[fltsim.0]
title=Qantas Airways 747-338 Qantas Nalanji Dreaming
sim=747-300RR
model=
panel=
sound=
texture=
checklists=

atc_airline=Qantas
atc_id=VH-EBU
atc_flight_number=5123
atc_heavy=1

ui_manufacturer=Boeing
ui_type=747-300
ui_variation=Qantas "Nalanji Dreaming"
visual_damage=1
description=Project Opensky \nBoeing 747-300\nVersion 2002.5.3\n\nEngine Type RR RB.211-524\n\n747-200 Commercial Version \n\nModel Designers\n   Mitsushi Yutaka\n   Hiroshi Igami  \n\nFlight Dynamics Designer\n   Warren C. Daniel, Nick Peterson\n\nTechnical Resource\n   Simon Ng\n   Shigeo Kitaguchi\n\nTest Pilots\n   Project Opensky Members\n\nMaximun Range: 6,620 nm\n\nTypical city pairs: \n   Tokyo-NY\n   Bangkok-Paris\n   London-Johannesburg\n\nFor proper operation: See B747 manual at: \n  www.project-opensky.com


[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=2.0
aileron_effectiveness=1.2
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[forcefeedback]
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds


[pitot_static]
vertical_speed_time_constant=999                //Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=50
empty_weight=470756     // Aircraft Weight = Base Weight + PAX + Cargo     
empty_weight_roll_MOI=13155743.000
empty_weight_pitch_MOI=22600873.000
empty_weight_yaw_MOI=26751035.000
empty_weight_coupled_MOI=1000.000
max_gross_weight=713000
CG_forward_limit=0.000
CG_aft_limit=1.000
station_load.0=0.000000,0.000000,0.000000,0.000000

[fuel]
Center1=0.000,   0.0, -4.0, 19431.0, 3.0
LeftMain=-5.0, -35.0, -4.0, 16660.0, 3.0     
LeftAux=-11.5, -52.0, -3.0, 500.0, 3.0     
RightMain=-5.0,  35.0, -4.0, 16660.0, 3.0     
RightAux=-11.5,  52.0, -3.0, 500.0, 3.0     
fuel_type=2                                     //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1 
electric_pump=1

[airplane_geometry]
wing_area=5500.000
wing_span=196.000
wing_root_chord=23.000
wing_dihedral=6.998
wing_incidence=2.000
wing_twist=-0.994
oswald_efficiency_factor=0.830
wing_winglets_flag=0
wing_sweep=37.500
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=1470.000
htail_span=72.750
htail_pos_lon=-17.167
htail_pos_vert=0.000
htail_incidence=-4.000
htail_sweep=37.500
vtail_area=1060.000
vtail_span=37.121
vtail_sweep=45.000
vtail_pos_lon=-16.500
vtail_pos_vert=6.083
elevator_area=326.800
aileron_area=225.200
rudder_area=229.900
elevator_up_limit=13.751
elevator_down_limit=10.313
aileron_up_limit=31.513
aileron_down_limit=31.513
rudder_limit=17.189
elevator_trim_limit=19.167
spoiler_limit=25.783
spoilerons_available=0
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=11.459
min_flaps_for_spoilerons=0.000

[contact_points]
//0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
//1  Longitudinal Position        (feet)
//2  Lateral Position             (feet)
//3  Vertical Position            (feet)
//4  Impact Damage Threshold      (Feet Per Minute)
//5  Brake Map                    (0=None, 1=Left, 2=Right)
//6  Wheel Radius                 (feet)
//7  Steer Angle                  (degrees)
//8  Static Compression           (feet)  (0 if rigid)
//9  Max/Static Compression Ratio
//10 Damping Ratio                (0=Undamped, 1=Critically Damped)
//11 Extension Time               (seconds)
//12 Retraction Time              (seconds)
//13 Sound Type
//14 Airspeed limit for retraction     (KIAS)
//15 Airspeed that gear gets damage at (KIAS)

