[fltsim.0]
title = PZL 104 wilga Tundra Tires
sim = wilgaT
model =
panel =
sound =
texture =
visual_damage=1
panel_alias =
sound_alias =
kb_checklists = wilga_check
kb_reference = wilga_ref
atc_id =
atc_id_color =
atc_parking_types =
atc_parking_code =
ui_manufacturer = PZL
ui_type = Tundra Wilga
ui_variation = BPH Bank
description =Designed as a successor to the Polish built Yak-1 and PZL 101, the prototype PZL 104 Wilga first flew in 1962.  A four-seat light aircraft, the Wilga has been used for liaison, club flying, glider towing, parachuting, agricultural use and as an air ambulance. 
PZL has sold around 900 variants.  Wilga is polish for "Thrush".
 


[General]
performance= see ref.

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= -1.500, 0.000, 0.000
max_number_of_stations=6
station_load.0= 170.000, 1.00,  1.40, -.50, 
station_load.1= 170.000, 1.00, -1.40,-.50, 
station_load.2= 170.000, 1.00, -1.40,-.50, 


empty_weight= 2156.0
max_gross_weight= 2866.0
empty_weight_roll_MOI= 20000.000
empty_weight_pitch_MOI= 10000.000
empty_weight_yaw_MOI= 25000.000
empty_weight_coupled_MOI= 0.000

CG_forward_limit= 1.000
CG_aft_limit= 1.000

[fuel]
LeftMain= -2.000, 2.000, 2.750, 22.000, 0.000
RightMain= -2.000, -2.000, 2.750, 22.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area= 306.0
wing_span= 42.000
wing_root_chord= 7.300
wing_dihedral= 1.000
wing_incidence= 2.00
wing_twist= 0.000
oswald_efficiency_factor= 0.90
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 2.558
htail_area= 29.000
htail_span= 10.500
htail_pos_lon= -16.000
htail_pos_vert= 1.292
htail_incidence= -0.500
htail_sweep= 0.000
vtail_area= 25.000
vtail_span= 6.000
vtail_sweep= 0.000
vtail_pos_lon= -16.000
vtail_pos_vert= 2.000
elevator_area= 28.000
aileron_area= 22.000
rudder_area= 15.000
elevator_up_limit= 26.500
elevator_down_limit= 26.500
aileron_up_limit= 20.000
aileron_down_limit= 20.000
rudder_limit= 25.000
elevator_trim_limit= 15.500
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, -18.917, 0.000, -3.41, 1574.803, 0.000, 0.518, 60.000, 0.250, 2.500, 0.900, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 2.500, -4.0, -6.20, 1574.803, 1.000, 0.518, 10.000, 0.250, 2.500, 0.900, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 2.500, 4.0, -6.20, 1574.803, 2.000, 0.518, 10.000, 0.250, 2.500, 0.900, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, -1.000, -18.167, 2.083, 1574.803, 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, -1.000, 18.167, 2.083, 1574.803, 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, -19.917, 0.000, 1.417, 1574.803, 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, 3.583, 0.000, 1.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 6.500
static_cg_height= 5.168


[GeneralEngineData]
engine_type= 0
Engine.0= 8.000, 0.000, 0.000
fuel_flow_scalar= 0.5
min_throttle_limit=0.000000

[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.7
idle_rpm_mechanical_efficiency_scalar=0.5
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=.10
cylinder_displacement= 60.85
compression_ratio= 8.000
number_of_cylinders= 7
max_rated_rpm= 2600.000
max_rated_hp= 260.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.500
turbocharged= 0
max_design_mp= 00.000
min_design_mp= 00.000
critical_altitude= 000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 1
auto_ignition= 1
power_scalar=1.00

[propeller]
propeller_type= 0
propeller_diameter= 6.500
propeller_blades= 2
propeller_moi= 8.000
beta_max= 45.000
beta_min= 15.000
min_gov_rpm= 2000.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
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= 0.000
minimum_reverse_beta= 0.000
thrust_scalar=1.28

[Reference Speeds]
flaps_up_stall_speed= 64.000
full_flaps_stall_speed= 62.000
cruise_speed= 139.000
max_indicated_speed=190.000000  //

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000 

[Views]
eyepoint= -1.5, -0.89, 2.3

[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

[autopilot]
autopilot_available=0
flight_director_available=1
default_vertical_speed=0.000000
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=1.000000

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

[LIGHTS]
//---------------------------------------------------------
//Types:1=beacon, 2=strobe, 3=navigation, 4=cockpit,
//      5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo
//---------------------------------------------------------            
light.0=3,    -0.55, -18.33,   3.75,  fx_navred 
light.1=3,    -0.55,  18.33,   3.75,  fx_navgre 
//light.2=3,  -19.50,   0.00,  -1.25,  fx_navwhi 
light.3=1,  -18.55,   0.00,   5.80,  fx_beacon 
light.4=4,   -1.50,   0.00,   2.00,  fx_vclight
//--------------Wing Vortex--------------------------------
light.5=2,   -3.20, -17.70,   3.50,  fx_ICFX_Wingtip
light.6=2,   -3.20,  17.70,   3.50,  fx_ICFX_Wingtip
//--------------Flap Vortex--------------------------------
light.7=9,   -2.80, -10.20,  2.50,  fx_ICFX_F4F4_Flaptip
light.8=9,   -2.80,  10.20,  2.50,  fx_ICFX_F4F4_Flaptip
//--------------Exhaust Flame------------------------------
//light.9=6,    4.20,  -2.55,   0.02,  fx_ICFX_F6F3_exh_Left
//light.10=6,   4.20,   2.55,   0.02,  fx_ICFX_F6F3_exh_Right
//---------------------------------------------------------
light.9=4,   0,   0.00,   2.00,  fx_vclight

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

[direction_indicators]
direction_indicator.0=1,0

[SMOKESYSTEM]

smoke.0= 0.00, -1.9,  -0.95,  fx_fullthrottle_r
smoke.1= 0.00, -1.9,  0.95,  fx_fullthrottle_r

[flight_tuning]
cruise_lift_scalar=1.800
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
parasite_drag_scalar=1.08
induced_drag_scalar=1.0
elevator_effectiveness=1.05
aileron_effectiveness=1.05
rudder_effectiveness=.5
elevator_trim_effectiveness=.82
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
p_factor_on_yaw          = .90
torque_on_roll           = .80
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0


[folding_wings]
wing_fold_system_type = 4                       ;0=None
fold_rates = 0.5,0.5                          ;Percent per second

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 125.000
blowout-speed= 145.000
lift_scalar= 1.3
drag_scalar= 0.9
pitch_scalar= 0.01
flaps-position.0= 0.000, 0.000
flaps-position.1= 21.000, 0.000
flaps-position.2= 44.000, 0.000


[brakes]
toe_brakes_scale=1.0
parking_brake=1
differential_braking_scale = 1.0     

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0


[folding_wings]
wing_fold_system_type = 4                       ;0=None
fold_rates = 0.5,0.5                          ;Percent per second

[exits]
number_of_exits = 2
exit_rate.0 = 0.3                               ;Percent per second
exit_rate.1 = 0.3                               ;Percent per second

[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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