2016-11-07 15:39:53 +00:00
<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name= "A320family" version= "2.0" release= "BETA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader >
2017-06-05 23:42:02 +00:00
<author > Joshua Davidson (it0uchpods)</author>
<version > Pre V1.0</version>
<description > A3XX FDE</description>
2016-11-07 15:39:53 +00:00
</fileheader>
<metrics >
<wingarea unit= "FT2" > 1319.79 </wingarea>
<wingspan unit= "FT" > 111.26 </wingspan>
<wing_incidence > 1.03 </wing_incidence>
<chord unit= "FT" > 13.76 </chord>
<htailarea unit= "FT2" > 334.24 </htailarea>
<htailarm unit= "FT" > 57.88 </htailarm>
<vtailarea unit= "FT2" > 248.79 </vtailarea>
<vtailarm unit= "FT" > 57.33 </vtailarm>
2016-12-05 23:20:24 +00:00
<!-- location name="AERORP" unit="IN">
<x > 642.122 </x>
<y > 0 </y>
<z > -25.2091 </z>
< /location -->
2016-11-07 15:39:53 +00:00
<location name= "AERORP" unit= "IN" >
2017-04-07 18:09:40 +00:00
<x > 700.00 </x>
2016-12-05 23:20:24 +00:00
<y > 0 </y>
<z > 0.00 </z>
2016-11-07 15:39:53 +00:00
</location>
2016-12-05 23:20:24 +00:00
2016-11-07 15:39:53 +00:00
<location name= "EYEPOINT" unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 80 </x>
<y > -30 </y>
<z > 70 </z>
2016-11-07 15:39:53 +00:00
</location>
2016-12-05 23:20:24 +00:00
2016-11-07 15:39:53 +00:00
<location name= "VRP" unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 661.1 </x>
<y > 0 </y>
<z > -37 </z>
2016-11-07 15:39:53 +00:00
</location>
2016-12-05 23:20:24 +00:00
2016-11-07 15:39:53 +00:00
</metrics>
<mass_balance >
2017-06-24 20:55:07 +00:00
<ixx unit= "SLUG*FT2" > 611903 </ixx>
<iyy unit= "SLUG*FT2" > 1735389 </iyy>
<izz unit= "SLUG*FT2" > 2301293 </izz>
<!--
___________________A320_________A330__________A340
BOW_____________178000________270000________283925
SPAN______________144___________198___________209
LENGTH____________153___________209___________209
ROLL MOI_________1725000______5727777_______10613448
PITCH MOI________2550000______19040141_______13904249
YAW MOI_________3950000______23089847_______24848934
<ixx unit= "SLUG*FT2" > 2262183 </ixx>
<iyy unit= "SLUG*FT2" > 3172439 </iyy>
<izz unit= "SLUG*FT2" > 3337024 </izz>
<ixx unit= "SLUG*FT2" > 1725000</ixx>
<iyy unit= "SLUG*FT2" > 2550000</iyy>
<izz unit= "SLUG*FT2" > 3950000</izz> -->
<ixy unit= "SLUG*FT2" > 0 </ixy>
<ixz unit= "SLUG*FT2" > 0 </ixz>
<iyz unit= "SLUG*FT2" > 0 </iyz>
<emptywt unit= "LBS" > 80431</emptywt> <!-- #ref - 1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs -->
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- location name="CG" unit="IN">
<! - -x> 642.122 < /x- - >
<x > 650.122 </x> <! - - At zero load of fuel and cargo/pax the CG goes to 642 - - >
<y > 0 </y>
<z > -41.7398 </z>
< /location -->
2016-11-07 15:39:53 +00:00
<location name= "CG" unit= "IN" >
2017-04-07 18:09:40 +00:00
<x > 652.00 </x>
2016-12-05 23:20:24 +00:00
<y > 0 </y>
<z > 0.00 </z>
2016-11-07 15:39:53 +00:00
</location>
2016-12-05 23:20:24 +00:00
<pointmass name= "Cockpit Crew" >
<weight unit= "LBS" > 400</weight> <!-- MAX: 400lbs, two pilots -->
2016-11-07 15:39:53 +00:00
<location name= "POINTMASS" unit= "IN" >
<x > 200</x>
<y > 0</y>
<z > 0</z>
</location>
</pointmass>
2016-12-05 23:20:24 +00:00
<pointmass name= "Cabin Crew" >
<weight unit= "LBS" > 600</weight> <!-- MAX: 1320lbs, up to six flight - attendants -->
2016-11-07 15:39:53 +00:00
<location name= "POINTMASS" unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 696</x>
