[fltsim.0]
title=Dreamwings Dash8 Q300 
sim=Dash8 Q300
model=
panel=
sound=
texture=beta
ui_manufacturer=De Havilland
ui_type=Dash 8 Q300
ui_variation=Test
description=Dreamwings DeHavilland Dash 8 Q300
kb_checklists=
atc_heavy=0
atc_id=N436YV
atc_airline=Beta
atc_flight_number=



[WEIGHT_AND_BALANCE]
max_gross_weight = 43000.000
empty_weight = 26000.000

reference_datum_position     = 0.00, 0.000, 0.000
empty_weight_CG_position     = 1.500, 0.000, 0.000

max_number_of_stations=4

station_load.0 =170.000000, 22.000000, -2.000000, 0.000000, Pilot
station_load.1 =170.000000, 22.000000, 2.000000, 0.000000, Co-Pilot
station_load.2 =750.000000, 0.000000, 0.000000, 0.000000, PAX
station_load.3 =450.000000, -14.000000, 0.000000, 0.000000, Bagage

;Moments of Inertia
empty_weight_pitch_MOI  = 98556.000
empty_weight_roll_MOI   = 110566.000
empty_weight_yaw_MOI    = 202117.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar=1.00
pitch_stability=1.5
roll_stability=1.0
yaw_stability=1.0
parasite_drag_scalar=0.6
induced_drag_scalar=1.85
elevator_effectiveness=1.0
aileron_effectiveness=1.00
rudder_effectiveness=1.0
elevator_trim_effectiveness=0.40
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=2.0

[GeneralEngineData]
engine_type = 5
Engine.0 = -6.665, -13.300, 4.000
Engine.1 = -6.665, 13.300, 4.000
fuel_flow_scalar        = 1.000
min_throttle_limit = -0.25

[propeller]
thrust_scalar=2.571
propeller_type=0
propeller_diameter=12.992
propeller_blades=4
propeller_moi=90.000
beta_max=45.000
beta_min=12.000
min_gov_rpm=7200.000
prop_tc=0.004
gear_reduction_ratio=24.000
fixed_pitch_beta=0.000
low_speed_theory_limit=80.000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=350.000
beta_feather=79.300
power_absorbed_cf=0.900
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=1.000
minimum_reverse_beta=-14.000

[TurbineEngineData]
fuel_flow_gain.0=35, 0.001              
fuel_flow_gain.1=40, 0.008
fuel_flow_gain.2=65,  0.01
fuel_flow_gain.3=69,  0.04  
//fuel_flow_gain          = 0.03
inlet_area=1.000 
rated_N2_rpm=33000.000 
static_thrust=1200.000 
afterburner_available=0 


[turboprop_engine]
power_scalar=1.2500 
maximum_torque=2900.000 
max_rpm_mechanical_efficiency_scalar=1.012
idle_rpm_mechanical_efficiency_scalar=0.914
max_rpm_friction_scalar=0.927
idle_rpm_friction_scalar=1.052



[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, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 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_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

        //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, 25.500, 0.000, -5.700, 3000.000, 0.000, 0.24, 75.000, 0.2039, 1.25, 0.80, 4.800, 4.800, 0.000, 0.000, 0.000
point.1= 1.000, -7.650, -13.500, -5.800, 1574.000, 1.000, 0.39, 0.000, 0.1656, 1.25, 0.80, 4.500, 5.200, 2.000, 0.000, 0.000
point.2= 1.000, -7.650, 13.500, -5.800, 1574.000, 2.000, 0.39, 0.000, 0.1656, 1.25, 0.80, 4.500, 5.200, 2.000, 0.000, 0.000
point.3= 2.000, -7.330, -44.920, 6.000, 787.000, 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, -7.330, 44.920, 6.000, 787.000, 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, -37.670, 0.000, 0.000, 787.000, 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, 31.510, 0.000, -1.900, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch = -1.000
static_cg_height = 7.100
gear_system_type=1      //Hydraulic
[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  0.0     //Flap angle that activates warning at idle
flap_limit_power   = 16.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 1.5  //Brake scalar

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

[Views]
eyepoint = 22.505, -1.78, 1.843

[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

[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 = 150, 250
aileron  = 150, 250
rudder   = 150, 250

