[fltsim.0]
title=YAK12B
sim=YAK12
model=
panel=
[fltsim.0]
title=YAK12G
sim=YAK12
model=
panel=
sound=
texture=G
prop_anim_ratio=-1.75
description=Yak-12A for MSFS2004 created by Ilya Sheen V2.0
atc_id=13
atc_airline=DOSAAF-VVS
atc_flight_number=
ui_manufacturer=Yakovlev
ui_type=Yak-12
ui_variation=Green

[General]
performance=---------  Основные характеристики  ---------\nДвигатель поршневой АИ-14Р       260 л.с.\nМаксимальная скорость                  178 км/ч\nКрейсерская скорость                     140 kм/ч\nПрактический потолок                    4100 м\nВместимость топливных баков     125 л\nМаксимальная дальность полета  670 kм\nМасса пустого самолета                  1026 кг\nМаксимальная взлетная масса       1500 кг\nПолезная нагрузка                              476 кг\nДлина      9 м           Размах крыла     12.6 м\nВысота    3.12 м\nВместимость      1  пилот  и  3  пассажира\n---------------------------------------------------------
atc_type=Yakovlev
atc_model=YAK12A
editable = 0
visual_damage = 1

[pitot_static]
vertical_speed_time_constant = 2

[WEIGHT_AND_BALANCE]
max_gross_weight = 3300
empty_weight = 2257

reference_datum_position = 0, 0, 0
empty_weight_CG_position  = 0, 0, 0
CG_forward_limit = 0
CG_aft_limit = 1

max_number_of_stations = 6
station_load.0 = "170,  0.50, -1.30, -1.0, Pilot"
station_load.1 = "110,  0.50,  1.30, -1.0, Front Passenger"
station_load.2 = "0,   -5.50, -1.30, -1.0, L Rear Passanger"
station_load.3 = "0,   -5.50,  1.30, -1.0, R Rear Passanger"
station_load.4 = "177, -8.85,  0.50,  0.0, Cargo max 120kg"

empty_weight_pitch_MOI = 4175
empty_weight_roll_MOI = 3269
empty_weight_yaw_MOI = 5868
empty_weight_coupled_MOI = 0

[flight_tuning]
cruise_lift_scalar=1.1
hi_alpha_on_roll=1.05
hi_alpha_on_yaw=0.95

parasite_drag_scalar=0.92
induced_drag_scalar=0.85

elevator_effectiveness=1.25
aileron_effectiveness=1.0
rudder_effectiveness=0.2

pitch_stability=1.0
roll_stability=1.15
yaw_stability=1.0

elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

p_factor_on_yaw=1.0
torque_on_roll=1.0
gyro_precession_on_roll=1.1
gyro_precession_on_yaw=1.0

[GeneralEngineData]
engine_type = 0
Engine.0 = 7.437, 0, 0
fuel_flow_scalar = 0.670
min_throttle_limit=0.000000

[piston_engine]
power_scalar = 1.0
cylinder_displacement = 96.875
compression_ratio = 5.9
number_of_cylinders = 9
max_rated_rpm = 2350
max_rated_hp = 260
fuel_metering_type = 1
cooling_type = 0
normalized_starter_torque = 0.3
turbocharged = 1
max_design_mp = 32.0
min_design_mp = 1.0
critical_altitude = 5000
emergency_boost_type = 0
emergency_boost_mp_offset = 0
emergency_boost_gain_offset = 0
fuel_air_auto_mixture = 0
auto_ignition = 0
max_rpm_mechanical_efficiency_scalar = 1
idle_rpm_mechanical_efficiency_scalar = 1.5
max_rpm_friction_scalar = 1
idle_rpm_friction_scalar = 1

[propeller]
thrust_scalar = 1
propeller_type=0
propeller_diameter=9
propeller_blades=2
propeller_moi=30.0
//propeller_moi=6.75
beta_max=32
beta_min=20
min_gov_rpm=1350.000
prop_tc=0.02
gear_reduction_ratio=1.65
fixed_pitch_beta=20.000
low_speed_theory_limit=80.000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000
beta_feather=0.000
power_absorbed_cf=0.000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=20.000
minimum_reverse_beta=20.000
feathering_switches = 0

