[General]
performance=Maximum Cruise Speed: mach 0.80, Passengers: 72, Range: 2100 nm
atc_type=EMBRAER           //Embraer SA Brazilia
atc_model=E-170
editable=1
Category=airplane

[CameraDefinition.0]
Title = "Right Side Window"
Guid = {26BD9014-0ECA-4367-AC91-BF988CF045AB}
Description = View of the right wing from the passenger cabin
Origin = Virtual Cockpit
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
ShowWeather = Yes
//InitialXyz = side 3.2, alt 1.8,long -5
InitialXyz = 1.3, -0.2, -12.52
InitialPbh = 5, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum


[CameraDefinition.1]
Title = "Cabin view"
Guid = {7FDB2276-0619-482f-B52C-A41EF1A7D27C}
Description = View of the passenger cabin
Origin = Virtual Cockpit
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.2
ShowWeather = Yes
InitialXyz = 0.80, -0.2, -7.82
InitialPbh = 5, 0, -10
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum


[CameraDefinition.001]
Title = "Right Seat"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .8
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.0.1.0, 3.2
InitialPbh=10, 0, 0

[CameraDefinition.002]
Title = "overhead view"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.4, -0.4, 0.43
//InitialXyz=0.53, -0.4, 0.43
InitialPbh=-80, 0, 0

[CameraDefinition.003]
Title = "Navigation and Communication"
Guid = {4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.43, -0.2, 0.48
InitialPbh=40, 0, 0

[CameraDefinition.5]
Title = "Landing Gear"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .52
ShowWeather = Yes
InitialXyz = -2.5, -1.8, -5
InitialPbh = 0, 0, 13
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[pitot_static]

vertical_speed_time_constant=99
pitot_heat=1.000000

[WEIGHT_AND_BALANCE]

empty_weight=45636.000                        //Basic Operating Weight presented
max_gross_weight=82365                        //Maximal Ramp Weight presented

reference_datum_position =- 40.334, 0.0, -6.1 //Reference pointed over the MAC apex(MAC approximated to 3.1m)   
empty_weight_CG_position =-1.83, 0.0, -6.1    //Pointed over 18% MAC in accordance with See Gee calculator 

empty_weight_pitch_MOI=300000.000
empty_weight_roll_MOI=260000.000 
empty_weight_yaw_MOI=340000.000
empty_weight_coupled_MOI=0.000

CG_forward_limit=-0.72                        //Pointed over 7%MAC  (never exceeded)
CG_aft_limit=-2.74                            //Pointed over 27%MAC (never exceeded)


max_number_of_stations=40                   


station_load.0=4650, 17.934, 0, 0             //Section A load corrected 
station_load.1=3020, 4.538, 0, 0              //FWD baggage section load corrected
station_load.2=6662, -5.084, 0, 0             //Section B load corrected
station_load.3=4650, -39.865, 0, 0            //Section C corrected   
station_load.4=2270, -32.97, 0, 0             //AFT baggage section corrected


station_name.0="Sec.A-max.4650"               //Section A defined to first 24 pax seats
station_name.1="FWDBB-max.3020"               //Under the seats of section A
station_name.2="Sec.B-max.6662"               //Section B defined to middle 24 pax seats
station_name.3="Sec.C-max.4650"               //section C defined to the last 24 pax seats
station_name.4="AftBB-max.2270"               //Under the seats of section C



[flight_tuning]
cruise_lift_scalar=1.000                      //cruise lift scalar

parasite_drag_scalar=1.000                    //parazite drag scalar
induced_drag_scalar=1.000                     //induced drag scalar

elevator_effectiveness=1.000                  //elevetor effect
aileron_effectiveness=1.000                   //aileron effect
rudder_effectiveness=1.000                    //ruder effect

pitch_stability=1.00                          //pitch effect  
roll_stability=1.000                          //roll effect
yaw_stability=1.000                           //yaw stability

elevator_trim_effectiveness=1.00              //elevator trim
aileron_trim_effectiveness=1.000              //aileron trim
rudder_trim_effectiveness=1.000               //rudder trim

hi_alpha_on_roll=2                            //roll on high AoA
hi_alpha_on_yaw=2                             //yaw on high AoA




[GeneralEngineData]                           

engine_type=1                                 //Turbofan bypass 5.5


Engine.0=5.74, -12.8, -3.583                  //Left engine N1     
Engine.1=5.74, 12.8, -3.583                   //Right engine N2

fuel_flow_scalar=2.000000                     //Engines fuel consumption factor   
min_throttle_limit=-0.35
max_contrail_temperature=-35                  //engine high altitude tracks temperature


