//Copyright 2003
//Barry Blaisdell
//Premair Aircraft Design
[fltsim.0]
title=PAD_De Havilland Dash8-100
sim=PAD_DHC8
model=
panel=
sound=
texture=
kb_checklists=DASH8_check
kb_reference=DASH8_ref
atc_id=LV-YTA
atc_airline=Southern Winds
atc_flight_number=809
ui_manufacturer=De Havilland
ui_type=Dash8
ui_variation=Southern Winds
description=FS2004\/2002Pro DeHavilland DHC8-Q200 SOUTHERN WINDS.\n Paint by Sacchi Facundo.\nBuenos Aires, Argentina. 2004\n\n \n
atc_heavy=0
atc_airline=
atc_flight_number=
editable=1
[General]
performance=37 Pax Regional Airliner\nLength: 73 ft\nWing Span: 85 ft\nHt: 24 ft-7 in\nWeight:22,100 lb Empty\nMax T\/O Weight:34,500 lb\nPower: 2 x 2150SHP P&W 123C Turboprops\nMax Cruise: 288 Kts TAS\nStall Speed 72 Kts\nCeiling: 25,000 ft\nRange: 935 Naut Miles\nConcept\/FD\/Cfg Files\/Panel: Barry Blaisdell\nRemapping: Udo Lemmob\nMaster Textures & Livery:Bob May
atc_type=DEHAVILLAND
atc_model=DH8A
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=Landing
light.0 = 3, -30.5, -42.3, 4.7, fx_navred ,
light.1 = 3, -30.5, 42.3, 4.7, fx_navgre ,
light.2 = 2, -31.0, 42.6, 4.7, fx_strobeh ,
light.3 = 2, -31.0, -42.6, 4.7, fx_strobeh ,
light.4 = 1, -65.0, 0.00, 18.3, fx_beacon ,
light.5 = 3, -68.90, 0.00, 2.30, fx_navwhi ,
light.6 = 4, -7.91, 0.00, 2.64,fx_vclighth.fx ,
light.7 = 5, -28.10, -15.00, 4.30, fx_landing ,
light.8 = 5, -28.10, -16.00, 4.30, fx_landing ,
light.9 = 5, -28.10, 16.00, 4.30, fx_landing ,
light.10 = 5, -28.10, 15.00, 4.30, fx_landing ,
light.11 = 1, -28.0, 0.00, -4.00, fx_beacon ,
light.12 = 2, -68.90, 0.00, 2.30, fx_strobeh ,
damage=0
prop_anim_ratio=1.70
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
use_no_default_bank=1
use_no_default_pitch=1
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
[WEIGHT_AND_BALANCE]
max_gross_weight = 34500.000
empty_weight = 22700.000
reference_datum_position= 31.000, 0.000, 0.000
empty_weight_CG_position= -26.000, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = 0.000, 0.000, 0.000, 0.000
station_load.1 = "170, -9.8, 1.75, 0.0, Front Passenger" //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "5000, -27.0, 0.0, 0.0, Payload" //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 111701.000
empty_weight_roll_MOI = 61201.000
empty_weight_yaw_MOI = 161691.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.5
aileron_effectiveness=1.5
rudder_effectiveness=1.5
pitch_stability=1.3
roll_stability=1.3
yaw_stability=1.3
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type = 5
Engine.0 = -28.400, -13.300, 2.700
Engine.1 = -28.400, 13.300, 2.700
fuel_flow_scalar = 1.000
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
[propeller]
thrust_scalar = 1.2 //Propeller thrust scalar
propeller_type = 0
propeller_diameter = 13.000
propeller_blades = 4
propeller_moi = 77.000
beta_max = 45.000
beta_min = 12.000
min_gov_rpm = 25520.000
prop_tc = 0.004
gear_reduction_ratio = 17.000
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 = 700.000
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 = 0.011
inlet_area = 1.000
rated_N2_rpm = 29920.000
static_thrust = 200.000
afterburner_available= 0
[turboprop_engine]
power_scalar = 1.2 //Scalar on Turboprop power
maximum_torque = 7878.000
[electrical]
//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
//BusType, MaxAmpLoad, MinVoltage
autopilot = 0, 5 , 1.0
avionics_bus = 0, 10, 10.0
avionics = 1, 5 , 10.0
gear_warning = 0, 2 , 1.0
fuel_pump = 0, 5 , 1.0
light_nav = 0, 5 , 1.0
light_beacon = 0, 5 , 1.0
light_landing = 0, 5 , 7.0
light_taxi = 0, 5 , 7.0
light_strobe = 0, 5 , 7.0
light_panel = 0, 5 , 1.0
pitot_heat = 0, 15, 1.0
additional_system = 0, 20, 1.0
marker_beacon = 1, 2, 1.0
starter1 = 0, 20, 1.0
starter2 = 0, 20, 1.0
starter3 = 0, 20, 1.0
starter4 = 0, 20, 1.0
auto_brakes = 0, 15, 1.0
hydraulic_pump = 0, 2, 1.0
fuel_transfer_pump = 0, 5, 1.0
max_battery_voltage=36.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=160.0
electric_always_available=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, -5.000, 0.000, -7.100, 1500.000, 0.000, 1.617, 25.000, 0.500, 2.500, 0.900, 5.000, 6.000, 0.000, 0.000, 0.000
point.1 = 1.000, -29.000, -12.990, -7.300, 3000.000, 1.000, 0.633, 0.000, 0.675, 2.500, 0.800, 6.000, 7.000, 0.000, 0.000, 0.000
point.2 = 1.000, -29.000, 12.990, -7.300, 3000.000, 2.000, 0.633, 0.000, 0.675, 2.500, 0.800, 6.000, 7.000, 0.000, 0.000, 0.000
point.3 = 2.000, -31.600, -42.500, 5.390, 1200.000, 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, -31.600, 42.500, 5.390, 1200.000, 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, -68.600, 0.000, 1.220, 1200.000, 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, 0.000, 0.000, -3.920, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
max_number_of_points = 21
static_pitch = -0.300
static_cg_height = 7.200
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 = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.06 //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= -8.8, -1.45, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
LeftMain = -31.100, -9.100, 3.900, 420.000, 0.000
RightMain = -31.100, 9.100, 3.900, 420.000, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 585.000
wing_span = 85.000
wing_root_chord = 7.000
wing_dihedral = 2.500
wing_incidence = 0.500
wing_twist = -3.000
oswald_efficiency_factor= 0.700
wing_winglets_flag = 0
wing_sweep = 3.000
wing_pos_apex_lon = -25.000
wing_pos_apex_vert = 0.000
htail_area = 97.000
htail_span = 26.000
htail_pos_lon = -58.900
htail_pos_vert = 0.000
htail_incidence = 1.000
htail_sweep = 8.000
vtail_area = 106.000
vtail_span = 11.700
vtail_sweep = 30.000
vtail_pos_lon = -54.900
vtail_pos_vert = 3.400
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 = 30.000
elevator_trim_limit = 15.000
spoiler_limit = 60.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 92.000
full_flaps_stall_speed = 72.000
cruise_speed = 265.000
max_mach = 0.58
max_indicated_speed = 240 //Red line (KIAS)
[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
[stall_warning]
type=1
[direction_indicators]
direction_indicator.0=3,0
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
[direction_indicators]
direction_indicator.0=3,0
[brakes]
toe_brakes_scale=1.062532
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
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 30.000, 0.000
