From 665b1fa1c6c1dec52970617ec40ac9f7bc7b0d27 Mon Sep 17 00:00:00 2001
From: Joshua Davidson <joshuadavidson2000@gmail.com>
Date: Sun, 7 May 2017 19:10:46 -0400
Subject: [PATCH] FDE Fix cruise lift

---
 A319-100-IAE.xml | 4 ++--
 A320-200-IAE.xml | 7 ++++---
 A321-200-IAE.xml | 4 ++--
 ACJ-IAE.xml      | 7 ++++---
 4 files changed, 12 insertions(+), 10 deletions(-)

diff --git a/A319-100-IAE.xml b/A319-100-IAE.xml
index 3807075f..34770e4c 100644
--- a/A319-100-IAE.xml
+++ b/A319-100-IAE.xml
@@ -915,8 +915,8 @@ YAW MOI_________3950000______23089847_______24848934
 					<table>
 						<independentVar lookup="row">aero/alpha-rad</independentVar>
 						<tableData>
-							-0.20 -0.520
-							 0.00  0.505
+							-0.20 -0.900
+							 0.00  0.205
 							 0.23  1.800
 							 0.60  1.000
 						</tableData>
diff --git a/A320-200-IAE.xml b/A320-200-IAE.xml
index 17ed55c9..4bb6db6b 100644
--- a/A320-200-IAE.xml
+++ b/A320-200-IAE.xml
@@ -915,9 +915,10 @@ YAW MOI_________3950000______23089847_______24848934
 					<table>
 						<independentVar lookup="row">aero/alpha-rad</independentVar>
 						<tableData>
-							-0.20 -0.520
-							 0.00  0.505
-							 0.23  1.800
+							-0.20 -0.900
+							 0.00  0.103
+							 0.15  1.600
+							 0.23  1.900
 							 0.60  1.000
 						</tableData>
 					</table>
diff --git a/A321-200-IAE.xml b/A321-200-IAE.xml
index b6d1a381..071d3c4d 100644
--- a/A321-200-IAE.xml
+++ b/A321-200-IAE.xml
@@ -915,8 +915,8 @@ YAW MOI_________3950000______23089847_______24848934
 					<table>
 						<independentVar lookup="row">aero/alpha-rad</independentVar>
 						<tableData>
-							-0.20 -0.520
-							 0.00  0.505
+							-0.20 -0.900
+							 0.00  0.205
 							 0.23  1.800
 							 0.60  1.000
 						</tableData>
diff --git a/ACJ-IAE.xml b/ACJ-IAE.xml
index e587a808..a6a2f472 100644
--- a/ACJ-IAE.xml
+++ b/ACJ-IAE.xml
@@ -915,9 +915,10 @@ YAW MOI_________3950000______23089847_______24848934
 					<table>
 						<independentVar lookup="row">aero/alpha-rad</independentVar>
 						<tableData>
-							-0.20 -0.520
-							 0.00  0.505
-							 0.23  1.800
+							-0.20 -0.900
+							 0.00  0.103
+							 0.15  1.600
+							 0.23  1.900
 							 0.60  1.000
 						</tableData>
 					</table>