[fltsim.0]
title= Qantas Dash8-Q300
sim=fsp_dash8
model=
panel=
sound=
texture=QL
kb_checklists=
kb_reference=
atc_id=TQY
atc_airline=QANTAS
atc_flight_number=TQY
ui_manufacturer=De Havilland
ui_type=Dash8-Q300
ui_variation=QANTAS Link
description=QANTAS LINK flies daily routes out of Sydney (YSSY) and many regional centres in NSW, Lord Howe Island, Victoria and Queensland. Original model by FSpainters Japan. www.members.tripod.co.jp/FSpainter \nRepaint by Mike Hill
[fltsim.1]
title=Dash8-Q300 JSQ
sim=fsp_dash8
model=
panel=
sound=
texture=NJ
kb_checklists=
kb_reference=
atc_id=JSQ
atc_airline=NATIONAL JET
atc_flight_number=JSQ
ui_manufacturer=De Havilland
ui_type=Dash8-Q300
ui_variation=NATIONAL JET
description=This aircraft flies twice daily between Adelaide (YPAD) and Moomba (YOOM). Original model by FSpainters Japan. www.members.tripod.co.jp/FSpainter \nRepaint by Mike Hill.
[General]
atc_type=De Havilland
atc_model=Dash8-Q300
editable=0
performance=50\/56 Pax Regional Airliner\nLength:84 ft\nWing Span 90 ft\nHeight:26'\nWt:25,888 lb Empty\nMax T\/O Weight: 43,000 lb\nPower:2x2500 SHP P&W 123B Turboprops\nMax Cruise: 284 Kts\nStall Speed 102 \/ 78\nCeiling: 25,000 ft\nRange: Range: 878 Naut Miles\nOriginal model by FSpainters Japan. www.members.tripod.co.jp/FSpainter\nLivery by Mike Hill \nAugust 2002\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 34500 // (pounds)
empty_weight = 22730 // (pounds)
reference_datum_position = 31.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -26.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -9.8, -1.75, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -9.8, 1.75, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 5660, -27.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 111701
empty_weight_roll_MOI = 61201
empty_weight_yaw_MOI = 161691
empty_weight_coupled_MOI = 0
[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 = 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
[GeneralEngineData]
engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -28.4, -13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -28.4, 13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
[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)
[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 = 200 //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar = 1.0 //Scalar on Turboprop power
maximum_torque = 7878 //Maximum torque available (ft-lbs)
[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
//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, -5.0, 0.00, -7.15, 1500, 0, 1.617, 25.0, 0.500, 2.5, 0.9, 5.0, 6.0, 0
point.1 = 1, -29.0, -12.99, -7.35, 3000, 1, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 2
point.2 = 1, -29.0, 12.99, -7.35, 3000, 2, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 3
point.3 = 2, -31.6, -42.50, 5.39, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -31.6, 42.50, 5.39, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6
point.5 = 2, -68.6, 0.00, 1.22, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9
point.6 = 2, 0.0, 0.00, -3.92, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4
max_number_of_points = 21
static_pitch = -0.5 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height = 6.84 //feet, altitude of CG when at rest on the ground
[Views]
eyepoint= -8.8, -1.45, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum
[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
[fuel]
LeftMain = -31.1, -9.1, 3.9, 417.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -31.1, 9.1, 3.9, 417.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[airplane_geometry]
wing_area = 585.0 //Square feet
wing_span = 85.0 //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= 0.7 //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 = 265.0 //Knots True (KTAS)
[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
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available= 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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.1 = 3, -24.8, -43.9, 5.3, fx_navred ,
light.2 = 3, -24.8, 43.9, 5.3, fx_navgre ,
light.3 = 3, -24.8, -43.9, 5.3, fx_navred ,
light.4 = 3, -24.8, 43.9, 5.3, fx_navgre ,
light.5 = 2, -25.5, 44.5, 5.28, fx_strobe ,
light.6 = 2, -25.5, -44.5, 5.28, fx_strobe ,
light.7 = 1, -64.2, 0.00, 18.1, fx_beacon ,
[direction_indicators]
direction_indicator.0=3,0
