[fltsim.0]
title=Bombardier Global Express XRS N552RS
sim=Bombardier_BD_700
model=XRS
panel=ws
sound=
texture=N552RS
kb_checklists=Bombardier_BD700_check
kb_reference=Bombardier_BD700_ref
atc_id=N552RS
atc_airline=
atc_parking_codes=GLEX
atc_parking_types=RAMP
atc_heavy=0
ui_manufacturer="Bombardier"
ui_type="Global Express XRS"
ui_variation="N552RS"
ui_typerole="Business Jet"
ui_createdby="RFS"
description=The Global Express is a growth from the Challanger  601 series.  The Global Express cruises at an airspeed of 488 kts and has a maximum altitude of 51,000 ft.. The aircraft is powered by 2 BMW\/Rolls Royce  BR700-710A2-20 Turbofan engines, rated at 14,750 pounds takeoff thrust.\n\n\n\n

[fltsim.1]
title=Bombardier Global Express XRS N929LM
sim=Bombardier_BD_700
model=XRS
panel=ws
sound=
texture=N929LM
kb_checklists=Bombardier_BD700_Primus_check
kb_reference=Bombardier_BD700_ref
atc_airline=
ui_manufacturer="Bombardier"
ui_type="Global Express"
ui_variation="N929LM"
ui_typerole="Business Jet"
atc_heavy=0
atc_id=N929LM
atc_flight_number=1
atc_parking_codes=GLEX
atc_parking_types=RAMP
description=The Global Express is a growth from the Challanger  601 series.  The Global Express cruises at an airspeed of 488 kts and has a maximum altitude of 51,000 ft.. The aircraft is powered by 2 BMW\/Rolls Royce  BR700-710A2-20 Turbofan engines, rated at 14,750 pounds takeoff thrust.\n\n\n\n

[fltsim.2]
title=Bombardier Global Express XRS N30GL
sim=Bombardier_BD_700
model=XRS
panel=ws
sound=
texture=N30GL
kb_checklists=Bombardier_BD700_Primus_check
kb_reference=Bombardier_BD700_ref
atc_airline=
ui_manufacturer="Bombardier"
ui_type="Global Express"
ui_variation="N30GL"
ui_typerole="Business Jet"
atc_heavy=0
atc_id=N30GL
atc_flight_number=1
atc_parking_codes=GLEX
atc_parking_types=RAMP
description=The Global Express is a growth from the Challanger  601 series.  The Global Express cruises at an airspeed of 488 kts and has a maximum altitude of 51,000 ft.. The aircraft is powered by 2 BMW\/Rolls Royce  BR700-710A2-20 Turbofan engines, rated at 14,750 pounds takeoff thrust.\n\n\n\n


[fltsim.3]
title=Bombardier Global Express XRS N43GL
sim=Bombardier_BD_700
model=XRS
panel=ws
sound=
texture=N43GL
kb_checklists=Bombardier_BD700_Primus_check
kb_reference=Bombardier_BD700_ref
atc_airline=
ui_manufacturer="Bombardier"
ui_type="Global Express"
ui_variation="N43GL"
ui_typerole="Business Jet"
atc_heavy=0
atc_id=N43GL
atc_flight_number=1
atc_parking_codes=GLEX
atc_parking_types=RAMP
description=The Global Express is a growth from the Challanger  601 series.  The Global Express cruises at an airspeed of 488 kts and has a maximum altitude of 51,000 ft.. The aircraft is powered by 2 BMW\/Rolls Royce  BR700-710A2-20 Turbofan engines, rated at 14,750 pounds takeoff thrust.\n\n\n\n


[General]
atc_type=BOMBARDIER
atc_model=GLEXP
performance=Passengers: 8 to 25 depending on config.\nCrew: 2+1 \n\nTotal Baggage Volume: 473 cu ft \n\nDimensions:\nSpan 94 ft 4 in\nLength 99 ft 5 in\nHeight 24 ft 5in \n\nEngines: 2 BMWVRolls Royce BR700-710A2-20 Turbofans\nTO Thrust Rating: 14,750 lb\n\nMax Fuel Cap.: 44,716 lb. 6674 US gal.\nMaxTOW: 98,000 lb with SB 11-016\nZFW: 51,200 lb\n\nTypical Cruise Speed @ FL410: \nM.80 - Normal Cruise\nRange: 6,400 nm w/NBAA IFR reserves\nM.85 - High Speed Cruise\nRange: 6,100 nm with 8 Pax.\nMax Landing weight is 78,600 lbs. which allows 3770 ga. of max fuel at approach point,\n\
editable=0
Category=airplane

