///////////////Аэропракт А-22ЛС - В. Жигульский, Киев, Украина.
/////=============================================================
[fltsim.0]
title=Aeroprakt Foxbat UR-ARPI
sim=A22LS
model=
panel=
sound=
texture=
atc_id=ARPI
atc_airline=Aeroprakt
atc_flight_number=ARPI
ui_manufacturer=Aeroprakt-zh
ui_type=A-22LS Foxbat
ui_variation=UR-ARPI желтый
visual_damage=1
prop_anim_ratio=-2.43
description=Aeroprakt A-22LC 'Foxbat', produced by Aeroprakt in the Kiev, Ukraine. Украина - аэродром Аэропракт-Наливайковка, желтый.
/////=============================================================
[fltsim.1]
title=Aeroprakt Foxbat UR-ARPL
sim=A22LS
model=
panel=
sound=
texture=ARPL
atc_id=ARPL
atc_airline=Aeroprakt
atc_flight_number=ARPL
ui_manufacturer=Aeroprakt-zh
ui_type=A-22LS Foxbat
ui_variation=UR-ARPL синий
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.2]
title=Aeroprakt Foxbat SP-YDL
sim=A22LS
model=
panel=
sound=
texture=YDF
atc_id=YDF
atc_airline=Dolny Slask
atc_flight_number=YDF
ui_manufacturer=Aeroprakt-zh
ui_type=A-22LS Foxbat
ui_variation=SP-YDF bialy
visual_damage=1
prop_anim_ratio=-2.43
description=Aeroprakt A-22LS 'Foxbat', produced by Aeroprakt in the Kiev, Ukraine. Polska, Dolny Slask, Wroclaw.
/////=============================================================
[fltsim.3]
title=Aeroprakt Foxbat EW-289SL
sim=A22LS
model=
panel=
sound=
texture=EW
atc_id=EW28
atc_airline=Foxbat-Belorussia
atc_flight_number=EW28
ui_manufacturer=Aeroprakt-zh
ui_type=A-22LS Foxbat
ui_variation=EW-289SL серый
visual_damage=1
prop_anim_ratio=-2.43
description=Aeroprakt A-22LS 'Foxbat', produced by Aeroprakt in the Kiev, Ukraine. Белоруссия.
/////=============================================================
[fltsim.4]
title=Aeroprakt Foxbat G-CHHB
sim=A22LS
model=
panel=
sound=
texture=CHHB
atc_id=CHHB
atc_airline=Foxbat-UK
atc_flight_number=CHHB
ui_manufacturer=Aeroprakt-zh
ui_type=A-22LS Foxbat
ui_variation=G-CHHB gray
visual_damage=1
prop_anim_ratio=-2.43
description=Aeroprakt A-22LS 'Foxbat', produced by Aeroprakt in the Kiev, Ukraine. Foxbat-UK.
/////=============================================================
[fltsim.5]
title=Aeroprakt Шарик ZH-SHR
sim=A22LS
model=
panel=
sound=
texture=SHR
atc_id=SHR
atc_airline=ZH-Cargo VLA
atc_flight_number=SHR
ui_manufacturer=Aeroprakt-zh
ui_type=A-22LS Foxbat
ui_variation=ZH-SHaRik
visual_damage=1
prop_anim_ratio=-2.43
description=Aeroprakt A-22LS 'Foxbat', produced by Aeroprakt in the Kiev, Ukraine. Шарик - виртуальная текстура.
/////=============================================================
[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 = 3.80
gear_system_type =4
tailwheel_lock =0
point.0= 1, 3.12, 0.0, -3.86, 1900, 0, 0.554, 30.0, 0.18, 1.5, 0.5, 0.0, 0.0, 0
point.1= 1, -1.20, -2.8, -4.11, 2500, 1, 0.554, 0.0, 0.45, 1.6, 0.5, 0.0, 0.0, 2
point.2= 1, -1.20, 2.8, -4.11, 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