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Paha_S7

Wilco Airbus vol.1 & vol.2 + Simmer's Sky

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Инструкция по мержеванию(соединению) панелей от Wilco и визуальных моделей SMS Overland

 

Ув.пользователи на данный момент готовы:

А319-100, спасибо VRP

А320-214, спасибо ROCK_AVIA

А330-200 и А330-300

А340-300 и A340-600

 

все остальные только визуальная часть рабочая

 

На форуме есть множество тем по мержеванию, не буду отрицать, что некоторые данные для своей темы я взял с других тем. Мне захотелось собрать в одну тему всю информацию по мержеванию семейства Эйрбас.

Пожалуй начнем с начала:

1. Выбираем какой тип ВС будем скрещивать. Мне интересно семейство А330-х, 200 или 300 по барабану если честно... Заходим в папку, в данном случае - Aircraft\feelThere PIC A332GE и следуем моему примеру

2. Выбираем папку Model, заходим разумеется и удаляем 2 файла:

визуальную модель

текстовый файл

Далее вместо старых WILCO-моделей сливаем в нее(в папку) необходимые нам те же самые 2 файла, только от новой модели SMS Overland. У меня они располагаются в архиве по адресу SMS_A330-200\model.GE1. Получается с визуальной частью мы процентов на 80 разобрались. Остальные 20% это наши текстуры.

 

А как устанавливать текстуры?!

 

1. Перемещаем/Распаковываем папку с текстурами для модели в нужную директорию(как правило это папка с самим самолетом :) )

2. Открываем aircraft.cfg

и на нашем же примере смотрим начиная с верха...

исходное значение:

[fltsim.0]

title=feelThere A330-200 House Colore

sim=FeelThere_A330-200

sound=GE

model=

texture=

panel=

checklists=

atc_id=F-GZCJ

atc_airline=Airbus Industries

atc_flight_number=009

atc_heavy=1

ui_manufacturer=Airbus

ui_type=A330-200

ui_variation=Airbus Industries

visual_damage=1

description=Airbus Series Vol.2\nDeveloped by www.feelThere.com \nPublished by Wilco Publishing www.wilcopub.com\n\nSupport at www.wilcopub.com

 

а получить нам нужно вот это:

[fltsim.0]

title=Airbus A330-200 Air France

sim=FeelThere_A330-200

sound=GE

model=

texture=AFRC

panel=

checklists=

atc_id=F-GZCJ

atc_airline=Air France

atc_flight_number=009

atc_heavy=1

ui_manufacturer=Airbus

ui_type=A330-200

ui_variation=Air France

visual_damage=1

description=Airbus Series Vol.2\nDeveloped by www.feelThere.com \nPublished by Wilco Publishing www.wilcopub.com\n\nSupport at www.wilcopub.com

 

скажу сразу, ниже написанное изменяем при смене самих названий файлов, или смене директорий:

sim=FeelThere_A330-200 - отвечает за указание расположения .air файла, при некорректном вводе самолет отображться НИ ГДЕ не будет .

sound=GE - звуки для нашего ВС. При некорректном вводе всего лишь будем иметь глухую картинку.

model= - как раз таки указание директории с моделью ВС. При некорректном визуальную модель Вы в симе не увидите.

panel= - указание директории содержащую приборы. При некорректном вводе панели не будет совсем, ни 2Д, ни ВК.

с этим я считаю разобрались...

 

а эти как раз таки меняем:

title=Airbus A330-200 Air France - наименование нашего ВС для сима, допустим если ставим мы ливрею Air France то и разумно будет написать, что это Airbus A330-200 Air France.

texture=AFRC - указание директории с текстурой. Обратите внимание, сама папка будет называться Texture.AFRC - т.е. берем то, что написано после точки.

atc_airline=Air France - Наименование авиакомпании которой принадлежит ВС, также разумно будет указать реальную

atc_id=F-GZCJ - б\н нашего ВС.

atc_flight_number=009 - Номер рейса. Я не меняю...

ui_manufacturer=Airbus - Фирма-производитель ВС. Моему глазу приятнее когда написано реальное название, а не feelThere Wilco vol.2.

ui_type=A330-200 - Модель ВС, при желании можно указать и более конкретно: A330-243 GE.

ui_variation=Air France - Указание цветов АК при выборе ВС в симе.

 

 

Отвлеклись? Продолжаем...

Как Вы помните, мы остановились на установке ливреи. Это если честно было самое сложное, далее все много-много проще. Я насчитал 4-5 операций:

1. Выбрать ниже в посте нужный нам ВС, напоминаю наш пример это Airbus A330-200 с двигателями GE.

2. Открыть спойлер с в разделе "Данные для двигателей CFM/GE" с названием "Airbus A330-200".

3. Скопировать ВСЕ из под спойлера.

4. Вставить(выделить все ниже и заменить на скопированное) это в наш aircraft.cfg ниже информации о ливрее, начинаем со слова [exits] и до конца...

// FeelThere A330-200 GE

 

[fltsim.0]

title=Airbus A330-200 Air France

sim=FeelThere_A330-200

sound=GE

model=

texture=AFRC

panel=

checklists=

atc_id=F-GZCJ

atc_airline=Air France

atc_flight_number=009

atc_heavy=1

ui_manufacturer=Airbus

ui_type=A330-200

ui_variation=Air France

visual_damage=1

description=Airbus Series Vol.2\nDeveloped by www.feelThere.com \nPublished by Wilco Publishing www.wilcopub.com\n\nSupport at www.wilcopub.com

 

 

[exits]

number_of_exits=2

exit.0 = 0.25, 78.0, -7.5, 8.5, 0

exit.1 = 0.05, -37.0, 7.0, -4.0, 1

 

5. Сохраняем.

6. Запускаем СИМ и тестим :)

 

Данные для двигателей CFM/GE

 

Airbus A319

 

[exits]

number_of_exits=2

exit.0 = 0.25, 35.5, -5.5, 2.8, 0

exit.1 = 0.4, -18.5, 5.0, -2.2, 1

 

[Views]

eyepoint=43.13, -1.85, 5.19

 

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0=3, -5.81, -54.7, 3.49, fx_navred ,

light.1=3, -5.81, 54.7, 3.49, fx_navgre ,

light.2=2, -6.42, -55.3, 3.59, fx_strobe ,

light.3=2, -6.42, 55.3, 3.59, fx_strobe ,

light.4=1, 14.15, 0.0, -4.90, fx_beaconh ,

light.5=1, 11.52, 0.0, 9.55, fx_beaconh ,

light.6=2,-54.23, 0.17, 5.19, fx_strobe ,

light.7=3,-54.23, -0.17, 5.19, fx_navwhi ,

light.8 = 4, 39, 0, 5.7, fx_vclighth

 

