[fltsim.0]
title=Qantas B767-238ER
sim=767-200ER-PW-JT9D-7A
model=
panel=
sound=
texture=
checklists=

atc_airline=QANTAS
atc_id=VH-EAQ
atc_flight_number=405
atc_heavy=0

ui_manufacturer=Boeing
ui_type=767-200ER
ui_variation=Qantas VH-EAQ
visual_damage=1

description=Project Opensky Boeing 767-200ER\nVersion 2002.4.4\n\nQantas B767-238ER VH-EAQ "City of Launceston".\n\nModel Designers\n   Mitsushi Yutaka\n   Hiroshi Igami  \n\nQantas Textures\n  James Kaminski\n\nFlight Dynamics Designer\n   Warren C. Daniel\n\nTechnical Advisors\n   Nick Peterson\n   Simon Ng\n\nTest Pilots\n   Project Opensky Members\n\nMaximun Range: 6,610 nautical miles \n\nTypical city pairs: \n   NY-London

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[General]
performance=Maximum Take-off Weight\n 156,500 kg\/345,000 lb \nWing Span\n 47.57 metres\/156.1 ft \nOverall Length\n 48.51 metres\/159.2 ft \nVertical Fin Height\n 15.85 metres\/52.0 ft \nCabin Width\n 4.72 metres\/15.5 ft \nWing Area\n 283.3 sq m\/3,050 sq ft \nAverage Cruise Speed\n 857 kph\/533 mph \nCruise Altitude\n 35-41,000 ft \nMaximum Fuel Capacity\n 77,412 litres\/17,028 gallons \nRange With Full Payload\n 7,034 km\/4,371 miles \nMaximum Thrust\n 221.5 kilonewton\/49,800 lb \nEngines\n Pratt & Whitney JT9 D-7R4E \n

atc_type=BOEING AIRCRAFT
atc_model=B762

[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
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=248000.000
empty_weight_roll_MOI=4378085.000
empty_weight_pitch_MOI=7971735.000
empty_weight_yaw_MOI=12879901.000
empty_weight_coupled_MOI=0.000
max_gross_weight=345000.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[flight_tuning]
cruise_lift_scalar=1.00
parasite_drag_scalar=0.773
induced_drag_scalar=0.963
elevator_effectiveness=1.00
aileron_effectiveness=1.00
rudder_effectiveness=1.20
pitch_stability=1.00
roll_stability=1.00
yaw_stability=1.00
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[fuel]
Center1=0.000, 0.000, 0.000, 8197.000, 3.000
LeftMain=0.000, -5.000, 0.000, 6122.000, 3.000
RightMain=0.000, 5.000, 0.000, 6122.000, 3.000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=3050.000
wing_span=156.083
wing_root_chord=20.000
wing_dihedral=6.498
wing_incidence=-1.000
wing_twist=1.000
oswald_efficiency_factor=0.653
wing_winglets_flag=0
wing_sweep=31.500
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=733.000
htail_span=53.750
htail_pos_lon=-91.667
htail_pos_vert=0.000
htail_incidence=1.994
htail_sweep=45.000
vtail_area=325.000
vtail_span=20.555
vtail_sweep=35.000
vtail_pos_lon=-87.500
vtail_pos_vert=5.000
elevator_area=60.000
aileron_area=20.000
rudder_area=56.200
elevator_up_limit=31.513
elevator_down_limit=10.313
aileron_up_limit=24.000
aileron_down_limit=18.000
rudder_limit=32.000
elevator_trim_limit=18.335
spoiler_limit=45.000
spoilerons_available=1
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=9.969
min_flaps_for_spoilerons=0.000

//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)

