[fltsim.0]
title=Dreamwings Dash8Q-400 G-UKBD
sim=Dash8Q400
model=
panel=
sound=
texture=ukd
checklists=
ui_manufacturer=UK Direct Airways
ui_type=Dash8-Q400
ui_variation=G-UKBD
description=Dreamwings Dash8 Q400
atc_id=G-UKBD
atc_heavy=0
atc_airline=UKD
atc_flight_number=
atc_parking_codes=UKD
atc_parking_types=RAMP
kb_checklists=dh84_check
kb_reference=dh84_ref

[General]
performance=Model Designer: Tommy Hansson\nFDE: John Cillis\n\nFlightcrew:\t2 Pilots and 2-3 Cabin Crew\nPax:\t70\nMax cruising speed:\t360kts\nMax certificated ceiling:\t25,000ft\nMax range with 70 passengers and reserves:\t1362nm\n\nWing span\t28.42m (93ft 3in)\nLength\t32.84m (107ft 9in)\nHeight\t8.38m (27ft 5in)\nWing area\t63.1m2 (679.0sq ft).
atc_type=BOMBARDIER
atc_model=DH8C
editable=1
Category=airplane

[WEIGHT_AND_BALANCE]
empty_weight = 37888.000
max_gross_weight = 64500.000
reference_datum_position = 0.000, 0.000, 0.000

max_number_of_stations=6
CG_forward_limit=0.000
CG_aft_limit=1.000

station_load.0 = "500, 30.0, 0.0, 0.0, Flight Crew"
station_load.1 = "500, -15.0, 0.0, 0.0, Galleys"
station_load.2 = "2000, 0.0, 0.0, 0.0, Baggage"
station_load.3 = "2500, 0.0, 0.0, 0.0, Cargo" 
station_load.4 = "2500, 10.0, 0.0, 0.0, Front Pax Cabin"
station_load.5 = "2500, -10.0, 0.0, 0.0, Rear Pax Cabin"

empty_weight_pitch_MOI=340000
empty_weight_roll_MOI=400000
empty_weight_yaw_MOI=460000
empty_weight_coupled_MOI = 0
empty_weight_CG_position=0.00000,0.000000,.000000

//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, 47.000, 0.000, -7.4, 1500.000, 0.000, 1.364, 55.000, 0.500, 1.500, 0.4, 5.000, 5.000, 0.000, 0.000, 170.000
point.1= 1.000, -2.000, -12.99, -7.6, 1574.803, 1.000, 2.014, 0.000, 0.900, 1.500, 0.500, 5.000, 5.000, 2.000, 0.000, 170.000
point.2= 1.000, -2.000, 12.99, -7.6, 1574.803, 2.000, 2.014, 0.000, 0.900, 1.500, 0.500, 5.000, 5.000, 3.000, 0.000, 170.000
point.3=2,  5.0, -47.8,  6.3, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5
point.4=2,  5.0, 47.8,  6.3, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6
point.5=2,  -33.6,   0.00,  1.22, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9
point.6=2,  40.0,   0.00, 1.22, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4 

max_number_of_points=21

static_pitch=-0.4 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.1 //feet, altitude of CG when at rest on the ground
gear_system_type=0

[GROUND_REACTION]
MAX_STEERING_ANGLE=80

[Views]
eyepoint=28.400, -2.5,  0.0 //3.0 (feet) longitudinal, lateral, vertical distance from reference datum

[GeneralEngineData]
engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=0, -13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=0, 13.3, 2.7 
fuel_flow_scalar=0.9
min_throttle_limit=-0.250000

[propeller]
thrust_scalar=1.0
propeller_type= 0
propeller_diameter= 13.0
propeller_blades= 6
propeller_moi= 77
beta_max= 47
beta_min= 12
min_gov_rpm= 00000
prop_tc= 0.004
gear_reduction_ratio= 17.0
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= 700
beta_feather= 79.3
power_absorbed_cf= 0.9
defeathering_accumulators_available= 0
prop_reverse_available= 1
minimum_on_ground_beta= 1.500
minimum_reverse_beta= -14.000

