[fltsim.0]
title=Yakovlev Yak-50 - DM-WQT
sim=Yak50
model=
panel=
sound=
texture=DM-WQT
kb_checklists=
description=SerialNumber 791504 \n(c) Ralf Kreibich 2004
ui_manufacturer=Yakovlev
ui_type=Yak-50
ui_variation=Gesellschaft fьr Sport und Technik
atc_heavy=0
atc_id=DM-WQT
atc_airline=GST
atc_flight_number=130862

[fltsim.1]
title=Yakovlev Yak-50 - D-EJGS
sim=Yak50
model=
panel=
sound=
texture=D-EJGS
kb_checklists=
description=SerialNumber 791505 \n(c) Ralf Kreibich 2004
ui_manufacturer=Yakovlev
ui_type=Yak-50
ui_variation=MFC Stahnsdorf - Critical Mass
atc_heavy=0
atc_id=D-EJGS
atc_airline=MFC Stahnsdorf
atc_flight_number=300662

[fltsim.2]
title=Yakovlev Yak-50 - G-IVAR
sim=Yak50
model=
panel=
sound=
texture=G-IVAR
kb_checklists=
description=R. Goodes' Yak-50\n ex DM-WQT \n SerialNumber 791504 \n (c) Ralf Kreibich 2004
ui_manufacturer=Yakovlev
ui_type=Yak-50
ui_variation=Aerobatic Team Gloucestershire
atc_heavy=0
atc_id=G-IVAR
atc_airline=
atc_flight_number=271063

[fltsim.3]
title=Yakovlev Yak-50 - DDR-Flugzeuge.de
sim=Yak50
model=
panel=
sound=
texture=DDR
kb_checklists=
description=Yakovlev Yak-50 in fiktiver Werbebemalung \n (c) Ralf Kreibich 2004
ui_manufacturer=Yakovlev
ui_type=Yak-50
ui_variation=DDR-Flugzeuge.de
atc_heavy=0
atc_id=?????
atc_airline=unbekannt
atc_flight_number=271064



[WEIGHT_AND_BALANCE]
empty_weight=1750				// (pounds)
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, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000

;Moments of Inertia
empty_weight_pitch_MOI=3181.10
empty_weight_roll_MOI=2396.69
empty_weight_yaw_MOI=3475.84
empty_weight_coupled_MOI=0.000000
max_gross_weight=2100.000000

[fuel]
Center1=0.000000,0.000000,0.000000,45.00,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=2.0
aileron_effectiveness=1.5
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[piston_engine]
power_scalar=1.0
cylinder_displacement=85.000000
compression_ratio=6.500000
number_of_cylinders=9
max_rated_rpm=3500.000000
max_rated_hp=365.000000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=40.999999
min_design_mp=1.000000
critical_altitude=21653.000000
emergency_boost_type=2
emergency_boost_mp_offset=5.000000
emergency_boost_gain_offset=0.480000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
thrust_scalar=1.0
propeller_type=0
propeller_diameter=10.833000
propeller_blades=2
propeller_moi=41.400000
beta_max=65.000000
beta_min=21.000000
min_gov_rpm=1800.000000
prop_tc=0.010000
gear_reduction_ratio=1.850000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

[exits]
number_of_exits=1
exit_rate.0=0.4  				;Percent per second

[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0

[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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)

point.0=1, -14.702, 0.00, -1.7, 1600, 0, 0.33, 85.0, 0.20, 1.0, 1.0, 0.0, 0.0, 0, 0, 300
point.1=1, 3.40, -3.95, -5.35, 2200, 1, 1.00,  0.0, 0.50,1.50, 1.00, 7.5, 7.5, 2, 0, 200
point.2=1, 3.40, 3.91, -5.35, 2200, 2, 1.00,  0.0, 0.50, 1.50, 1.00, 6.0, 6.0, 3, 0, 200

point.3=2,   0.00,-20.00, -1.25, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5
point.4=2,   0.00, 20.00, -1.25, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6
point.5=2, -16.25,  0.00, 0.00, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9
point.6=2,   6.41,  0.00, -1.70, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4

static_cg_height=4.30           //feet, altitude of CG when at rest on the ground
static_pitch=11.6698         //degrees (pitch when loaded on ground)
gear_system_type=0



[Views]
eyepoint=-3.05,0.000000,3.16

[LIGHTS]
panel=0.00, 0.15, -0.80, fx_vclight

[airplane_geometry]
wing_area=177.000000
wing_span=31.160000
wing_root_chord=5.916667
wing_dihedral=4.998779
wing_incidence=0.0
wing_twist=0.000000
oswald_efficiency_factor=0.75
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=32.000000
htail_span=12.250000
htail_pos_lon=-16.416667
htail_pos_vert=0.000000
htail_incidence=0.0
htail_sweep=0.000000
vtail_area=29.000000
vtail_span=6.140033
vtail_sweep=0.000000
vtail_pos_lon=-17.916667
vtail_pos_vert=1.500000
elevator_area=12.820000
aileron_area=18.070000
rudder_area=8.230000
elevator_up_limit=30.00
elevator_down_limit=25.00
aileron_up_limit=16.999658
aileron_down_limit=16.999658
rudder_limit=30.00
elevator_trim_limit=19.996227
spoiler_limit=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[brakes]
toe_brakes_scale=1.000000
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

[GeneralEngineData]
engine_type=0
Engine.0=7.500000,0.000000,0.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000

[Reference Speeds]
flaps_up_stall_speed=102.000000
full_flaps_stall_speed=81.600000
cruise_speed=250.000000
max_indicated_speed=760.500000

[keyboard_response]
elevator=300.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
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

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks5
touchdown=fx_tchdwn_s5, 1

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

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[direction_indicators]
direction_indicator.0=1,0

[General]
performance=Max speed: 426mph@21650ft with MW50, 357mph@sea level\nInitial climb rate: around 3500ft\/min\nEmpty weight: 7694lbs (some sources say: 7720 or 7964lb)\nArmament: two 13mm MG and two 20mm cannons\nOne 1100lb bomb or rockets

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=15.000058,0.000000