[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

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

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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3,   -5.5, -44.43,  6.433, fx_navred ,
light.1 = 3,   -5.5,  44.43,  6.433, fx_navgre ,
light.2 = 3, -46.200,   0.00,  19.315, fx_navwhi ,
light.3 = 2,   -5.05, -44.21,  6.433, fx_strobe ,
light.4 = 2,   -5.05,  44.21,  6.433, fx_strobe ,
light.5 = 1, -45.603,   0.00,  19.334, fx_beacon ,
light.6 = 2,  -48.251,  0.00, 3.960, fx_strobe ,
light.7 = 3, -47.914,   0.00,  2.841, fx_navwhi ,
light.8 = 4,   24.212,   2.00,  1.910, fx_vclight,
light.9 = 4,   24.212,   -2.00,  1.810, fx_vclight,
light.10 = 4,   22,   0.00,  3.80, fx_vclight,

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

[fuel]
LeftMain  = -6.000, -17.000, 5.500, 417.500, 0.000
RightMain = -6.000, 17.000, 5.500, 417.500, 0.000
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1


[airplane_geometry]
wing_area               = 605.000
wing_span               = 90.000
wing_root_chord         = 7.000
wing_dihedral           = 2.800
wing_incidence          = 0.000
wing_twist              = 2.000
oswald_efficiency_factor= 0.700
wing_winglets_flag      = 0
wing_sweep              = 3.000
wing_pos_apex_lon       = 25.000
wing_pos_apex_vert      = 11.000
htail_area              = 130.000
htail_span              = 26.000
htail_pos_lon           = -22.600
htail_pos_vert          = 0.000
htail_incidence         = -0.500
htail_sweep             = 8.000
vtail_area              = 130.000
vtail_span              = 14.500
vtail_sweep             = 30.000
vtail_pos_lon           = -20.500
vtail_pos_vert          = 4.100
elevator_area           = 53.500
aileron_area            = 12.100
rudder_area             = 46.400
elevator_up_limit       = 17.000
elevator_down_limit     = 15.500
aileron_up_limit        = 18.000
aileron_down_limit      = 18.000
rudder_limit            = 14.000
elevator_trim_limit     = 15.000
spoiler_limit           = 60.000
spoilerons_available    = 1
aileron_to_spoileron_gain = 0.500
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
auto_spoiler_available=0
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

[Reference Speeds]
flaps_up_stall_speed    = 92.000
full_flaps_stall_speed  = 72.000
cruise_speed            = 295.000
max_mach                = 0.58
max_indicated_speed=305.000000

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
pitch_takeoff_ga=8.000000

[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=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

[stall_warning]
type=1
stick_shaker=1



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


[General]
performance=Max Cruise Speed\t     268 kts (496 km\/h)\nMaximum Range\t     (37 pax) 1,020 nm\nService Ceiling\t     25,000 ft (7,620 m)\nMax Gross Weight\t     36,300 lb (16,466 kg) \nSeating\t\t     35-37\nMaximum payload        9,059 lb (4,109 kg)\nPayload with full fuel   7,681 lb (3,484 kg)\nFuel capacity              835 gallon (3,160 L)\n\nAirfield Performance:  \nFAR takeoff field length (SL, ISA) at MTO 3,250 ft \nFAR landing field length (SL) at MLW \n2,575 ft \n\nNoise Level: dB \nTakeoff   80.5 \nSideline   85.6 \nApproach    94.8 \n\n
atc_type=
atc_model=DH8C
Category=airplane


[TailHook]    
tailhook_length=1                               ;(feet)
tailhook_position = 0.0, 0.0, 0.0            ;(feet) longitudinal, lateral, vertical positions from datum


[folding_wings]  
wing_fold_system_type = 4                       ;0=None
fold_rates = 0.05,0.05                          ;Percent per second
cable_force_adjust = 1.0

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 15.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 310.000
lift_scalar= 1.200
drag_scalar= 2.100
pitch_scalar= 0.200
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 35.000, 0.000
[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=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2

[GPWS]
max_warning_height         = -1000
sink_rate_fpm              = -1500
excessive_sink_rate_fpm    = -2000
climbout_sink_rate_fpm     = -100
flap_and_gear_sink_rate_fpm= -100
