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777-300ER.xml
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<!--777-300 ER yasim
Specs:
777-300ER - 512 kN (115,300lb) General Electric GE90-115B
Typical Cruise = 0.84 Mach / 35000 ft
Max Speed = 0.87 / 35000 ft
777-300ER - Range with 365 passengers 14,685km (7,930nm) - 15hrs.
Wing span: 64.8m
Length: 73.9 m
Tail Height: 18.5m
Diameter : 6.19 m
Max Fuel :47,890 US gal
Max TO weight: 775,000 lbs
Max Landing weight: 554,000 lbs
TO speed : 145 kt
Landing speed : 131 kt
Leading edge MAC = -3.132
Vr 137
V2 147
Datum 92.5 in forward of nose - 2.3495 m
MAC 278.51 in - 7.074154 m
FLAPS
30 25 20
WEIGHT/lbs Vref
550,000 151 159 164
528,000 148 156 161
506,000 145 152 158
484,000 142 149 154
462,000 139 145 150
440,000 135 142 147
418,000 132 138 143
396,000 128 134 139
374,000 124 131 135
352,000 121 127 131
330,000 117 123 127
308,000 113 118 123
-->
<airplane mass="366940" version="YASIM_VERSION_32">
<!-- Approach configuration -->
<approach speed="145" aoa="3" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle-act" value="0.25"/>
<control-setting axis="/controls/engines/engine[1]/throttle-act" value="0.25"/>
<control-setting axis="/controls/flight/flaps" value="1"/>
<control-setting axis="/surface-positions/slats" value="1"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="45000"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="512" alt="35000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle-act" value="0.95"/>
<control-setting axis="/controls/engines/engine[1]/throttle-act" value="0.95"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/flight/elevator-trim" value="0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="45000"/>
</cruise>
<!-- Cockpit position -->
<cockpit x="28.0381" y="0.5" z="0.75"/>
<!-- Fuselage -->
<fuselage ax="30.5981" ay="0" az="-0.64" bx="21.4691" by="0.00" bz="0.0"
width="6.2" taper="0.0" midpoint="1.0"/>
<fuselage ax="21.4691" ay="0" az="0" bx="-24.7003" by="0.00" bz="0.0"
width="6.2" taper="1.0" midpoint="0.5"/>
<fuselage ax="-24.7003" ay="0" az="0" bx="-41.7003" by="0.00" bz="1.2"
width="6.2" taper="0.0" midpoint="0.0"/>
<!-- Engines body -->
<fuselage ax="4.0" ay="9.8" az="-3" bx="-1.8" by="9.8" bz="-3"
width="3.8" taper="1.0"/>
<fuselage ax="4.0" ay="-9.8" az="-3" bx="-1.8" by="-9.8" bz="-3"
width="3.8" taper="1.0"/>
<!-- Wings -->
<wing x="-0.0" y="3.095" z="-1.66" length="31.6" chord="12.8" sweep="32"
taper="0.15" dihedral="7" camber="0.01" incidence="2" twist="-2">
<stall aoa="16" width="6" peak="1.5"/>
<flap0 start="0" end=".56" lift="1.5" drag="1.7"/>
<flap1 start=".64" end=".88" lift="1.5" drag="1.2"/>
<slat start="0" end="1" aoa="2" drag="1"/>
<spoiler start="0.2" end="0.6" lift="0.2" drag="2.0"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-input axis="/surface-positions/flap-pos-norm" control="SLAT"
src0="0" dst0="0" src1="0.1428" dst1="1.0"/>
<control-output control="SLAT" prop="/surface-positions/slats"/>
<control-speed control="FLAP0" transition-time="78"/>
<control-input axis="/controls/flight/speedbrake" control="SPOILER"/>
<control-output control="SPOILER" prop="/surface-positions/speedbrake-pos-norm"/>
<control-speed control="SPOILER" transition-time="2"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
<control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
</wing>
<hstab x="-35.7003" y="1.5" z="1.0" chord="6.0" length="10.84" taper=".20"
sweep="40" dihedral="7" incidence="0" effectiveness="1" camber="-0.01">
<stall aoa="15" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.6" drag="1.2"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-trim-tab-pos-norm"/>
</hstab>
<vstab x="-34.7003" y="0.00" z="2.7" chord="8.0" length="12.2" taper="0.3"
sweep="35">
<stall aoa="14" width="5" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
min="1" max="-1"/>
</vstab>
<!-- GE90-115B -->
<jet x="1.16" y="9.89" z="-2.995" mass="19315" thrust="115540" spool-time="3"
egt="825" tsfc="0.25" n1-idle="18.5" n1-max="110.5" n2-idle="70" n2-max="121" reverse="0.4">
