[fltsim.0]
title=Emb 314 FAD PAINT
sim=Emb 314
model=ALX
panel=
sound=
texture=2901
kb_checklists=Emb314_check
kb_reference=Emb314_ref
description=En agosto de 2001, Embraer anunciу la firma de un contrato con la Repъblica Dominicana por 10 aviones Sъper Tucano, que se utilizarб para la formaciуn de pilotos, la seguridad interior, la patrulla fronteriza y la lucha contra el narcotrбfico misiones de trata de personas. La orden fue reducida a ocho aviones en enero de 2009, por un importe total de EE.UU. $ 93 millones.  Los dos primeros aviones Super Tucano fueron entregados a la Repъblica Dominicana el 18 de diciembre de 2009. Tres fueron entregados en junio de 2010 y los tres restantes en octubre de 2010\n.TEXTURE FAD by Robert Serrata....Fiebre Aerea Dominicana http:\/\/fiebreaereadominicana.blogspot.com\/
ui_manufacturer=Embraer
ui_type=ALX T29
ui_variation=TANK & MISIL.2901 FAD
atc_heavy=0
atc_id=2901
atc_airline=Air Force
atc_flight_number=2901

[fltsim.1]
title=Emb 314 FAD
sim=Emb 314
model=AFA
panel=
sound=
texture=2900
kb_checklists=Emb314_check
kb_reference=Emb314_ref
description=En agosto de 2001, Embraer anunciу la firma de un contrato con la Repъblica Dominicana por 10 aviones Sъper Tucano, que se utilizarб para la formaciуn de pilotos, la seguridad interior, la patrulla fronteriza y la lucha contra el narcotrбfico misiones de trata de personas. La orden fue reducida a ocho aviones en enero de 2009, por un importe total de EE.UU. $ 93 millones.  Los dos primeros aviones Super Tucano fueron entregados a la Repъblica Dominicana el 18 de diciembre de 2009. Tres fueron entregados en junio de 2010 y los tres restantes en octubre de 2010\n.TEXTURE FAD by Robert Serrata....Fiebre Aerea Dominicana http:\/\/fiebreaereadominicana.blogspot.com\/
ui_manufacturer=Embraer
ui_type=ALX T29
ui_variation=CLEAN.2900.FAD
atc_heavy=0
atc_id=2900
atc_airline=Air Force
atc_flight_number=2900


[General]
atc_type=ALX
atc_model=T29
editable=1
performance=Maximum Speed\n303 kts (TAS)      560 km\/hr\nCruise Speed\n286 kts (TAS)      530 km\/hr at 20,000 ft\n\nEngine\nPratt & Whitney Canada, Inc., PT6A-68-3 \n1.600 shp\nPropeller\nFive-Bladed, Constant Speed, Full Feathering, Reversible  Hartzell, 96-inch diameter\n\nMaximum range\nInt. tanks - 809 nm ( 1,500 km )\nWith external tanks - 1,242 nm ( 2,300 km  )\nService Ceiling\n32,860 ft            10,668 m\n\nFuel Capacity\n180  gal (internal)   695 L\n\nEmpty Weight               5,330 lb\nMaximum Gross Weight 10,837 lb\nLength       37.1 ft \nWingspan   36.1 ft\n


[WEIGHT_AND_BALANCE]
max_gross_weight = 10837.000
empty_weight = 5330.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations = 50

;Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.0 = 170.000, -1.000, 0.000, 0.000          
;station_load.1 ="500.00, 1.50,-7.00,-1.00, pylon LI"   //Max 800 lb (bomb) or 582 lb (fuel)
;station_load.2 ="500.00, 1.50, 7.00,-1.00, pylon RI"   //Max 800 lb (bomb) or 582 lb (fuel)
station_load.3 ="190.00, 0.50,-8.50,-1.00, pylon LE"    //Max 500 lb
station_load.4 ="190.00, 0.50, 8.50,-1.00, pylon RE"    //Max 500 lb

;Moments of Inertia
empty_weight_pitch_MOI   = 8730.000
empty_weight_roll_MOI    = 4880.000
empty_weight_yaw_MOI     = 8530.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =1.000
induced_drag_scalar    =1.000
elevator_effectiveness =1.000
aileron_effectiveness  =1.500
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
p_factor_on_yaw          = 0.5
torque_on_roll           = 0.5

[GeneralEngineData]
engine_type = 5
Engine.0 = 6.000, 0.000, 0.000
fuel_flow_scalar   = 0.750
min_throttle_limit = -0.25                      //Min percent throttle. negative for turb revsr

[propeller]
thrust_scalar           =1.201
propeller_type          = 0
propeller_diameter      = 7.800
propeller_blades        = 5
propeller_moi           = 24.000
beta_max                = 45.000
beta_min                = 10.000
min_gov_rpm             = 25000.000
prop_tc                 = 0.004
gear_reduction_ratio    = 15.550
fixed_pitch_beta        = 0.000
low_speed_theory_limit  = 80.000
prop_sync_available     = 0
prop_deice_available    = 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather     = 700.000
beta_feather            = 88.000
power_absorbed_cf       = 0.400
defeathering_accumulators_available= 0
prop_reverse_available  = 1
minimum_on_ground_beta  = 0.000
minimum_reverse_beta    = -14.000

