[fltsim.0]
title=cubana Yak-40
sim=Yak40v4
model=
panel=
sound=
texture=
checklists=
atc_airline=cubana new colors
atc_id=cubana40
atc_flight_number=450
ui_manufacturer=Yakovlev
ui_type=Yakolev 40
ui_variation=Cubana new Paint
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, Original aircraft y D.Samborski,re-paint by George Perez
atc_heavy=0
[fltsim.1]
title=cubana Yak-40d
sim=Yak40v4
model=
panel=
sound=
texture=1
checklists=
atc_airline=cubana
atc_id=cubana40
atc_flight_number=450
ui_manufacturer=Yakovlev
ui_type=Yakolev 40
ui_variation=Cubana
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, aircraft by D.Samborski,re-paint by George Perez
atc_heavy=0
[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\nsamdim@chez.com \nPanel by Mathias Liebkrecht\n\nFlight dynamics is from Avro RJ85 model. Credits...\n
atc_type=
atc_model=
[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= -17.000, 0.000, 1.000
fuel_flow_scalar= 1.000
Engine.2= -15.000, 9.100, 1.500
min_throttle_limit=-0.250000
[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= 1.000, 21.667, 0.000, -9.500, 1400.000, 0.000, 0.750, 70.000, 0.700, 1.800, 0.949, 4.000, 4.200, 0.000, 0.000, 0.000
point.1= 1.000, -4.583, -8.700, -10.900, 1850.000, 1.000, 1.070, 0.000, 1.700, 1.100, 0.830, 5.500, 5.700, 2.000, 0.000, 0.000
point.2= 1.000, -4.583, 8.700, -10.900, 1850.000, 2.000, 1.070, 0.000, 1.700, 1.100, 0.830, 5.500, 5.700, 3.000, 0.000, 0.000
point.3= 2.000, -14.167, -47.333, 0.000, 787.402, 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, -14.167, 47.333, 0.000, 787.402, 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, -26.000, 0.000, 2.833, 787.402, 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, 26.667, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 0.494
static_cg_height= 8.911
gear_system_type=0
[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;
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
[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
electric_pump=0
[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
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= 0.700
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
[brakes]
toe_brakes_scale=0.885037
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=1,1,1,0
normal_pressure=3000.000000
[stall_warning]
type=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
