[fltsim.0]
title=De Havilland Dash 8-100 #2
sim=DH_Dash8_100
model=
panel=
sound=
texture=
kb_checklists=DH_Dash8_100_check
kb_reference=DH_Dash8_100_ref
atc_id=SX-BIR
atc_airline=OLYMPIC
atc_flight_number=293
ui_manufacturer=De Havilland
ui_type=Dash 8-100
ui_variation=Olympic Aviation
description=This is a default Dash8-100 by Microsoft repainted to the Olypmpic Aviation Colour and modified as flyable model by Maximos Sevastopoulos (c) 2003 pastor@otenet.gr
atc_heavy=0
[General]
atc_type=DEHAVILLAND
atc_model=DH8A
performance=Length: 22.25m (73 ft 0 in)\nSpan: 25.91m (85 ft 0 in)\nWeight: 15,649kg (34,500lb) @ MTOW\nPower: 2 x 1,490kw (2,000 shp) P&W\nRange: 2,130km (1,150nm) Max payload
[WEIGHT_AND_BALANCE]
max_gross_weight = 34500.000
empty_weight = 22730.000
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 = 170.000, -9.800, -1.750, 0.000
station_load.1 = 170.000, -9.800, 1.750, 0.000
station_load.2 = 5660.000, -27.000, 0.000, 0.000
;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 = 1.0
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
Engine.0 = -28.400, -13.300, 2.700
Engine.1 = -28.400, 13.300, 2.700
fuel_flow_scalar = 1.000
min_throttle_limit=-0.250000
[propeller]
thrust_scalar = 1.0 //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 = 1.0 //Scalar on Turboprop power
maximum_torque = 7878.000
[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 = 1.000, -5.000, 0.000, -7.450, 1500.000, 0.000, 1.617, 25.000, 0.500, 2.500, 0.900, 5.000, 6.000, 0.000, 100.000, 712.383
point.1 = 1.000, -29.000, -12.990, -7.550, 3000.000, 1.000, 0.633, 0.000, 0.675, 2.500, 0.800, 6.000, 7.000, 2.000, 100.000, 712.383
point.2 = 1.000, -29.000, 12.990, -7.550, 3000.000, 2.000, 0.633, 0.000, 0.675, 2.500, 0.800, 6.000, 7.000, 3.000, 100.000, 712.383
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 = -0.400
static_cg_height = 7.100
gear_system_type=0
[Views]
eyepoint= -8.8, -1.45, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum
[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, 417.500, 0.000
RightMain = -31.100, 9.100, 3.900, 417.500, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 585.000
wing_span = 85.000
wing_root_chord = 7.000
wing_dihedral = 2.500
wing_incidence = 1.000
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_indicated_speed=265.000000
max_mach=0.579980
[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= 8.000
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
[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.0 = 3, -30.1, -42, 5, fx_navred ,
light.1 = 3, -30.1, 42, 5, fx_navgre ,
light.2 = 2, -29.9, 41.7, 5, fx_strobe ,
light.3 = 2, -29.9, -41.7, 5, fx_strobe ,
light.4 = 1, -65.0, 0.00, 18.4, fx_beacon ,
light.5 = 4, -7.91, 0.00, 2.64, fx_vclight,
[direction_indicators]
direction_indicator.0=3,0
[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= 10.000, 0.000
flaps-position.2= 30.000, 0.000
flaps-position.3= 40.000, 0.000
[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
