Update 717-200 fuel profile.

Author: JetStream96

src/QSP/PerformanceData/FuelCalc/Default/717200.xml

@@ -8,39 +8,37 @@
        all fuel flows (FF) in kg/min.
   -->
 
-  <!-- 26k with winglet -->
-
   <ProfileName>Boeing 717-200</ProfileName>
   <HoldingFuelFlow>23.83</HoldingFuelFlow>
   <HoldingFuelRefWt>30000</HoldingFuelRefWt>
-  <TaxiFuelFlow>12.2</TaxiFuelFlow>'
+  <TaxiFuelFlow>10</TaxiFuelFlow>
   <ApuFuelFlow>0.8333</ApuFuelFlow>
-  <ClimbIAS>280</ClimbIAS>'
-  <DescentIAS>280</DescentIAS>'
+  <ClimbIAS>280</ClimbIAS>
+  <DescentIAS>250</DescentIAS>
 
-  <DataPoint>'
-    <Weight>40000</Weight>
-    <CruiseFF>27.1</CruiseFF>
-    <CruiseIAS>215.9772</CruiseIAS>
+  <DataPoint>
+    <Weight>30000</Weight>
+    <CruiseFF>22.066</CruiseFF>
+    <CruiseIAS>221</CruiseIAS>
     <ClimbGrad>0.0900</ClimbGrad>
-    <ClimbFF>85.42</ClimbFF>
+    <ClimbFF>68.4</ClimbFF>
     <DescentGrad>0.0668</DescentGrad>
-    <DescentFF>13.08</DescentFF>
-    <OptCruiseAlt>43829</OptCruiseAlt>
+    <DescentFF>10.4</DescentFF>
+    <OptCruiseAlt>37000</OptCruiseAlt>
     <EtopsCruiseTAS>0</EtopsCruiseTAS>
     <!-- Placeholder -->
     <EtopsCruiseFF>0</EtopsCruiseFF>
   </DataPoint>
 
-  <DataPoint>'
-    <Weight>85000</Weight>
-    <CruiseFF>53.1</CruiseFF>
-    <CruiseIAS>297</CruiseIAS>
+  <DataPoint>
+    <Weight>60000</Weight>
+    <CruiseFF>45.97</CruiseFF>
+    <CruiseIAS>301</CruiseIAS>
     <ClimbGrad>0.0430</ClimbGrad>
-    <ClimbFF>94.1</ClimbFF>
+    <ClimbFF>75.3</ClimbFF>
     <DescentGrad>0.0466</DescentGrad>
-    <DescentFF>14.4</DescentFF>
-    <OptCruiseAlt>30072</OptCruiseAlt>
+    <DescentFF>11.5</DescentFF>
+    <OptCruiseAlt>30800</OptCruiseAlt>
     <EtopsCruiseTAS>0</EtopsCruiseTAS>
     <EtopsCruiseFF>0</EtopsCruiseFF>
   </DataPoint>