[fltsim.0]
title=Aeroflot Yakovlev Yak-18T
sim=Yak-18T
model=D100NoC
panel=1
sound=
texture=1
checklists=
atc_id=81576
atc_airline=AEROFLOT
atc_flight_number=44486
ui_manufacturer=Yakovlev
ui_type=Yak- 18T
ui_variation=Aeroflot CCCP-81576
visual_damage=0
description=SM-92 aircraft in ROSTO livery
atc_heavy=0
atc_parking_codes=AVL
atc_parking_types=RAMP


[General]
performance=Maximum IAS: 300kph/162kts\nCruise IAS: 230kph/124kts\nRange: 1500km/810nm\nService Ceiling: 4000m/13100ft\nWingspan: 11.16m/36ft 7in\nLength: 8.35m/26ft 43in\nEngine: M-14P 360hp\nGross Weight: 1650kg/3637lbs\n\n
atc_type=YAKOVLEV
atc_model=YAK18

[forcefeedback]
gear_bump_nose_magnitude=5000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=5000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=5000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3000
ground_bumps_angle1=8900
ground_bumps_intercept1=4.0
ground_bumps_slope1=0.4
ground_bumps_magnitude2=600
ground_bumps_angle2=9100
ground_bumps_intercept2=1.0
ground_bumps_slope2=0.5
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000


[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


[WEIGHT_AND_BALANCE]
max_gross_weight=3636.0                              // (pounds)
empty_weight=2670.0
reference_datum_position=0.0, 0.0, 0.0               // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.0, 0.0, 0.0               // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=05
station_load.0=176.4,0.16,-0.92,0.33,Left Pilot
station_load.1=176.4,0.16,0.92,0.33,Right Pilot
station_load.2=176.4,-2.62,-0.92,0.33,Left Passenger
station_load.3=176.4,-2.62,0.92,0.33,Right Passenger
empty_weight_roll_MOI=2524.0
empty_weight_pitch_MOI=6862.0
empty_weight_yaw_MOI=2552.0
empty_weight_coupled_MOI=0.0


[pitot_static]
vertical_speed_time_constant=1.0              //Increasing this value will cause a more instantaneous reaction in the VSI


[fuel]
LeftMain=-0.89, -7.05, -1.12, 23.76, 1.72
RightMain=-0.89, 7.05, -1.12, 23.76, 1.72
fuel_type=1
number_of_tank_selectors=1
electric_pump=1


[airplane_geometry]
wing_area=202.0                 //Square feet
wing_span=36.583                //Feet
wing_root_chord=7.083           //Feet
wing_dihedral=5.43              //Degrees
wing_incidence=2.0              //Degrees
wing_twist=-1.0                 //Degrees
oswald_efficiency_factor=0.6    //Measure of lift effeciency of wing
wing_winglets_flag=0            //Are winglets available?
wing_sweep=0.0                  //Degrees, wing leading edge
wing_pos_apex_lon=0.0           //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0          //Feet, vertical distance from reference point, positive going up
htail_area=35.0                 //Square feet
htail_span=12.0                 //Feet
htail_pos_lon=-17.5             //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0              //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0             //Degrees
htail_sweep=0.0                 //Degrees, horizontal tail leading edge
vtail_area=18.0                 //Square feet
vtail_span=5.348                //Feet, tip to body
vtail_sweep=0.0                 //Degrees, vertical tail leading edge
vtail_pos_lon=-16.5             //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=1.5              //Feet, vertical distance from reference point, positive going up
elevator_area=15.05             //Square feet
aileron_area=20.64              //Square feet
rudder_area=10.5565             //Square feet
elevator_up_limit=25.5          //Degrees
elevator_down_limit=23.5        //Degrees
aileron_up_limit=22.0           //Degrees
aileron_down_limit=15.0         //Degrees
rudder_limit=27.01              //Degrees
elevator_trim_limit=23.3        //Degrees
spoiler_limit=0                 //Degrees
spoilerons_available=0          //Spoilerons Available?
aileron_to_spoileron_gain=0.0   //Aileron to spoileron gain
min_ailerons_for_spoilerons=0.0 //Degrees
min_flaps_for_spoilerons=0.0    //Minimum flap handle position when spoilerons activate


[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage=24.0
generator_alternator_voltage=28.5
max_generator_alternator_amps=100.0
electric_always_available=1
avionics=0,0.1,24.0
pitot_heat=0,0.1,24.0
additional_system=0,0.1,24.0
marker_beacon=0,0.1,24.0
gear_warning=0,0.1,24.0
fuel_pump=0,0.1,24.0
starter1=0,0.1,24.0
light_nav=0,0.1,24.0
light_landing=0,0.1,24.0
light_taxi=0,0.1,24.0
light_strobe=0,0.1,24.0
light_panel=0,0.1,24.0


