//ISDT ATR42-300 Flight Dynamics V1.0
[fltsim.0]
title=iSDT ATR 42-300 Santa Barbara Airlines YV1422 "Virgen De Coromoto"
sim=atr42300
model=
panel=
sound=
texture=YV1422
ui_manufacturer=ATR
ui_type=42-300
ui_variation=SB Airlines YV1422 "Virgen De Coromoto"
description=ISDT ATR 42-300 V1.0 Santa Barbara Airlines YV1422 "Virgen De Coromoto" Repaint By Carlos Eduardo Salas.
kb_checklists=
atc_heavy=0
atc_id=YV1422
atc_airline=Barbara
atc_flight_number=
atc_parking_codes=BBR
[WEIGHT_AND_BALANCE]
max_gross_weight = 37740.000
empty_weight = 22414.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 1.000, 0.000, 0.000
max_number_of_stations=4
station_load.0 =190.000000, 35.000000, -2.000000, 0.000000, Pilot
station_load.1 =190.000000, 35.000000, 2.000000, 0.000000, Co-Pilot
station_load.2 =7850.000000, 0.000000, 0.000000, 0.000000, PAX
station_load.3 =450.000000, -40.000000, 0.000000, 0.000000, Bagage
;Moments of Inertia
empty_weight_pitch_MOI = 98556.000
empty_weight_roll_MOI = 110566.000
empty_weight_yaw_MOI = 202117.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.5
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=0.7
aileron_effectiveness=1.0
rudder_effectiveness=1.0
elevator_trim_effectiveness=0.5
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[GeneralEngineData]
engine_type = 5
Engine.0 = -6.165, -13.150, 4.891
Engine.1 = -6.165, 13.150, 4.891
fuel_flow_scalar = 0.900
min_throttle_limit = -0.25
[propeller]
thrust_scalar=1.1
propeller_type= 0
propeller_diameter= 13.0
propeller_blades= 4
propeller_moi= 78.000
beta_max= 46.000
beta_min= 10.200
min_gov_rpm= 15100.000
prop_tc= 0.004
gear_reduction_ratio= 17.000
fixed_pitch_beta= 0.000
low_speed_theory_limit= 90.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather= 500.000
beta_feather= 80
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 1
minimum_on_ground_beta= 1.000
minimum_reverse_beta= -18.000
[TurbineEngineData]
fuel_flow_gain= 0.006
inlet_area= 1.000
rated_N2_rpm= 20816
static_thrust= 200.000
afterburner_available= 0
[turboprop_engine]
power_scalar=1.4
maximum_torque= 10180
max_rpm_mechanical_efficiency_scalar=1.0
idle_rpm_mechanical_efficiency_scalar=1.0
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=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, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 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, 29.0, 0, -7.03, 1500, 0, 0.75, 62, 0.128, 1.25, 0.80, 7.0, 7.5, 0, 250, 250
point.1 = 1, -1.13, -6.4, -8.28, 2000, 1, 1.38, 0, 0.70, 1.2, 0.85, 10.5, 10.5, 2, 250, 250
point.2 = 1, -1.13, 6.4, -8.28, 2000, 2, 1.38, 0, 0.70, 1.2, 0.85, 10.3, 10.3, 3, 250, 250
point.3= 2.000, -3.330, -23.920, -3.000, 787.000, 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, -3.330, 23.920, -3.000, 787.000, 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, -22.670, 0.000, 0.000, 787.000, 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, 23.080, 0.000, -1.500, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = -1.000
static_cg_height = 7.400
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 0 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //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 = 27.505, -1.08, 1.843
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[keyboard_response]
elevator = 100, 220
aileron = 100, 220
rudder = 100, 220
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 2.05, -38.88, 5.45, fx_navred ,
light.1 = 3, 2.05, 38.88, 5.45, fx_navgre ,
light.3 = 2, 2.05, -38.88, 5.45, fx_strobe ,
light.4 = 2, 2.05, 38.88, 5.45, fx_strobe ,
light.5 = 1, -39.85, 0.00, 18.90, fx_beacon ,
light.6 = 2, 1.1, 0.00, -6.40, fx_strobe ,
light.7 = 3, -40.25, 0.00, 2.05, fx_navwhi ,
light.8 = 4, 22.212, 0, 0.610, fx_vclight,
light.9 = 4, -17.870, 0, 0.710, fx_vclight, //main exit
light.10 = 4, 27.71, 0.00, 0.610, fx_vclight, //flightdack
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = 3.000, -17.000, 4.200, 501.100, 0.000
RightMain = 3.000, 17.000, 4.200, 501.100, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 697.000
wing_span = 82.000
wing_root_chord = 8.830
wing_dihedral = 1.500
wing_incidence = 1.500
wing_twist = -1.500
oswald_efficiency_factor= 0.700
wing_winglets_flag = 0
wing_sweep = 3.000
wing_pos_apex_lon = 4.000
wing_pos_apex_vert = 0.000
htail_area = 128.000
htail_span = 24.500
htail_pos_lon = -22.600
htail_pos_vert = 0.000
htail_incidence = -0.500
htail_sweep = 8.000
vtail_area = 150.000
vtail_span = 14.500
vtail_sweep = 30.000
vtail_pos_lon = -20.500
vtail_pos_vert = 4.100
elevator_area = 41.500
aileron_area = 31.000
rudder_area = 68.400
elevator_up_limit = 20.000
elevator_down_limit = 18.000
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 15.000
elevator_trim_limit = 15.000
spoiler_limit = 0
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
auto_spoiler_available=-1
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
[Reference Speeds]
flaps_up_stall_speed = 90.000
full_flaps_stall_speed = 80.000
cruise_speed = 260.000
max_mach = 0.58
max_indicated_speed=269.000000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 100.0
autothrottle_available= 0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.6
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
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
[stall_warning]
type=1
stick_shaker=1
[exits]
number_of_exits=4
exit_rate.0=0.18
exit_rate.1=0.08
exit_rate.2=0.15
exit_rate.3=0.15
exit.1=0.05, -18.3, 7.8, -2.0, 1 //FSX Cars
[General]
performance=ISDT ATR 42-300 model for FS2004. For more information and updates go to www.isdt-israel.com
atc_type=
atc_model=ATR42
Category=airplane
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 12.000
system_type= 1
damaging-speed= 235.000
blowout-speed= 255.000
lift_scalar= 1.600
drag_scalar= 1.200
pitch_scalar= 0.200
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2