[fltsim.0]
title=NAMC YS-11A - 309 A.L.A. (1969)
sim=Ys11ala
model=
panel=
sound=
texture=
checklists=
description=Aerotransportes Litoral Argentino NAMC\nYS-11A-309 c\/n 2086 as it looked in\n1969
ui_manufacturer=NAMC
ui_type=YS-11
ui_variation=Aerotransportes Litoral Argentino (1969)
atc_heavy=0
atc_id=LV-JII
atc_airline=ALA
atc_flight_number=

[General]
performance=Length:26.3 m\nWing span:32.0 m\nWeight:15,462 kg\nPower:RR Dart Mk542  3,060 shp\na\n
atc_type=NAMC
atc_model=YS11

[WEIGHT_AND_BALANCE]
max_gross_weight=55111.000
empty_weight=33000.000

reference_datum_position=36.489, 0.000, 0.000
empty_weight_CG_position=-36.750, 0.000, 2.000
max_number_of_stations=50

station_load.0=8500.000, -36.750, 0.000, 2.000

;Moments of Inertia
empty_weight_pitch_MOI=268022.000
empty_weight_roll_MOI=227153.000
empty_weight_yaw_MOI=579108.000
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=0.600
aileron_effectiveness=1.000
rudder_effectiveness=1.100
pitch_stability=1.250
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=-25.700, -14.000, 2.500
Engine.1=-25.700, 14.000, 2.500
fuel_flow_scalar=0.425

[propeller]
thrust_scalar=0.600
propeller_type=0
propeller_diameter=14.740
propeller_blades=4
propeller_moi=112.000
beta_max=27.500
beta_min=14.000
min_gov_rpm=600.000
prop_tc=0.09

gear_reduction_ratio=12.900
fixed_pitch_beta=3.000
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=50.000
beta_feather=84.000
power_absorbed_cf=1.00
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=1.500
minimum_reverse_beta=-14.000

[TurbineEngineData]
fuel_flow_gain=0.011
inlet_area=3.900
rated_N2_rpm=15000.000
static_thrust=637.000
afterburner_available=0

[turboprop_engine]
power_scalar=1.70
maximum_torque=11560.000
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.0000
max_rpm_friction_scalar=1.2000
idle_rpm_friction_scalar=1.000

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=1, 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

//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=1.0, -13.579, 0.0, -6.2, 800.0, 0.000, 0.850, 75.000, 0.600, 1.100, 0.900, 6.000, 6.000, 0.000, 200.0, 220.0
point.1=1.0, -42.479, -14.0, -6.2, 1500.0, 1.0, 1.400, 0.000, 0.500, 1.100, 0.800, 3.000, 3.200, 2.000, 200.000, 220.2
point.2=1.0, -42.479, 14.0, -6.2, 1500.0, 2.0, 1.400, 0.000, 0.500, 1.100, 0.800, 3.000, 3.300, 3.000, 200.0, 220.000
point.3=2.000, -36.400, -52.500, 3.000, 1200.0, 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, -36.400, 52.500, 3.000, 1200.0, 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, -72.690, 0.000, 0.000, 1200.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.6=2.000, -1.990, 0.000, -2.000, 1200.0, 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=0.000
static_cg_height=6.300

[Views]
eyepoint=-7.3, -1.82, 5.0    //(feet) longitudinal, lateral, vertical distance from reference datum

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI


[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -38.489,  52.30,  4.50, fx_navgrem ,
light.1=3, -38.489, -52.30,  4.50, fx_navredm ,
light.2=4, -10.589,    0.00,  4.50, fx_vclighth ,
light.3=1, -38.389,   0.00,  8.60, fx_beaconh ,
light.4=1, -60.289,   0.00,  -1.6, fx_beaconb ,
light.5=3, -84.989,   0.00,  5.72, fx_navwhih ,


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

[fuel]
Center1=-35.750, 0.000, 0.000, 220.000, 3.000
Center2=-35.750, 0.000, 0.000, 357.000, 3.000
LeftMain=-35.750, -9.600, 0.000, 662.500, 3.000
RightMain=-35.750, 9.600, 0.000, 662.500, 3.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1


[airplane_geometry]
wing_area=1020.420
wing_span=105.000
wing_root_chord=13.800
wing_dihedral=6.320
wing_incidence=1.000
wing_twist=0.000
oswald_efficiency_factor=0.750
wing_winglets_flag=0
wing_sweep=3.000
wing_pos_apex_lon=-32.000
wing_pos_apex_vert=0.000
htail_area=245.890
htail_span=36.880
htail_pos_lon=-74.250
htail_pos_vert=7.040
htail_incidence=4.000
htail_sweep=15.640
vtail_area=156.076
vtail_span=28.800
vtail_sweep=38.000
vtail_pos_lon=68.500
vtail_pos_vert=8.960
elevator_area=64.000
aileron_area=46.000
rudder_area=63.000
elevator_up_limit=20.000
elevator_down_limit=20.000
aileron_up_limit=25.000
aileron_down_limit=25.000
rudder_limit=25.000
elevator_trim_limit=17.000
spoiler_limit=95.000
spoilerons_available=0
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=10.000
min_flaps_for_spoilerons=0.000

[Reference Speeds]
flaps_up_stall_speed=100.000
full_flaps_stall_speed=85.000
cruise_speed=190.000

[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=150.0, 250.0
aileron=150.0, 250.0
rudder=150.0, 250.0

[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=1
pitch_takeoff_ga=8;
use_no_default_pitch=1
use_no_default_bank=1

[Radios]
// Radio Type=available, 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

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.2                               ;Percent per second

[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

[direction_indicators]
direction_indicator.0=3,0

[Flaps.0]
type=1
span-outboard=0.280
extending-time=15.000
system_type=1
damaging-speed=200.000
blowout-speed=220.000
lift_scalar=0.540
drag_scalar=0.900
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=10.000, 0.000
flaps-position.2=15.000, 0.000
flaps-position.3=20.000, 0.000
flaps-position.4=25.000, 0.000
flaps-position.5=35.000, 0.000

[Flaps.1]
type=1
span-outboard=0.280
extending-time=15.000
system_type=1
damaging-speed=200.000
blowout-speed=220.000
lift_scalar=0.540
drag_scalar=0.900
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=10.000, 0.000
flaps-position.2=15.000, 0.000
flaps-position.3=20.000, 0.000
flaps-position.4=25.000, 0.000
flaps-position.5=35.000, 0.000


[SMOKESYSTEM]
Smoke.0= 2.500, -25.700, -14.000, fx_smoke_rx
Smoke.1=-2.500, -25.700,  14.000, fx_smoke_rx