2016-11-07 15:39:53 +00:00
<y > 0</y>
<z > 0</z>
</location>
</pointmass>
2016-12-05 23:20:24 +00:00
<pointmass name= "PAX 0A (60 seats)" >
<weight unit= "LBS" > 6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<location name= "POINTMASS" unit= "IN" >
<x > 470.1711</x>
2016-11-07 15:39:53 +00:00
<y > 0</y>
2016-12-05 23:20:24 +00:00
<z > 0</z>
2016-11-07 15:39:53 +00:00
</location>
</pointmass>
2016-12-05 23:20:24 +00:00
<pointmass name= "PAX 0B (60 seats)" >
<weight unit= "LBS" > 6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<location name= "POINTMASS" unit= "IN" >
<x > 809.5669</x>
2016-11-07 15:39:53 +00:00
<y > 0</y>
2016-12-05 23:20:24 +00:00
<z > 0</z>
2016-11-07 15:39:53 +00:00
</location>
</pointmass>
2016-12-05 23:20:24 +00:00
<pointmass name= "PAX 0C (54 seats)" >
<weight unit= "LBS" > 5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<location name= "POINTMASS" unit= "IN" >
<x > 1163.2729</x>
2016-11-07 15:39:53 +00:00
<y > 0</y>
2016-12-05 23:20:24 +00:00
<z > 0</z>
2016-11-07 15:39:53 +00:00
</location>
</pointmass>
2016-12-05 23:20:24 +00:00
<pointmass name= "Cargo Hold 1" >
<weight unit= "LBS" > 2000</weight> <!-- MAX: 7500.126lbs -->
2016-11-07 15:39:53 +00:00
<location name= "POINTMASS" unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 383.4792</x>
<y > 0</y>
<z > -29.5</z> <!-- 1.5m and now half of it for the center point of the load -->
2016-11-07 15:39:53 +00:00
</location>
</pointmass>
2016-12-05 23:20:24 +00:00
<!-- Cargo Hold 2 doesn't exist, that is the center tank -->
<pointmass name= "Cargo Hold 3" >
<weight unit= "LBS" > 2000</weight> <!-- MAX: 5384.414lbs -->
2016-11-07 15:39:53 +00:00
<location name= "POINTMASS" unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 849.1324</x>
<y > 0</y>
<z > -29.5</z>
</location>
</pointmass>
<pointmass name= "Cargo Hold 4" >
<weight unit= "LBS" > 1500</weight> <!-- MAX: 4651.754lbs -->
<location name= "POINTMASS" unit= "IN" >
<x > 931.0653</x>
<y > 0</y>
<z > -29.5</z>
</location>
</pointmass>
<pointmass name= "Cargo Hold 5" >
<weight unit= "LBS" > 2000</weight> <!-- MAX: 3300.320lbs -->
<location name= "POINTMASS" unit= "IN" >
<x > 1068.2634</x>
<y > 0</y>
<z > 0</z> <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
2016-11-07 15:39:53 +00:00
</location>
</pointmass>
</mass_balance>
<ground_reactions >
2016-12-05 23:20:24 +00:00
<!-- REF - 1 page 165 + 271 -->
2016-11-07 15:39:53 +00:00
<contact type= "BOGEY" name= "NOSE_LG" >
<location unit= "IN" >
<x > 197.6772 </x>
<y > 0 </y>
<z > -137.9617 </z>
</location>
<static_friction > 0.8 </static_friction>
<dynamic_friction > 0.5 </dynamic_friction>
<rolling_friction > 0.02 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 30935.5 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 16978.5 </damping_coeff>
<max_steer unit= "DEG" > 70 </max_steer> <!-- REF - 1 page 133 -->
<brake_group > NONE </brake_group>
<retractable > 1</retractable>
</contact>
<contact type= "BOGEY" name= "LEFT_MLG" >
<location unit= "IN" >
<!-- <x> 699.9243 </x> -->
<x > 695.3149 </x>
<y > -149.4094 </y>
<z > -150.4824 </z>
</location>
<!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction? -->
<static_friction > 0.8 </static_friction>
<dynamic_friction > 0.5 </dynamic_friction>
<rolling_friction > 0.02 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 59785 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 23957 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > LEFT </brake_group>
