[fltsim.0]
title=Yak40 UT AIR
sim=Yak40v5
model=
panel=
sound=
texture=
checklists=
kb_checklists=Yak-40_check
kb_reference=Yak-40_ref
atc_airline=
atc_id=UT AIR
atc_flight_number=
ui_manufacturer=Yakovlev
ui_type=Yak-40
ui_variation=UT AIR
description=First flown on October 8th 1966, the Yak-40 commuter was designed to operate from small airport with minimum external assistance on the ground, 1011 aircrafts were built, 125 were sold to foreign countries, some of them in VIP version.\n
atc_parking_types=RAMP,GATE,CARGO
atc_parking_codes=UTA


[General]
performance=Passengers   27\nCrew             2\nCruise Speed     510 km\/h\nCruise altitude    6000 m\nRange               1500 km\nLenght         20.36 m\nWingspan    25.0 m\nHeight           6.5 m\nEngines : 3x Ivchenko AI-25 (3x1120kgs)\nTakeoff runway     715m\nLanding runway     550-750m\n\nDynamics by Andrew Sheyback\n
atc_type=YAKOVLEV
atc_model=YAK40

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

[WEIGHT_AND_BALANCE]
max_gross_weight = 38069.325
empty_weight = 21928.725

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = -2.000, 0.000, 0.000

max_number_of_stations = 50

station_load.0  = "353, 20.0,  0.0, 0.0, Crew (2x80kg)"        // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1  = "441, 0.0,  0.0, 0.0,  Equipment 200kg"        // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2  = "0, -2.0,  0.0, 0.0, Pass (22x80kg)"        // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.2  = "0, -2.0,  0.0, 0.0, Pass (27x80kg)"        // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3  = "0, -10.0,  0.0, 0.0, Bagg (22x10kg) +5kg"        // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
//empty_weight_pitch_MOI= 180439.000
//empty_weight_roll_MOI= 180183.000
//empty_weight_yaw_MOI= 130024.000
empty_weight_pitch_MOI= 120803.000
empty_weight_roll_MOI= 79042.000
empty_weight_yaw_MOI= 157851.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar=2.500
parasite_drag_scalar=1.800
induced_drag_scalar=1.000
elevator_effectiveness=0.40
aileron_effectiveness=3.00
rudder_effectiveness=1.00
pitch_stability=1.00
roll_stability=1.00
yaw_stability=1.00
elevator_trim_effectiveness=2.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
hi_alpha_on_roll=3.0	 

[GeneralEngineData]
engine_type= 1
Engine.0 = -14.800, -5.800, 0.600
Engine.1 = -22.800, 0.000, 1.800
Engine.2 = -14.800, 5.800, 0.600
fuel_flow_scalar= 1.700
min_throttle_limit=-0.500000

[TurbineEngineData]
fuel_flow_gain= 0.0015
//inlet_area= 8.000
inlet_area= 8.000
rated_N2_rpm= 29920.000
static_thrust= 3550.000
afterburner_available= 0
reverser_available= 1

[jet_engine]
thrust_scalar=1.000

[electrical]
max_battery_voltage = 27.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 400.0
electric_always_available=0

;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 24.0
gear_motor=0, 5 , 24.0
autopilot=0, 5 , 24.0
avionics_bus=0, 10, 20.0
avionics=1, 5 , 20.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 20.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 24.0
starter1=0, 20, 24.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 24.0
light_taxi=0, 5 , 24.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 20.0

//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]
// denokan model
point.0=1, 24.66,0.00,-8.1,  3800,  0, 1.00, 45, 0.4, 2.5,  0.8, 10.0, 10.20, 0, 220,250
point.1=1, -4.58,-8.7,-9.0,  3900,  1, 1.47, 0,  0.8,  1.25,  0.5, 12.2, 12.80, 2, 220,250
point.2=1, -4.58,8.7,-9.0,   3900,  2, 1.47, 0,  0.8,  1.25,  0.5, 12.8, 12.20, 3, 220,250
point.3= 2.000, 0.830, -40.000, -1.000, 787.400, 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, 0.830, 40.000, -1.000, 787.400, 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, -15.170, 0.000, -3.000, 787.400, 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, 28.470, 0.000, -4.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch=-0.0
static_cg_height=8.0
gear_system_type=1



[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


[SMOKESYSTEM]
smoke.0=-14.90,0.0,4.0,fx_smoke_rw
smoke.1=-14.90,0.0,-4.0,fx_smoke_rw
smoke.2=-15.90,0.5,0.0,fx_smoke_rw

[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, 250
aileron=150, 250
rudder=150, 250

[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

[exits]
number_of_exits=1
exit_rate.0=0.3                               ;Percent per second

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_m
windshield_rain_effect_available = 1            //Do draw rain on this windshield

[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 30.0
autothrottle_available= 0
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8
use_no_default_bank=1
use_no_default_pitch=1
default_bank_mode=0
default_pitch_mode=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=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

[fuel]
LeftMain= -5.000, -17.000, 0.000, 723.900, 17.820
RightMain= -5.000, 17.000, 0.000, 723.900, 17.820
//LeftAux= -5.000, -20.000, 0.000, 263.250, 0.000
//RightAux= -5.000, 20.000, 0.000, 263.250, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
                   

[airplane_geometry]
wing_area= 280.000
wing_span= 82.100
wing_root_chord= 10.000
wing_dihedral= 5.000
wing_incidence= 3.000
wing_twist= -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 42.700
htail_span= 33.000
htail_pos_lon= -50.000
htail_pos_vert= 13.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 32.800
vtail_span= 16.000
vtail_sweep= 35.000
vtail_pos_lon= -30.500
vtail_pos_vert= 8.000
elevator_area= 16.000
aileron_area= 12.100
rudder_area= 8.600
elevator_up_limit= 25.000
elevator_down_limit= 25.000
aileron_up_limit= 10.000
aileron_down_limit= 15.000
rudder_limit= 30.000
elevator_trim_limit= 6.000
spoiler_limit= 60.000
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= 129.000
full_flaps_stall_speed= 101.000
cruise_speed= 270.000
max_indicated_speed=320.000000
max_mach=0.700000

[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= 0.800
extending-time= 17.500
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.700
drag_scalar= 3.000
pitch_scalar= 3.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 35.000, 0.000


[brakes]
toe_brakes_scale=0.5
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.061035
flap_limit_power=25.496622
flap_limit_idle=5.042029

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=2600.000000

[stall_warning]
type=2

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[Views]
//eyepoint=0.8, -1.709736,2.409367
eyepoint=23.2, -1.6, 2.35

[LIGHTS]        
// Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -0.20, -41.0, 0.9, fx_navred 
light.1=3, -0.20, 41.0, 0.9, fx_navgre
light.2=1, -26.3, 0.00, 13.6, fx_beaconb 
light.3=1, -7.7, 0.00, -4.0, fx_beacon 
//light.4=4,  24.00,   0.00,  2.25, fx_vclight,
light.4=4,  23.50,   0.00,  0.20, fx_vclight,
light.5=10,  23.00,   -1.70,  2.00, fx_vclightwhi,
light.6=10,  23.00,   1.70,  2.00, fx_vclightwhi,
light.7=4,  16.00,   0.00,  2.25, fx_vclighth,
light.8=4,  -1.00,   0.00,  2.25, fx_vclighth,