[fltsim.0]
title=AI Yak-42 Blank
sim=Yak_42
model=
texture=
atc_airline=TEST
ui_manufacturer=AI CasioDesign
ui_type=Yakovlev Yak-42
ui_variation=Blank
description=Yakovlev 42\nEngine Type: General Electric CF34-8E\nModel Designer Carl Selin\nFlight Dynamics Designer Carl Selin & John Cillis\nTexture Designer Tommy Hansson\nTechnical Resource Rui Cristina\nSound Albert Ramic\nTest flown by Dream Wings members
atc_parking_types=GATE
atc_parking_codes=
[fltsim.1]
title=AI Yak-42 Aeroflot USSR 90
sim=Yak_42
model=
texture=USSR
atc_airline=Aeroflot
ui_manufacturer=AI CasioDesign
ui_type=Yakovlev Yak-42
ui_variation=Aeroalot 90
description=Yakovlev 42\nEngine Type: General Electric CF34-8E\nModel Designer Carl Selin\nFlight Dynamics Designer Carl Selin & John Cillis\nTexture Designer Tommy Hansson\nTechnical Resource Rui Cristina\nSound Albert Ramic\nTest flown by Dream Wings members
atc_parking_types=GATE
atc_parking_codes=AFL
[General]
performance=Maximum Cruise Speed: mach 0.80, Passangers: 70, Range: 2000 nm
atc_type=YAKOVLEV
atc_model=YAK42
editable=1
[pitot_static]
vertical_speed_time_constant=1
[WEIGHT_AND_BALANCE]
max_gross_weight=82012.000
empty_weight=46165.000
reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=8
//Weight-Fore/AFT-Right/Left-Up/Down
//Cabin
station_load.0=2096.000000,20.000000,-3.000000,4.000000 //FWD Left
station_load.1=2096.000000,20.000000,3.000000,4.000000 //FWD Right
station_load.2=2096.000000,0.000000,-3.000000,4.000000 //Center Left
station_load.3=2096.000000,0.000000,3.000000,4.000000 //Center Right
station_load.4=2096.000000,-15.000000,-3.000000,4.000000 //Rear Left
station_load.5=2096.000000,-15.000000,3.000000,4.000000 //Rear Right
//Baggage Cmpt
station_load.6=1194.000000,20.000000,0.000000,-2.000000 //FWD
station_load.7=1194.000000,-15.000000,0.000000,-2.000000 //Rear
;Moments of Inertia
empty_weight_pitch_MOI=2172439.000
empty_weight_roll_MOI=2262183.000
empty_weight_yaw_MOI=2337024.000
empty_weight_coupled_MOI=1300.000
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=2.000
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=4.750, -16.100, -2.500
Engine.1=4.750, 16.100, -2.500
fuel_flow_scalar=1.000000
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=17.75
static_thrust=14200.000000
afterburner_available=0
reverser_available=1
rated_N2_rpm=29920.000000
[jet_engine]
thrust_scalar=1.000
[electrical]
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
[contact_points]
//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
//point.0= 1.000, 36.500, 0.000, -10.200, 1574.000, 0.000, 1.500, 56.000, 0.355, 2.500, 0.595, 5.000, 5.000, 0.000, 0.000, 0.000
//point.1= 1.000, -4.000, -10.000, -10.300, 1574.000, 1.000, 1.500, 0.000, 0.355, 2.500, 0.595, 5.000, 5.000, 2.000, 0.000, 0.000
//point.2= 1.000, -4.000, 10.000, -10.300, 1574.000, 2.000, 1.500, 0.000, 0.355, 2.500, 0.595, 5.000, 5.000, 3.000, 0.000, 0.000
point.0 = 1, 43.7122, 0, -9.40, 1574, 0, 1.5, 56, 0.355, 2.5, 0.595, 5, 5, 0, 0, 0
point.1 = 1, -3.7283, -10, -9.55, 1574, 1, 1.5, 0, 0.355, 2.5, 0.595, 5, 5, 2, 0, 0
point.2 = 1, -7.4632, -10, -9.55, 1574, 2, 1.5, 0, 0.355, 2.5, 0.595, 5, 5, 2, 0, 0
point.3 = 1, -3.7283, 10, -9.55, 1574, 1, 1.5, 0, 0.355, 2.5, 0.595, 5, 5, 3, 0, 0