[TurbineEngineData]

fuel_flow_gain=0.002

inlet_area=19                                 //Engine subsonic inlet assy area

static_thrust=13300  //Maximum Take-off thrust;engine GE CF-34-8E2 rated at 86degF(30deg C) and below;FAA TCDS E00063EN
afterburner_available=0
reverser_available=1
rated_N2_rpm=17820   //maximal(100%) RPM for the gasgenerator and 100%FAN=7400;FAA TCDS E00063EN

[jet_engine]
thrust_scalar=1.000

[electrical]
max_battery_voltage = 25.5                     // Voltage of the batteries after cycle
generator_alternator_voltage = 29.5            // generator max voltage 
max_generator_alternator_amps = 400
electric_always_available = 1

                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 0 , 17.0
gear_motor         = 0, 0 , 17.0
autopilot          = 0, 0 , 17.0
avionics_bus       = 0, 0 , 17.0
avionics           = 0, 0 , 17.0
pitot_heat         = 0, 0 , 17.0
additional_system  = 0, 0 , 17.0
marker_beacon      = 0, 0 , 17.0
gear_warning       = 0, 0 , 17.0
fuel_pump          = 0, 0 , 17.0
starter1           = 0, 0 , 17.0
starter2           = 0, 0 , 17.0
light_nav          = 0, 0 , 17.0
light_beacon       = 0, 0 , 17.0
light_landing      = 0, 0 , 17.0
light_taxi         = 0, 0 , 17.0
light_strobe       = 0, 0 , 17.0
light_panel        = 0, 0 , 17.0
light_cabin        = 0, 0 , 17.0
auto_brakes        = 0, 0 , 17.0
standby_vacuum     = 0, 0 , 17.0
hydraulic_pump     = 0, 0 , 17.0
fuel_transfer_pump = 0, 0 , 17.0
light_recognition  = 0, 0 , 17.0
light_wing         = 0, 0 , 17.0
light_logo         = 0, 0 , 17.0
directional_gyro   = 0, 0 , 17.0
directional_gyro_slaving = 0, 0 , 17.0

[contact_points]

point.0= 1, 28.536, 0, -11.46, 16404, 0, 0.9, 152, 0.2, 1.7, 0.8, 16, 17.5, 0, 260, 290
point.1= 1, -6.2976, -8.528, -11.25, 16404, 1, 1.25, 0, 0.2, 1.5, 0.75, 16, 17.5, 2, 260, 290
point.2= 1, -6.2976, 8.528, -11.25, 16404, 2, 1.25, 0, 0.2, 1.5, 0.75, 16, 17.5, 3, 260, 290
point.3=0, -11.47, -34.44, -5, 0, 0, 0, 0, 0, 0, 0.3, 0, 0, 0, 0, 0
point.4=0, -11.47, -34.44, -5, 0, 0, 0, 0, 0, 0, 0, 0.3, 0, 0, 0, 0, 0 

max_number_of_points=5
emergency_extension_type=2

static_pitch=-0.4
static_cg_height=11.6
gear_system_type=1




[gear_warning_system]
gear_warning_available=0                             //None
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=20.0                                //Flap angle that activates warning at above idle

[brakes]
parking_brake=1                                      //Parking brake available
toe_brakes_scale=0.5                                 //Brake scalar
auto_brakes=4

[hydraulic_system]
normal_pressure=3000.0                               //PSI
electric_pumps=2                                     //no electric pumps
engine_map=1,1,0,0                                   //pumps on Eng1,2

[flaps.0]
type=1                                               // 1 - tail, 2 - lead
span-outboard=1.0                                    // 0.0 .. 1.0
extending-time=25                                    // seconds
flaps-position.0=0                                   // degrees
flaps-position.1=5         	                     // degrees
flaps-position.2=10                                  // degrees
flaps-position.3=20                                  // degrees
flaps-position.4=20                                  // degrees
flaps-position.5=20                                  // degrees
flaps-position.6=35                                  // degrees
damaging-speed=250                                   // KIAS
blowout-speed=300                                    // KIAS
system_type=0

