[fltsim.0]
title=Emb110 AEROPROYECTO
sim=Emb110
model=
panel=
sound=
texture=Aeroproyecto
kb_checklists=
kb_reference=
atc_id_color=
atc_id=CU-T1541
ui_manufacturer=AEROPROYECTO
ui_type="EMBRAER EMB-110 "Bandeirante""
ui_variation="Aeroproyecto Colors"
description="EMBRAER 110 (Bandeirante) R3.0 FreeWare \nAEROPROYECTO 1999-2014 \nBy Edgar Guinart Lуpez\[email protected] \n\nFor more details check files in Reference folder" 
visual_damage=1

[fltsim.1]
title=Emb110 SIMUCUBA
sim=Emb110
model=
panel=
sound=
texture=SimuCuba
kb_checklists=
kb_reference=
atc_id_color=
atc_id=CU-T1542
ui_manufacturer=AEROPROYECTO
ui_type="EMBRAER EMB-110 "Bandeirante""
ui_variation="SimuCuba Colors"
description="EMBRAER 110 (Bandeirante) R3.0 FreeWare \nAEROPROYECTO 1999-2014 \nBy Edgar Guinart Lуpez\[email protected] \n\nFor more details check files in Reference folder" 
visual_damage=1


[General]
atc_type=Embraer
atc_model=Emb110
editable=0
performance="Technical Data \nAccommodation : 2 crew + 18 pax \nDimensions \nSpan : 15.3m (50'4ft) \nLength : 14.22m (46'8ft) \nHeight : 4.92m (16'2ft) \nWeight \nEmpty: 3,062kg (6,737lbs) \nMax: 5,110kg (11,243lbs) \nPower Plant: 2x 680shp P&W PT6A-27 \nPerformance  \nMax speed: 418km/h (260mph-225knots) \nMax climb: 1,968ft/min (10m/sec) \nCeiling: 27,950ft (8,520m) -limited to 12000 feet due unpressurized cabin. \nRange: 1,850km (1,000nm)"
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight = 12383                        // (pounds)
empty_weight = 6799                             // (pounds) 6437 Plus 362 lbs of Crew and their stuffs

reference_datum_position     =  0, 0, 0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  1.0, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 10

station_load.0 = "450,   6.1, 0.0, 0.5, 1-3   Max 500"
station_load.1 = "450,   3.6, 0.0, 0.5, 4-6   Max 500"
station_load.2 = "450,   1.2, 0.0, 0.5, 7-9   Max 500"
station_load.3 = "450,  -1.2, 0.0, 0.5, 10-12 Max 500"
station_load.4 = "450,  -3.6, 0.0, 0.5, 13-15 Max 500" 
station_load.5 = "450,  -6.1, 0.0, 0.5, 16-18 Max 500"
station_load.6 = "200, -12.5, 0.0, 0.0, Bag   Max 528"  

;Moments of Inertia
empty_weight_pitch_MOI   	= 20160			// 20160 
empty_weight_roll_MOI    	= 15201			// 10134 (x 1.5 twin winged enine momment)
empty_weight_yaw_MOI     	= 21505			// 21505 
empty_weight_coupled_MOI = 0.0


[GeneralEngineData]
engine_type = 5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 7.9, -7.5, -0.1                      //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 7.9,  7.5, -0.1                      //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0                          //Scalar for fuel flow efficiency
min_throttle_limit = -0.25;                     //Minimum percent throttle.  Generally negative for turbine reverser

[propeller]
thrust_scalar           = 1.0                   //Propeller thrust scalar
propeller_type          = 0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter      = 7.75                  //Propeller Diameter, (feet)
propeller_blades        = 3                     //Number of propeller blades
propeller_moi           = 15                    //Propeller moment of inertia
beta_max                = 45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min                = 17.0                  //Minimum blade pitch angle for constant speed prop, (degrees) // 17.2 +/-2є (min vuelo)
min_gov_rpm             = 24255                 //Miminum governed RPM  // Free Turb. ~ 1650 Prop.
prop_tc                 = 0.004                 //Prop time-constant
gear_reduction_ratio    = 14.7                  //Propeller gear reduction ratio  // 0.068:1 Reduct.
fixed_pitch_beta        = 0                     //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit  = 80                    //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available     = 1                     //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available    = 0                     //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 1               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather     = 700                   //Minimum RPM for prop feathering
beta_feather            = 88.1                  //Feathering pitch angle (degrees)
power_absorbed_cf       = 0.9                   //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available  = 1                     //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta  = 1.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta    = -11.0                 //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain        	= 0.011                 //Gain on fuel flow
inlet_area              = 0.57                   //Square Feet, engine nacelle inlet area
rated_N2_rpm         	= 32340                  //RPM, second stage compressor rated value  // Free Turb.
static_thrust          	= 90                   //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar            = 1.0                   //Scalar on Turboprop power
maximum_torque          = 1628                  //Maximum torque available (ft-lbs)
max_rpm_mechanical_efficiency_scalar  =1.0
idle_rpm_mechanical_efficiency_scalar =1.0
max_rpm_friction_scalar               =1.0 
idle_rpm_friction_scalar              =1.0 