[General]

atc_type=AIRBUS

atc_model=A319

performance=Dimensions: Wing span: 111 ft 10 in (33.91 m) \n Length: 111 ft 0 in (33.84 m) \n Height: 38 ft 7 in (11.76 m) \n Weights: \n Empty: 89,000 lb \n Max take-off: 166,000 lb \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Maximum range: 3,700 miles (6,800 km) \n Powerplants: Two IAE V2525-A5 rated at 23.500 lbs (111.2 kN) or Two CFM International CFM56-5B4 rated at 22.000 lbs. Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position=0, 0, -4.4

max_number_of_stations=50

 

station_load.0 = "450, 42.0, 0.0, 0.0, Crew"

station_load.1 = "1000, 37.0, 0.0, 0.0, Galleys"

station_load.2 = "4000, 16.0, 0.0, 0.0, Baggage"

station_load.3 = "7000, 0.0, 0.0, 0.0, Cargo"

station_load.4 = "6200, 26.0, 0.0, 0.0, First"

station_load.5 = "17000, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 89500

max_gross_weight=167300

empty_weight_roll_MOI=1300000

empty_weight_pitch_MOI=2000000

empty_weight_yaw_MOI=2000000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=30

rated_N2_rpm=29920.000000

static_thrust=23200.000000

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type=1

Engine.0= 3.0, -17.5, -2.500000

Engine.1= 3.0, 17.5, -2.500000

fuel_flow_scalar=1.0000

min_throttle_limit=-0.499939

max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear

 

[jet_engine]

thrust_scalar =1.1

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=13.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=29.0 //ditto to accomodate flap 2

flaps-position.5=40.0 //More lift for patched solution to low lift RY

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000

LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000

RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000

LeftAux= 0.0, -13.0, 0.0, 227.000000, 0.000000

RightAux= 0.0, 13.0, 0.0, 227.000000, 0.000000

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=1320.000000

wing_span=111.9

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.8723

wing_winglets_flag=1

wing_sweep=22

wing_pos_apex_lon=15.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

point.0=1, 35.80, 0.00, -10.56, 1500, 0, 1.25, 60.12, 0.38, 2.4, 0.5135, 7.0, 8.2, 0, 0.0, 0.0

point.1=1, -4.25, -11.58, -11.06, 2200, 1, 2.15, 0.00, 1.11, 2.0, 0.5470, 9.7, 14.1, 2, 0.0, 0.0

point.2=1, -4.25, 11.58, -11.06, 2200, 2, 2.15, 0.00, 1.11, 2.0, 0.5470, 9.7, 14.1, 3, 0.0, 0.0

 

point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0

point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0

point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0

point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0

 

max_number_of_points=21

 

static_pitch= -0.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn)

static_cg_height=14.26 //feet, altitude of CG when at rest on the ground

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.86

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=352.000000

max_mach=0.84

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=2

 

 

[turn_indicators]

turn_indicator.0=1,0

 

Airbus A320

 

[exits]

number_of_exits=2

exit_rate.0=0.25

exit_rate.1=0.25

 

 

[Views]

eyepoint=53.95, -1.85, 5.13 //(feet) longitudinal, lateral, vertical distance from reference datum

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0=3, -5.81, -54.7, 3.09, fx_navredm ,

light.1=3, -5.81, 54.7, 3.09, fx_navgrem ,

light.2=2, -6.42, -55.3, 3.09, fx_strobeh ,

light.3=2, -6.42, 55.3, 3.09, fx_strobeh ,

light.4=1, 14.15, 0.0, -4.70, fx_beaconb ,

light.5=1, 11.52, 0.0, 9.15, fx_beaconh ,

light.6=2,-61.83, -0.17, 4.79, fx_strobe ,

light.7=3,-61.83, 0.17, 4.79, fx_navwhi ,

light.8 = 4, 53.5, 0, 5.4, fx_vclighth

 

 

[General]

atc_type=AIRBUS

atc_model=A320

performance=Dimensions: Wing span: 111 ft 10 in (33.91 m) \n Length: 123 ft 3 in (37.57 m) \n Height: 38 ft 9.50 in (11.80 m) \n Weights: \n Empty: 91,675 lb (41,583 kg) \n Max take-off: 169,765 lb (77,000 kg) \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Maximum range: 3,222 miles (5,185 km) \n Powerplants: Two IAE V2525-A5 rated at 25,000 lb (111.2 kN) or Two CFM International CFM56-5B4 rated at 26,500 lb (117.9 kN). Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position=0.000000,0.000000,-4.000000

max_number_of_stations=50

 

station_load.0 = "450, 42.0, 0.0, 0.0, Crew"

station_load.1 = "1000, 37.0, 0.0, 0.0, Galleys"

station_load.2 ="6598, 16.0, 0.0, 0.0, Baggage"

station_load.3 ="9499, 0.0, 0.0, 0.0, Cargo"

station_load.4 ="1653, 26.0, 0.0, 0.0, First"

station_load.5 ="18187, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 93500

max_gross_weight=169800

empty_weight_roll_MOI=1700000

empty_weight_pitch_MOI=2500000

empty_weight_yaw_MOI=2700000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=30

rated_N2_rpm=29920.000000

static_thrust=26200.000000

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type=1

Engine.0= -2.25, -18.9, -4.600000

Engine.1= -2.25, 18.9, -4.600000

fuel_flow_scalar=1.0000

min_throttle_limit=-0.499939

 

[jet_engine]

thrust_scalar =0.95

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=10.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000

LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000

RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000

LeftAux= 0.0, -13.0, 0.0, 227.000000, 0.000000

RightAux= 0.0, 13.0, 0.0, 227.000000, 0.000000

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=1320.000000

wing_span=111.9

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.8

wing_winglets_flag=1

wing_sweep=22

wing_pos_apex_lon=15.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

[contact_points]

 

point.0=1.0, 41.66, 0.00, -11.03, 6000.8, 0.00, 1.79, 75.00, 0.50, 2.50, 0.60, 9.00, 9.00, 0.00, 0.00, 0.00

point.1=1.0, -4.16, -12.33, -11.70, 6000.8, 1.00, 1.79, 0.00, 1.29, 2.50, 0.60, 12.00, 12.00, 2.00, 0.00, 0.00

point.2=1.0, -4.16, 12.33, -11.70, 6000.8, 2.00, 1.79, 0.00, 1.29, 2.50, 0.60, 13.00, 13.00, 3.00, 0.00, 0.00

;point.3=2.0, -14.16, -47.33, 0.00, 787.4, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00

;point.4=2.0, -14.16, 47.33, 0.00, 787.4, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00

;point.5=2.0, -54.00, 0.00, 2.83, 787.4, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00

;point.6=2.0, 42.66, 0.00 ,-3.75, 787.4, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00

 

 

static_pitch= 0.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn)

static_cg_height=15.02 //feet, altitude of CG when at rest on the ground

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.86

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=352.000000

max_mach=0.84

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

gs_proportional_control=19.0

gs_integrator_control=0.530

gs_derivative_control=0.00

gs_integrator_boundary=0.70

gs_derivative_boundary=0.00

yaw_damper_gain=0.000000

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=2

 

 

[turn_indicators]

turn_indicator.0=1,0

 

Airbus A321

 

[exits]

number_of_exits=2

exit.0 = 0.25, 53.5, -5.5, 2.8, 0

exit.1 = 0.4, -23.5, 5.0, -2.2, 1

 

