[fltsim.0]
title=Bombardier Dash 8 -Q400 Air France
sim=Dash8Q400
model=
panel=
sound=
texture=af
checklists=
ui_manufacturer=Bombardier 
ui_type=Dash 8 Q400
ui_variation=Air France
description=Dreamwings Dash8 Q400
atc_id=F-01AF
atc_heavy=0
atc_airline=BOMBARDIER
atc_flight_number=1123

[fltsim.1]
title=Bombardier Dash 8 -Q400 Alaska Airlines
sim=Dash8Q400
model=
panel=
sound=
texture=alaska
checklists=
ui_manufacturer=Bombardier 
ui_type=Dash 8 Q400
ui_variation=Alaska Airlines
description=Dreamwings Dash8 Q400
atc_id=N888AS
atc_heavy=0
atc_airline=BOMBARDIER
atc_flight_number=1123

[fltsim.2]
title=Bombardier Dash 8 -Q400 Air Canada
sim=Dash8Q400
model=
panel=
sound=
texture=ac_oc
checklists=
ui_manufacturer=Bombardier 
ui_type=Dash 8 Q400
ui_variation=Air Canada
description=Dreamwings Dash8 Q400
atc_id=C-GWWW
atc_heavy=0
atc_airline=BOMBARDIER
atc_flight_number=1123


[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

[WEIGHT_AND_BALANCE]
empty_weight = 37717 // (pounds)
max_gross_weight=64500 
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 =6
CG_forward_limit=0.25
CG_aft_limit=0.5

station_load.0 = "500, 60.0, 0.0, 0.0, Flight Crew"
station_load.1 = "500, -10.0, 0.0, 0.0, Galleys"
station_load.2 = "2000, -15.0, 0.0, 0.0, Baggage"
station_load.3 = "2500, 40.0, 0.0, 0.0, Cargo" 
station_load.4 = "2500, 60.0, 0.0, 0.0, Front Pax Cabin"
station_load.5 = "2500, 50.0, 0.0, 0.0, Rear Pax Cabin"

empty_weight_pitch_MOI=311701
empty_weight_roll_MOI=361201
empty_weight_yaw_MOI=361691
empty_weight_coupled_MOI = 1300
max_gross_weight=64500.000000

//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, 47.7, 0.00, -6.8, 1500.00, 0.000, 1.161, 60.000, 0.075, 2.500, 0.987, 5.000, 5.000, 0.000, 0.000, 0.000
point.1=1, -2.0, -12.99, -7.3, 1574.803, 1.000, 1.161, 0.000, 0.215, 2.500, 0.642, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1, -2.0, 12.99, -7.3, 1574.803, 2.000, 1.161, 0.000, 0.215, 2.500, 0.642, 5.000, 5.000, 3.000, 0.000, 0.000
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

[Views]
eyepoint=43.400, 0, 1.7 //(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 thrust scalar
propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter = 13.0 //Propeller Diameter, (feet)
propeller_blades = 6 //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 = 00000 //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)

[TurbineEngineData]
fuel_flow_gain=0.025 //Gain on fuel flow
inlet_area=2.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920 //RPM, second stage compressor rated value
static_thrust=200 //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar = 1.5 //Scalar on Turboprop power
maximum_torque = 7500 //Maximum torque available (ft-lbs)
max_rpm_mechanical_efficiency_scalar=0.960
idle_rpm_mechanical_efficiency_scalar=0.975

[fuel]
LeftMain= -10.000000,-14.500000,0.00000,862.00000,0.000000
RightMain= -10.000000,14.500000,0.00000,862.00000,0.000000
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 // 1 - tail, 2 - lead
span-outboard=0.8 // 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

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

[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= 2.0 //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=350.0 //Knots True (KTAS)
max_indicated_speed=265.000000
max_mach=0.60

[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, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.000000
autothrottle_available=1
pitch_takeoff_ga=8.000000
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.
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=0.75
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=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