<retractable > 1</retractable>
</contact>
<contact type= "BOGEY" name= "RIGHT_MLG" >
<location unit= "IN" >
<!-- <x> 697.3425 </x> It should be right left simetric
<x > 699.9243 </x> -->
<x > 695.3149 </x>
<y > 149.4094 </y>
<z > -150.4824 </z>
</location>
<!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction? -->
<static_friction > 0.8 </static_friction>
<dynamic_friction > 0.5 </dynamic_friction>
<rolling_friction > 0.02 </rolling_friction>
<!-- spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 33957 </damping_coeff-->
<spring_coeff unit= "LBS/FT" > 59785 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 23957 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > RIGHT </brake_group>
<retractable > 1</retractable>
</contact>
<contact type= "STRUCTURE" name= "NOSE_1" >
<location unit= "IN" >
<x > 37.7953 </x>
<y > 0 </y>
<z > -38.1374 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "NOSE_2" >
<location unit= "IN" >
<x > 128.1102 </x>
<y > 0 </y>
<z > -55.0271 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "CENTER_1" >
<location unit= "IN" >
<x > 274.0157 </x>
<y > 0 </y>
<z > -60.0665 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "CENTER_2" >
<location unit= "IN" >
<x > 930 </x>
<y > 0 </y>
<z > -60.0665 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "ENG_1" >
<location unit= "IN" >
<x > 589.735</x>
<y > -226.575</y>
<z > -95.567</z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "ENG_2" >
<location unit= "IN" >
<x > 589.735</x>
<y > 226.575</y>
<z > -95.567</z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.5 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "TAIL_1" >
<location unit= "IN" >
<x > 1097.9921 </x>
<y > 0 </y>
<z > -44.7722 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "TAIL_2" >
<location unit= "IN" >
<x > 1225 </x>
<y > 0 </y>
<z > -18.8067 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "TAIL_3" >
<location unit= "IN" >
<x > 1341.6142 </x>
<y > 0 </y>
<z > -10.2599 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "TAIL_4" >
<location unit= "IN" >
<x > 1469.0945 </x>
<y > 0 </y>
<z > 47.4138 </z>
</location>
<static_friction > 1.0 </static_friction>
2016-12-05 23:20:24 +00:00
<dynamic_friction > 1 </dynamic_friction>
<rolling_friction > 1 </rolling_friction>
2016-11-07 15:39:53 +00:00
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "WING_TIP_1" >
<location unit= "IN" >
<x > 838.8898 </x>
<y > -667.5197 </y>
<z > 35.7926 </z>
</location>
<static_friction > 1.0 </static_friction>
2016-12-05 23:20:24 +00:00
<dynamic_friction > 0.4 </dynamic_friction>
<rolling_friction > 0.4 </rolling_friction>
2016-11-07 15:39:53 +00:00
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
<contact type= "STRUCTURE" name= "WING_TIP_2" >
<location unit= "IN" >
<x > 838.8898 </x>
<y > 667.5197 </y>
<z > 35.7926 </z>
</location>
<static_friction > 1.0 </static_friction>
<dynamic_friction > 1 </dynamic_friction>
<rolling_friction > 1 </rolling_friction>
<spring_coeff unit= "LBS/FT" > 50000 </spring_coeff>
<damping_coeff unit= "LBS/FT/SEC" > 50000 </damping_coeff>
<max_steer unit= "DEG" > 0.0 </max_steer>
<brake_group > NONE </brake_group>
<retractable > 0</retractable>
</contact>
2016-12-05 23:20:24 +00:00
</ground_reactions>
2016-11-07 15:39:53 +00:00
<propulsion >
2016-12-05 23:20:24 +00:00
<engine file= "v2527_a5" >
2016-11-07 15:39:53 +00:00
<location unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 620.0683 </x>
2016-11-07 15:39:53 +00:00
<y > -226.575 </y>
