[fltsim.0]
title=EMBTUC
sim=EMBTUC
model=
panel=
sound=
texture=
kb_checklists=
description=FS2002/2004 Embraer EMB-312 Tucano FAA. Model by JRLucariny.\nTextures by Carlos José LAGIOIA. Quilmes, Buenos Aires. Argentina.
ui_manufacturer=EMBRAER
ui_type=EMB-312 TUCANO T-27 FAA
ui_variation=Fuerza Aérea Argentina
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
[General]
atc_type=
atc_model=
editable=1
performance=Origin: Brazil \nType: two-seat basic trainer \nMax Speed: 242kt \/ 278 mph \nMax Range range 1944 km \/ 1,146 miles \nDimensions: span 11.14 m \/ 36 ft 6.6 in\nlength 9.86 m \/ 32 ft 4.2 in\nheight 3.40 m \/ 11 ft 1.9 in \nWeight: empty 1810 kg \/ 3,990 Ib\nmax. take-off 3175 kg \/ 7,000 Ib \nPowerplant: one 559-kW (750-shp) Pratt & Whitney Canada PT6A-25C turboprop \nArmament: provision for up to 1000 kg (2,205 Ib) of disposable stores carried on four underwing hardpoints, and generally comprising 113-kg (250-lb) bombs, Avibras rocket-launcher pods, machine-gun pods, practice bombs etc \nOperators: Argentina, Brazil, Colombia, Egypt, France, Honduras, Iran, Kenya, Kuwait, Paraguay, Peru, United Kingdom, Venezuela \n
[SMOKESYSTEM]
smoke.0=-0.52, -10.02, 3.09, fx_smoke_w
smoke.1=-0.52, -12.02, 3.09, fx_smoke_w
smoke.2=-0.52, -14.02, 3.09, fx_smoke_w
[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
;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
station_load.0=0.000000,0.000000,0.000000,0.000000
[flight_tuning]
cruise_lift_scalar=0.752
parasite_drag_scalar=0.490
induced_drag_scalar=1.202
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=-2.400, 0.000, 0.000
fuel_flow_scalar=1.120
min_throttle_limit=-0.250000
[propeller]
thrust_scalar=1.202
propeller_type=0
propeller_diameter=8.500
propeller_blades=4
propeller_moi=19.000
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=158.000
afterburner_available=0
[turboprop_engine]
power_scalar=1.000
maximum_torque=1865.000
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, 1, 1
Nav.2=1, 1, 0
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, -9.850, 0.000, -4.950, 1500.000, 0.000, 0.580, 45.000, 0.300, 2.500, 0.700, 5.000, 5.000, 0.000, 0.000, 0.000
point.1=1.000, -17.500, -6.080, -5.100, 2500.000, 1.000, 0.845, 0.000, 0.300, 2.500, 0.700, 5.000, 7.000, 2.000, 0.000, 0.000
point.2=1.000, -17.500, 6.080, -5.100, 2500.000, 2.000, 0.845, 0.000, 0.300, 2.500, 0.700, 5.000, 6.000, 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=0.590
static_cg_height=5.100
gear_system_type=1
[Views]
eyepoint=-15.0, 0.0, 2.25 //(feet) longitudinal, lateral, vertical distance from reference datum
[fuel]
LeftMain=-18.400, -1.100, 2.500, 79.166, 3.600
RightMain=-18.400, 1.100, 2.500, 79.166, 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
[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=80.000
full_flaps_stall_speed=65.000
cruise_speed=260.000
max_indicated_speed=324.718750
max_mach=1.000000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2000.0
autothrottle_available=0
pitch_takeoff_ga=8.000
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
