// EMBRAER ERJ190-LR 
// VERSION 29
// FD update - by DC 10 Dec. 10, 2007; additions by JPB 13 Dec 2007
//US Airways livery by Fahim Safi 




[fltsim.0]
title=EMBRAER ERJ190-LR_USAIR
sim=EMB-190
model=
panel=bwb
sound=EMB
texture=usairways
kb_checklists=EMB-190_check
kb_reference=EMB-190_ref
atc_id=N952UW
atc_airline=USAIR
atc_flight_number=190
ui_manufacturer=EMBRAER
ui_type=ERJ-190 LR
ui_variation=US Airways Express
ui_typerole="Regional Jet"
ui_createdby="Premier Aircraft Design"
atc_parking_types=gate,ramp
atc_parking_codes=
description=Embraer ERJ90-LR\nA 98-114 passenger twin fanjet regional airliner. The E-190 family is a larger stretch of the E-170 model fitted with a new, larger wing and a new engine, the GE CF34-10E, rated at 18,500 lb (82.30 kN). Being in the 100 seat range, it competes with smaller jets including the Bombardier CRJ-900, Boeing 717-200 and 737-600 as well as the Airbus A318. The first flight of the E-190 was in March of 2004, with the first flight of the 195 in December of the same year. The launch customer of the E-190 was New York-based low cost carrier JetBlue with 100 orders and 100 options. European low cost carrier flybe is launching the E-195 with 14 orders and 12 options. As the 190/195 family is of mainline aircraft size, many airlines will operate them as such, fitting them with a business class section and operating them themselves, instead of having them flown by a commuter airline partner.

[General]
performance=Specifications\nWingspan 94 ft 3 in 28.72 m\nLength overall 118 ft 11 in 36.24 m\nHeight overall34 ft 7 in 10.55 m\nHorizontal stabilizer span32 ft 10 in 10.00 m\nPowerplant:Two 82.3kN (18,500lb) GE CF34-10E Fanjets\nMTOW: 106,924 lbs\nMax Cruise Speed: .82 mach\nMax Range in LR config: 2200nm, 4260km\n
editable=1 
atc_type=EMBRAER
atc_model=E190
Category=airplane

[Views]
eyepoint=41.900, -1.700, 2.950

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=2, -17.6, -45.6,  0.65, fx_strobeh ,
light.1=2, -17.6,  45.6,  0.65, fx_strobeh ,
light.2=1, 26.00,   0.00, 6.6, fx_beacon ,
light.3=4,  43.613,   0.00,  0.61, fx_vclightwhite ,
light.4=4,  43.8,   0.00,  0.17, fx_vclightwhite ,
light.5=2, -62.05,  0.00,  5.00, fx_strobeh ,
light.6=1, 10.24,   0.00, -6.380, fx_beacon ,
light.7=3, -17.6, -45.6,  0.65, fx_navredh ,
light.8=3, -17.6,  45.6,  0.65, fx_navgreh ,


[ground_reaction]
main_gear_static_compression=1.0		// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.8            // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=0.9		// Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=0.9		// Center gear strut damping, 0 = undamped osciallations, 1 = critically damped

[pitot_static]
vertical_speed_time_constant=99		//Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[WEIGHT_AND_BALANCE]

reference_datum_position     =  0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -2.600, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum
max_gross_weight=110893.000    
empty_weight=57250.000   
max_number_of_stations = 50

station_load.0 =   "170.0,  42.0, -1.5,	0.0, Pilot"              //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)        
station_load.1 =   "170.0,  42.0,  1.5,	0.0, Co-Pilot"           //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2 =   "510.0,   0.0,  0.0,	0.0, Crew"               //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3 =  "1460.0,  25.5,  0.0,	0.0, First Class"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.4 =  "4080.0,  11.0,  0.0,	0.0, Coach 3-10"         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.5 =  "4080.0, -10.0,  0.0,	0.0, Coach 11-18"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.6 =  "4080.0, -30.5,  0.0,	0.0, Coach 19-25"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.7 = "2000.0,  20.5,  0.0,	0.0, Forward Baggage"    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.8 =  "1800.0, -27.5,  0.0,	0.0, Aft Baggage"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