[CameraDefinition.0]
Title = "Aft Cabin"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the Cabin From aft area
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .52
ShowWeather = Yes
InitialXyz = 0.1, 0.2, -3.3    //Lateral, vertical, longitudinal
InitialPbh = 0, 0, 0
XyzAdjust = TRUE
Category=Cockpit		//Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title = "Forward Cabin"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking aft from behind the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0.0, 0.5, 7.25
InitialPbh = 0, 0, 180
XyzAdjust = TRUE
Category=VC		//Cockpit		//Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[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) 

point.0=1.0, -19.68000, 0.000000, -9.608, 1000.0, 0.0, 0.833333, 75.0, 0.536, 1.50, 0.655090 ,5.00, 5.00, 0.000, 200.00, 250.00      
point.1=1.0, -61.25400, -6.50000, -9.550, 1200.0, 1.0, 1.583333,  0.0, 0.583, 1.50, 0.655090, 6.50, 6.50, 2.000000, 200.00, 250.000   
point.2=1.0, -61.254000 ,6.50000, -9.550, 1200.0, 2.0, 1.583333,  0.0, 0.583, 1.50, 0.655090, 6.50, 6.50, 3.000000, 200.00, 250.000 

point.3=2.0, -12.500000,-35.416667,2.666667,1574.803150,0.00,0.00,0.00,0.00,0.000,0.00,0.00,0.00,5.00,0.0000,0.00
point.4=2.0, -12.500000, 35.416667,2.666667,1574.803150,0.000,0.00,0.000,0.000,0.000,0.000,0.000,0.000,6.00,0.00,0.000
point.5=2.0, -87.250, 0.00,-1.083333,1574.80,0.000,0.00,0.00,0.00,0.00,0.00,0.00,0.00,9.00,0.00,0.00
point.6=2.0, -35.417, 0.00,-1.083333,1574.80,0.000,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00

//static_pitch= 0.00                        //was= -0.390015
static_pitch = 0.0
static_cg_height=9.1067  //was 9.1643
gear_system_type=1                                        //Hydraulic
emergency_extension_type=2   //None=0,Pump=1,Gravity=2


[flaps.0]     //Inboard Leading Edge Slats
type             = 2                                    // 0 = no flaps 1 = trailing edge, 2 = leading edge.lead
span-outboard    = 0.85                                  // 0.0 .. 1.0
extending-time   = 5.00                                // seconds
flaps-position.0 = 0.0                                    // degrees
flaps-position.1 = 20.0                                 // degrees
flaps-position.2 = 20.0                                   // degrees
flaps-position.3 = 20.0                                   // degrees
flaps-position.4 = 20.0                                  // degrees
damaging-speed   = 260                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.2
pitch_scalar= 1.2
system_type = 1                                         //Hydraulic

[Flaps.1]       //Outboard Trailing Edge
type=1                                                // 0 = no flaps 1 = trailing edge, 2 = leading edge.lead
span-outboard    = 0.75                                   // 0.0 .. 1.0
extending-time   = 8.00                                   //  seconds
flaps-position.0 = 0.0                                  //  degrees  
flaps-position.1 = 0.0
flaps-position.2 = 6.0
flaps-position.3 = 16.0
flaps-position.4 = 30.0
damaging-speed   = 260                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[Flaps.2]       //Outboard Trailing Edge
type=1                                                // 0 = no flaps 1 = trailing edge, 2 = leading edge.lead
span-outboard    = 0.75                                   // 0.0 .. 1.0
extending-time   = 8.00                                   //  seconds
flaps-position.0 = 0.0                                  //  degrees    
flaps-position.1 = 0.0
flaps-position.2 = 6.0
flaps-position.3 = 16.0
flaps-position.4 = 30.0
ddamaging-speed   = 260                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[electrical]
//                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot          = 1, 5 , 17.0
flap_motor         = 4, 0 ,  1.0
gear_motor         = 0, 5 , 17.0
avionics_bus       = 0, 0 , 17.0
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 , 17.0
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 , 17.0
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