[Views]

eyepoint=61.73, -1.65, 5.25

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0= 1, 9.55, 0.0, -4.84, fx_beaconb ,

light.1= 1, 6.32, 0.0, 9.45, fx_beaconh ,

light.2= 2,-75.95, -0.17, 5.19, fx_strobe ,

light.3= 3,-75.95, 0.17, 5.19, fx_navwhi ,

light.4= 4, 60.90, 0.0, 6.70, fx_vclighth //61.73, -1.65, 5.25

 

 

[General]

atc_type=AIRBUS

atc_model=A321

performance=Dimensions: Wing span: 111 ft 10 in (33.91 m) \n Length: 123 ft 3 in (37.57 m) \n Height: 38 ft 9.50 in (11.80 m) \n Weights: \n Empty: 106,00 lb \n Max take-off: 196,000 lb \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Maximum range: 3,222 miles (5,185 km) \n Powerplants: Two IAE V2525-A5 rated at 25,000 lb (111.2 kN) or Two CFM International CFM56-5B4 rated at 32.000 lbs. Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position= 5, 0, -4.4

max_number_of_stations=50

 

station_load.0 = "450, 42.0, 0.0, 0.0, Crew"

station_load.1 = "1000, 37.0, 0.0, 0.0, Galleys"

station_load.2 = "5000, 16.0, 0.0, 0.0, Baggage"

station_load.3 = "7000, 0.0, 0.0, 0.0, Cargo"

station_load.4 = "7200, 26.0, 0.0, 0.0, First"

station_load.5 = "20000, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 106300

max_gross_weight=196210

empty_weight_roll_MOI=1700000

empty_weight_pitch_MOI=2500000

empty_weight_yaw_MOI=2700000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=30

rated_N2_rpm=29920.000000

static_thrust=31400.000000

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop

Engine.0=3.25, -18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datum

Engine.1=3.25, 18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datum

fuel_flow_scalar=1.26 //Scalar for fuel flow efficiency

min_throttle_limit=-0.330000

max_contrail_temperature = -30

 

[jet_engine]

thrust_scalar =1.0

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 0.0, 0.0, 0.0, 2118.000000, 0.000000

LeftMain= 0.0, -8.0, 0.0, 2001.000000, 0.000000

RightMain= 0.0, 8.0, 0.0, 2001.000000, 0.000000

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=1320.000000

wing_span=111.9

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.8723

wing_winglets_flag=1

wing_sweep=22

wing_pos_apex_lon=15.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

point.0=1, 54.80, 0.00, -10.61, 1500, 0, 1.25, 60.12, 0.50, 2.1, 0.8135,11.0, 13.2, 0, 0.0, 0.0

point.1=1, -3.95, -11.58, -11.56, 2200, 1, 2.15, 0.00, 1.51, 2.0, 0.7470, 9.7, 14.1, 2, 0.0, 0.0

point.2=1, -3.95, 11.58, -11.56, 2200, 2, 2.15, 0.00, 1.51, 2.0, 0.7470, 9.7, 14.1, 3, 0.0, 0.0

 

point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0

point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0

point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0

point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0

 

max_number_of_points=21

 

static_pitch=-0.22 //degrees, pitch when at rest on the ground (+=Up, -=Dn)

static_cg_height=14.56 //feet, altitude of CG when at rest on the ground

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.86

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=352.000000

max_mach=0.84

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=2

 

 

[turn_indicators]

turn_indicator.0=1,0

 

 

 

Airbus A330-200

 

[exits]

number_of_exits=2

exit.0 = 0.25, 78.0, -7.5, 8.5, 0

exit.1 = 0.05, -37.0, 7.0, -4.0, 1

 

[Views]

eyepoint=88.74, -1.80, 5.85

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.1 = 1, 30.66, 0.00, -7.58, fx_beaconb ,

light.2 = 1, 17.40, 0.00, 11.93, fx_beaconh ,

light.3 = 2, -97.42, 0.00, 9.00, fx_strobe ,

light.4 = 3, -97.42, 0.00, 9.00, fx_navwhi ,

light.5 = 4, 88.9, 0, 7.3, fx_vclighth

 

 

[General]

atc_type=AIRBUS

atc_model=A330-200

performance=Dimensions: Wing span: 197 ft 10 in \n Length: 188ft 8 in \n Height: 57ft 1 in \n Weights: \n Empty: 274,000 lb \n Max take-off: 513,000 \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Powerplants: Two RR Trent 700 rated at 68,000 lbs (111.2 kN) or Two CF6-80E1 rated at 67.500 lbs. Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position = 0.000, 0.000, -6.000

max_number_of_stations=50

 

station_load.0 = "750, 42.0, 0.0, 0.0, Crew"

station_load.1 = "2000, 37.0, 0.0, 0.0, Galleys"

station_load.2 ="29104, 16.0, 0.0, 0.0, Baggage"

station_load.3 ="23518, 0.0, 0.0, 0.0, Cargo"

station_load.4 ="2480, 26.0, 0.0, 0.0, First"

station_load.5 ="34556, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 264875

max_gross_weight=507050

empty_weight_roll_MOI=21100000

empty_weight_pitch_MOI=21400000

empty_weight_yaw_MOI=15800000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=55

rated_N2_rpm=29920.000000

static_thrust=72500.000000 // CF Engines

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type= 1

Engine.0= 12.600, -29.900, -6.100

Engine.1= 12.600, 29.900, -6.100

fuel_flow_scalar= 1.06

min_throttle_limit=-0.250000

 

[jet_engine]

thrust_scalar =0.96 //300-200 only

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 4.0, 0.0, 0.0, 10980.0, 0.0

Center2= -4.0, 0.0, 0.0, 1646.0, 0.0

LeftMain= -2.0, -4.0, 0.0, 11095.0, 0.0

RightMain= -2.0, 4.0, 0.0, 11095.0, 0.0

LeftAux= -7.0, -13.0, 0.0, 964.0, 0.0

RightAux= -7.0, 13.0, 0.0, 964.0, 0.0

 

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=3892

wing_span=198

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.8723

wing_winglets_flag=1

wing_sweep=30

wing_pos_apex_lon=35.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

 

point.0= 1.000, 75.420, 0.000, -14.220, 1181.100, 0.000, 1.777, 70.000, 0.500, 2.100, 0.814, 11.000, 13.200, 0.000, 0.000, 0.000

point.1= 1.000, -7.200, -15.800, -15.840, 1574.800, 1.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 2.000, 0.000, 0.000

point.2= 1.000, -7.200, 15.800, -15.840, 1574.800, 2.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 3.000, 0.000, 0.000

 

point.3= 2.000, -10.170, -47.330, 0.000, 787.400, 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, -10.170, 47.330, 0.000, 787.400, 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, -83.330, 0.000, 2.500, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

 

 

static_pitch= -0.830

static_cg_height= 20.670

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.66

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=358.000000

max_mach=0.865

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=1

 

 

[turn_indicators]

turn_indicator.0=1,0

 

 

 

Airbus A330-300

 

[exits]

number_of_exits=2

exit.0 = 0.25, 86.0, -7.5, 8.5, 0

exit.1 = 0.05, -42.0, 7.0, -4.0, 1

 

