[fltsim.0]
title=INTER Embraer 170
sim=emb170
model=
panel=
sound=
texture=
kb_checklists=emb170_check
kb_reference=emb170_ref
atc_id=C535MF
atc_airline=INTER
atc_flight_number=311
ui_manufacturer=Embraer
ui_type=170
ui_variation=INTER Regional
description=The 70-78 passenger Embraer 170 was designed to provide the best balance between passenger comfort and aircraft performance.  This one was made with FSDS by ABACUS.

[General]
atc_type=Embraer
atc_model=170
editable=1
performance=Cruise Speed:  470 kt\nFull Load Range:  2100 nm\nTime to FL 300:  17 min\nDesigner:  Chuck Dome\nDate:  March 2002

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]
max_gross_weight=138500                       // (pounds)
empty_weight=100792                           // (pounds)

reference_datum_position=0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=0.000000,0.000000,0.000000,0.000000

;Moments of Inertia
empty_weight_pitch_MOI=3172439
empty_weight_roll_MOI=200000
empty_weight_yaw_MOI=3337024
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=1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=4.75, -16.1, -2.5                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=4.75,  16.1, -2.5                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1                            //Scalar for fuel flow efficiency

[TurbineEngineData]
fuel_flow_gain=0.002                          //Gain on fuel flow
inlet_area=19.6                               //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                            //RPM, second stage compressor rated value
static_thrust=23500                           //Lbs, max rated static thrust at Sea Level
afterburner_available=0                       //Afterburner available?
reverser_available=1                          //Thrust reverser available?

[jet_engine]
thrust_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, 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,  40.00,   0.00, -8.30, 1181.1, 0, 1.442, 55.92, 0.8, 1.5, 0.9, 4.0, 4.0, 0, 0.0, 0.0
point.1=1,  -7.75,  -8.58, -8.68, 1574.8, 1, 1.442,  0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 0.0, 0.0
point.2=1,  -7.75,   8.58, -8.68, 1574.8, 2, 1.442,  0.00, 1.0, 2.5, 0.9, 7.1, 7.1, 3, 0.0, 0.0

point.3=2, -14.17, -47.33,  0.00,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -14.17,  47.33,  0.00,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -54.00,   0.00,  2.83,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2,  42.67,   0.00, -3.75,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0

max_number_of_points=21

static_pitch=0.62       //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.66   //feet, altitude of CG when at rest on the ground

[Views]
eyepoint=38.0, -1.9, 4.5   //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]       //Trailing Edge Flaps
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=20                                   // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=2                                    // degrees
flaps-position.2=5                                    // degrees
flaps-position.3=15                                   // degrees
flaps-position.4=20                                   // degrees
flaps-position.5=30                                   // degrees
flaps-position.6=40                                   // degrees
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
system_type=1                                         //Hydraulic

[flaps.1]       //Inboard Leading Edge Flaps
type=2                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=2                                    // seconds
flaps-position.0=0                                    // 
flaps-position.1=1.0                                  // 
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
system_type=1                                         //Hydraulic

[flaps.2]       //Outboard Leading Edge Slat
type=2                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=3                                    // seconds
flaps-position.0=0                                    // 
flaps-position.1=0.5                                  // 
flaps-position.4=1.0                                  // 
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
system_type=1                                         //Hydraulic

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3,  -8.00, -41.25,  2.00, fx_navredm ,
light.1=3,  -8.00,  41.25,  2.00, fx_navgrem ,
light.2=3, -49.25,   0.00,  5.00, fx_navwhih ,
light.3=2,  -7.00, -41.25,  2.00, fx_strobeh ,
light.4=2,  -7.00,  41.25,  2.00, fx_strobeh ,
light.5=2,  -2.65,   0.00, -4.50, fx_beaconb ,
light.6=1,   2.20,   0.00,  8.00, fx_beaconh ,

[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

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;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=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
use_no_default_bank=1

[fuel]
Center1=0, 0, 0, 2313, 0                      //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=-3, -19, 0, 1500, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-3,  19, 0, 1500, 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                    

[airplane_geometry]
wing_area=1137.0                //Square feet
wing_span=94.75                 //Feet
wing_root_chord=18.0                  //Feet
wing_dihedral=6.2                   //Degrees
wing_incidence=1.0                   //Degrees
wing_twist=-0.5                  //Degrees
oswald_efficiency_factor=0.75                  //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=25.0                  //Degrees, wing leading edge
wing_pos_apex_lon=8.0                   //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=338.0                 //Square feet
htail_span=41.7                  //Feet
htail_pos_lon=-35.0                 //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=0.0                   //Degrees
htail_sweep=30.0                  //Degrees, horizontal tail leading edge
vtail_area=224.0                 //Square feet
vtail_span=20.0                  //Feet, tip to body
vtail_sweep=35.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-35.8                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=5.8                   //Feet, vertical distance from reference point, positive going up
elevator_area=70.5                  //Square feet
aileron_area=26.9                  //Square feet
rudder_area=56.2                  //Square feet
elevator_up_limit=22.5                  //Degrees
elevator_down_limit=19.5                  //Degrees
aileron_up_limit=20.0                  //Degrees
aileron_down_limit=20.0                  //Degrees
rudder_limit=26.0                  //Degrees
elevator_trim_limit=20.0                  //Degrees
spoiler_limit=60.0                  //Degrees
spoilerons_available=1                     //Spoilerons Available?
aileron_to_spoileron_gain=3                   //Aileron to spoileron gain
min_ailerons_for_spoilerons=10                //Degrees
min_flaps_for_spoilerons=0                    //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed=142.0                 //Knots True (KTAS)
full_flaps_stall_speed=113.0                 //Knots True (KTAS)
cruise_speed=477.0                 //Knots True (KTAS)

[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