[flight_tuning]
cruise_lift_scalar     = 1.05			//1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.5
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 0.8
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[airplane_geometry]
wing_area=1022.000000
wing_span=99.42000000
wing_root_chord=20.0        
wing_dihedral=2.50
wing_incidence=2.50
wing_twist=-1.0
oswald_efficiency_factor=0.8
wing_winglets_flag=1
wing_sweep=28.0
wing_pos_apex_lon=-42.800      
wing_pos_apex_vert=-4.000000
htail_area=245.000000
htail_span=27.1000
htail_pos_lon=-93.2500
htail_pos_vert=13.670000
htail_incidence=0.000000
htail_sweep=38.000000
vtail_area=186.000000
vtail_span=15.757538
vtail_sweep=45.000000
vtail_pos_lon=-80.1
vtail_pos_vert=1.60
elevator_area = 42.1                  //Square feet
aileron_area  = 22.0                  //Square feet
rudder_area   = 21.4                  //Square feet
elevator_up_limit=24.0
elevator_down_limit=19.0
aileron_up_limit=26.5
aileron_down_limit=23.0
rudder_limit=37.0000
elevator_trim_limit=12.0000   
spoiler_limit=46.0
spoilerons_available=1
aileron_to_spoileron_gain=4.6
min_ailerons_for_spoilerons=5.0
min_flaps_for_spoilerons=0.000000
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000

[WEIGHT_AND_BALANCE]
max_gross_weight= 98250.0                    // This is Max gross weight. The Max Gross Takeoff Weight is 98,000 lbs
empty_weight= 49429.0                        // /Basic operating weight including crew, no fuel is 52,704 lbs = 11 pax, 3 crew + 470# bags

reference_datum_position     =  48.5, 0.0,  0.0    // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -56.4, 0.0, -3.0    // (feet) longitudinal, lateral, vertical distance from specified datum
Fwd_CG_limit= -43.9                  
Aft_CG_limit= -57.8

max_number_of_stations=15                                                 //Max Baggage wt with 8 pax is 475 lbs. and 4 crew 

station_load.0  =   200.0, -31.8, -2.4, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.1  =   200.0, -31.8,  2.4, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2  =   200.0, -35.1, -2.4, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3  =   200.0, -35.1,  2.4, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.4  =   200.0, -39.5, -2.4, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.5  =   200.0, -44.1, -2.4, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.6  =   200.0, -44.1, -0.5, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.7  =   200.0, -48.7, -2.4, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.8  =   200.0, -48.7, -0.5, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.9  =   200.0, -54.8,  2.4, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.10 =   200.0, -58.1,  2.4, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.11 =   475.0, -68.2,  0.0, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
//station_load.12 =   200.0, -21.1, -1.5, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
//station_load.13 =   200.0, -21.1,  1.5, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
//station_load.14 =   200.0, -26.2, -1.5, 0.0,	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 


station_name.0  = "Passenger 1"
station_name.1  = "Passenger 2"
station_name.2  = "Passenger 3"
station_name.3  = "Passenger 4"
station_name.4  = "Passenger 5"
station_name.5  = "Passenger 6"
station_name.6  = "Passenger 7"
station_name.7  = "Passenger 8"
station_name.8  = "Passenger 9"
station_name.9  = "Passenger 10"
station_name.10 = "Passenger 11"
station_name.11 = "Aft Baggage"
//station_name.12 = "Pilot"
//station_name.13 = "Co-Pilot"
//station_name.14 = "Attendant"

;Moments of Inertia
empty_weight_pitch_MOI=634280                  //was=541473           
empty_weight_roll_MOI=239091                     //was=153909.000
empty_weight_yaw_MOI=614487                    //was=882504.000             
empty_weight_coupled_MOI=0.000               //was=4305.000
                            
[fuel]  //Max fuel capacity is 6674 ga. or 44,975 lbs @6.75 lbs/gal US. FSX is set for 6.7 lb/gal US. 
Center2=-48.600000,0.000000,0.000000,1879.000000,6.000000			//was=43.6
Center1=-65.000000,0.000000,0.000000,337.000000,1.4000000
LeftMain=-56.20000,-8.000000,0.000000,2229.000000,9.000000			//was=58.2
RightMain=-56.20000,8.000000,0.000000,2229.000000,9.000000			//was=58.2
fuel_type=2.000000
number_of_tank_selectors=2
electric_pump=1

[GeneralEngineData]
engine_type=1
Engine.0=-74.42400,-7.83333, 1.597000 
Engine.1=-74.42400, 7.83333, 1.597000   
fuel_flow_scalar=0.98				//1.0                   
min_throttle_limit=-0.25