[contact_points]

point.0=1.000, 56.500, 0.000, -9.750, 1181.102, 0.000, 2.000, 70.000, 0.500, 0.500, 0.750, 9.000, 9.000, 0.000, 240.000, 797.870
point.1=1.000, -9.000, -15.250, -9.500, 1574.803, 1.000, 2.000, 0.000, 0.500, 0.500, 0.920, 11.900, 11.900, 2.000, 240.000, 797.870
point.2=1.000, -9.000, 15.250, -9.500, 1574.803, 2.000, 2.000, 0.000, 0.500, 0.500, 0.920, 13.100, 13.100, 3.000, 240.000, 797.870
point.3=2.000, 0.000, -78.000, 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.4=2.000, 0.000, 78.000, 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.5=2.000, -60.000, 0.000, 0.000, 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.6=2.000, 78.000, 0.000, 0.000, 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.7=2.000, 0.000, 78.000, 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.8=2.000, 0.000, 36.000, 0.000, 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=-1.000
static_cg_height=9.600

//Nose Gear
//point.0=1.000, 56.500, -1.500, -10.500, 1181.102, 0.000, 2.000, 70.000, 1.000, 2.500, 0.518, 9.000, 9.000, 0.000, 240.000, 280.000
//point.1=1.000, 56.500,  1.500, -10.500, 1181.102, 0.000, 2.000, 70.000, 1.000, 2.500, 0.518, 9.000, 9.000, 0.000, 240.000, 280.000
//
//Left Main Gear
//point.2=1.000, -9.000,  15.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 240.000, 280.000
//point.3=1.000, -9.000,  12.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 240.000, 280.000
//point.4=1.000, -4.000,  15.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 240.000, 280.000
//point.5=1.000, -4.000,  12.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 240.000, 280.000
//
//Right Main Gear
//point.6=1.000, -9.000,  -15.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 240.000, 280.000
//point.7=1.000, -9.000,  -12.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 240.000, 280.000
//point.8=1.000, -4.000,  -15.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 240.000, 280.000
//point.9=1.000, -4.000,  -12.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 240.000, 280.000

//Scrape Points
//point.10=2.000, 0.000, -59.000, 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.11=2.000, 0.000, 59.000, 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.12=2.000, -60.000, 0.000, 0.000, 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.13=2.000, 78.000, 0.000, 0.000, 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.14=2.000, 0.000, 78.000, 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.15=2.000, 0.000, 36.000, 0.000, 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=-1.000
//static_cg_height=9.600

[GeneralEngineData]
engine_type=1
Engine.0=6.000, -26.667, -5.583
Engine.1=6.000, 26.667, -5.583
fuel_flow_scalar=0.978

[TurbineEngineData]
bypass_ratio=4.7000
fuel_flow_gain=0.001
inlet_area=48.150
rated_N2_rpm=29920.000
static_thrust=48000.000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=118.000
full_flaps_stall_speed=94.400
cruise_speed=535.341

[keyboard_response]
elevator=100.000000,200.000000
aileron=100.000000,200.000000
rudder=100.000000,200.000000

[Views]
eyepoint=68.997949,-1.768578,8.753178

[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=120.000000
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 = Default to Wing Leveler mode, 1 = No default bank mode.

[Radios]
// Radio Type=availiable, 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]
direction_indicator.0=3,0

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

[LIGHTS]    
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 
light.1=1,  35.5.00,   0.00, 14, fx_beaconh ,

light.2=1,  12.5.00,   0.00, -3.8, fx_beaconh ,


[Flaps.0]
type=1
span-outboard=0.800
extending-time=30.000
system_type=1
damaging-speed=200.000
blowout-speed=250.000
lift_scalar=0.700
drag_scalar=0.900
pitch_scalar=0.500
flaps-position.0=0.000, 0.000
flaps-position.1=1.000, 0.000
flaps-position.2=5.000, 0.000
flaps-position.3=15.000, 0.000
flaps-position.4=20.000, 0.000
flaps-position.5=25.000, 0.000
flaps-position.6=30.000, 0.000

[Flaps.1]
type=2
span-outboard=0.800
extending-time=35.000
system_type=1
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=0.300
drag_scalar=0.100
pitch_scalar=0.100
flaps-position.0=0.000, 0.000
flaps-position.1=20.000, 0.000