[fltsim.0]
title=California Express Embraer ERJ 140 - New Livery
sim=erj135
model=
panel=
sound=
texture=
kb_checklists=
description=Embraer 140 \n\nEngine Type: AE 3007A1/3 Rolls-Royce turbofan\n\nModel Designer\n   Carl Selin\n\nFDE-John Cillis\n\nTexture Designer\n  Tommy Hansson\n\nSound\n   Albert Ramic\n\nTest flown by Dream Wings members\n\ Paint by Peter McKay  
ui_manufacturer=Embraer
ui_type=ERJ 140 W/Airstair
ui_variation=California Express
atc_heavy=0
atc_id=N33830
atc_airline=California Express
atc_flight_number=

[General]
performance=Maximum Cruise Speed: mach 0.78, Passangers: 38, Range: 1760 nm
atc_type=EMBRAER
atc_model=E-135
editable=1

[pitot_static]
vertical_speed_time_constant=1


[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight=25342.000000
max_gross_weight=44092.0000
empty_weight_pitch_MOI=1272439.000
empty_weight_roll_MOI=1162183.000 
empty_weight_yaw_MOI=1137024.000
empty_weight_coupled_MOI=1300.000
CG_forward_limit=0.000
CG_aft_limit=1.000

max_number_of_stations=8

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

//Cabin

station_load.0=950.000000,20.000000,-3.000000,4.000000 //FWD Left
station_load.1=950.000000,20.000000,3.000000,4.000000 //FWD Right
station_load.2=950.000000,0.000000,-3.000000,4.000000 //Center Left
station_load.3=950.000000,0.000000,3.000000,4.000000 //Center Right
station_load.4=950.000000,-15.000000,-3.000000,4.000000 //Rear Left
station_load.5=950.000000,-15.000000,3.000000,4.000000 //Rear Right

//Baggage Cmpt

station_load.6=750.000000,20.000000,0.000000,-2.000000 //FWD 
station_load.7=750.000000,-15.000000,0.000000,-2.000000 //Rear 

[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, 27.80,  0.00, -6.95, 1575, 0, 0.700, 71.0, 0.25, 1.665, 0.700, 6.0, 7.5, 0.000, 250, 275 // These are my contact points
point.1=1, -7.45, -6.20, -8.75, 1575, 1, 1.065,  0.0, 0.80, 2.000, 0.700, 8.0, 8.0, 2.000, 250, 275 // These are my contact points
point.2=1, -7.45,  6.20, -8.75, 1575, 2, 1.065,  0.0, 0.80, 2.000, 0.700, 7.0, 7.0, 3.000, 250, 275 // These are my contact points
point.3=2, -15.000, -32.500, 1.500,  1574.803, 0, 0.000,  0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 5.000, 000, 000
point.4=2, -15.000,  32.500, 1.500,  1574.803, 0, 0.000,  0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 6.000, 000, 000
point.5=2, -31.250,  0.000,  2.650,  1574.803, 0, 0.000,  0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 9.000, 000, 000
point.6=2,  40.0,    0.000, -2.30,   1575.0, 0, 0.000,  0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 4.000, 000, 000
static_pitch=-1.2381         //degrees (pitch when loaded on ground)
static_cg_height=8.008           //feet, altitude of CG when at rest on the ground
gear_system_type=0

[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

[airplane_geometry]
wing_area=600.000000
wing_span=65.750000
wing_root_chord=9.250000
wing_dihedral=6.218262
wing_incidence=0.000000
wing_twist=-0.499878
oswald_efficiency_factor=0.657569
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=156.000000
htail_span=12.000000
htail_pos_lon=-15.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=115.000000
vtail_span=12.227019
vtail_sweep=0.000000
vtail_pos_lon=-15.000000
vtail_pos_vert=5.833333
elevator_area=70.500000
aileron_area=26.800000
rudder_area=56.200000
elevator_up_limit=26.000825
elevator_down_limit=26.000825
aileron_up_limit=30.000070
aileron_down_limit=30.000070
rudder_limit=30.000070
elevator_trim_limit=19.996227
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=3.000000
min_ailerons_for_spoilerons=9.969466
min_flaps_for_spoilerons=0.000000

[Flaps.0]
type=1
span-outboard=0.5
extending-time=27.0
system_type=0
flaps-position.0=0.0,0.0
flaps-position.1=13.333333,0.0
flaps-position.2=26.666666,0.0
flaps-position.3=40.000000,0.0

[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

[GeneralEngineData]
engine_type=1
Engine.0=-20, -5.100, 2.500
Engine.1=-20, 5.100, 2.500
fuel_flow_scalar=1.35
min_throttle_limit=0.000 // This is my non-reverser mod (Thanks to Fraser Turner of SGA)

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=10.5
static_thrust=7201.00
afterburner_available=0
reverser_available=0 // This is my non-reverser mod (Thanks to Fraser Turner of SGA)
rated_N2_rpm=29920.000000

[jet_engine]
thrust_scalar=1.000

[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=3,  -11.0, -32.0,   -1.63, fx_navred ,
light.1=3,  -11.0,  32.0,   -1.63, fx_navgre ,
light.2=3, -47.0,   0.00,  12.40,  fx_navwhi  ,
light.3=2,  -11.3, -32.2,   -1.63, fx_strobe  ,
light.4=2,  -11.3,  32.2,   -1.63, fx_strobe  ,
light.5=2, -47.0,   0.00,  12.45,  fx_strobe  ,
light.6=1,  3.54,   0.00,   3.8,   fx_beaconb ,
light.7=1,   -3.08,   0.00,  -5.3, fx_beaconb ,
light.8=4,  29.0, 0.0, 2.5  ,      fx_vclight ,
light.9=3,  7.4,   3.6, -3.0, fx_navwhi ,
light.10=3, 7.4,  -3.6, -3.0,  fx_navwhi ,

[Views]
eyepoint=24.0, -1.31, 0   //(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=1800
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]
Center1=0.000000,0.000000,0.000000,705.000000,0.000000
LeftMain=-3.000000,-19.000000,0.000000,500.000000,0.000000
RightMain=-3.000000,19.000000,0.000000,500.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=2.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[Reference Speeds]
flaps_up_stall_speed=142.000000
full_flaps_stall_speed=113.600000
cruise_speed=250.000000
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