[fltsim.0]
title=Yak40 Aeroflot
sim=Yak40v4
model=
panel=
sound=
texture=
checklists=
atc_airline=Aeroflot
atc_id=
atc_flight_number=450
ui_manufacturer=Yakovlev
ui_type=Yak-40
ui_variation=Aeroflot
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

[fltsim.1]
title=Yak40 Business Jet
sim=Yak40v4
model=
panel=
sound=
texture=biz
checklists=
atc_airline=Business Jet
atc_id=
atc_flight_number=550
ui_manufacturer=Yakovlev
ui_type=Yak-40
ui_variation=Samara
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


[General]
performance=Passengers   32\nCrew             2\nCruise Speed     510 km\/h\nCruise altitude    8100 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\nModel and painting by Samdim  © 2002\[email protected] \nPanel by Mathias Liebkrecht\n\nFlight dynamics is from Avro RJ85 model. Credits...\n
[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= 88000.000
empty_weight= 49985.000

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

max_number_of_stations=50

station_load.0= 19000.000, 0.000, 0.000, 0.000

;Moments of Inertia
empty_weight_pitch_MOI= 1872439.000
empty_weight_roll_MOI= 1262183.000
empty_weight_yaw_MOI= 1737024.000
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=1.000
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

[GeneralEngineData]
engine_type= 1
Engine.0= -15.000, -9.100, 1.500
Engine.1= -15.000, 9.100, 1.500
fuel_flow_scalar= 1.000

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 13.000
rated_N2_rpm= 29920.000
static_thrust= 13850.000
afterburner_available= 0
reverser_available= 1

[jet_engine]
thrust_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=0, 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=1.000000,21.666667,0.000000,-9.50000, 1400, 0.000000,0.75,70, 0.7, 1.80,0.948932,4.0,4.20,0.000000,0.000000,0.000000
point.1=1.000000,-4.583333,-8.7,-10.9,1850, 1.000000,1.07,0.000,1.7,1.100000,0.829880,5.5,5.70,2.000000,0.000000,0.000000
point.2=1.000000,-4.583333,8.7,-10.9, 1850, 2.000000,1.07,0.000,1.7,1.100000,0.829880,5.5,5.70,3.000000,0.000000,0.000000
point.3=2.000000,-14.166667,-47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-14.166667,47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-26.00000,0.000000,2.833333,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,26.666667,0.000000,-3.750000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.494385
static_cg_height=8.911109

[Views]
eyepoint=-2,-1.409736,2.409367

[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

[LIGHTS]        
// Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, 0.94, -41.38, -0.12, fx_navredh 
light.1=3, 0.94, 41.38, -0.12, fx_navgreh
light.2=1, -24.27, 0.00, 13.31, fx_beaconb 
light.4=3, -28.45, 0.00, 3.69, fx_navwhih
[SMOKESYSTEM]
smoke.0=-14.90,0.0,4.0,fx_smoke_rx
smoke.1=-14.90,0.0,-4.0,fx_smoke_rx
smoke.2=-15.90,0.5,0.0,fx_smoke_rx

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

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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;

[fuel]
Center1= 0.000, 0.000, 0.000, 900.000, 0.000
LeftMain= -5.000, -17.000, 0.000, 1100.000, 0.000
RightMain= -5.000, 17.000, 0.000, 1100.000, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
                   

[airplane_geometry]
wing_area= 1006.400
wing_span= 92.100
wing_root_chord= 12.000
wing_dihedral= 2.000
wing_incidence= 0.500
wing_twist= -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag= 0
wing_sweep= 20.000
wing_pos_apex_lon= 7.000
wing_pos_apex_vert= 0.000
htail_area= 150.000
htail_span= 33.000
htail_pos_lon= -42.000
htail_pos_vert= 13.000
htail_incidence= 0.000
htail_sweep= 30.000
vtail_area= 138.000
vtail_span= 16.000
vtail_sweep= 35.000
vtail_pos_lon= -36.500
vtail_pos_vert= 8.000
elevator_area= 59.000
aileron_area= 22.000
rudder_area= 54.000
elevator_up_limit= 22.000
elevator_down_limit= 19.000
aileron_up_limit= 20.000
aileron_down_limit= 20.000
rudder_limit= 28.000
elevator_trim_limit= 19.000
spoiler_limit= 60.000
spoilerons_available= 1
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= 440.000

[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= 0.700
extending-time= 12.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.750
drag_scalar= 1.200
pitch_scalar= 1.200
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 5.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 30.000, 0.000
flaps-position.5= 40.000, 0.000

[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 7.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.300
drag_scalar= 0.500
pitch_scalar= 0.300
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.500, 0.000
flaps-position.3= 0.500, 0.000
flaps-position.4= 1.000, 0.000
flaps-position.5= 1.700, 0.000