;Moments of Inertia
empty_weight_pitch_MOI  =  800000
empty_weight_roll_MOI   = 1000000
empty_weight_yaw_MOI    = 1600000
empty_weight_coupled_MOI = 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=1.000, 38.300, 0.000, -10.600, 1181.102, 0.000, 1.200, 55.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1=1.000, -8.800, -10.000, -10.900, 1574.803, 1.000, 1.400, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000
point.2=1.000, -8.800, 10.000, -10.900, 1574.803, 2.000, 1.400, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000
point.3=2.000, -24.167, -47.250, 6.000, 787.402, 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, -24.167, 47.250, 6.000, 787.402, 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, -66.400, 0.000, 3.600, 787.402, 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, 52.500, 0.000, -2.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7=5.000, -30.900,  0.000, -7.300, 1600, 0.000, 0.000, 50.000, 0.000,  0.000, 1.000, 1.100, 1.500,0.000, 0.000, 0.000
static_pitch=-0.500
static_cg_height=10.100
gear_system_type=1      //Hydraulic

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2
number_of_tank_selectors=1
Center1    = 0,   0, 0, 2340, 0
LeftMain=0.000, -10.000, 0.000,1000.000, 0.000
RightMain=0.000, 10.000, 0.000, 1000.000, 0.000
electric_pump=0

[airplane_geometry]
wing_area=947.040
wing_span=94.00
wing_root_chord=13.000
wing_dihedral=2.500
wing_incidence=-4.000
wing_twist=-1.500
oswald_efficiency_factor=0.750
wing_winglets_flag=1
wing_sweep=25.000
wing_pos_apex_lon=6.000
wing_pos_apex_vert=-3.200
htail_area=281.000
htail_span=33.000
htail_pos_lon=-52.000
htail_pos_vert=3.000
htail_incidence=-4.350
htail_sweep=25.000
vtail_area=202.770
vtail_span=17.800
vtail_sweep=35.000
vtail_pos_lon=-50.800
vtail_pos_vert=5.400
elevator_area=70.500
aileron_area=26.800
rudder_area=56.200
elevator_up_limit=10.0
elevator_down_limit=10.0
aileron_up_limit=30.000
aileron_down_limit=30.000
rudder_limit=20.000
elevator_trim_limit=15.000
spoiler_limit=80.000
spoilerons_available=0
aileron_to_spoileron_gain=0
min_ailerons_for_spoilerons=0
min_flaps_for_spoilerons=0.000
auto_spoiler_available=1
spoiler_extension_time=1.500000
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

[GeneralEngineData]
engine_type=1
Engine.0=2.750, -14.700, -5.600
Engine.1=2.750, 14.700, -5.600
fuel_flow_scalar=0.800
min_throttle_limit = -0.25                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature = -30                  //Temperature (deg C) below which contrails may appear

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=19.000
rated_N2_rpm=29920.000
static_thrust=18500.000
afterburner_available=0
reverser_available=1

[jet_engine]
thrust_scalar=1.000

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.050
induced_drag_scalar=1.000
pitch_stability=1.150
roll_stability=1.100
yaw_stability=1.000
elevator_effectiveness=1.400
aileron_effectiveness=1.100
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.350
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[Reference Speeds]
flaps_up_stall_speed=115.000   //Knots True (KTAS)
full_flaps_stall_speed=95.600   //Knots True (KTAS)
cruise_speed=380.000    //Knots True (KTAS)
max_indicated_speed=350.000000   //Red line (KIAS)
max_mach=0.8400

