[fltsim.0]
title=Luxair Dash 8Q400
sim=dhc84
model=
panel=
sound=
texture=lux
checklists=
ui_manufacturer=Bombardier
ui_type=Dash 8Q400
ui_variation=Luxair
atc_airline=luxair
atc_flight_number=201
description=Bombardier Dash 8Q400\Luxair 
atc_id=LX-DEF
atc_parking_types=
atc_parking_codes=
visual_damage=0
atc_heavy=0

[General]
performance=Max Cruise Speed\t350kts\nMaximum Range\t1,362 nm\nService Ceiling\t27,000 ft\nMax Gross Weight\t64,500 lb\nSeating\t\tUp to 70
atc_type=Bombardier
atc_model=DHC84
editable=0

[WEIGHT_AND_BALANCE]
empty_weight = 37717                            // (pounds)
reference_datum_position     =  0.000000,0.000000,0.000000      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  0.000000,0.000000,0.000000      // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations =50

station_load.0 = 15400,    0,  0, 0.0      //Payload

;Moments of Inertia
empty_weight_roll_MOI = 205716
empty_weight_pitch_MOI = 231761
empty_weight_yaw_MOI = 330944
empty_weight_coupled_MOI = 1300
max_gross_weight=64500.000000

[fuel]
LeftMain=0.000000,-14.500000,0.00000,862.00000,0.000000
RightMain=0.000000,14.500000,0.00000,862.00000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=1

[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,   35.72,   0.00, -5.259, 1500, 0, 1.671, 80, 0.250, 0.572, 0.9, 7.0, 5.0, 0, 120, 250
point.1=1, -0.917, -5.604, -5.696, 1574.803, 1.000, 1.014, 0.000, 0.272, 2.500, 0.9, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1, -0.917, 5.604, -5.696, 1574.803, 2.000, 1.014, 0.000, 0.272, 2.500, 0.9, 5.000, 5.000, 3.000, 0.000, 0.000

point.3=2.000, -0.500, -42.667, 3.833, 1574.803, 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, -0.500, 42.667, 3.833, 1574.803, 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, -20.333, 0.000, 0.000, 1574.803, 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, 24.083, 0.000, 0.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=0.000000
static_cg_height=5.506865
gear_system_type=0

[forcefeedback]
gear_bump_nose_magnitude=3000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=2800
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=3100
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=1450
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


[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light rocognition=0, 2 , 0
light_wing=0, 2 , 0
light_logo=0, 2 , 0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0


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


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1700.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=100000.000000
use_no_default_pitch=1 
use_no_default_bank=1
pitch_takeoff_ga=8.000000
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

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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3,  -3.379, -46.32,  6.716, fx_navred ,
light.1 = 3,  -3.379,  46.32,  6.716, fx_navgre ,
light.2 = 2,  -3.379,  46.32,  6.716, fx_strobe ,
light.3 = 2,  -3.379, -46.32,  6.716, fx_strobe ,
light.4 = 1,  -3.737,   0.00,  6.811, fx_beacon , // Boven
light.5 = 1,   0.000,   0.00,  -2.369, fx_beacon , // Onder
light.6 = 1,  -54.31,   0.00,  5.249, fx_strobeh , // Achter
electric_pump=0

[airplane_geometry]
wing_area               = 1179.0                //Square feet
wing_span               = 93.3                  //Feet
wing_root_chord         = 7.0                   //Feet
wing_dihedral           = 2.5                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -3.0                  //Degrees
oswald_efficiency_factor= 1.7                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 3.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = 25.0                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 97.0                  //Square feet
htail_span              = 26.0                  //Feet
htail_pos_lon           = -58.9                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 1.0                   //Degrees
htail_sweep             = 8.0                   //Degrees, horizontal tail leading edge
vtail_area              = 106.0                 //Square feet
vtail_span              = 11.7                  //Feet, tip to body
vtail_sweep             = 30.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -54.9                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 3.4                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 53.5                  //Square feet
aileron_area            = 12.1                  //Square feet
rudder_area             = 46.4                  //Square feet
elevator_up_limit       = 17.0                  //Degrees
elevator_down_limit     = 15.5                  //Degrees
aileron_up_limit        = 18.0                  //Degrees
aileron_down_limit      = 18.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 15.0                  //Degrees
spoiler_limit           = 60.0                  //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed    = 92.0                  //Knots True (KTAS)
full_flaps_stall_speed  = 72.0                  //Knots True (KTAS)
cruise_speed            =330
max_mach                = 0.62
max_indicated_speed     = 300                  //Red line (KIAS)

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.7                                  // 0.0 .. 1.0
extending-time   = 5                                    // seconds
flaps-position.0 = 0                                    // degrees, KIAS
flaps-position.1 = 10                                   // degrees, KIAS
flaps-position.2 = 30                                   // degrees, KIAS
flaps-position.3 = 40                                   // degrees, KIAS
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS

[flight_tuning]
cruise_lift_scalar=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=2.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=2.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0


[GeneralEngineData]
engine_type=5
Engine.0=9.500000,-8.500000,2.333333
Engine.1=9.500000,8.500000,2.333333
fuel_flow_scalar=0.9
min_throttle_limit=-0.250000


[TurbineEngineData]
fuel_flow_gain=0.011                 //Gain on fuel flow
inlet_area=1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                //RPM, second stage compressor rated value
static_thrust=465                   //Lbs, max rated static thrust at Sea Level

[propeller]
thrust_scalar           = 1.0                   //Propeller thrust scalar
propeller_type          = 0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter      = 13.0                  //Propeller Diameter, (feet)
propeller_blades        = 4                     //Number of propeller blades
propeller_moi           = 77                    //Propeller moment of inertia
beta_max                = 45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min                = 12                    //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm             = 25520                 //Miminum governed RPM
prop_tc                 = 0.004                 //Prop time-constant
gear_reduction_ratio    = 17.0                  //Propeller gear reduction ratio
fixed_pitch_beta        = 0                     //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit  = 80                    //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available     = 1                     //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available    = 1                     //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 1               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather     = 700                   //Minimum RPM for prop feathering
beta_feather            = 79.3                  //Feathering pitch angle (degrees)
power_absorbed_cf       = 0.9                   //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available  = 1                     //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta  = 1.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta    = -14.0                 //Minimum pitch angle in reverse, (degrees)

[turboprop_engine]
maximum_torque=12198                  //Maximum torque available (ft-lbs)

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

[Views]
eyepoint=1.03, -1.8, 3.26

[direction_indicators]
direction_indicator.0=3,0

[SmokeSystem]
smoke.0=-0.5,-2.333,-4.833, fx_smoke_rx                 
smoke.1=-0.5,-2.333,4.833, fx_smoke_rx


[brakes]
toe_brakes_scale=0.495224
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494

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

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[exits]
number_of_exits= 2
exit_rate.0= 0.25                              ;Percent per second
exit_rate.1= 0.35                              ;Percent per second