 

[Views]

eyepoint=98.07, -1.80, 5.85

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.1 = 1, 30.66, 0.00, -7.58, fx_beaconb ,

light.2 = 1, 17.40, 0.00, 11.93, fx_beaconh ,

light.3 = 2, -97.42, 0.00, 9.00, fx_strobe ,

light.4 = 3, -97.42, 0.00, 9.00, fx_navwhi ,

light.5 = 4, 88.9, 0, 7.3, fx_vclighth

 

 

[General]

atc_type=AIRBUS

atc_model=A330-300

performance=Dimensions: Wing span: 197 ft 10 in \n Length: 165ft 3 in \n Height: 55ft in \n Weights: \n Empty: 274,000 lb \n Max take-off: 513,000 \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Powerplants: Two RR Trent 700 rated at 68,000 lbs (111.2 kN) or Two CF6-80E1 rated at 72.500 lbs. Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position=0.000, 0.000, -6.000

max_number_of_stations=50

 

station_load.0 = "750, 42.0, 0.0, 0.0, Crew"

station_load.1 = "2000, 37.0, 0.0, 0.0, Galleys"

station_load.2 ="41324, 16.0, 0.0, 0.0, Baggage"

station_load.3 ="35482, 0.0, 0.0, 0.0, Cargo"

station_load.4 ="4960, 26.0, 0.0, 0.0, First"

station_load.5 ="40013, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 267000

max_gross_weight=509000

empty_weight_roll_MOI=21300000

empty_weight_pitch_MOI=21900000

empty_weight_yaw_MOI=16100000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=55

rated_N2_rpm=29920.000000

static_thrust=72500.000000

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type= 1

Engine.0= 10.600, -29.900, -6.100

Engine.1= 10.600, 29.900, -6.100

fuel_flow_scalar= 0.8900

min_throttle_limit=-0.350000

 

[jet_engine]

thrust_scalar =0.98

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 4.0, 0.0, 0.0, 0.0, 0.0

Center2= -4.0, 0.0, 0.0, 1615.0, 0.0

LeftMain= -2.0, -4.0, 0.0, 11025.0, 0.0

RightMain= -2.0, 4.0, 0.0, 11025.0, 0.0

LeftAux= -7.0, -13.0, 0.0, 974.0, 0.0

RightAux= -7.0, 13.0, 0.0, 974.0, 0.0

 

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=3892

wing_span=198

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.892

wing_winglets_flag=1

wing_sweep=30

wing_pos_apex_lon=35.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

 

point.0= 1.000, 84.420, 0.000, -14.220, 1181.100, 0.000, 1.777, 70.000, 0.500, 2.100, 0.814, 11.000, 13.200, 0.000, 0.000, 0.000

point.1= 1.000, -7.200, -15.800, -15.840, 1574.800, 1.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 2.000, 0.000, 0.000

point.2= 1.000, -7.200, 15.800, -15.840, 1574.800, 2.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 3.000, 0.000, 0.000

 

point.3= 2.000, -10.170, -47.330, 0.000, 787.400, 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, -10.170, 47.330, 0.000, 787.400, 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, -83.330, 0.000, 2.500, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

 

 

static_pitch= -0.830

static_cg_height= 20.670

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.66

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=358.000000

max_mach=0.865

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=1

 

 

[turn_indicators]

turn_indicator.0=1,0

 

 

 

Airbus A340-300

 

[exits]

number_of_exits=3

exit.0 = 0.25, 86.0, -7.5, 8.5, 0

exit.1 = 0.05, -42.0, 7.0, -4.0, 1

 

 

[Views]

eyepoint=98.07, -1.80, 5.85

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.1 = 1, 30.30, 0.00, -8.08, fx_beaconb ,

light.2 = 1, 17.40, 0.00, 11.99, fx_beaconh ,

light.3 = 2,-102.92, 0.00, 9.00, fx_strobe ,

light.4 = 3,-102.92, 0.00, 9.00, fx_navwhi ,

light.5 = 4, 99.02, 0, 5.3, fx_vclighth

 

 

[General]

atc_type=AIRBUS

atc_model=A340-300

performance=Dimensions: Wing span: 197 ft 10 in \n Length: 208 ft \n Height: 56 ft. 9 in \n Weights: \n Empty: 286,150 lb \n Max take-off: 573,200 lbs \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Powerplants: Four CFM rated at 32,550 lbs Thrust

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position = 0.000, 0.000, -6.000

max_number_of_stations=50

 

station_load.0 = "750, 42.0, 0.0, 0.0, Crew"

station_load.1 = "3000, 37.0, 0.0, 0.0, Galleys"

station_load.2 ="37797, 16.0, 0.0, 0.0, Baggage"

station_load.3 ="30588, 0.0, 0.0, 0.0, Cargo"

station_load.4 ="3306, 26.0, 0.0, 0.0, First"

station_load.5 ="38029, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 286150

max_gross_weight=573200

empty_weight_roll_MOI=33200000

empty_weight_pitch_MOI=34400000

empty_weight_yaw_MOI=22800000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=57

rated_N2_rpm=29920.000000

static_thrust=34000.000000 // Trent Engines for A340-600

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type= 1

Engine.0= -8.420, -63.700, 1.350

Engine.1= 12.600, -29.900, -3.100

Engine.2= 12.600, 29.900, -3.100

Engine.3= -8.420, 63.700, 1.350

fuel_flow_scalar= 0.79

min_throttle_limit=-0.320000

 

[jet_engine]

thrust_scalar =1.5 //340-300 only!

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

lift_scalar=0.77

drag_scalar=1.0

pitch_scalar=0.0

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.7

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 4.0, 0.0, 0.0, 11207.0, 0.0 // Middle Fuselage Main Centre Tank

Center2= -33.0, 0.0, 0.0, 1646.0, 0.0 // Trim Tank in Tail-plane sectin

LeftMain= -2.0, -6.0, 0.0, 11301.0, 0.0 // Inner Wing Tank 1 Left

RightMain= -2.0, 6.0, 0.0, 11301.0, 0.0 // Inner Wing Tank 2 Right

LeftAux= -6.0, -15.0, 0.0, 964.0, 0.0 // Outer Wing Tank 1 Left

RightAux= -6.0, 15.0, 0.0, 964.0, 0.0 // Outer Wing Tank 2 Right

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=3892

wing_span=197.85

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.94

wing_winglets_flag=1

wing_sweep=30

wing_pos_apex_lon=38.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

 

point.0= 1.000, -6.350, 0.001, -15.250, 1574.800, 1.000, 2.368, 0.000, 2.000, 2.500, 0.900, 11.000, 9.0, 1.000, 0.000, 0.000

point.1= 1.000, 84.420, 0.000, -14.580, 1181.100, 0.000, 1.777, 60.000, 0.500, 3.500, 0.900, 9.000, 8.0, 0.000, 0.000, 0.000

point.2= 1.000, -6.200, -15.800, -15.600, 1574.800, 1.000, 2.368, 0.000, 1.400, 2.500, 0.900, 11.000, 9.0, 2.000, 0.000, 0.000

point.3= 1.000, -6.200, 15.800, -15.600, 1574.800, 2.000, 2.368, 0.000, 1.400, 2.500, 0.900, 11.000, 9.0, 3.000, 0.000, 0.000