<z > -45.567 </z>
</location>
<orient unit= "DEG" >
<roll > 0.0 </roll>
<pitch > 2.2 </pitch>
<yaw > 1 </yaw>
</orient>
2017-06-09 16:53:49 +00:00
<feed > 7</feed>
2016-11-07 15:39:53 +00:00
<thruster file= "direct" >
<location unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 655.4820 </x>
2016-11-07 15:39:53 +00:00
<y > -226.575 </y>
2016-12-05 23:20:24 +00:00
<z > 0.000 </z>
2016-11-07 15:39:53 +00:00
</location>
<orient unit= "DEG" >
<roll > 0.0 </roll>
<pitch > 2.2 </pitch>
<yaw > 1 </yaw>
</orient>
</thruster>
</engine>
2016-12-05 23:20:24 +00:00
<engine file= "v2527_a5" >
2016-11-07 15:39:53 +00:00
<location unit= "IN" >
2017-05-07 19:26:41 +00:00
<x > 620.0683 </x>
2016-11-07 15:39:53 +00:00
<y > 226.575 </y>
<z > -45.567 </z>
</location>
<orient unit= "DEG" >
<roll > 0.0 </roll>
<pitch > 2.2 </pitch>
<yaw > -1 </yaw>
</orient>
2017-06-09 16:53:49 +00:00
<feed > 8</feed>
2016-11-07 15:39:53 +00:00
<thruster file= "direct" >
<location unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 655.4820 </x>
2016-11-07 15:39:53 +00:00
<y > 226.575 </y>
2016-12-05 23:20:24 +00:00
<z > 0.000 </z>
2016-11-07 15:39:53 +00:00
</location>
<orient unit= "DEG" >
<roll > 0.0 </roll>
<pitch > 2.2 </pitch>
<yaw > -1 </yaw>
</orient>
</thruster>
</engine>
2016-12-05 23:20:24 +00:00
<tank type= "FUEL" > <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
2016-11-07 15:39:53 +00:00
<location unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 783.0709 </x>
2016-11-07 15:39:53 +00:00
<y > -574.4148 </y>
<z > 3.1080 </z>
</location>
2017-02-20 14:33:59 +00:00
<capacity unit= "LBS" > 412 </capacity> <!-- need review --> <!-- would be 1 percent of max load per each wing, 412 each. Needs temp rise of 20C at max load to fill -->
2016-11-07 15:39:53 +00:00
<contents unit= "LBS" > 0 </contents>
<priority > 4</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
2016-12-05 23:20:24 +00:00
<tank type= "FUEL" > <!-- Left Tank (Outer) 1 -->
2016-11-07 15:39:53 +00:00
<location unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 739.5669 </x>
2016-11-07 15:39:53 +00:00
<y > -457.4259 </y>
<z > -8.0898 </z>
</location>
2016-12-05 23:20:24 +00:00
<capacity unit= "LBS" > 1520.00 </capacity> <!-- need review -->
2017-02-20 14:33:59 +00:00
<contents unit= "LBS" > 1520 </contents> <!-- outer filled first than inner -->
2016-11-07 15:39:53 +00:00
<standpipe unit= "LBS" > 21</standpipe> <!-- minimun fuel on pipes -->
<priority > 2</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
2016-12-05 23:20:24 +00:00
<tank type= "FUEL" > <!-- Left Tank (Inner) 2 -->
2016-11-07 15:39:53 +00:00
<location unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 652.5591 </x>
2016-11-07 15:39:53 +00:00
<y > -236.2992 </y>
<z > -33.9470 </z>
</location>
2017-02-20 14:33:59 +00:00
<capacity unit= "LBS" > 11982 </capacity> <!-- correct by FCOM -->
2017-05-08 01:34:45 +00:00
<contents unit= "LBS" > 4480 </contents>
2016-11-07 15:39:53 +00:00
<standpipe unit= "LBS" > 31</standpipe> <!-- minimun fuel on pipes -->
<priority > 3</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
2016-12-05 23:20:24 +00:00
<tank type= "FUEL" > <!-- Center Tank 3 -->
2016-11-07 15:39:53 +00:00
<location unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 522.0473 </x>
2016-11-07 15:39:53 +00:00
<y > 0 </y>
<z > -47.0 </z>
</location>
2017-02-20 14:33:59 +00:00
<capacity unit= "LBS" > 14281 </capacity> <!-- correct by FCOM -->