// Nose gear
point.0=1.000, 67.333, -1.500, -14.203, 1181.102, 0.000, 2.000, 70.000, 1.059, .800, 0.518, 9.000, 11.000, 0.000, 240.000, 280.000
point.1=1.000, 67.333,  1.500, -14.203, 1181.102, 0.000, 2.000, 70.000, 1.059, .800, 0.518, 9.000, 11.000, 0.000, 240.000, 280.000

// Main Wing Gear (left)
point.2=1.000,  -7.583, -18.000, -15.533, 1574.803, 1.000, 2.000, 0.000, 2.52, 1.00, 0.651, 12.900, 14.900, 2.000, 240.000, 280.000
point.3=1.000,  -7.583, -14.000, -15.533, 1574.803, 1.000, 2.000, 0.000, 2.52, 1.00, 0.651, 12.900, 14.900, 2.000, 240.000, 280.000
point.4=1.000,  -2.583, -18.000, -15.533, 1574.803, 1.000, 2.000, 0.000, 2.52, 1.00, 0.651, 12.900, 14.900, 0.000, 240.000, 280.000
point.5=1.000,  -2.583, -14.000, -15.533, 1574.803, 1.000, 2.000, 0.000, 2.52, 1.00, 0.651, 12.900, 14.900, 2.000, 240.000, 280.000

// Main Wing Gear (right)
point.6=1.000,  -7.583, 18.000, -15.533, 1574.803, 2.000, 2.000, 0.000, 2.52, 1.00, 0.651, 15.100, 16.400, 3.000, 240.000, 280.000
point.7=1.000,  -7.583, 14.000, -15.533, 1574.803, 2.000, 2.000, 0.000, 2.52, 1.00, 0.651, 15.100, 16.400, 3.000, 240.000, 280.000
point.8=1.000,  -2.583, 18.000, -15.533, 1574.803, 2.000, 2.000, 0.000, 2.52, 1.00, 0.651, 15.100, 16.400, 3.000, 240.000, 280.000
point.9=1.000,  -2.583, 14.000, -15.533, 1574.803, 2.000, 2.000, -0.000, 2.52, 1.00, 0.651, 15.100, 16.400, 3.000, 240.000, 280.000

// Main Center Gear (left)
point.10=1.000, -18.583, -8.000, -15.533, 1574.803, 1.000, 2.000, 13.000, 2.52, 1.00, 0.651, 13.400, 14.900, 2.000, 240.000, 280.000
point.11=1.000, -18.583, -4.000, -15.533, 1574.803, 1.000, 2.000, 13.000, 2.52, 1.00, 0.651, 13.400, 14.900, 2.000, 240.000, 280.000
point.12=1.000, -12.583, -8.000, -15.533, 1574.803, 1.000, 2.000, 13.000, 2.52, 1.00, 0.651, 13.400, 14.900, 2.000, 240.000, 280.000
point.13=1.000, -12.583, -4.000, -15.533, 1574.803, 1.000, 2.000, 13.000, 2.52, 1.00, 0.651, 13.400, 14.900, 2.000, 240.000, 280.000

// Main Center Gear (right)
point.14=1.000, -18.583,  8.000, -15.533, 1574.803, 2.000, 2.000, 13.000, 2.52, 1.00, 0.651, 11.500, 17.500, 3.000, 240.000, 280.000
point.15=1.000, -18.583,  4.000, -15.533, 1574.803, 2.000, 2.000, 13.000, 2.52, 1.00, 0.651, 11.500, 17.500, 3.000, 240.000, 280.000
point.16=1.000, -12.583,  8.000, -15.533, 1574.803, 2.000, 2.000, 13.000, 2.52, 1.00, 0.651, 11.500, 17.500, 3.000, 240.000, 280.000
point.17=1.000, -12.583,  4.000, -15.533, 1574.803, 2.000, 2.000, 13.000, 2.52, 1.00, 0.651, 11.500, 17.500, 3.000, 240.000, 280.000