 

point.4= 2.000, -10.170, -47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000

point.5= 2.000, -10.170, 47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000

point.6= 2.000, -83.330, 0.000, 2.500, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000

point.7= 2.000, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

 

static_pitch= -0.480

static_cg_height= 21.000

gear_system_type=0

 

 

 

[brakes]

toe_brakes_scale=0.78

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=358.000000

max_mach=0.865

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=2

 

 

[turn_indicators]

turn_indicator.0=1,0

 

 

 

Данные для двигателей RR Trent/IAE

 

Airbus A319

 

[exits]

number_of_exits=2

exit.0 = 0.25, 35.5, -5.5, 2.8, 0

exit.1 = 0.4, -18.5, 5.0, -2.2, 1

 

[Views]

eyepoint=43.13, -1.85, 5.19

 

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0=3, -5.81, -54.7, 3.49, fx_navred ,

light.1=3, -5.81, 54.7, 3.49, fx_navgre ,

light.2=2, -6.42, -55.3, 3.59, fx_strobe ,

light.3=2, -6.42, 55.3, 3.59, fx_strobe ,

light.4=1, 14.15, 0.0, -4.90, fx_beaconh ,

light.5=1, 11.52, 0.0, 9.55, fx_beaconh ,

light.6=2,-54.23, 0.17, 5.19, fx_strobe ,

light.7=3,-54.23, -0.17, 5.19, fx_navwhi ,

light.8 = 4, 39, 0, 5.7, fx_vclighth

 

[General]

atc_type=AIRBUS

atc_model=A319

performance=Dimensions: Wing span: 111 ft 10 in (33.91 m) \n Length: 111 ft 0 in (33.84 m) \n Height: 38 ft 7 in (11.76 m) \n Weights: \n Empty: 89,000 lb \n Max take-off: 166,000 lb \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Maximum range: 3,700 miles (6,800 km) \n Powerplants: Two IAE V2525-A5 rated at 23.500 lbs (111.2 kN) or Two CFM International CFM56-5B4 rated at 22.000 lbs. Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position=0, 0, -4.4

max_number_of_stations=50

 

station_load.0 = "450, 42.0, 0.0, 0.0, Crew"

station_load.1 = "1000, 37.0, 0.0, 0.0, Galleys"

station_load.2 = "4000, 16.0, 0.0, 0.0, Baggage"

station_load.3 = "7000, 0.0, 0.0, 0.0, Cargo"

station_load.4 = "6200, 26.0, 0.0, 0.0, First"

station_load.5 = "17000, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 89500

max_gross_weight=167300

empty_weight_roll_MOI=1300000

empty_weight_pitch_MOI=2000000

empty_weight_yaw_MOI=2000000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=30

rated_N2_rpm=29920.000000

static_thrust=22700.000000

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type=1

Engine.0= 3.0, -17.5, -2.500000

Engine.1= 3.0, 17.5, -2.500000

fuel_flow_scalar=1.0000

min_throttle_limit=-0.499939

max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear

 

[jet_engine]

thrust_scalar =1.1

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=13.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=29.0 //ditto to accomodate flap 2

flaps-position.5=40.0 //More lift for patched solution to low lift RY

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000

LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000

RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000

LeftAux= 0.0, -13.0, 0.0, 227.000000, 0.000000

RightAux= 0.0, 13.0, 0.0, 227.000000, 0.000000

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=1320.000000

wing_span=111.9

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.8723

wing_winglets_flag=1

wing_sweep=22

wing_pos_apex_lon=15.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

point.0=1, 35.80, 0.00, -10.56, 1500, 0, 1.25, 60.12, 0.38, 2.4, 0.5135, 7.0, 8.2, 0, 0.0, 0.0

point.1=1, -4.25, -11.58, -11.06, 2200, 1, 2.15, 0.00, 1.11, 2.0, 0.5470, 9.7, 14.1, 2, 0.0, 0.0

point.2=1, -4.25, 11.58, -11.06, 2200, 2, 2.15, 0.00, 1.11, 2.0, 0.5470, 9.7, 14.1, 3, 0.0, 0.0

 

point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0

point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0

point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0

point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0

 

max_number_of_points=21

 

static_pitch= -0.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn)

static_cg_height=14.26 //feet, altitude of CG when at rest on the ground

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.86

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=352.000000

max_mach=0.84

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=2

 

 

[turn_indicators]

turn_indicator.0=1,0

 

 

 

Airbus A320

 

[exits]

number_of_exits=2

exit_rate.0=0.25

exit_rate.1=0.25

 

 

[Views]

eyepoint=53.95, -1.85, 5.13 //(feet) longitudinal, lateral, vertical distance from reference datum

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0=3, -5.81, -54.7, 3.09, fx_navredm ,

light.1=3, -5.81, 54.7, 3.09, fx_navgrem ,

light.2=2, -6.42, -55.3, 3.09, fx_strobeh ,

light.3=2, -6.42, 55.3, 3.09, fx_strobeh ,

light.4=1, 14.15, 0.0, -4.70, fx_beaconb ,

light.5=1, 11.52, 0.0, 9.15, fx_beaconh ,

light.6=2,-61.83, -0.17, 4.79, fx_strobe ,

light.7=3,-61.83, 0.17, 4.79, fx_navwhi ,

light.8 = 4, 53.5, 0, 5.4, fx_vclighth

 

 

[General]

atc_type=AIRBUS

atc_model=A320

performance=Dimensions: Wing span: 111 ft 10 in (33.91 m) \n Length: 123 ft 3 in (37.57 m) \n Height: 38 ft 9.50 in (11.80 m) \n Weights: \n Empty: 91,675 lb (41,583 kg) \n Max take-off: 169,765 lb (77,000 kg) \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Maximum range: 3,222 miles (5,185 km) \n Powerplants: Two IAE V2525-A5 rated at 25,000 lb (111.2 kN) or Two CFM International CFM56-5B4 rated at 26,500 lb (117.9 kN). Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position=0.000000,0.000000,-4.000000

max_number_of_stations=50

 

station_load.0 = "450, 42.0, 0.0, 0.0, Crew"

station_load.1 = "1000, 37.0, 0.0, 0.0, Galleys"

station_load.2 ="6598, 16.0, 0.0, 0.0, Baggage"

station_load.3 ="9499, 0.0, 0.0, 0.0, Cargo"

station_load.4 ="1653, 26.0, 0.0, 0.0, First"

station_load.5 ="18187, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 93500

max_gross_weight=169800

empty_weight_roll_MOI=1700000

empty_weight_pitch_MOI=2500000

empty_weight_yaw_MOI=2700000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=30

rated_N2_rpm=29920.000000

static_thrust=27000.000000

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type=1

Engine.0= -2.25, -18.9, -4.600000

Engine.1= -2.25, 18.9, -4.600000

fuel_flow_scalar=1.0000

min_throttle_limit=-0.499939

 

