///////////////Аэропракт А-22ЛС-AI - В. Жигульский, Киев, Украина.
/////=============================================================

[fltsim.0]
title=AI Aeroprakt Blue
sim=A22LS
model=
panel=
sound=
texture=B
atc_id=ARPK
atc_airline=Aeroprakt
atc_flight_number=ARPL
ui_manufacturer=AI
ui_type=A-22LS Foxbat
ui_variation=UR-ARPL синий
atc_parking_types=RAMP
atc_parking_codes=A22L
visual_damage=1 
prop_anim_ratio=-2.43 
description=Aeroprakt A-22LS 'Foxbat',  produced by Aeroprakt in the Kiev, Ukraine. Украина - аэродром Аэропракт-Наливайковка, синий.

[fltsim.1]
title=AI Aeroprakt Yellow
sim=A22LS
model=
panel=
sound=
texture=Y
atc_id=ARPL
atc_airline=Aeroprakt
atc_flight_number=ARPL
ui_manufacturer=AI
ui_type=A-22LS Foxbat желтый
atc_parking_types=RAMP
atc_parking_codes=A22L
visual_damage=1 
prop_anim_ratio=-2.43 
description=Aeroprakt A-22LS 'Foxbat',  produced by Aeroprakt in the Kiev, Ukraine. Украина - аэродром Аэропракт-Наливайковка, желтый.

/////=============================================================
[General]
atc_type=Ultralight
atc_model=AP22
editable=1
performance=Aeroprakt 
Category = airplane

/////=============================================================
/////=============================================================
/////=============================================================

[WEIGHT_AND_BALANCE]
max_gross_weight =992.0 
empty_weight =568.0 

reference_datum_position =0.0, 0.0, 0.0
empty_weight_CG_position = 0.0, 0.0, 0.0
max_number_of_stations =7

;Moments of Inertia
empty_weight_pitch_MOI =534.0
empty_weight_roll_MOI =320.0
empty_weight_yaw_MOI =700                  //665.0
empty_weight_coupled_MOI =0.0

CG_forward_limit = 0.0
CG_aft_limit = -3.0

station_load.0= "170, -0.27, -2.0, -1.3, Pilot"
station_load.1= "170, -0.27, 2.0, -1.3, Passenger"
station_load.2= "20, 0.0, 0.0, -0.9, Luggage"
station_load.3= "4, 0.0, 0.0, -3.5, Wheelspats"
station_load.4= "5, 0.0, 0.0, 2.2, lightingKit"

/////=============================================================
/////=============================================================


[GeneralEngineData]
engine_type =0
Engine.0 =4.8, 0.0, 0.7
ThrustAnglesPitchHeading.0 = 0, 0       
fuel_flow_scalar =0.7
min_throttle_limit = 0.0

[piston_engine]
power_scalar =1.0
cylinder_displacement =20.65
compression_ratio =10.5
number_of_cylinders =4
max_rated_rpm =5800.0
max_rated_hp =100.0
fuel_metering_type =2
cooling_type =1
normalized_starter_torque =0.02
turbocharged =0
max_design_mp =29.92
min_design_mp =0.0
critical_altitude =0.0
emergency_boost_type =0
emergency_boost_mp_offset =0.0
emergency_boost_gain_offset =0.0
fuel_air_auto_mixture =0
auto_ignition =0
max_rpm_mechanical_efficiency_scalar =1.0
idle_rpm_mechanical_efficiency_scalar =1.0
max_rpm_friction_scalar =0.78
idle_rpm_friction_scalar =0.75
emergency_boost_duration =0.0

[propeller]
thrust_scalar =0.97
rotation = -1
propeller_type =1
propeller_diameter =5.6
propeller_blades =3
propeller_moi =5.6
beta_max =12.0
beta_min =10.0
min_gov_rpm =0.0
prop_tc =0.1
gear_reduction_ratio =2.43
fixed_pitch_beta =11.0
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
propeller.0 = 0,0, -0.9
defeathering_accumulators_available =0 
prop_reverse_available =0
minimum_on_ground_beta =0.0
minimum_reverse_beta =0.0

[fuel]
LeftMain   = 0.0, -5.1, 1.4, 11.9, 0.2
RightMain = 0.0, 5.1, 1.4, 11.9, 0.2
fuel_type = 1
number_of_tank_selectors = 1                    
electric_pump = 1