[TurbineEngineData]
fuel_flow_gain= 0.025
inlet_area= 2.0
rated_N2_rpm= 29920
static_thrust= 200

[turboprop_engine]
power_scalar=1.0
maximum_torque= 12000
max_rpm_mechanical_efficiency_scalar=1
idle_rpm_mechanical_efficiency_scalar=1

[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

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=0.9
induced_drag_scalar=0.9
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[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_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

[Flaps.0]
type=1
system_type=0
span-outboard=0.700000
extending-time=8.000000
damaging-speed= 250.000
blowout-speed= 300.000

flaps-position.0 = 0                                    // degrees, KIAS
flaps-position.1 = 5                                  // degrees, KIAS
flaps-position.2 = 10                                   // degrees, KIAS
flaps-position.3 = 15                                   // degrees, KIAS
flaps-position.4 = 35                                   // degrees, KIAS



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

[airplane_geometry]
wing_area= 697.0
wing_span= 93.3
wing_root_chord= 10.5
wing_dihedral= 2.5
wing_incidence= 0.9
wing_twist= -0.5
oswald_efficiency_factor= 0.7
wing_winglets_flag= 0
wing_sweep= 3.0
wing_pos_apex_lon= 0.0
wing_pos_apex_vert= 0.0
htail_area= 180.0
htail_span= 26.0
htail_pos_lon= -55.0
htail_pos_vert= 25.0
htail_incidence= 0.5
htail_sweep= 0.0
vtail_area= 152.0
vtail_span= 15.0
vtail_sweep= 0.0
vtail_pos_lon= -50.0
vtail_pos_vert= 18.8
elevator_area= 55.0
aileron_area= 14.0
rudder_area= 46.4
elevator_up_limit= 17.0
elevator_down_limit= 15.5
aileron_up_limit= 18.0
aileron_down_limit= 17.0
rudder_limit= 14.0
elevator_trim_limit= 20.0
spoiler_limit= 60.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0
min_ailerons_for_spoilerons= 0
min_flaps_for_spoilerons= 0
auto_spoiler_available=1
spoiler_extension_time=3.000000
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= 92.0
full_flaps_stall_speed= 72.0
cruise_speed=350.0
max_indicated_speed=265.000000
max_mach=0.60

[STALL_WARNING]
filename=c182_stallhorn
type=1
stick_shaker=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=150.0, 250.0
aileron=150.0, 250.0
rudder=150.0, 250.0

[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, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.0
autothrottle_available=1
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=8
autothrottle_max_rpm=18000
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=1.000000

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3, 5.0, -47.2, 6.2, fx_navred ,
light.1=3, 5.0, 47.2, 6.2, fx_navgre ,
light.2=2, 5.3, 47.8, 6.3, fx_strobe ,
light.3=2, 5.3, -47.8, 6.3, fx_strobe ,
light.4 = 3, -50.069, -0.016, 19.965, fx_strobeh ,
light.5 = 1, 17.875, -0.007, 4.644, fx_beacon ,
light.6 = 2, -59.003, 0, 18.829, fx_navwhih ,
light.7=4, -7.91, 0.00, 2.64, fx_vclight,

[direction_indicators]
direction_indicator.0=3,0

[brakes]
toe_brakes_scale=0.90
parking_brake=1
auto_brakes=4

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=5.722988
flap_limit_idle=17.011494

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

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1

[exits]
number_of_exits=3
exit_rate.0=0.25 ;Percent per second
exit_rate.1=0.35 ;Percent per second
exit_rate.2=0.30 ;Percent per second

//[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 = 0.15,0.15 ;Percent per second
//cable_force_adjust = 1.0

[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

[pitot_static]
vertical_speed_time_constant=70.0





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=1