[contact_points]
max_number_of_points = 6
point.0 = 1, -18.928,   0,     -1.73, 1570.0,  0,  0.45,  180, 0.35,  1.6, 0.62, 0, 0, 0, 0, 0
point.1 = 1,   1.90,   -4.70,  -5.64, 3570.0,  1,  0.9,     0, 0.35,  1.8, 0.62, 0, 0, 2, 0, 0
point.2 = 1,   1.90,    4.70,  -5.64, 3570.0,  2,  0.9,     0, 0.35,  1.8, 0.62, 0, 0, 3, 0, 0
point.3 = 2,  -1.4,   -22.75,  2.881, 1574.8,  0,  0,       0, 0,     0,   0,    0, 0, 5
point.4 = 2,     0,    22.75,  2.881, 1574.8,  0,  0,       0, 0,     0,   0,    0, 0, 6
point.5 = 2,   7.419,   0,    -1.605, 1574.8,  0,  0,       0, 0,     0,   0,    0, 0, 4

static_pitch= 11.3
static_cg_height= 4.9
tailwheel_lock = 0

[Views]
eyepoint= -1.75, -0.8, 1.7

[Flaps.0]
type= 1
span-outboard= 0.62
extending-time= 2.5
system_type= 2
damaging-speed= 120.000
blowout-speed= 150.000
lift_scalar= 1.700
drag_scalar= 1.300
pitch_scalar= 1.200
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000


[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 50
electric_always_available = 0

avionics_bus =      0, 5, 17
avionics =          1, 5, 17
pitot_heat =        0, 3, 17
additional_system = 0, 2, 17
starter1 =          0, 8, 17
light_nav =         0, 4, 17
light_landing =     0, 5, 17
light_panel =       0, 2, 17

[keyboard_response]
elevator = 350, 500
aileron  = 450, 1000
rudder   = 200, 1000

[direction_indicators]
direction_indicator.0 = 1, 0

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

[LIGHTS]      
light.0 = 4, -0.2, 0.0, 0.5, fx_vclight

[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 1
autothrottle_available = 0
autothrottle_arming_required = 0
autothrottle_max_rpm =  0
autothrottle_takeoff_ga = 0
pitch_takeoff_ga = 0
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]
LeftMain = 0.4, -4.647, 3.5, 24.18,  0
RightMain = 0.4, 4.647, 3.5, 24.18,  0
fuel_type =  1
number_of_tank_selectors = 1
electric_pump=1

[airplane_geometry]
wing_area = 256.68
wing_span = 41.328
wing_root_chord = 6.48
wing_dihedral = 3.5
wing_incidence = 2
wing_twist = 0
oswald_efficiency_factor = 0.89
wing_winglets_flag = 0
wing_sweep  = 0
wing_pos_apex_lon = 1.4
wing_pos_apex_vert = 3.0
htail_area = 22.27
htail_span = 15.0
htail_pos_lon = -19.1
htail_pos_vert = 1.5
htail_incidence = -1.3
htail_sweep = 0
vtail_area = 13.45
vtail_span = 5.3
vtail_sweep = 0
vtail_pos_lon  = -17.0
vtail_pos_vert = 3.2
elevator_area = 27
aileron_area = 25
rudder_area = 2
elevator_up_limit = 30
elevator_down_limit = 20
aileron_up_limit = 23
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 25
spoiler_limit = 25
spoilerons_available = 0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0

[Reference Speeds]
flaps_up_stall_speed    = 50.0
full_flaps_stall_speed  = 45.5
cruise_speed            = 80
max_indicated_speed     = 190

[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[brakes]
parking_brake= 1
toe_brakes_scale= 0.5
differential_braking_scale = 1.5

[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=2

[turn_indicators]
turn_indicator.0=1,0

[direction_indicators]
direction_indicator.0=2,0