//ISDT ATR42-300 Flight Dynamics V1.0 

[fltsim.0]
title=iSDT ATR 42-300 UT Air
sim=atr42300
model=
panel=
sound=
texture=UTair
ui_manufacturer=Alenia Aerospace
ui_type=ATR 42-300
ui_variation=UTair
description=ISDT ATR 42-300 V1.0
kb_checklists=
atc_heavy=0
atc_id=VP-BLN
atc_airline=AIR TYUMEN
atc_flight_number=
atc_parking_types=RAMP
atc_parking_codes=TMN

[General]
performance=ISDT ATR 42-300V2 model for FS2004. For more information and updates go to www.isdt-israel.com
atc_type=AEROSPATIALE 
atc_model=AT43 
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight =37740.0
empty_weight =22414.00000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 1.000, 0.000, 0.000

max_number_of_stations=6


;Moments of Inertia
empty_weight_pitch_MOI  =129880.00000
empty_weight_roll_MOI   =77866.00000
empty_weight_yaw_MOI    =161801.37000
empty_weight_coupled_MOI=0.00000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0= 190, 35.000, -2.000, 0.000, Pilot
station_load.1= 190, 35.000, 2.000, 0.000, Co-Pilot
station_load.2= 2616, -24.000, 0.000, 0.000, PAX1
station_load.3= 2616, 0.000, 0.000, 0.000, PAX2
station_load.4= 2616, 19.000, 0.000, 0.000, PAX3
station_load.5= 450, -40.000, 0.000, 0.000, Bagage

[flight_tuning]
cruise_lift_scalar=1.00000
pitch_stability=1.00000
roll_stability=1.00000
yaw_stability=1.00000
parasite_drag_scalar=1.00000
induced_drag_scalar=1.00000
elevator_effectiveness=1.00000
aileron_effectiveness=1.00000
rudder_effectiveness=1.00000
elevator_trim_effectiveness=1.20000
aileron_trim_effectiveness=1.00000
rudder_trim_effectiveness=1.00000
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=1.00000
torque_on_roll=1.00000
gyro_precession_on_roll=1.00000
gyro_precession_on_yaw=1.00000

[GeneralEngineData]
engine_type =5
Engine.0 =0.400, -13.150, 1.000
Engine.1 =0.400, 13.150, 1.000
fuel_flow_scalar        =1.00000
min_throttle_limit =-0.25000

[propeller]
thrust_scalar=1.00000
propeller_type=0
propeller_diameter=13.00000
propeller_blades=4
propeller_moi=249.51300
beta_max=46.00000
beta_min=16.50000
min_gov_rpm=15100.00000
prop_tc=0.00400
gear_reduction_ratio=17.00000
fixed_pitch_beta=0.00000
low_speed_theory_limit=90.00000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=500.00000
beta_feather=80.00000
power_absorbed_cf=0.90000
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=1.00000
minimum_reverse_beta=-18.00000

[TurbineEngineData]
fuel_flow_gain=0.01100
inlet_area=1.00000
rated_N2_rpm=20816.00000
static_thrust=225.00000
afterburner_available=0
reverser_available=0
afterburner_throttle_threshold=0.00600
ThrustSpecificFuelConsumption=0.00600
AfterBurnThrustSpecificFuelConsumption=0.00600

[turboprop_engine]
power_scalar=1.00000
maximum_torque=10979.92465
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]

static_pitch = -1.000
static_cg_height = 7.400
gear_system_type=1
max_number_of_points=7
tailwheel_lock=0
point.0= 1, 29.000, 0.000, -7.030, 1500, 0, 0.750, 65.000, 0.128, 1.250, 0.800, 7.000, 7.500, 0, 250.0, 250.0
point.1= 1, -1.130, -6.400, -8.280, 2000, 1, 1.380, 0.000, 0.700, 1.200, 0.850, 10.500, 10.500, 2, 250.0, 250.0
point.2= 1, -1.130, 6.400, -8.280, 2000, 2, 1.380, 0.000, 0.700, 1.200, 0.850, 10.300, 10.300, 3, 250.0, 250.0
point.3= 2, -3.330, -23.920, -3.000, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -3.330, 23.920, -3.000, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -22.670, 0.000, 0.000, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, 23.080, 0.000, -1.500, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4

[gear_warning_system]
gear_warning_available =0
pct_throttle_limit =0.10000
flap_limit_idle    =22.50000
flap_limit_power   =16.00000

[brakes]
parking_brake =1
toe_brakes_scale =1.00000
auto_brakes=0
hydraulic_system_scalar=0.00000
differential_braking_scale=0.00000

[hydraulic_system]
normal_pressure =3000.00000
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 = 90, 190
aileron  = 150, 250
rudder   = 150, 250

[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  = 2.000, -10.000, 2.200, 501.100, 0.000
RightMain = 2.000, 10.000, 2.200, 501.100, 0.000

fuel_type =2
number_of_tank_selectors =2                    
electric_pump=1
fuel_dump_rate=0.02000
anemometer_pump=0
engine_driven_pump=0
manual_pump=0