[exits]
number_of_exits = 1
exit_rate.0 = 1.0                               ;Percent per second


[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes: 0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
electric_always_available = 0
flap_motor = 			0, 0, 17.0
gear_motor = 			0, 0, 17.0
autopilot = 			1, 0, 17.0
avionics_bus = 			0, 0, 17.0
avionics = 			1, 0, 17.0
pitot_heat = 			0, 0, 17.0
additional_system = 		0, 0, 17.0
marker_beacon = 		1, 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
light_recognition = 		0, 0, 17.0
light_wing = 			0, 0, 0.0
light_logo = 			0, 0, 0.0
prop_sync = 			0, 0, 17.0
auto_feather = 			0, 0, 17.0
standby_vacuum = 		0, 0, 17.0
hydraulic_pump = 		0, 0, 17.0
fuel_transfer_pump = 		0, 0, 17.0
propeller_deice = 		0, 0, 17.0
directional_gyro = 		1, 0, 17.0
directional_gyro_slaving = 	1, 0, 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,   12.2,   0.00, -5.70,   1200.0, 0, 0.9, 57.0,     0.3, 4.0, 0.8,    5.0,  3.0, 0, 300.0, 184.0
point.1=1,  -1.31,  -8.00, -5.65,   1900.0, 1, 1.1,  0.0,     0.4, 2.5, 0.6,    6.0,  4.0, 2, 300.0, 184.0
point.2=1,  -1.31,   8.00, -5.65,   1900.0, 2, 1.1,  0.0,     0.4, 2.5, 0.6,    6.0,  4.0, 3, 300.0, 184.0
//CRASH POINTS
point.3=2,   0.0,  -25.5,   1.6,    1787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 5, 0.0, 0.0
point.4=2,   0.0,   25.5,   1.6,    1787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 6, 0.0, 0.0
point.5=2, -25.5,    0.0,   1.3,    1787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 9, 0.0, 0.0
point.6=2,  19.5,    0.0,  -1.0,    1787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 4, 0.0, 0.0
//HARD POINTS
point.7 = 4,  -0.5,  -7.6,   -2.8,  2600, 0, 0.00,  0.0, 0.3, 2.5, 0.6, 0.0, 0.0, 7, 0.0, 0.0
point.8 = 4,  -0.5,   7.6,   -2.8,  2600, 0, 0.00,  0.0, 0.3, 2.5, 0.6, 0.0, 0.0, 7, 0.0, 0.0
point.9 = 4,  15.0,   0.0,   -2.5,  2600, 0, 0.00,  0.0, 0.5, 2.5, 0.5, 0.0, 0.0, 7, 0.0, 0.0


static_pitch = 0.0
static_cg_height = 5.6
gear_system_type=1      //Hydraulic

[Views]
eyepoint = 9.4, -1.26, 2.7

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.6                                  // 0.0 .. 1.0
extending-time   = 12                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 9.5                                   // degrees
flaps-position.2 = 19.0                                   // degrees
flaps-position.3 = 28.5                                   // degrees
flaps-position.4 = 38.0                                   // degrees
damaging-speed   = 180                                  // KIAS
blowout-speed    = 200                                  // KIAS
system_type = 0						//0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
lift_scalar = 1.0                                       
drag_scalar = 1.0
pitch_scalar= 1.0

[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, 0
Adf.1         = 1
Adf.2         = 1
Transponder.1 = 1
Marker.1      = 1

[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 = 100, 180
aileron  = 130, 200
rudder   = 130, 200

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    = 15.0     //Flap angle that activates warning at idle
flap_limit_power   = 30.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.6  //Brake scalar   ---> 0.6 is OK
// differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected

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

[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 = 2 

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

[airspeed_indicators]
airspeed_indicator.0 = 1

[altimeters]
altimeter.0=1

[deice_system]
structural_deice_type=0        //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots

[vacuum_system]
max_pressure=5.15   //PSI
vacuum_type=0       //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[pitot_static]
vertical_speed_time_constant = 1.0
pitot_heat=1.0

[stall_warning]
type=1
stick_shaker=0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0  = 3,   -0.6, -25.1,  1.6, fx_navred
light.1  = 3,   -0.6,  25.1,  1.6, fx_navgre
light.2  = 3,  -25.8,  0.0,  2.15, fx_navwhi
light.3  = 2,   -0.7, -25.1,  1.6, fx_strobe
light.4  = 2,   -0.7,  25.1,  1.6, fx_strobe
light.5  = 1, -24.6,   0.00,  11.8, fx_beacon
light.6  = 1, -1.15,   0.00,  -2.19, fx_beacon
light.7  = 2,  -25.8,   0.0,   2.3, fx_strobe
light.8  = 8,    7.9, -7.5,   -0.1, EMB110_OnFire
light.9  = 9,    7.9,  7.5,   -0.1, EMB110_OnFire
light.10 = 4,   11.0,   0.0,   2.7, fx_vclight
light.11 = 7,   4.9,  -2.9,   1.0, EMB110_WingLights
light.12 = 7,   4.9,   2.9,   1.0, EMB110_WingLights
light.13 = 10,   4.00,   0.0,   3.0, EMB110_CabinLights
light.14 = 10,  -3.00,   0.0,   3.0, EMB110_CabinLights
light.15 = 10, -12.00,   0.0,   3.0, EMB110_CabinLights


[EFFECTS]
wake     = fx_wake
water    = fx_spray
dirt     = fx_tchdrt
concrete = fx_sparks
touchdown= fx_tchdwn_s, 1
startup  = EMB110_Start


[fuel]
LeftMain   = -1.31, -7.5, 0.0, 210, 7.5     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -1.31,  7.5, 0.0, 210, 7.5     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2                    
electric_pump=1


[airplane_geometry]
wing_area               = 312.0                 //Square *** 312 Data (Tip-To-Tip)
wing_span               = 50.26                  //Feet
wing_root_chord         = 7.2                   //Feet
wing_dihedral           = 5.0                   //Degrees
wing_incidence          = 2.5                   //Degrees
wing_twist              = -1.5                  //Degrees
oswald_efficiency_factor= 0.7                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = 1.9                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = -1.3                   //Feet, vertical distance from reference point, positive going up
htail_area              = 64.0                  //Square feet
htail_span              = 26.0                  //Feet
htail_pos_lon           = -19.0                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 2.4                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.7                   //Degrees
htail_sweep             = 2.0                  //Degrees, horizontal tail leading edge
vtail_area              = 53.0                  //Square feet
vtail_span              = 8.6                   //Feet, tip to body
vtail_sweep             = 36.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -20.6                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 3.3                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 32.0                  //Square feet
aileron_area            = 31.0                  //Square feet
rudder_area             = 25.0                   //Square feet
elevator_up_limit       = 32.0                  //Degrees
elevator_down_limit     = 20.0                  //Degrees
aileron_up_limit        = 22.0                  //Degrees
aileron_down_limit      = 14.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 20.0                  //Degrees
spoiler_limit           = 0.0                  //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0.0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0.0                 //Degrees
min_flaps_for_spoilerons = 0.0                    //Minimum flap handle position when spoilerons activate
spoiler_handle_available = 0                    //Defaults to True if spoiler limit > 0, else False.  Should be False for spoilerons only
auto_spoiler_available   = 0
positive_g_limit_flaps_up=4.006410
positive_g_limit_flaps_down=2.670940
negative_g_limit_flaps_up=-1.869658
negative_g_limit_flaps_down=-0.534188


[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
p_factor_on_yaw=0.6
torque_on_roll=0.6
gyro_precession_on_yaw=1.0
gyro_precession_on_pitch=1.0
hi_alpha_on_roll=1.0
hi_alpha_on_yaw=1.0
hi_alpha_on_pitch=1.0

[Reference Speeds]
flaps_up_stall_speed    = 69.0                  //Knots True (KTAS)
full_flaps_stall_speed  = 57.0                  //Knots True (KTAS)
cruise_speed            = 200.0                 //Knots True (KTAS)
max_mach                = 0.58
max_indicated_speed     = 230                   //Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 000.0
autothrottle_available= 0
pitch_takeoff_ga=0.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
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=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
// use_no_default_bank=1	    //For no wing leveler when AP On
// use_no_default_pitch=0	    //For no pitch holding when AP On
default_pitch_mode=1
default_bank_mode=0

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
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=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 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