[fltsim.0]
title=Embraer_EMB-312_Tucano
sim=Embraer_EMB-312_Tucano_AT-27
model=eda
panel=
sound=
texture=
checklists=
ui_manufacturer=Embraer
ui_type=Embraer EMB-312 Tucano
ui_variation=T-27 EDA 7
visual_damage=1
description=Painted by Cristiano Magnani
description= Todos os direitos reservados - FSFAB Denis da Silva e Daniel da Silva, textura foto realistica Cristiano Magnani
atc_heavy=0
atc_id=EDA
atc_airline=AIR FORCE
atc_flight_number=
[General]
performance=País de origem: Brasil \nFabricante: Embraer \nTipo: Avião de treinamento e ataque ao solo \nMotores: Pratt & Whitney PT6A-25C turboélice de 750 SHP \nDesempenho - \nVel. máx. a 3.050 m: 457 km\/h \nTeto: 9.936 m \nAlcance: 2.112 km \nPeso - \nVazio: 1.810 kg \nMáx decolagem: 3.175 kg \nDimensões - \nEnvergadura: 11,14 m \nComprimento: 9,86 m \nAltura: 3,40 m \nÁrea de asa: 19,40 m2 \nOperadores: Brasil, Paraguai, Iraque, Egito, Inglaterra, França, Honduras, Argentina, Colômbia, Venezuela, Peru e Katar.
atc_type=EMBRAER
atc_model=E312
[Views]
eyepoint=-13.9 ,-0.1, 2.8
[SMOKESYSTEM]
smoke.0=-1,-2,4.09,fx_smoke_w
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -14.5,-19, 0.7, fx_navredh ,
light.1=3, -14.5, 19, 0.7, fx_navgreh ,
light.2=4, -17,0 , 2.9, fx_vclight,
light.3=2, -14.5,-19, 0.7, fx_strobeh ,
light.4=2, -14.5, 19, 0.7, fx_strobeh ,
light.5=4, -12.5, 0.000000, 2.3, fx_vclight
[WEIGHT_AND_BALANCE]
max_gross_weight=5952.000
empty_weight=3074.000
reference_datum_position=16.200, 0.000, 0.000
empty_weight_CG_position=-16.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=170.000, -16.000, -1.500, 0.000
;Moments of Inertia
empty_weight_pitch_MOI=4524.000
empty_weight_roll_MOI=2477.000
empty_weight_yaw_MOI=6121.000
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=0.490
induced_drag_scalar=1.206
elevator_effectiveness=1.000
aileron_effectiveness=2.002
rudder_effectiveness=1.750
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
[GeneralEngineData]
engine_type=5
Engine.0=-7.000, 0.000, 0.000
fuel_flow_scalar=1.120
min_throttle_limit=-0.349915
[propeller]
thrust_scalar=1.206
propeller_type=0
propeller_diameter=8.500
propeller_blades=3
propeller_moi=16.000
beta_max=65.000
beta_min=10.000
min_gov_rpm=25520.000
prop_tc=0.004
gear_reduction_ratio=17.400
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=0.900
defeathering_accumulators_available=1
prop_reverse_available=1
minimum_on_ground_beta=1.000
minimum_reverse_beta=-14.000
[TurbineEngineData]
fuel_flow_gain=0.011
inlet_area=1.000
rated_N2_rpm=33000.000
static_thrust=160.000
afterburner_available=0
[turboprop_engine]
power_scalar=1.000
maximum_torque=2370.000
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, 1
Com.2=1, 1
Nav.1=1
Nav.2=1
Adf.1=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=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
//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, -7.100, 0.000, -4.780, 1500.000, 0.000, 0.500, 35.000, 0.300, 2.500, 0.700, 3.000, 4.000, 0.000, 0.000, 0.000
point.1=1.000, -17.500, -4.000, -4.800, 2500.000, 1.000, 0.500, 0.000, 0.300, 2.500, 0.700, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1.000, -17.500, 4.000, -4.800, 2500.000, 2.000, 0.500, 0.000, 0.300, 2.500, 0.700, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2.000, -15.900, -26.000, 3.000, 1800.000, 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, -15.900, 26.000, 3.000, 1800.000, 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, -39.230, 0.000, 0.000, 1800.000, 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, -2.500, 0.000, -2.170, 1800.000, 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, -42.000, 0.000, 10.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
max_number_of_points=21
static_pitch=0.240
static_cg_height=5.250
gear_system_type=1
[fuel]
LeftMain=-18.400, -1.100, 2.500, 91.000, 3.600
RightMain=-18.400, 1.100, 2.500, 91.000, 3.600
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1
[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=175.000
wing_span=33.250
wing_root_chord=6.400
wing_dihedral=3.900
wing_incidence=1.000
wing_twist=-1.000
oswald_efficiency_factor=0.850
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=-16.000
wing_pos_apex_vert=0.000
htail_area=39.000
htail_span=11.700
htail_pos_lon=-30.900
htail_pos_vert=0.000
htail_incidence=2.000
htail_sweep=5.000
vtail_area=38.000
vtail_span=5.800
vtail_sweep=0.000
vtail_pos_lon=-28.800
vtail_pos_vert=1.500
elevator_area=18.360
aileron_area=12.240
rudder_area=21.000
elevator_up_limit=28.000
elevator_down_limit=28.000
aileron_up_limit=25.000
aileron_down_limit=15.000
rudder_limit=24.000
elevator_trim_limit=19.500
spoiler_limit=20.000
spoilerons_available=0
aileron_to_spoileron_gain=1.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000
[Reference Speeds]
flaps_up_stall_speed=69.000
full_flaps_stall_speed=55.200
cruise_speed=213.000
max_indicated_speed=330.000000
max_mach=0.431006
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
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=0.000000
[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
[Flaps.0]
type=1
span-outboard=0.500
extending-time=4.700
system_type=0
damaging-speed=155.000
blowout-speed=160.000
lift_scalar=1.000
drag_scalar=2.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=20.000, 0.000
flaps-position.2=40.000, 0.000
[brakes]
toe_brakes_scale=0.640889
parking_brake=1
[gear_warning_system]
gear_warning_available=2
pct_throttle_limit=0.099976
flap_limit_power=20.053523
flap_limit_idle=13.178029
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