[jet_engine]

thrust_scalar =0.95

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=10.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000

LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000

RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000

LeftAux= 0.0, -13.0, 0.0, 227.000000, 0.000000

RightAux= 0.0, 13.0, 0.0, 227.000000, 0.000000

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=1320.000000

wing_span=111.9

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.8

wing_winglets_flag=1

wing_sweep=22

wing_pos_apex_lon=15.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

[contact_points]

 

point.0=1.0, 41.66, 0.00, -11.03, 6000.8, 0.00, 1.79, 75.00, 0.50, 2.50, 0.60, 9.00, 9.00, 0.00, 0.00, 0.00

point.1=1.0, -4.16, -12.33, -11.70, 6000.8, 1.00, 1.79, 0.00, 1.29, 2.50, 0.60, 12.00, 12.00, 2.00, 0.00, 0.00

point.2=1.0, -4.16, 12.33, -11.70, 6000.8, 2.00, 1.79, 0.00, 1.29, 2.50, 0.60, 13.00, 13.00, 3.00, 0.00, 0.00

;point.3=2.0, -14.16, -47.33, 0.00, 787.4, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00

;point.4=2.0, -14.16, 47.33, 0.00, 787.4, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00

;point.5=2.0, -54.00, 0.00, 2.83, 787.4, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00

;point.6=2.0, 42.66, 0.00 ,-3.75, 787.4, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00

 

 

static_pitch= 0.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn)

static_cg_height=15.02 //feet, altitude of CG when at rest on the ground

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.86

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=352.000000

max_mach=0.84

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

gs_proportional_control=19.0

gs_integrator_control=0.530

gs_derivative_control=0.00

gs_integrator_boundary=0.70

gs_derivative_boundary=0.00

yaw_damper_gain=0.000000

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=2

 

 

[turn_indicators]

turn_indicator.0=1,0

 

 

Airbus A321

 

[exits]

number_of_exits=2

exit.0 = 0.25, 53.5, -5.5, 2.8, 0

exit.1 = 0.4, -23.5, 5.0, -2.2, 1

 

[Views]

eyepoint=61.73, -1.65, 5.25

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0= 1, 9.55, 0.0, -4.84, fx_beaconb ,

light.1= 1, 6.32, 0.0, 9.45, fx_beaconh ,

light.2= 2,-75.95, -0.17, 5.19, fx_strobe ,

light.3= 3,-75.95, 0.17, 5.19, fx_navwhi ,

light.4= 4, 60.90, 0.0, 6.70, fx_vclighth //61.73, -1.65, 5.25

 

 

[General]

atc_type=AIRBUS

atc_model=A321

performance=Dimensions: Wing span: 111 ft 10 in (33.91 m) \n Length: 123 ft 3 in (37.57 m) \n Height: 38 ft 9.50 in (11.80 m) \n Weights: \n Empty: 106,00 lb \n Max take-off: 196,000 lb \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Maximum range: 3,222 miles (5,185 km) \n Powerplants: Two IAE V2525-A5 rated at 25,000 lb (111.2 kN) or Two CFM International CFM56-5B4 rated at 32.000 lbs. Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position= 5, 0, -4.4

max_number_of_stations=50

 

station_load.0 = "450, 42.0, 0.0, 0.0, Crew"

station_load.1 = "1000, 37.0, 0.0, 0.0, Galleys"

station_load.2 = "5000, 16.0, 0.0, 0.0, Baggage"

station_load.3 = "7000, 0.0, 0.0, 0.0, Cargo"

station_load.4 = "7200, 26.0, 0.0, 0.0, First"

station_load.5 = "20000, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 106300

max_gross_weight=196210

empty_weight_roll_MOI=1700000

empty_weight_pitch_MOI=2500000

empty_weight_yaw_MOI=2700000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=30

rated_N2_rpm=29920.000000

static_thrust=33000.000000

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop

Engine.0=3.25, -18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datum

Engine.1=3.25, 18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datum

fuel_flow_scalar=1.26 //Scalar for fuel flow efficiency

min_throttle_limit=-0.330000

max_contrail_temperature = -30

 

[jet_engine]

thrust_scalar =1.0

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 0.0, 0.0, 0.0, 2118.000000, 0.000000

LeftMain= 0.0, -8.0, 0.0, 2001.000000, 0.000000

RightMain= 0.0, 8.0, 0.0, 2001.000000, 0.000000

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=1320.000000

wing_span=111.9

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.8723

wing_winglets_flag=1

wing_sweep=22

wing_pos_apex_lon=15.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

point.0=1, 54.80, 0.00, -10.61, 1500, 0, 1.25, 60.12, 0.50, 2.1, 0.8135,11.0, 13.2, 0, 0.0, 0.0

point.1=1, -3.95, -11.58, -11.56, 2200, 1, 2.15, 0.00, 1.51, 2.0, 0.7470, 9.7, 14.1, 2, 0.0, 0.0

point.2=1, -3.95, 11.58, -11.56, 2200, 2, 2.15, 0.00, 1.51, 2.0, 0.7470, 9.7, 14.1, 3, 0.0, 0.0

 

point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0

point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0

point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0

point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0

 

max_number_of_points=21

 

static_pitch=-0.22 //degrees, pitch when at rest on the ground (+=Up, -=Dn)

static_cg_height=14.56 //feet, altitude of CG when at rest on the ground

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.86

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=352.000000

max_mach=0.84

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=2

 

 

[turn_indicators]

turn_indicator.0=1,0

 

 

Airbus A330-200

 

[exits]

number_of_exits=2

exit.0 = 0.25, 78.0, -7.5, 8.5, 0

exit.1 = 0.05, -37.0, 7.0, -4.0, 1

 

[Views]

eyepoint=88.74, -1.80, 5.85

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.1 = 1, 30.66, 0.00, -7.58, fx_beaconb ,

light.2 = 1, 17.40, 0.00, 11.93, fx_beaconh ,

light.3 = 2, -97.42, 0.00, 9.00, fx_strobe ,

light.4 = 3, -97.42, 0.00, 9.00, fx_navwhi ,

light.5 = 4, 88.9, 0, 7.3, fx_vclighth

 

 

[General]

atc_type=AIRBUS

atc_model=A330-200

performance=Dimensions: Wing span: 197 ft 10 in \n Length: 188ft 8 in \n Height: 57ft 1 in \n Weights: \n Empty: 274,000 lb \n Max take-off: 513,000 \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Powerplants: Two RR Trent 700 rated at 68,000 lbs (111.2 kN) or Two CF6-80E1 rated at 67.500 lbs. Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position = 0.000, 0.000, -6.000

max_number_of_stations=50

 

station_load.0 = "750, 42.0, 0.0, 0.0, Crew"

station_load.1 = "2000, 37.0, 0.0, 0.0, Galleys"

station_load.2 ="29104, 16.0, 0.0, 0.0, Baggage"

station_load.3 ="23518, 0.0, 0.0, 0.0, Cargo"

station_load.4 ="2480, 26.0, 0.0, 0.0, First"

station_load.5 ="34556, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 264875

max_gross_weight=507050

empty_weight_roll_MOI=21100000

empty_weight_pitch_MOI=21400000

empty_weight_yaw_MOI=15800000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=55

rated_N2_rpm=29920.000000

static_thrust=71100.000000 // CF Engines

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type= 1

Engine.0= 12.600, -29.900, -6.100

Engine.1= 12.600, 29.900, -6.100

fuel_flow_scalar= 1.06

min_throttle_limit=-0.250000

 