<control-input axis="/controls/engines/engine[0]/throttle-act" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/reverser-act" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[0]"/>
<control-speed control="REVERSE_THRUST" transition-time="3"/>
<actionpt x="-2.7" y="9.89" z="-2.995"/>
</jet>
<jet x="1.16" y="-9.89" z="2.995" mass="19315" thrust="115540" spool-time="3"
egt="825" tsfc="0.25" n1-idle="18.5" n1-max="110.5" n2-idle="70" n2-max="121" reverse="0.4">
<control-input axis="/controls/engines/engine[1]/throttle-act" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/reverser-act" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[1]"/>
<control-speed control="REVERSE_THRUST" transition-time="3"/>
<actionpt x="-2.7" y="-9.89" z="-2.995"/>
</jet>
<!-- nose -->
<gear x="24.5181" y="0.00" z="-5.55"
compression="0.7" spring="1.2" damp="1" sfric="1.5" dfric="1.0">
<!-- up to 70 degrees max steering angle with tiller, input is limited to 7 degrees with rudder (see Nasal/ground_steering.nas) -->
<control-input control="STEER" axis="/controls/gear/nosegear-steering-cmd-norm" src0="-1.0" dst0="-1.2217304764" src1="1.0" dst1="1.2217304764" />
<control-output control="STEER" prop="/controls/gear/nosegear-steering-angle-rad" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
<control-speed control="EXTEND" transition-time="19"/>
</gear>
<gear x="-6.39" y="5.6" z="-5.7" compression="0.8" spring="1.0" sfric="1" dfric="0.9">
<control-input axis="/autopilot/autobrake/left-brake-output" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
<control-speed control="EXTEND" transition-time="20"/>
</gear>
<gear x="-6.39" y="-5.6" z="-5.7" compression="0.8" spring="1.0" sfric="1" dfric="0.9">
<control-input axis="/autopilot/autobrake/right-brake-output" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
<control-speed control="EXTEND" transition-time="20"/>
</gear>
<!-- aft axle on left main gear -->
<gear x="-7.8" y="5.6" z="-6.22" compression="3.0" spring="1.2" >
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/>
<control-speed control="EXTEND" transition-time="20"/>
<!-- 8 degrees main gear steering when nose gear steering above 13 degrees commanded (see Nasal/ground_steering.nas) -->
<control-input control="STEER" axis="/controls/gear/maingear-steering-cmd-norm" src0="-1.0" dst0="-0.1396263402" src1="1.0" dst1="0.1396263402" />
<control-output control="STEER" prop="/controls/gear/maingear-l-steering-angle-rad" />
</gear>
<!-- aft axle on right main gear -->
<gear x="-7.8" y="-5.6" z="-6.22" compression="3.0" spring="1.2">
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/>
<control-speed control="EXTEND" transition-time="20"/>
<!-- 8 degrees main gear steering when nose gear steering above 13 degrees commanded (see Nasal/ground_steering.nas) -->
<control-input control="STEER" axis="/controls/gear/maingear-steering-cmd-norm" src0="-1.0" dst0="-0.1396263402" src1="1.0" dst1="0.1396263402" />
<control-output control="STEER" prop="/controls/gear/maingear-r-steering-angle-rad" />
</gear>
<!-- fake gear as tail contact point for tailstrikes -->
<gear x="-19.84" y="0.00" z="-3.38"
compression="0.1" spring="1" damp="1" sfric="0.5" dfric="0.5">
</gear>
<!-- apu -->
<vstab x="0" y="0" z="0" length="0" chord="0">
<flap0 start="0" end="1" lift="0" drag="0"/>
<control-input axis="/controls/APU/running" control="FLAP0"/>
<control-output control="FLAP0" prop="controls/APU/rpm"/>
<control-speed control="FLAP0" transition-time="30"/>
</vstab>
<tank x="-4.3" y="5" z="-1.5" jet="true" capacity="69000"/>
<tank x="-4.3" y="0" z="-2.5" jet="true" capacity="182800"/>
<tank x="-4.3" y="-5" z="-1.5" jet="true" capacity="69000"/>
<weight x="27.2381" y="0" z="0" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="-9.0003" y="0" z="0" mass-prop="/sim/weight[1]/weight-lb"/>
<ballast x="-34.7003" y="0" z="4" mass="-70000"/>
<thruster x="24.5181" y="0.00" z="-5.55" vx="1" vy="0" vz="0" thrust="20000">
<control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE"
src0="-1" src1="1" dst0="-1" dst1="1"/>
</thruster>
</airplane>