[airplane_geometry]
wing_area               =586.00000
wing_span               =80.60000
wing_root_chord         =7.27000
wing_dihedral           =1.50000
wing_incidence          =0.00000
wing_twist              =0.00000
oswald_efficiency_factor=0.70000
wing_winglets_flag      =0
wing_sweep              =0.00000
wing_pos_apex_lon       =2.97975
wing_pos_apex_vert      =0.00000
htail_area              =127.00000
htail_span              =24.30000
htail_pos_lon           =-41.80000
htail_pos_vert          =13.00000
htail_incidence         =0.00000
htail_sweep             =0.00000
vtail_area              =162.00000
vtail_span              =14.50000
vtail_sweep             =0.00000
vtail_pos_lon           =-34.00000
vtail_pos_vert          =1.10000
elevator_area           =55.45000
aileron_area            =58.00000
rudder_area             =56.50000
elevator_up_limit       =22.00000
elevator_down_limit     =22.00000
aileron_up_limit        =18.00000
aileron_down_limit      =18.00000
rudder_limit            =24.00000
elevator_trim_limit     =15.00000
spoiler_limit           =0.00000
spoilerons_available    =0
aileron_to_spoileron_gain =0.00000
min_ailerons_for_spoilerons =0.00000
min_flaps_for_spoilerons =0.00000
auto_spoiler_available=-1
positive_g_limit_flaps_up=3.50000
positive_g_limit_flaps_down=2.45000
negative_g_limit_flaps_up=-2.80000
negative_g_limit_flaps_down=-2.10000
spoiler_extension_time=2.00000
spoiler_handle_available=0
load_safety_factor=1.00000

[Reference Speeds]
flaps_up_stall_speed    =110
full_flaps_stall_speed  =89
cruise_speed            =260.00000
max_mach                =0.58000
max_indicated_speed=269.00000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=100
autothrottle_available=0
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25
max_bank_acceleration=1.6
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=9
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain =1
pitch_takeoff_ga=8
default_pitch_mode=0
default_bank_mode=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90
use_no_default_bank=1
use_no_default_pitch=1

[forcefeedback]
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[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

[Flaps.0]
type= 1
system_type=1
span-outboard= 1.000
extending-time= 11.0
damaging-speed=235.0
blowout-speed=255.0
flaps-position.0=0.00
flaps-position.1=10.00
flaps-position.2=20.00
flaps-position.3=30.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=1.00


[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
[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100
[AirWrench]
Aircraft_Length=68.51000
Vmax_sl=379.75707
Vmax_ca=397.01876
V_rc=218.64801
Climb_Rate=2900.30000
Climb_Weight=37806.70000
Max_gforce=3.50000
Emergency_hp=0.00000
VSI_Weight=31092.00000
static_margin=0.09000
nose_position_lon=23.98000
ActualIncidence=0.00000
ActualTwist=0.00000
ActualTailIncidence=0.00000
Aircraft_Type=4
FlowCorrection=1.00000
ReheatCutoff=1.20000
OptimumMach=0.90000
Power_Calibration=1.00000
IdleRPM=0.00000
piston_research=0.00000
JetAltitude=0.00000
turboprop_critical_altitude=15893.20000
target_roll_Vopt=746.62542
target_roll_rate=73.20000
pitch_damping=1.00000
yaw_damping=1.00000
weathervane=1.00000
elevator_scalar=1.00000
aileron_scalar=0.30000
rudder_scalar=1.00000
dihedral_scalar=1.00000
sideslip_scalar=1.00000
prop_yaw_damping_scalar=1.00000
Elevator_FF=100.00000
Aileron_FF=-100.00000
Roll_Response=10.00000
Adverse_Yaw=100.00000
Control_Response=100.00000
V_Max_Control=309.55955
V_Zero_Control=619.11910
V_Max_RdrControl=309.55955
V_Zero_RdrControl=619.11910
Spin_Stability=20.00000
Roll_Off=-1.50000
glide_ratio=21.11379
CritAoA=16.00000
ClAoA_k0=1.00000
ClAoA_k1=1.00000
ClAoA_k2=0.85000
ClAoA_k3=0.80000
Elevator_Propwash=0.80000
Rudder_Propwash=0.80000
afterburner_thrust=220.00000
prop_design_altitude=5000.00000
prop_material_type=1
protect_airfile=0
spoiler_type=0
spoiler_cd=0.00000
spoiler_cl=-0.10000
spoiler_cm=0.00000
flaps_type=1
flaps_cd_scalar=0.70000
flaps_cm_scalar=0.00000
vfe_enabled=0
gear_cd_scalar=1.00000
gear_cm_scalar=0.00000
critical_mach_number=0.80000
max_mach_cd0=60
direct_edit_drag=0
cylinder_head_temperature=501.00000
exhaust_gas_temperature=826.00000
fuel_pressure=16.50000
oil_pressure=135.00000
oil_temperature=141.00000
radiator_temperature=211.00000
lo_rpm_friction=1.00000
hi_rpm_friction=1.00000
exhaust_pressure_ratio=1.40000
interstage_turbine_temperature=1941.00000
knots_flag=1
cfs1_flag=0
cfs2_flag=0
AI_flag=0
edit_tp_torque=0
direct_edit_mach=0
direct_edit_2dtab=0
fixed_wing_pos=0
range_est_alt=0.00000
range_est_rpm=0.00000
range_est_mp=29.92000
range_est_fuel=1002.20000
contact_light_flags=0
AirWrenchVersion=1.01.63