[jet_engine]

thrust_scalar =0.96 //300-200 only

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 4.0, 0.0, 0.0, 10980.0, 0.0

Center2= -4.0, 0.0, 0.0, 1646.0, 0.0

LeftMain= -2.0, -4.0, 0.0, 11095.0, 0.0

RightMain= -2.0, 4.0, 0.0, 11095.0, 0.0

LeftAux= -7.0, -13.0, 0.0, 964.0, 0.0

RightAux= -7.0, 13.0, 0.0, 964.0, 0.0

 

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=3892

wing_span=198

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.8723

wing_winglets_flag=1

wing_sweep=30

wing_pos_apex_lon=35.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

 

point.0= 1.000, 75.420, 0.000, -14.220, 1181.100, 0.000, 1.777, 70.000, 0.500, 2.100, 0.814, 11.000, 13.200, 0.000, 0.000, 0.000

point.1= 1.000, -7.200, -15.800, -15.840, 1574.800, 1.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 2.000, 0.000, 0.000

point.2= 1.000, -7.200, 15.800, -15.840, 1574.800, 2.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 3.000, 0.000, 0.000

 

point.3= 2.000, -10.170, -47.330, 0.000, 787.400, 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, -10.170, 47.330, 0.000, 787.400, 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, -83.330, 0.000, 2.500, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

 

 

static_pitch= -0.830

static_cg_height= 20.670

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.66

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=358.000000

max_mach=0.865

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=1

 

 

[turn_indicators]

turn_indicator.0=1,0

 

 

 

Airbus A330-300

 

[exits]

number_of_exits=2

exit.0 = 0.25, 86.0, -7.5, 8.5, 0

exit.1 = 0.05, -42.0, 7.0, -4.0, 1

 

 

[Views]

eyepoint=98.07, -1.80, 5.85

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.1 = 1, 30.66, 0.00, -7.58, fx_beaconb ,

light.2 = 1, 17.40, 0.00, 11.93, fx_beaconh ,

light.3 = 2, -97.42, 0.00, 9.00, fx_strobe ,

light.4 = 3, -97.42, 0.00, 9.00, fx_navwhi ,

light.5 = 4, 88.9, 0, 7.3, fx_vclighth

 

 

[General]

atc_type=AIRBUS

atc_model=A330-300

performance=Dimensions: Wing span: 197 ft 10 in \n Length: 165ft 3 in \n Height: 55ft in \n Weights: \n Empty: 274,000 lb \n Max take-off: 513,000 \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Powerplants: Two RR Trent 700 rated at 68,000 lbs (111.2 kN) or Two CF6-80E1 rated at 72.500 lbs. Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position=0.000, 0.000, -6.000

max_number_of_stations=50

 

station_load.0 = "750, 42.0, 0.0, 0.0, Crew"

station_load.1 = "2000, 37.0, 0.0, 0.0, Galleys"

station_load.2 ="41324, 16.0, 0.0, 0.0, Baggage"

station_load.3 ="35482, 0.0, 0.0, 0.0, Cargo"

station_load.4 ="4960, 26.0, 0.0, 0.0, First"

station_load.5 ="40013, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 267000

max_gross_weight=509000

empty_weight_roll_MOI=21300000

empty_weight_pitch_MOI=21900000

empty_weight_yaw_MOI=16100000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=55

rated_N2_rpm=29920.000000

static_thrust=71100.000000

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type= 1

Engine.0= 10.600, -29.900, -6.100

Engine.1= 10.600, 29.900, -6.100

fuel_flow_scalar= 0.8900

min_throttle_limit=-0.350000

 

[jet_engine]

thrust_scalar =0.98

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 4.0, 0.0, 0.0, 0.0, 0.0

Center2= -4.0, 0.0, 0.0, 1615.0, 0.0

LeftMain= -2.0, -4.0, 0.0, 11025.0, 0.0

RightMain= -2.0, 4.0, 0.0, 11025.0, 0.0

LeftAux= -7.0, -13.0, 0.0, 974.0, 0.0

RightAux= -7.0, 13.0, 0.0, 974.0, 0.0

 

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=3892

wing_span=198

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.892

wing_winglets_flag=1

wing_sweep=30

wing_pos_apex_lon=35.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

 

point.0= 1.000, 84.420, 0.000, -14.220, 1181.100, 0.000, 1.777, 70.000, 0.500, 2.100, 0.814, 11.000, 13.200, 0.000, 0.000, 0.000

point.1= 1.000, -7.200, -15.800, -15.840, 1574.800, 1.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 2.000, 0.000, 0.000

point.2= 1.000, -7.200, 15.800, -15.840, 1574.800, 2.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 3.000, 0.000, 0.000

 

point.3= 2.000, -10.170, -47.330, 0.000, 787.400, 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, -10.170, 47.330, 0.000, 787.400, 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, -83.330, 0.000, 2.500, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

 

 

static_pitch= -0.830

static_cg_height= 20.670

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.66

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=358.000000

max_mach=0.865

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=1

 

 

[turn_indicators]

turn_indicator.0=1,0

 

 

 

Airbus A340-600

 

[exits]

number_of_exits=2

exit_rate.0=0.25

exit_rate.1=0.25

 

[Views]

eyepoint=117.02, -1.75, 3.88

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.1 = 1, 27.70, -0.01, -9.85, fx_beaconb ,

light.2 = 1, 10.40, -0.01, 10.10, fx_beaconh ,

light.3 = 2, -112.08, 0.00, 7.00, fx_strobe ,

light.4 = 3, -112.08, 0.00, 7.00, fx_navwhi ,

light.5 = 4, 98.5, 0, 4.4, fx_vclighth

 

[General]

atc_type=AIRBUS

atc_model=A340-600

performance=Dimensions: Wing span: 208 ft 2 in \n Length: 200 ft \n Height: 56 ft. 9 in \n Weights: \n Empty: 390,220 lb \n Max take-off: 804,675 \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Powerplants: Four RR Trent 700 rated at 56,000 lbs (111.2 kN)

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position = 2.000, 0.000, -4.000

empty_weight_CG_position = -4.000, 0.000, 0.000

max_number_of_stations=50

 

station_load.0 = "950, 42.0, 0.0, 0.0, Crew"

station_load.1 = "5000, 37.0, 0.0, 0.0, Galleys"

station_load.2 ="45357, 16.0, 0.0, 0.0, Baggage"

station_load.3 ="36706, 0.0, 0.0, 0.0, Cargo"

station_load.4 ="4960, 26.0, 0.0, 0.0, First"

station_load.5 ="57043, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 390220

max_gross_weight=804675

empty_weight_pitch_MOI= 18587807.000

empty_weight_roll_MOI = 10295476.000

empty_weight_yaw_MOI = 30160328.000

empty_weight_coupled_MOI=0.0

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=57

rated_N2_rpm=29920.000000

static_thrust=56000.000000 // Trent Engines for A340-600

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type= 1

Engine.0= -17.420, -67.700, -5.550

Engine.1= 6.600, -31.900, -9.300

Engine.2= 6.600, 31.900, -9.300

Engine.3= -17.420, 67.700, -5.550

fuel_flow_scalar= 0.79

min_throttle_limit=-0.250000

 