/////============================================
//=============================================
[FLIGHT_TUNING]
cruise_lift_scalar=1.14
parasite_drag_scalar=1.2       /////DYN   1.1
induced_drag_scalar=0.9      ////DYN  0.9
elevator_effectiveness=1.00
aileron_effectiveness=1.00
rudder_effectiveness=1.00       ////DYN  1.000
pitch_stability=1.00
roll_stability=1.00
yaw_stability=1.89      ///DYN  1.70
elevator_trim_effectiveness = 0.75
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0
p_factor_on_yaw          = 0.74    
torque_on_roll           = 1.0
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0

//=============================================

[flaps.0]    
type = 1
system_type = 3
span-outboard = 0.5
extending-time = 1.0
damaging-speed = 90.0
blowout-speed = 100.0
flaps-position.0 = 0.00
flaps-position.1 = 5.0
flaps-position.2 = 8.0
lift_scalar = 1.1
drag_scalar = 2.0  ////DYN  1.1
pitch_scalar = 1.19   ////DYN  1.0

//=============================================
//=============================================
//=============================================

[contact_points]
        //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)

max_number_of_points =8
static_pitch = 0.0
static_cg_height = 0.90

gear_system_type =4
tailwheel_lock =0

point.0= 1,    3.12,     0.0, -0.96, 1900, 0, 0.554, 30.0, 0.18, 1.5, 0.5, 0.0, 0.0, 0
point.1= 1,  -1.20,    -2.8, -1.21, 2500, 1, 0.554, 0.0, 0.45, 1.6, 0.5, 0.0, 0.0, 2
point.2= 1,  -1.20,     2.8, -1.21, 2500, 2, 0.554, 0.0, 0.45, 1.6, 0.5, 0.0, 0.0, 3
//point.3= 2, -12.51,    0.0, -1.19, 1500, 0, 0.296, 0.0, 0.00, 1.5, 0.5, 0.0, 0.0, 1
//point.4= 2,    0.65, -15.6,   2.20,   300, 0,    0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5
//point.5= 2,    0.65,  15.6,   2.20,   300, 0,    0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6
//point.6= 2,    3.68,    0.0,  -1.65,   300, 0,    0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4
//point.7= 2,   -1.85,   0.0,  -1.81,   300, 0,     0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4
point.3 = 5,   0.00,  0.00,  0.00,    0, 0, 0.00,  0., 0.0,   0.0, 0.0,  1, 1, 0, 0,  0   ; for Water rudder

//=============================================
//=============================================
//=============================================

[Views]
eyepoint = 0.00, -0.80, 1.70
//=============================================
//=============================================
//=============================================

////////////==============================================
[TailHook]
tailhook_length=1                             ;(feet)
tailhook_position=-15.0, 0.0, 1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.1

[folding_wings]
// for parking equipment key
wing_fold_system_type =  4
fold_rates =  0.6, 0.6

[SMOKESYSTEM]
smoke.0=-500.00, -15.50, -0.40, fx_smoke_w   /////// z ,x,y

[effects]
wake = fx_wake
water = fx_spray
dirt =FX_A22dust.fx 
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1

////================================================
[exits]
number_of_exits=2
exit_rate.0 =0.7
exit_rate.1 =0.7

////================================================

[LIGHTS]
/// DEFAULTS LIGTS
\\\ light.0 = 3, 1.30, -15.4,  2.10, fx_navred ,
\\\ light.1 = 3, 1.30,  15.4,  2.10, fx_navgre ,
\\\ light.2 = 4, 1.5, 0, 0.9, fx_vclight,
\\\ light.4 = 2,  1.35, -15.5, 2.10, fx_strobe
\\\ light.5 = 2,  1.35,  15.5, 2.10, fx_strobe

///lShockwave light
light.0 = 3, 1.30, -15.5,  2.10, fx_shockwave_navred
light.1 = 3, 1.30,  15.5,  2.10,  fx_shockwave_navgre
light.2 = 4, 1.5, 0, 0.9, fx_shockwave_vclight
light.3 = 5, 6.90, -1.16, -1,  fx_shockwave_landing_light_small	
light.4 = 2,  1.35, -15.5, 2.10, fx_shockwave_strobe_2
light.5 = 2,  1.35,  15.5, 2.10, fx_shockwave_strobe_3