[flaps.1]
type=2                                                // 1 - tail, 2 - lead
span-outboard=1.0                                     // 0.0 .. 1.0
extending-time=15                                     // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=15         	                      // degrees
flaps-position.2=15                                   // degrees
flaps-position.3=15                                   // degrees
flaps-position.4=25                                   // degrees
flaps-position.5=25                                   // degrees
flaps-position.6=25                                   // degrees
damaging-speed=275                                    // KIAS
blowout-speed=310
system_type=0


[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, 1
Adf.1=1
Adf.2=1
Transponder.1=1
Marker.1=1

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=2, -57.50,   0.00,  2.80, fx_strobeh  ,
light.1=2,  0.35,   0.00, -6.95, fx_beaconb  ,
light.2=1,   0.65,   0.00,  5.5, fx_beaconh ,
light.3=2, -14.00,   40.00,  0.00, fx_strobeh  ,
light.4=2, -14.00,   -40.00,  0.00, fx_strobeh  ,
light.5=3, -14.20,   -40.00,  0.00, fx_navredm ,
light.6=3, -14.20,   40.00,  0.00, fx_navgrem ,
light.7=2, -18.80,   40.00,  0.00, fx_strobeh  ,
light.8=2, -18.80,   -40.00,  0.00, fx_strobeh  ,

[Views]
eyepoint=27, -1.31, 2.4                                 //(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

[exits]
number_of_exits = 3
exit.0 = 0.4,  23.00, -4.0, 1.0, 0    //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1 = 0.4,  -23.00, 5.85, -3.5, 1  //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.2 = 0.4,  29.90, 6.0,  1.0, 2    //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
contrail=fx_contrail_l
startup=fx_engstrt
//vaportrail_l=fx_vaportrail_l
//vaportrail_r=fx_vaportrail_r
l_wingtipvortice=fx_wingtipvortice_l
r_wingtipvortice=fx_wingtipvortice_r
EngineFire=fx_engfire
EngineDamage=fx_engsmoke
EngineOilLeak=fx_OilLeak
WheelSnowSpray=fx_WheelSnowSpray
WheelWetSpray=fx_WheelWetSpray
windshield_rain_effect_available=1


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8
max_pitch=8
max_pitch_acceleration=2.0
max_pitch_velocity_lo_alt=1.5
max_pitch_velocity_hi_alt=1.0
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=2.0
max_bank_velocity=2.0
max_throttle_rate=0.5 // 0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0


[fuel]

LeftMain = -2.44, -26.24, 1.24, 1551.12, 0   //Left fuel keson 6.7lb/ US gallon
RightMain= -2.44,  26.24, 1.24, 1551.12, 0    //Right fuel keson 6.7 lb/Us gallon

fuel_type=2                                    //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=2
electric_pump=1


[airplane_geometry]   //everywhere the presented parameters are isolated 
wing_area=645
wing_span=74.15
wing_root_chord=16.072
wing_dihedral=6
wing_incidence=0
wing_twist=3
oswald_efficiency_factor=1.0575
wing_winglets_flag=1
wing_sweep=25.4
wing_pos_apex_lon=5.576
wing_pos_apex_vert=-1.4956
htail_area=203.976
htail_span=28.166667
htail_pos_lon=-39.668
htail_pos_vert=4.237
htail_incidence=0
htail_sweep=35.6
vtail_area=174.4
vtail_span=16.4
vtail_sweep=40
vtail_pos_lon=-30.504
vtail_pos_vert=8.7248
elevator_area=72.65
aileron_area=15.06
rudder_area=64.58
elevator_up_limit=25
elevator_down_limit=20
aileron_up_limit=20
aileron_down_limit=15
rudder_limit=26
elevator_trim_limit=15
spoiler_limit=60
spoilerons_available=1
aileron_to_spoileron_gain=1
min_ailerons_for_spoilerons=3.000
min_flaps_for_spoilerons=5.000
auto_spoiler_available=1
spoiler_extension_time=0.500000
positive_g_limit_flaps_up=2.5000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.000000
negative_g_limit_flaps_down=0.000000
load_safety_factor=1.5


[Reference Speeds]
flaps_up_stall_speed=142.000
full_flaps_stall_speed=113.000
cruise_speed=477.000
max_indicated_speed=320.0
max_mach=0.825

[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=0
stick_shaker=1

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2 
attitude_indicator.1 = 1 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0

[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=2,0

[airspeed_indicators]                     //IAS adjustmet parameters
airspeed_indicator.0 = 0.9826, 0.0        //Appropriate values for Jet AC

[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=0