//Scrape points
point.18=2.000, -14.167, -96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.19=2.000, -14.167, 96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.20=2.000, -132.667, 0.000, 2.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.21=2.000, 88.167, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.22=2.000, -14.167, -96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.23=2.000, -132.667, 0.000, 55.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000

static_pitch=-1.300
static_cg_height=13.625
gear_system_type=0

[GeneralEngineData]
engine_type=1
Engine.0=-14.916667,-69.500000,0.000000
Engine.1=14.916667,-39.166667,-7.000000
Engine.2=14.916667,39.166667,-7.000000
Engine.3=-14.916667,69.500000,0.000000
fuel_flow_scalar=1.02
min_throttle_limit=-0.399902

[TurbineEngineData]
bypass_ratio=4.970000
fuel_flow_gain=0.002000
inlet_area=37.558941
rated_N2_rpm=26928.000000
static_thrust=53110.000000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=150.000
full_flaps_stall_speed=126.000
cruise_speed=494.337
max_indicated_speed=350.000000
max_mach=0.900000

[keyboard_response]
elevator=100.000, 200.000
aileron=100.000, 200.000
rudder=150.000, 250.000

[Views]
eyepoint=83.000, -2.000, 14.800    // Longitude, 

[General]
performance=Passengers\n3-class conf: 366 \n2-class conf: 452 \n1-class conf: N\/A\n\nCargo\nTotal lower hold volume:\n   5,497 ft3 (155.6 m3)  \n\nDimensions\nSpan 195 ft 8 in\nLength 231 ft 10 in\nHeight 63 ft 5 in\n\nEngines: RR RB.211-524\nTO Thrust: 53,110 lb x 4\n\nMax Fuel Cap.: 52,410 US Gal.\nMaxTOW: 833,000 lbs\nMLW: 630,000 lbs\nZFW: 538,340 lbs\nOEW: 388,010 lbs\n\nMax Range: 6,620 mi \nTypical Cruise Speed \n   @ FL350: M.84

atc_type=BOEING AIRCRAFT
atc_model=B743
editable=0

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=105.000000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=1 // 0 = Def
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.4                                  // 0.0 .. 1.0
extending-time=25                                   // seconds
flaps-position.0=0                                   // degrees
flaps-position.1=5                                    // degrees
flaps-position.2=10                                    // degrees
flaps-position.3=15                                   // degrees
flaps-position.4=20                                   // degrees
flaps-position.5=25                                   // degrees
flaps-position.6=30                                   // degrees
damaging-speed=200                                  // KIAS
blowout-speed=250                                  // KIAS
lift_scalar=0.42
drag_scalar=.47
pitch_scalar=0.9
system_type=1                                         //Hydraulic

[flaps.1]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.4                                 // 0.0 .. 1.0
extending-time=25                                   // seconds
flaps-position.0=0                                   // degrees
flaps-position.1=5                                    // degrees
flaps-position.2=10                                    // degrees
flaps-position.3=15                                   // degrees
flaps-position.4=20                                   // degrees
flaps-position.5=25                                   // degrees
flaps-position.6=30                                   // degrees
damaging-speed=200                                  // KIAS
blowout-speed=250                                  // KIAS
lift_scalar=0.42
drag_scalar=.47
pitch_scalar=0.9
system_type=1                                         //Hydraulic

[flaps.2]
type=2                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=12                                    // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=20.0                                  // degrees
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=0.27
drag_scalar=.7
pitch_scalar=0.1
system_type=1                                         //Hydraulic

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[direction_indicators]
direction_indicator.0=3,0