<contents unit= "LBS" > 0 </contents> <!-- wing tanks always filled first -->
2016-11-07 15:39:53 +00:00
<standpipe unit= "LBS" > 43</standpipe> <!-- minimun fuel on pipes -->
<priority > 1</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
2016-12-05 23:20:24 +00:00
<tank type= "FUEL" > <!-- Right Tank (Inner) 4 -->
2016-11-07 15:39:53 +00:00
<location unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 652.5591 </x>
2016-11-07 15:39:53 +00:00
<y > 236.2992 </y>
<z > -33.9470 </z>
</location>
2017-02-20 14:33:59 +00:00
<capacity unit= "LBS" > 11982 </capacity> <!-- correct by FCOM -->
2017-05-08 01:34:45 +00:00
<contents unit= "LBS" > 4480 </contents>
2016-12-05 23:20:24 +00:00
<standpipe unit= "LBS" > 31</standpipe> <!-- minimum fuel on pipes -->
2016-11-07 15:39:53 +00:00
<priority > 3</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
2016-12-05 23:20:24 +00:00
<tank type= "FUEL" > <!-- Right Tank (Outer) 5 -->
2016-11-07 15:39:53 +00:00
<location unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 739.5669 </x>
2016-11-07 15:39:53 +00:00
<y > 457.4259 </y>
<z > -8.0898 </z>
</location>
2017-02-20 14:33:59 +00:00
<capacity unit= "LBS" > 1520 </capacity> <!-- correct by FCOM -->
<contents unit= "LBS" > 1520 </contents> <!-- outer filled before inner -->
2016-11-07 15:39:53 +00:00
<standpipe unit= "LBS" > 21</standpipe> <!-- minimun fuel on pipes -->
<priority > 2</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
2016-12-05 23:20:24 +00:00
<tank type= "FUEL" > <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
2016-11-07 15:39:53 +00:00
<location unit= "IN" >
2016-12-05 23:20:24 +00:00
<x > 783.0709 </x>
2016-11-07 15:39:53 +00:00
<y > 574.4148 </y>
<z > 3.1080 </z>
</location>
2017-02-20 14:33:59 +00:00
<capacity unit= "LBS" > 412 </capacity> <!-- need review --> <!-- 1 percent of max, see left surge tank, is 412 lb each -->
2016-11-07 15:39:53 +00:00
<contents unit= "LBS" > 0 </contents>
<priority > 4</priority>
<type > JET-A1</type>
<temperature > 50</temperature>
</tank>
2017-06-09 16:53:49 +00:00
<tank type= "FUEL" > <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
<location unit= "IN" >
<x > 589.735</x>
<y > -226.575</y>
<z > -45.567</z>
</location>
<capacity unit= "LBS" > 100 </capacity> <!-- need review -->
<contents unit= "LBS" > 0 </contents>
<priority > 1</priority>
<type > JET-A1</type>
</tank>
<tank type= "FUEL" > <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
<location unit= "IN" >
<x > 589.735</x>
<y > 226.575</y>
<z > -45.567</z>
</location>
<capacity unit= "LBS" > 100 </capacity> <!-- need review -->
<contents unit= "LBS" > 0 </contents>
<priority > 1</priority>
<type > JET-A1</type>
</tank>
2016-11-07 15:39:53 +00:00
</propulsion>
<system file= "pushback" />
2017-06-09 16:53:49 +00:00
<system file= "fuel" />
2017-04-17 04:10:36 +00:00
<system file= "glass-effect1" />
<system file= "it-fbw" />
2017-05-19 15:17:27 +00:00
<system file= "fmgc" />
2017-06-08 00:14:22 +00:00
<system file= "fcs" />
2016-11-07 15:39:53 +00:00
2017-06-08 00:14:22 +00:00
<flight_control name= "none" />
2016-11-07 15:39:53 +00:00
2017-06-09 22:10:13 +00:00
<aerodynamics file= "Systems/a319-aerodynamics.xml" />
2016-12-05 23:20:24 +00:00
2017-06-09 22:10:13 +00:00
<external_reactions >
<force name= "pushback" frame= "BODY" >
<location unit= "IN" >
<x > 294</x>
<y > 0</y>
<z > -149</z>
</location>
<direction >
<x > 1</x>
<y > 0</y>
<z > 0</z>
</direction>
</force>
</external_reactions>
2016-11-07 15:39:53 +00:00
</fdm_config>