[contact_points]
point.0=1, 5.15, 0.0, -5.01, 900.0, 0, 0.66, 0.0, 0.2, 2.2, 0.6, 5.0, 5.0, 0.0, 135.0, 140.0
point.1=1, -1.36, -4.82, -4.95, 1200.0, 1, 0.82, 0.0, 0.3, 2.5, 0.7, 5.2, 4.8, 2.0, 135.0, 140.0
point.2=1, -1.36, 4.82, -4.95, 1200.0, 2, 0.82, 0.0, 0.3, 2.5, 0.7, 4.8, 5.2, 3.0, 135.0, 140.0
point.3=2, -0.2, -18.11, 0.1, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -0.2, 18.11, 0.1, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -16.25, 0.0, -0.049, 1200.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 7.84, 0.0, -3.87, 196.8, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
max_number_of_points=21
static_pitch=2.0
static_cg_height=4.4
gear_system_type=0


[GeneralEngineData]
engine_type=0                                   //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=5.74, 0.0, 0.0                         //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0                            //Fuel flow scalar
min_throttle_limit=0.100000


[piston_engine]
power_scalar=1.0                                //Piston power scalar
cylinder_displacement=95.75                     //Cubic inches per cylinder
compression_ratio=6.4                           //Compression ratio
number_of_cylinders=9                           //Number of cylinders
max_rated_rpm=2918                              //Max rated RPM
max_rated_hp=360                                //Max rated HP
fuel_metering_type=2                            //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type=0                                  //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.35                  //Starter torque factor
turbocharged=1                                  //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=34.8                              //Max design manifold pressure, (inHg)
min_design_mp=0.0                               //Min design manifold pressure, (inHg)
critical_altitude=9800.0                        //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0                          //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_gain_offset=0.0                 //Multiplier on manifold pressure due to emergency boost
emergency_boost_mp_offset=0.0                   //Additional manifold pressure supplied by emergency boost
fuel_air_auto_mixture=0                         //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0                                 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0        //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0       //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0                     //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0                    //Scalar on idle RPM friction


[propeller]
thrust_scalar=1.0
propeller_type=0
propeller_diameter=7.874
propeller_blades=2
propeller_moi=3.7
beta_max=34.5
beta_min=14.5
min_gov_rpm=1200.0
prop_tc=0.02
gear_reduction_ratio=1.0
fixed_pitch_beta=0.0
low_speed_theory_limit=80.0
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.0
beta_feather=0.0
power_absorbed_cf=0.0
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=14.5
minimum_reverse_beta=14.5


[Reference_Speeds]
flaps_up_stall_speed=66.4
full_flaps_stall_speed=61.6
cruise_speed=124.19
max_indicated_speed=183.6


[keyboard]
elevator=180,250
aileron=180,250
rudder=180,250


[Views]
eyepoint=-0.16,-0.92,2.12


[autopilot]
autopilot_available=0
flight_director_available=0
default_vertical_speed=700.0
autothrottle_available=0
use_no_default_pitch=1
use_no_default_bank=1
pitch_takeoff_ga=8.0


[direction_indicators]
direction_indicator.0=2,0


[Flaps.0]
type=1
span-outboard=0.35
extending-time=3.000
flaps-position.0=0.0
flaps-position.1=50.0
damaging-speed=135.0
blowout-speed=140.0
lift_scalar=1.0
drag_scalar=0.4
pitch_scalar=1.0
system_type=2


[exits]
number_of_exits=1
exit_rate.0=0.33


[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=2,-16.077,0.0,5.48,fx_beaconh
light.1=4,-0.34,0.0,2.85,fx_vclight
light.2=4,-0.345,0.0,2.85,fx_vclight
light.3=4,-0.35,0.0,2.85,fx_vclight
light.4=4,2.165,0.0,1.608,fx_vclight
light.5=4,2.159,-1.171,1.483,fx_vclight
light.6=4,2.159,1.171,1.483,fx_vclight
light.7=4,1.969,-1.28,0.984,fx_vclight
light.8=4,1.969,1.28,0.984,fx_vclight


[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1,0
Com.2=0,0
Nav.1=0,0,0
Nav.2=0,0,0
Adf.1=1
Transponder.1=0
Marker.1=1


[smokesystem]
smoke.0=-2.36,0.0,-1.87,fx_smoke_w


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


[keyboard_response]
elevator=55.0,85.0
aileron=55.0,85.0
rudder=55.0,85.0


[brakes]
toe_brakes_scale=2.0
parking_brake=1
differential_braking_scale=1


[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.0
flap_limit_power=0.0
flap_limit_idle=0.0


[hydraulic_system]
normal_pressure=0.0


[stall_warning]
type=1


[attitude_indicators]
attitude_indicator.0=1


[turn_indicators]
turn_indicator.0=1,0


[Reference Speeds]
flaps_up_stall_speed=70.000000
full_flaps_stall_speed=56.000000
cruise_speed=151.093736
max_indicated_speed=185.000000