[TurbineEngineData]
fuel_flow_gain          = 0.011
inlet_area              = 1.000
rated_N2_rpm            = 33000.000
static_thrust           = 190.000
afterburner_available   = 0

[turboprop_engine]
power_scalar            =1.000
maximum_torque          = 4451.400
max_rpm_mechanical_efficiency_scalar =1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI

[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            
light.0 = 3,  -0.58, -17.99, -0.05, fx_navred
light.1 = 3,  -0.58,  17.99, -0.05, fx_navgre
light.2 = 3, -24.00,   0.00, -1.77, fx_navwhi
light.3 = 2,  -0.60, -18.10, -0.05, fx_strobe
light.4 = 2,  -0.60,  18.10, -0.05, fx_strobe
light.5 = 1, -12.49,   0.00,  0.96, fx_beacon
light.6 = 4,   1.58,   0.00,  2.25, fx_vclight
light.7 = 5,   1.25, -11.40, -0.80, fx_landing
light.8 = 5,   1.25,  11.40, -0.80, fx_landing
;light.9 = 5,   9.75,   0.00, -3.01, fx_landing

[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  = 200, 1000
rudder   = 200, 1000

[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 
attitude_indicator.1 = 2

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

[airspeed_indicators]
airspeed_indicator.0 = 1.183, -24.75

[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus       = 0, 5 , 9.5
avionics           = 1, 5 , 9.5
additional_system  = 0, 2 , 9.5
marker_beacon      = 1, 2 , 9.0
fuel_pump          = 0, 5 , 9.0

        //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
[contact_points]
point.0= 1.000, 9.140, 0.000, -5.450, 1900.000, 0.000, 0.550, 40.000, 0.300, 2.200, 0.800, 3.500, 3.500, 0.000, 0.000, 0.000
point.1= 1.000, -1.540, -6.000, -5.700, 2000.000, 1.000, 0.900, 0.000, 0.300, 2.000, 0.700, 3.500, 3.500, 2.000, 0.000, 0.000
point.2= 1.000, -1.540, 6.000, -5.700, 2000.000, 2.000, 0.900, 0.000, 0.300, 2.000, 0.700, 3.500, 3.500, 3.000, 0.000, 0.000
point.3= 2.000, -1.000, -18.000, 0.000, 800.000, 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, -1.000, 18.000, 0.000, 800.000, 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, -22.000, 0.000, -2.450, 800.000, 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, 0.000, 0.000, -2.450, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, -22.800, 0.000, 5.780, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

max_number_of_points = 21

static_pitch    = -1.955
static_cg_height= 5.380
gear_system_type= 0

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 0.68  //Brake scalar

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

[Views]
eyepoint= -1.4, 0.0, 2.3    //(feet) longitudinal, lateral, vertical distance from reference datum

[fuel]
//Long(ft), Lat(ft), Vert(ft), usable(gl), Unusable(gl) 
LeftMain  = 0.000, -1.600, 0.500, 180.000, 0.400
RightMain = 0.000, 1.600, 0.500, 180.000, 0.400
;LeftAux   =  1.500, -7.000, -1.000, 90.000, 0.000         
;RightAux  =  1.500,  7.000, -1.000, 90.000, 0.000

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

[SMOKESYSTEM]
//?,long,lat from ref datum
smoke.0= -14.55, 2.75,9.00, fx_hueyR1.fx
smoke.1= -14.55, 2.75, -9.00, fx_hueyL1.fx


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

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

[airplane_geometry]
wing_area               = 190.500
wing_span               = 36.100
wing_root_chord         = 7.700
wing_dihedral           = 4.100
wing_incidence          = 2.000
wing_twist              = -1.000
oswald_efficiency_factor= 0.700
wing_winglets_flag      = 0
wing_sweep              = 0.000
wing_pos_apex_lon       = 0.000
wing_pos_apex_vert      = 0.000
htail_area              = 54.000
htail_span              = 15.400
htail_pos_lon           = -24.300
htail_pos_vert          = 0.000
htail_incidence         = -1.500
htail_sweep             = 0.000
vtail_area              = 36.000
vtail_span              = 5.200
vtail_sweep             = 18.000
vtail_pos_lon           = -24.700
vtail_pos_vert          = 0.500
elevator_area           = 21.980
aileron_area            = 24.300
rudder_area             = 16.200
elevator_up_limit       = 28.000
elevator_down_limit     = 26.000
aileron_up_limit        = 23.000
aileron_down_limit      = 18.000
rudder_limit            = 24.000
elevator_trim_limit     = 18.000
spoiler_limit           = 0.000
spoilerons_available    = 0
aileron_to_spoileron_gain = 1.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoiler_handle_available = 0                    //Defaults to True if spoiler limit > 0, else False.  Should be False for spoilerons only

[Reference Speeds]
flaps_up_stall_speed    = 78.000
full_flaps_stall_speed  = 66.800
cruise_speed            = 286.000
max_mach                = 0.65
max_indicated_speed     = 303                   ////Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
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=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
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

[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=2

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 210.000
blowout-speed= 250.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000