-diff -ruN 747-8i.orig/747-8f-set.xml 747-8i/747-8f-set.xml
---- 747-8i.orig/747-8f-set.xml	2015-01-20 03:42:28.000000000 +0800
-+++ 747-8i/747-8f-set.xml	2015-03-14 16:44:05.729357514 +0800
+diff -ruN 747-8i/747-8f-set.xml 747-8i.new/747-8f-set.xml
+--- 747-8i/747-8f-set.xml	2015-01-20 03:42:28.000000000 +0800
++++ 747-8i.new/747-8f-set.xml	2015-06-11 21:59:26.305368055 +0800
 @@ -272,13 +272,13 @@
  
  		<weight n="0">

 	}elsif(me.step==6){
 			ma_spd=getprop("/velocities/mach");
 			banklimit=getprop("/instrumentation/afds/inputs/bank-limit-switch");
diff -ruN 747-8i.orig/Nasal/auto_refuel.nas 747-8i/Nasal/auto_refuel.nas
--- 747-8i.orig/Nasal/auto_refuel.nas	1970-01-01 08:00:00.000000000 +0800
+++ 747-8i/Nasal/auto_refuel.nas	2015-03-14 21:39:39.581645008 +0800
@@ -0,0 +1,299 @@
+var fuel_up = func(stage) {
+	var tot_level = props.globals.getNode("consumables/fuel/total-fuel-gal_us",1);

 		<maximum-landing-mass-lbs>763000</maximum-landing-mass-lbs>
 		<maximum-zero-fuel-mass-lbs>727000</maximum-zero-fuel-mass-lbs>
 	    </mass-and-balance>
+		<estimated-range-nm>3700</estimated-range-nm>
 	</limits>
 
 	<aircraft>
diff -ruN 747-8i/747-8i-set.xml 747-8i.new/747-8i-set.xml
--- 747-8i/747-8i-set.xml	2015-01-20 03:42:28.000000000 +0800
+++ 747-8i.new/747-8i-set.xml	2015-06-11 21:53:29.489366041 +0800
@@ -287,13 +287,13 @@
 
 		<weight n="0">