[autopilot]
autopilot_available                  = 1.000
flight_director_available            = 1.000
default_vertical_speed               = 1800.000
autothrottle_available               = 1.000
autothrottle_arming_required         = 1.000
autothrottle_takeoff_ga              = 1.000
autothrottle_max_rpm                 = 90.000
pitch_takeoff_ga                     = 8;
max_pitch                            = 10.000
max_pitch_acceleration               = 1.000
max_pitch_velocity_lo_alt            = 2.000
max_pitch_velocity_hi_alt            = 1.500
max_pitch_velocity_lo_alt_breakpoint = 20000.000
max_pitch_velocity_hi_alt_breakpoint = 28000.000
max_bank                             = 22.000
max_bank_acceleration                = 1.500
max_bank_velocity                    = 2.500
max_throttle_rate                    = 0.100
nav_proportional_control             = 9.000
nav_integrator_control               = 0.250
nav_derivative_control               = 0.000
nav_integrator_boundary              = 2.500
nav_derivative_boundary              = 0.000
gs_proportional_control              = 9.520
gs_integrator_control                = 0.260
gs_derivative_control                = 0.000
gs_integrator_boundary               = 0.700
gs_derivative_boundary               = 0.000
yaw_damper_gain                      = 1.000
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0

[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

[gear_warning_system]
gear_warning_available = 0    //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 = 0.90  //Brake scalar
auto_brakes=4

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

[stall_warning]
type=1
stick_shaker=0

[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 = 0.6                              ;Percent per second
exit_rate.1 = 0.6                               ;Percent per second

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

[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

[electrical]
max_battery_voltage=28.0
generator_alternator_voltage=24.0
max_generator_alternator_amps=260.0
flap_motor=0, 0, 1
gear_motor=0, 0, 1
autopilot=0, 0, 1
avionics_bus=0, 0, 1
avionics=1, 0, 1
pitot_heat=0, 0, 1
additional_system=0, 0, 1
marker_beacon=1, 0, 1
gear_warning=0, 0, 1
fuel_pump=0, 0, 1
starter1=0, 0, 1
starter2=0, 0, 1
starter3=0, 0, 1
light_nav=0, 0, 1
light_beacon=0, 1, 1
light_landing=0, 0, 1
light_taxi=0, 0, 1
light_strobe=0, 1, 1
light_panel=0, 0, 1
auto_brake=0, 0, 1
standby_vacuum=0, 0, 1
hydraulic_pump=0, 0, 1
fuel_transfer_pump=0, 0, 1
light_recognition=0, 0, 1
light_wing=0, 0, 1
light_logo=0, 0, 1
electric_always_available=0

//[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 = 1                                    // degrees
//flaps-position.2 = 2                                    // degrees
//flaps-position.3 = 5                                    // degrees
//flaps-position.4 = 10                                   // degrees
//flaps-position.5 = 15                                   // degrees
//flaps-position.6 = 25                                   // degrees
//flaps-position.7 = 30                                   // degrees
//flaps-position.8 = 40                                   // degrees
//damaging-speed   = 250                                  // KIAS
//blowout-speed    = 300                                  // KIAS
//lift_scalar = 1.05
//drag_scalar = 1.35
//pitch_scalar= 0.01
//system_type = 1                                         //Hydraulic

[flaps.0]       
//Trailing Edge Flaps
type             = 1                                  // 1 - tail, 2 - lead

span-outboard    = 0.8                           // 0.0 .. 1.0
extending-time   = 12                              // seconds
flaps-position.0 = 0                                  // UP
flaps-position.1 = 2                                 // degrees
flaps-position.2 = 8                                // degrees
flaps-position.3 = 15                              // degrees
flaps-position.4 = 30                           // degrees
flaps-position.5 = 37                             // degrees
flaps-position.6 = 40                              // FULL
damaging-speed   = 280                      // KIAS
blowout-speed    = 340                         // KIAS
lift_scalar = 0.950
drag_scalar = 0.900
pitch_scalar= 1.100
system_type = 1                                      //Hydraulic




[flaps.1]       //Inboard Leading Edge Flaps
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.2                                 // 0.0 .. 1.0
extending-time   = 4                                    // seconds
flaps-position.0 = 0                                    // 
flaps-position.1 = 1.0                                  // 
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.05
drag_scalar = 1.15
pitch_scalar= 0.01
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   = 5                                    // 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 = 1.05
drag_scalar = 1.30
pitch_scalar= 0.01
system_type = 1                                         //Hydraulic


[folding_wings]
wing_fold_system_type = 4                       ;0=None
fold_rates = 0.12,0.11                          ;Percent per second

[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