[TurbineEngineData]  //BD700
fuel_flow_gain=0.0025000 
thrustspecificfuelconsumption=0.2517                  //was=0.275   0.2734
inlet_area=9.400000   
rated_N2_rpm=29920.00 
static_thrust=14750.00
afterburner_available=0
reverser_available=1

[jet_engine]
thrust_scalar =1.0

[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, 1
Adf.1         = 1
Adf.2         = 1
Transponder.1 = 1
Marker.1      = 1

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator = 100, 200
aileron  = 100, 200
rudder   = 100, 200

[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

[exits]
number_of_exits = 4
exit_rate.0 = 0.15, 21.364, -2,9775, -3.0928, 0    ;Percent per second
exit_rate.1 = 0.2, -20.1978, -3.9104, 0.5781, 1    ;Percent per second
exit_rate.2 = 0.2,  -2.5333, 4.093, 0.6562, 2      ;Percent per second
exit_rate.3 = 0.2, -43.4450, 0.8648, 1.9943, 0     ;Percent per second

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

[Reference Speeds]
flaps_up_stall_speed    =  115.0                  //Knots True (KTAS)
full_flaps_stall_speed  =   96.0                  //Knots True (KTAS)
cruise_speed            =  459.0                  //Knots True (KTAS)
max_indicated_speed     =  335.0
max_mach=0.89980

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 0.000
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 96.0
pitch_takeoff_ga= 10.000
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.
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=27,17
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=16.000000
nav_integrator_control=0.20000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=25.00000
gs_integrator_control=0.53000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=1.000000

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
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=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 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=35999                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=35999                   ; 0 - 35999 degrees
crash_period2=75000000                     ; in microseconds
crash_duration2=25000000                 ; in microseconds

[Views]
eyepoint= -20.8217, -1.4688,  1.41  //Glexp interior Pilot
//eyepoint= -20.8217, 0.0,  1.21  //Glexp interior center
//eyepoint= -20.8217, 1.4688,  1.21  //Glexp interior Co-Pilot		
zoom=0.5		//zoom=1.0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=Landing, 6=Taxi, 7=Recognition, 8=Wing, 9=Logo, 10=Cabin
  
light.0=3, -74.000, -44.9537, -2.451,  fx_navredh ,
light.1=3, -74.000,  44.9537, -2.451,  fx_navgreh ,
light.2=3,-105.300,   0.0000, 13.926,  fx_navwhih ,
light.3=2, -79.695, -45.3945, -2.266,  fx_strobeh ,
light.4=2, -79.695,  45.3945, -2.266,  fx_strobeh ,
light.5=1, -31.750,    0.00,   4.7500, fx_beacon ,
light.6=1, -49.725,    0.00,  -6.358,  fx_beacon ,
light.7=4, -23.10,     1.50,   2.700,  fx_vclightmed ,			//was -19.10, xxx.xx, 2.29	
light.8=4, -23.10,    -1.50,   2.700,  fx_vclightmed ,	
light.9=10, -27.20,    0.00,   3.500,  fx_vclighth ,
light.10=10,-40.50,    0.00,   3.500,  fx_vclighth ,
light.11=10,-49.50,    0.00,   3.500,  fx_vclighth ,
light.12=10,-55.50,    0.00,   3.500,  fx_vclighth ,
light.13=10,-68.50,    0.00,   3.500,  fx_vclighth ,
light.14=10,-20.82,    0.00,   1.500,  fx_vclighth ,

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 1.2  //Brake scalar
auto_brakes = 3
hydraulic_system_scalar = 1  //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure


[hydraulic_system]
electric_pumps=4         //no electric pumps
engine_map=1,1,0,0      //pumps on Eng1,2
normal_pressure=3000.0  //PSI

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  6.0     //Flap angle that activates warning at idle
flap_limit_power   = 20.0     //Flap angle that activates warning at above idle

[stall_warning]
type=2
stick_shaker=1

[deice_system]
structural_deice_type=1

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 2 
attitude_indicator.0=1

[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1

[altimeters]
altimeter.0=1
altimeter.1=1

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
turn_indicator.1=0,0

[pitot_static]
pitot_heat=1.000000

[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=30.000000
bleed_air_scalar=1.0000

[pressurization]
design_cabin_pressure = 12.927     //was=12.227
max_pressure_differential =10.15  //was=9.833

[GPWS]
max_warning_height         =  1500
sink_rate_fpm              = -1500
excessive_sink_rate_fpm    = -2000
climbout_sink_rate_fpm     = -100
flap_and_gear_sink_rate_fpm= -100