[stored information]
cargo_config=auto
cargo_container_type=
cargo1=0
cargo2=0
cargo3=0
cargo4=0
cargo5=0
cargo6=0
cargo7=0
cargo8=0
cargo9=0
cargo10=0
cargo11=0
cargo12=0
cargo13=0
cargo14=0
cargo15=0
cargo16=0
cargo17=0
cargo18=0
cargo19=0
cargo20=0
cargo21=0
cargo22=0
cargo23=0
cargo24=0
cargo25=0
cargo26=0
cargo27=0
cargo28=0
cargo29=0
cargo30=0
cargo_bulk=0
main_deck_cargo=0
main_deck_cargo_type=
per_pax_weight=51
forward_cargo=0
aft_cargo=0
total_passengers=356
pax_config=simple
pax_upper=0
pax1=0
pax2=0
pax3=0
pax4=0
pax5=0
pax6=0
aircraft_type=747-300
seating_type=Basic Mixed-Class
[default information]
empty_weight=489520
max_gross_weight=820000
Center1=0.000,   0.0, -4.0, 19431.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=-5.0, -35.0, -4.0, 16660.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=-11.5, -52.0, -3.0, 500.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-5.0,  35.0, -4.0, 16660.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=-11.5,  52.0, -3.0, 500.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
station_load.0=0.000000,0.000000,0.000000,0.000000

[TailHook]    // For opening cargo door.
tailhook_length=1                               ;(feet)
tailhook_position=0.0, 0.0, 0.0            ;(feet) longitudinal, lateral, vertical positions from datum

[folding_wings]  // For opening main deck cargo door.
wing_fold_system_type=4                       ;0=None
fold_rates=0.05,0.05                          ;Percent per second
cable_force_adjust=1.0

[exits]
number_of_exits=2
exit_rate.0=0.4
exit_rate.1=0.4

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing                   
light.0=1,   65.200,    0.600,  19.100,  Opensky_beacon ,
light.1=1,   13.500,    0.000,  -7.080,  Opensky_beacon ,
light.2=2,  -46.20, -95.300,  8.85,  fx_strobeh ,
light.3=2,  -46.20,  95.300, 8.85,  fx_strobeh ,
light.4=3, -122.700,   -0.250,   12.300, Opensky_nav_yellow ,
light.5=3, -122.700,    0.250,   12.300, Opensky_nav_yellow ,
light.6=2, -121.900,    0.000,   11.450, fx_strobeh ,
light.7=3,   84.850,    0.000,   14.850, fx_vclighth ,
light.8=3, -111.500,   -4.500,   43.750, Opensky_wing_light ,
light.9=3, -111.500,    4.500,   43.750, 

[electrical]
//                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=1, 0 ,  1.0
gear_motor=0, 5 , 17.0
avionics_bus=0, 0 ,  1.0
avionics=1, 5 , 17.0
pitot_heat=0, 0 ,  1.0
additional_system=0, 0 ,  1.0
marker_beacon=1, 2 , 17.0
gear_warning=7, 0 , 99.0
gear_motor=4, 0 ,  1.0
fuel_pump=0, 0 ,  1.0
fuel_transfer_pump=0, 0 ,  1.0
starter1=0, 20, 17.0
starter2=0, 0 ,  1.0
light_nav=0, 0 ,  1.0
light_beacon=0, 0 ,  1.0
light_landing=0, 0 ,  1.0
light_taxi=0, 0 ,  1.0
light_strobe=0, 0 ,  1.0
light_panel=0, 7 , 99.0
light_recognition=0, 0 ,  1.0
light_wing=0, 0 ,  1.0
marker_beacon=0, 0 ,  1.0
standby_vacuum=0, 0 ,  1.0
auto_brakes=0, 0 ,  1.0
hydraulic_pump=0, 0 ,  1.0
propeller_device=0, 0 ,  1.0


[Radios]
// Radio Type=available, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type=4
direction_indicator.0=3,0
[aircraft.cfg id]
ProjectOpenSky=747-300 with Rolls Royce RB-211-524 Engines
model_version=747-300 FSDS Version

[brakes]
toe_brakes_scale=0.915555
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029

[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0