!--
-#########################################
-# Copyright (c) it0uchpods Design Group #
-#########################################
--->
-
-<turbine_engine name="V2522_A5">
-
-	<milthrust>     26600 </milthrust>
-	<bypassratio>     8.1 </bypassratio>
-	<tsfc>            0.5 </tsfc>
-	<bleed>          0.03 </bleed>
-	<idlen1>         22.4 </idlen1>
-	<idlen2>         60.9 </idlen2>
-	<n1spinup>        0.2 </n1spinup>
-	<n2spinup>        2.0 </n2spinup>
-	<maxn1>         103.8 </maxn1>
-	<maxn2>          99.6 </maxn2>
-	<augmented>         0 </augmented>
-	<injected>          0 </injected>
-
-	<function name="IdleThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			    -10000   0       10000   20000   30000   40000   50000
-			0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467
-			0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
-			0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
-			0.6  0.0     0.0     0.0     0.0     0.0276  0.0718  0.1073
-			0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900
-			1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800
-			</tableData>
-		</table>
-	</function>
-
-	<function name="MilThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			     -10000   0       10000   20000   30000   40000   50000
-			0.0   1.2600  1.0000  0.7400  0.5440  0.3720  0.2410  0.0000
-			0.2   1.1710  0.9740  0.6970  0.5160  0.3650  0.2310  0.0000
-			0.4   1.1500  0.9570  0.6920  0.5260  0.3670  0.2230  0.0000
-			0.6   1.1810  0.9410  0.7210  0.5460  0.3380  0.1880  0.0000
-			0.8   1.2290  1.0200  0.7820  0.5370  0.2840  0.1450  0.0000
-			0.9   1.2580  1.0200  0.7820  0.5020  0.2510  0.0650  0.0000
-			1.0   1.1810  0.9510  0.7210  0.4210  0.1540  0.0150  0.0000
-			1.2   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			1.4   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			</tableData>
-		</table>
-	</function>
-	
-</turbine_engine>
diff --git a/Engines/v2533_a5.xml b/Engines/v2533_a5.xml
deleted file mode 100644
index 530c6f49..00000000
--- a/Engines/v2533_a5.xml
+++ /dev/null
@@ -1,59 +0,0 @@
-<?xml version="1.0"?>
-
-<!--
-#########################################
-# Copyright (c) it0uchpods Design Group #
-#########################################
--->
-
-<turbine_engine name="V2533_A5">
-
-	<milthrust>     26600 </milthrust>
-	<bypassratio>     8.1 </bypassratio>
-	<tsfc>            0.5 </tsfc>
-	<bleed>          0.03 </bleed>
-	<idlen1>         22.4 </idlen1>
-	<idlen2>         60.9 </idlen2>
-	<n1spinup>        0.2 </n1spinup>
-	<n2spinup>        2.0 </n2spinup>
-	<maxn1>         103.8 </maxn1>
-	<maxn2>          99.6 </maxn2>
-	<augmented>         0 </augmented>
-	<injected>          0 </injected>
-
-	<function name="IdleThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			    -10000   0       10000   20000   30000   40000   50000
-			0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467
-			0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
-			0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
-			0.6  0.0     0.0     0.0     0.0     0.0276  0.0718  0.1073
-			0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900
-			1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800
-			</tableData>
-		</table>
-	</function>
-
-	<function name="MilThrust">
-		<table>
-			<independentVar lookup="row">velocities/mach</independentVar>
-			<independentVar lookup="column">atmosphere/density-altitude</independentVar>
-			<tableData>
-			     -10000   0       10000   20000   30000   40000   50000
-			0.0   1.2600  1.0000  0.7400  0.5440  0.3720  0.2410  0.0000
-			0.2   1.1710  0.9740  0.6970  0.5160  0.3650  0.2310  0.0000
-			0.4   1.1500  0.9570  0.6920  0.5260  0.3670  0.2230  0.0000
-			0.6   1.1810  0.9410  0.7210  0.5460  0.3380  0.1880  0.0000
-			0.8   1.2290  1.0200  0.7820  0.5370  0.2840  0.1450  0.0000
-			0.9   1.2580  1.0200  0.7820  0.5020  0.2510  0.0650  0.0000
-			1.0   1.1810  0.9510  0.7210  0.4210  0.1540  0.0150  0.0000
-			1.2   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			1.4   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000
-			</tableData>
-		</table>
-	</function>
-	
-</turbine_engine>
diff --git a/revision.txt b/revision.txt
index 546fc17a..fd1e854c 100644
--- a/revision.txt
+++ b/revision.txt
@@ -1 +1 @@
-2141
\ No newline at end of file
+2142
\ No newline at end of file