[fltsim.0]
title=Embraer 170 UTAIR		
sim=embraer170
model=
panel=
sound=
texture=UTAIR_UT-AEB
kb_checklists=
description=Embraer 170 \n\nEngine Type: General Electric CF34-3B1\ливрея: Дмитрий Числов 
ui_manufacturer=Embraer
ui_type=Embraer 170
ui_variation=UTAIR UT-AEB 
atc_heavy=0
atc_id=UT-AEB
atc_airline=UTAIR
atc_flight_number=170

[General]
performance=Maximum Cruise Speed: mach 0.80, Passangers: 70, Range: 2000 nm
atc_type=EMBRAER
atc_model=E170
editable=1

[pitot_static]
vertical_speed_time_constant=1

[WEIGHT_AND_BALANCE]
max_gross_weight=82012.000
empty_weight=46165.000

reference_datum_position     =  0.0000, 0.0000, 0.0000       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.000, 0.000, 0.000

max_number_of_stations=8

//Weight-Fore/AFT-Right/Left-Up/Down

//Cabin

station_load.0=1950.000000,20.000000,-3.000000,4.000000,Sec.A(Rws 1-6)L
station_load.1=2340.000000,20.000000,3.000000,4.000000,Sec.A(Rws 1-6)R
station_load.2=2340.000000,0.000000,-3.000000,4.000000,Sec.B(Rws 7-12)L
station_load.3=2340.000000,0.000000,3.000000,4.000000,Sec.B(Rws 7-12)R
station_load.4=2340.000000,-15.000000,-3.000000,4.000000,Sec.C(Rws 13-18)L
station_load.5=2340.000000,-15.000000,3.000000,4.000000,Sec.C(Rws 13-18)R

//Baggage Cmpt

station_load.6=1194.000000,20.000000,0.000000,-2.000000, Forward Bin 
station_load.7=1194.000000,-15.000000,0.000000,-2.000000, Rear Bin

;Moments of Inertia
empty_weight_pitch_MOI=2172439.000
empty_weight_roll_MOI=2262183.000 
empty_weight_yaw_MOI=2337024.000
empty_weight_coupled_MOI=1300.000
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=.50
aileron_effectiveness=1.75
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[GeneralEngineData]
engine_type=1
Engine.0=4.750, -16.100, -2.500
Engine.1=4.750, 16.100, -2.500
fuel_flow_scalar=1.000000
min_throttle_limit=-0.250000

[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=17.75
static_thrust=14200.000000
afterburner_available=0
reverser_available=1
rated_N2_rpm=29920.000000

[jet_engine]
thrust_scalar=1.000

[electrical]
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

[contact_points]

//0  Class
//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


point.0= 1.000, 36.500, 0.000, -10.200, 1574.000, 0.000, 1.500, 56.000, 0.355, 2.500, 0.595, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -4.000, -10.000, -10.300, 1574.000, 1.000, 1.500, 0.000, 0.355, 2.500, 0.595, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -4.000, 10.000, -10.300, 1574.000, 2.000, 1.500, 0.000, 0.355, 2.500, 0.595, 5.000, 5.000, 3.000, 0.000, 0.000

static_pitch=0.000
static_cg_height=9.796
gear_system_type=1

[gear_warning_system]
gear_warning_available=1    //Normal
pct_throttle_limit=0.1     //Percent throttle that activates warning
flap_limit_idle=5.0     //Flap angle that activates warning at idle
flap_limit_power=25.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake=1         //Parking brake available
toe_brakes_scale=0.885  //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


[Flaps.0]
type=1
span-outboard= 0.500
extending-time= 7.000
system_type=1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar           = 0.4
drag_scalar           = 0.7
pitch_scalar          = 1.2
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.0, 0.000
flaps-position.2= 10.0, 0.000
flaps-position.3= 20.0, 0.000
flaps-position.4= 25.0, 0.000
flaps-position.5= 30.0, 0.000
flaps-position.6= 35.0, 0.000


[Flaps.1]
type= 2
span-outboard  = 0.800
extending-time = 12.000
system_type    = 1
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 = 15.000, 0.000
flaps-position.2 = 15.000, 0.000
flaps-position.3 = 25.000, 0.000


[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=4,  42.5,    0.00,   1.7, fx_vclighth ,
light.1=2, -48.50,   0.00,  2.80, fx_strobeh  ,
light.2=2,  10.35,   0.00, -6.15, fx_beaconb  ,
light.3=1,   21.65,   0.00,  5.9, fx_beaconh
light. =  2, 2.10009966777409, -50.1666666666667, 0, fx_strobe
light. =  2, 2.10009966777409, 50.1666666666667, 0, fx_strobe

[Views]
eyepoint=40, -1.31, 2.7   //(feet) longitudinal, lateral, vertical distance from reference datum

[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, 250   
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=0,0


[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.1                               ;Percent per second

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
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=1.0
use_no_default_pitch=1
default_pitch_mode=0

[fuel]
LeftMain=-3.000, -19.000, 0.000, 900.000, 0.000
RightMain=-3.000, 19.000, 0.000, 900.000, 0.000
Center1=0.000, 0.000, 0.000, 1317.000, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=2                    
electric_pump=1


[airplane_geometry]
wing_area=750.000
wing_span=85.750
wing_root_chord=16.000
wing_dihedral=6.200
wing_incidence=1.000
wing_twist=-0.500
oswald_efficiency_factor=0.750
wing_winglets_flag=1
wing_sweep=25.000
wing_pos_apex_lon=8.000
wing_pos_apex_vert=0.000
htail_area=260.000
htail_span=32.700
htail_pos_lon=-35.000
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=30.000
vtail_area=150.000
vtail_span=17.000
vtail_sweep=35.000
vtail_pos_lon=-35.800
vtail_pos_vert=5.800
elevator_area=70.500
aileron_area=26.900
rudder_area=56.200
elevator_up_limit=22.500
elevator_down_limit=19.500
aileron_up_limit=20.000
aileron_down_limit=20.000
rudder_limit=26.000
elevator_trim_limit=20.000
spoiler_limit=60.000
spoilerons_available=0
aileron_to_spoileron_gain=.5
min_ailerons_for_spoilerons=10.000
min_flaps_for_spoilerons=35.000

[Reference Speeds]
flaps_up_stall_speed=190.000
full_flaps_stall_speed=113.000
cruise_speed=455.0
max_indicated_speed=340.000000
max_mach=0.820020

[forcefeedback]
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=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 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
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