////================================================

[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 500.0
autothrottle_available = 0
pitch_takeoff_ga = 8.0
max_pitch = 8.0
max_pitch_acceleration = 1.0
max_pitch_velocity_lo_alt = 2.0
max_pitch_velocity_hi_alt = 1.0
max_pitch_velocity_lo_alt_breakpoint = 5000.0
max_pitch_velocity_hi_alt_breakpoint = 10000.0
max_bank = 20.0
max_bank_acceleration = 1.2
max_bank_velocity = 2.0
max_throttle_rate = 0.25
nav_proportional_control = 9.0
nav_integrator_control = 0.25
nav_derivative_control = 0.0
nav_integrator_boundary = 2.5
nav_derivative_boundary = 0.0
gs_proportional_control = 9.52
gs_integrator_control = 0.26
gs_derivative_control = 0.0
gs_integrator_boundary = 0.7
gs_derivative_boundary = 0.0
yaw_damper_gain = 0.0
autothrottle_arming_required = 0
default_pitch_mode =0
default_bank_mode =0
use_no_default_bank = 1
use_no_default_pitch = 1
autothrottle_takeoff_ga = 1.0
autothrottle_max_rpm = 90.0

////================================================
[Radios]
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

////================================================
[brakes]
parking_brake = 1        
toe_brakes_scale =0.7

////================================================
[airplane_geometry]
wing_area  = 102.6
wing_span  = 31.2
wing_root_chord  = 3.29
wing_dihedral = 1.7
wing_incidence = 0.0
wing_twist = 0.0
oswald_efficiency_factor = 0.7
wing_winglets_flag = 0
wing_sweep = 0.0
wing_pos_apex_lon  = 0.822
wing_pos_apex_vert = 3.0
htail_area  = 16.0
htail_span  = 9.8
htail_pos_lon = -12.3 
htail_pos_vert = 0.0 
htail_incidence = 0.0 
htail_sweep = 0.0 
vtail_area = 8.0
vtail_span = 4.8
vtail_sweep = 0.0
vtail_pos_lon = -12.5
vtail_pos_vert = 0.0
elevator_area = 9.0
aileron_area = 10.0
rudder_area = 5.0
elevator_up_limit = 25.0
elevator_down_limit = 25.0
aileron_up_limit = 10.0
aileron_down_limit = 20.0
rudder_limit = 21.0
elevator_trim_limit = 19.50
spoiler_limit = 30.0
spoilerons_available = 1            \\\0 - for motor cover!
spoiler_extension_time=1.000000
aileron_to_spoileron_gain = 0.0
min_ailerons_for_spoilerons = 0.0
min_flaps_for_spoilerons = 0.0
positive_g_limit_flaps_up  = 4.0          
positive_g_limit_flaps_down = 2.0             
negative_g_limit_flaps_up = -2.0           
negative_g_limit_flaps_down = -1.0           
load_safety_factor = 1.5              
auto_spoiler_available=0

////================================================
[electrical]    
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 0, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 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_strobe       = 0, 5 , 17.0
light_panel        = 0, 5 , 17.0

////================================================
////================================================
////================================================
[hydraulic_system]
normal_pressure =50.0
engine_map=1,0,0,0

[direction_indicators]
direction_indicator.0 = 2,0

[attitude_indicators]
attitude_indicator.0 = 2 

[turn_indicators]
turn_indicator.0 =1,1 

[keyboard_response]
elevator = 100,  180
aileron  = 200, 1000
rudder   = 200, 1000

[stall_warning]
type = 1
stick_shaker=0

[Reference Speeds]
flaps_up_stall_speed = 37.5
full_flaps_stall_speed =27.0
cruise_speed = 87.0
max_indicated_speed = 140.0 //dive speed

[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
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[pitot_static]
pitot_heat=1.0

[vacuum_system]
max_pressure=5.15
vacuum_type=1
electric_backup_pressure=0.0
engine_map=1,0,0,0

[pneumatic_system]
max_pressure=18.0
bleed_air_scalar=0.15

[deice_system]
structural_deice_type=0
\\\===================================END===============
[piston_engine]
cylinder_displacement=20.650000
compression_ratio=10.500000
number_of_cylinders=4
max_rated_rpm=5800.000000
max_rated_hp=100.000000
fuel_metering_type=2
cooling_type=1
normalized_starter_torque=0.343117
turbocharged=0
max_design_mp=29.919999
min_design_mp=0.000000
critical_altitude=0.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
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