[fltsim.0]
title=DW DHC7 Arkia NC
sim=DeHaviland Dash-7 AI
model=
panel=
sound=
texture=Arkia\New
kb_checklists=
prop_anim_ratio=-1.76
atc_heavy=0
atc_id=
atc_airline=ARKIA
atc_flight_number=
atc_parking_types=RAMP
atc_parking_codes=
ui_manufacturer=Dee Waldron
ui_type=DeHavilland Dash-7
ui_variation=Arkia NC
description=DeHavilland DHC7 Dash 7 Regional commuter airliner.\nFSDS2 design: Dee Waldron\n
[General]
atc_type=DeHavilland
atc_model=DHC7
editable=1
performance=AI model
[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, -24.6, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-28.4, -12.6, 2.7
Engine.2=-28.4, 12.6, 2.7
Engine.3=-28.4, 24.6, 2.7
fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=10.0 //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=TRUEprop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=1.000000
minimum_reverse_beta=-14.000000
prop_reverse_available=1
[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=158 //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar=1.0 //Scalar on Turboprop power
maximum_torque=3939 //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, -7.70, 1500, 0, 1.617, 25.0, 0.500, 2.5, 0.9, 5.0, 6.0, 0, 100, 250
point.1=1, -29.0, -12.99, -8.35, 3000, 1, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 2, 100, 250
point.2=1, -29.0, 12.99, -8.35, 3000, 2, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 3, 100, 250
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=-0.4 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.4 //feet, altitude of CG when at rest on the ground
gear_system_type=0
[Views]
eyepoint= -7.7, -1.45, 1.6 //(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
electric_pump=0
[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)
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=8.000000
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, -31.95, -48.9, 5.7, fx_navredm ,
light.1=3, -31.95, 48.9, 5.7, fx_navgrem ,
light.2=2, -32.0, 48.9, 5.7, fx_strobeh ,
light.3=2, -32.0, -48.9, 5.7, fx_strobeh ,
light.4=1, -73.1, 0.00, 18.9, fx_beacon ,
light.5=1, -32.0, 0.00, -5.5, fx_beaconb ,
light.6=4, -7.7, 0.00, 1.7, fx_vclight,
[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=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