point.4 = 1, -7.4632, 10, -9.55, 1574, 2, 1.5, 0, 0.355, 2.5, 0.595, 5, 5, 3, 0, 0
static_pitch=0.000
static_cg_height=9.796
gear_system_type=1
[gear_warning_system]
gear_warning_available=1 //Normal
pct_throttle_limit=0.1 //Percent throttle that activates warning
flap_limit_idle=5.0 //Flap angle that activates warning at idle
flap_limit_power=25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake=1 //Parking brake available
toe_brakes_scale=0.885 //Brake scalar
[hydraulic_system]
normal_pressure=3000.0 //PSI
electric_pumps=0 //no electric pumps
engine_map=1,1,0,0 //pumps on Eng1,2
[Flaps.0]
type=1
span-outboard=0.800
extending-time=20.000
system_type=1
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=5.000, 0.000
flaps-position.2=10.000, 0.000
flaps-position.3=20.000, 0.000
flaps-position.4=35.000, 0.000
[Flaps.1]
type=2
span-outboard=0.800
extending-time=2.000
system_type=1
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=1.000, 0.000
[Flaps.2]
type=2
span-outboard=0.800
extending-time=3.000
system_type=1
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=0.500, 0.000
flaps-position.2=1.000, 0.000
[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
Transponder.1=1
Marker.1=1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -15.45, -55.55, -1.87, fx_navredh
light.1 = 3, -15.45, 55.55, -1.87, fx_navgreh
light.2 = 4, 48.68, 0, 6.29, fx_vclighth
light.3 = 2, -47.68, 0, 6.39, fx_strobeh
light.4 = 2, 10.30, 0, -4.13, fx_beaconb
light.5 = 1, 21.90, 0, 8.50, fx_beaconh
light.6 = 2, -18.6, 10.1, 4.2, fx_nicksmokeAI_lrglear-MD-7x
light.7 = 2, -18.6, -10.1, 4.2, fx_nicksmokeAI_lrglear-MD-7x
light.8 = 2, -40.88, 0, 2.91, fx_nicksmokeAI_lrglear-MD-7x
[Views]
eyepoint=40, -1.31, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
[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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.1 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 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=1.0
use_no_default_pitch=1
default_pitch_mode=0
[fuel]
Center1=0.000, 0.000, 0.000, 1317.000, 0.000
LeftMain=-3.000, -19.000, 0.000, 900.000, 0.000
RightMain=-3.000, 19.000, 0.000, 900.000, 0.000
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=750.000
wing_span=85.750
wing_root_chord=16.000
wing_dihedral=6.200
wing_incidence=1.000
wing_twist=-0.500
oswald_efficiency_factor=0.750
wing_winglets_flag=0
wing_sweep=25.000
wing_pos_apex_lon=8.000
wing_pos_apex_vert=0.000
htail_area=260.000
htail_span=32.700
htail_pos_lon=-35.000
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=30.000
vtail_area=150.000
vtail_span=17.000
vtail_sweep=35.000
vtail_pos_lon=-35.800
vtail_pos_vert=5.800
elevator_area=70.500
aileron_area=26.900
rudder_area=56.200
elevator_up_limit=22.500
elevator_down_limit=19.500
aileron_up_limit=20.000
aileron_down_limit=20.000
rudder_limit=26.000
elevator_trim_limit=20.000
spoiler_limit=60.000
spoilerons_available=1
aileron_to_spoileron_gain=.5
min_ailerons_for_spoilerons=10.000
min_flaps_for_spoilerons=0.000
[Reference Speeds]
flaps_up_stall_speed=142.000
full_flaps_stall_speed=113.000
cruise_speed=477.000
max_indicated_speed=340.000000
max_mach=0.820020
[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
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0