[fltsim.0]
title=Concorde Qantas Airways
sim=Concorde
model=
panel=
sound=
texture=
kb_checklists=Concorde_check
kb_reference=Concorde_ref
atc_id=G-BOAC
atc_id_enable=1
atc_airline=Qantas
atc_flight_number=1123
ui_manufacturer=Aerospatiale
ui_type=Concorde
ui_variation=Qantas Airways
visual_damage=1
description=See ref notes for detatails. 

[General]
performance=Max speed 2,5 Mach\nCruise speed 2 Mach\nMax range 3371 mn \nCealing 60000 feet 


[WEIGHT_AND_BALANCE]
empty_weight=172930.0				// (pounds)

reference_datum_position=0.0,   0, 0	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-50.333, 0, 0    // (feet) longitudinal, lateral, vertical distance from specified datum

station_load.0=1760,   1.00, 0.0, 0.0		//Weight Crew (lbs),         longitudinal, lateral, vertical positions from datum (feet)
station_load.1=3342, -29.00, 0.0, 0.0		//Weight Galleys(lbs),       longitudinal, lateral, vertical positions from datum (feet)
station_load.2=300,   8.00, 0.0, 0.0		//Weight Baggage 1 (lbs),    longitudinal, lateral, vertical positions from datum (feet)
station_load.3=500,  -4.00, 0.0, 0.0		//Weight Baggage 2 (lbs),    longitudinal, lateral, vertical positions from datum (feet)
station_load.4=2562, -82.00, 0.0, 0.0		//Weight Baggage 3 (lbs),    longitudinal, lateral, vertical positions from datum (feet)
station_load.5=3040,  18.00, 0.0, 0.0		//Weight Psgr Sect OA (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6=3040,   2.00, 0.0, 0.0		//Weight Psgr Sect OB (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7=4370, -28.00, 0.0, 0.0		//Weight Psgr Sect OC (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8=6080, -53.00, 0.0, 0.0		//Weight Psgr Sect OD (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight_roll_MOI=695703.000000
empty_weight_pitch_MOI=9295118.000000
empty_weight_yaw_MOI=4906663.000000
empty_weight_coupled_MOI=0.000000

[ground_reaction]
main_gear_static_compression=1.5		// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=1.5            // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=0.95		// Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=0.95		// Center gear strut damping, 0 = undamped osciallations, 1 = critically damped

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
fuel_transfer_pump=0, 10, 17.0

[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



[contact_points]
point.0=1.000000,5.666667,0.000000,-15.500000,1181.102362,0.000000,3.336104,34.080000,1.500000,2.500000,0.950000,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,-54.000000,-13.000000,-15.000000,1574.803150,1.000000,3.336104,0.000000,1.500000,2.500000,0.950000,7.900000,7.900000,2.000000,0.000000,0.000000
point.2=1.000000,-54.000000,13.000000,-15.000000,1574.803150,2.000000,3.336104,0.000000,1.500000,2.500000,0.950000,8.100000,8.100000,3.000000,0.000000,0.000000
point.3=2.000000,-14.166667,-47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-14.166667,47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-116.666667,0.000000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,42.666667,0.000000,-3.750000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.280151
static_cg_height=12.720257

[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=16.000000
rated_N2_rpm=29920.000000
static_thrust=35500.000000
afterburner_available=1
reverser_available=1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1 	
use_no_default_bank=1

[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

[fuel]
Center1=-21.000000,0.000000,0.000000,7680.000000,0.000000
Center2=-98.500000,0.000000,0.000000,3500.000000,0.000000
LeftMain=-54.200000,-14.600000,-4.500000,10170.000000,0.000000
RightMain=-54.200000,14.600000,-4.500000,10170.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=4262.000000
wing_span=83.833333
wing_root_chord=66.166667
wing_dihedral=0.000000
wing_incidence=0.247192
wing_twist=0.000000
oswald_efficiency_factor=0.903612
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=0.000000
htail_span=0.000000
htail_pos_lon=0.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=249.000000
vtail_span=17.991665
vtail_sweep=0.000000
vtail_pos_lon=-35.833333
vtail_pos_vert=5.833333
elevator_area=70.500000
aileron_area=26.800000
rudder_area=56.200000
elevator_up_limit=29.793805
elevator_down_limit=29.793805
aileron_up_limit=29.793805
aileron_down_limit=29.793805
rudder_limit=30.000070
elevator_trim_limit=19.996227
spoiler_limit=0.000000
spoilerons_available=1
aileron_to_spoileron_gain=3.000000
min_ailerons_for_spoilerons=9.969466
min_flaps_for_spoilerons=0.000000

[GeneralEngineData]
engine_type=1
Engine.0=-38.000000,-19.250000,-1.000000
Engine.1=-38.000000,-15.250000,-1.000000
Engine.2=-38.000000,15.250000,-1.000000
Engine.3=-38.000000,19.250000,-1.000000
fuel_flow_scalar=1.000000



[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=59.388328,-1.307210,4.267655

[direction_indicators]
direction_indicator.0=3,0

[Reference Speeds]
flaps_up_stall_speed=120.000
full_flaps_stall_speed=90.000
cruise_speed=750.000

[Flaps.0]
type=1
span-outboard=0.500
extending-time=8.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=2.500
pitch_scalar=0.500
flaps-position.0=0.000, 0.000
flaps-position.1=0.050, 0.000
flaps-position.2=0.100, 0.000
flaps-position.3=0.200, 0.000
flaps-position.4=0.400, 0.000
flaps-position.5=0.800, 0.000
flaps-position.6=1.000, 0.000
flaps-position.7=1.300, 0.000
flaps-position.8=2.000, 0.000