[jet_engine]

thrust_scalar =0.96 //340-600 only

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.5

drag_scalar=0.1

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 4.0, 0.0, 0.0, 14521.0, 0.0 // Middle Fuselage Main Centre Tank

Center2= -33.0, 0.0, 0.0, 2209.0, 0.0 // Trim Tank in Tail-plane sectin

LeftMain= -2.0, -6.0, 0.0, 9182.0, 0.0 // Inner Wing Tank 2 Left

RightMain= -2.0, 6.0, 0.0, 9182.0, 0.0 // Inner Wing Tank 3 Right

LeftAux= -6.0, -15.0, 0.0, 6472.0, 0.0 // Inner Wing Tank 1 Left

RightAux= -6.0, 15.0, 0.0, 6472.0, 0.0 // InnerWing Tank 4 Right

LeftTip= -12.0, -20.0, 0.0, 1623.0, 0.0 // Outer Tank Left

RightTip= -12.0, 20.0, 0.0 1623.0 0.0 // Outer Tank Right

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=4729

wing_span=208.1

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.94

wing_winglets_flag=1

wing_sweep=30

wing_pos_apex_lon=38.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

 

//0 Class <0=none,1=wheel, 2=scrape, 3=float>

//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)

 

 

//Nose Gear

point.0 = 1.000, 116.854, -1.333, -21.017, 1181.102, 0.000, 2.422, 65.200, 1.000, 3.217, 0.510, 7.000, 9.000, 0.000, 280.000, 300.000

point.1 = 1.000, 116.854, 1.333, -21.017, 1181.102, 0.000, 2.422, 65.200, 1.000, 3.217, 0.510, 7.000, 9.000, 0.000, 280.000, 300.000

 

//Main Gear (Left)

point.2 = 1.000, -11.067, -19.821, -21.200, 1574.803, 1.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000

point.3 = 1.000, -11.067, -15.239, -21.200, 1574.803, 1.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000

point.4 = 1.000, -7.817, -19.821, -21.200, 1574.803, 1.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000

point.5 = 1.000, -7.817, -15.239, -21.200, 1574.803, 1.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000

 

//Main Gear (Right)

point.6 = 1.000, -11.067, 19.821, -21.200, 1574.803, 2.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000

point.7 = 1.000, -11.067, 15.239, -21.200, 1574.803, 2.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000

point.8 = 1.000, -7.817, 19.821, -21.200, 1574.803, 2.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000

point.9 = 1.000, -7.817, 15.239, -21.200, 1574.803, 2.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000

 

// Main Gear (Center)

point.10= 1.000, -11.067, 1.916, -21.200, 1574.803, 2.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000

point.11= 1.000, -11.067, -1.916, -21.200, 1574.803, 1.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000

point.12= 1.000, -7.817, 1.916, -21.200, 1574.803, 2.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000

point.13= 1.000, -7.817, -1.916, -21.200, 1574.803, 1.000, 2.422, -8.000, 1.000, 1.200, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000

 

// Scrape Points

// Fuselage

point.14 = 2, 120.000, 0.000, 3.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Nose

point.15 = 2, 110.000, 0.000, -6.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom fwd

point.16 = 2, 0.000, 0.000, -9.250, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom center

point.17 = 2, -60.000, 0.000, -9.250, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom aft

 

point.18 = 2, 110.000, 0.000, 6.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top fwd

point.19 = 2, 0.000, 0.000, 9.250, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top center

point.20 = 2, -60.000, 0.000, 9.250, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top aft

 

point.21= 2, 80.000, -9.250, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width fwd lt

point.22= 2, 80.000, 9.250, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width fwd rt

point.23= 2, 0.000, -9.250, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width center lt

point.24= 2, 0.000, 9.250, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width center rt

point.25= 2, -60.000, -9.250, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width aft left

point.26= 2, -60.000, 9.250, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width aft right

point.27= 2, -100.000, 0.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Tailskid aft

point.28= 2, -124.000, 0.000, 8.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Tail-APU

 

// Tailplane, vert/horiz stabs

point.29= 2, -118.000, 0.000, 41.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7, 0.000, 0.000 // Vertical stab fwd

point.30= 2, -130.000, 0.000, 41.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7, 0.000, 0.000 // Vertical stab aft

point.31= 2, -121.000, -37.600, 11.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Horizontal Stab aft lt

point.32= 2, -133.000, 37.600, 11.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Horizontal Stab aft rt

 

// Wings

point.33= 2, -33.000, -104.080, 7.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wingtip fwd

point.34= 2, -46.000, -104.080, 7.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wingtip aft

point.35= 2, -33.000, 104.080, 7.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wingtip fwd

point.36= 2, -46.000, 104.080, 7.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wingtip aft

point.37= 2, 4.000, -50.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wing-mid fwd

point.38= 2, -22.000, -50.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wing-mid aft

point.39= 2, 4.000, 50.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wing-mid fwd

point.40= 2, -22.000, 50.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wing-mid aft

 

// Inboard Engines

point.41= 2, 20.000, -30.740, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine fwd

point.42= 2, 20.000, 30.740, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine fwd

point.43= 2, 20.000, -30.740,-17.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine bottom

point.44= 2, 20.000, 30.740,-17.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine bottom

 

// Outboard Engines

point.45= 2, 0.000, -63.220, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine fwd

point.46= 2, 0.000, 63.220, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine fwd

point.47= 2, 0.000, -63.220, -9.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine bottom

point.48= 2, 0.000, 63.220, -9.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine bottom

 

max_number_of_points = 50

static_pitch= -0.600 //degrees, pitch when at rest on the ground (+=Up, -=Dn)

static_cg_height= 20.000 //feet, altitude of CG when at rest on the ground

gear_system_type=0 //Hydraulic

 

 

 

 

static_pitch=0.0

static_cg_height=17.4

gear_system_type=0

 

 

 

 

[brakes]

toe_brakes_scale=0.78

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=358.000000

max_mach=0.865

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

 

Данные для двигателей PW

 

Airbus A330-200

 

[exits]

number_of_exits=2

exit.0 = 0.25, 78.0, -7.5, 8.5, 0

exit.1 = 0.05, -37.0, 7.0, -4.0, 1

 

[Views]

eyepoint=88.74, -1.80, 5.85

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.1 = 1, 30.66, 0.00, -7.58, fx_beaconb ,

light.2 = 1, 17.40, 0.00, 11.93, fx_beaconh ,

light.3 = 2, -97.42, 0.00, 9.00, fx_strobe ,

light.4 = 3, -97.42, 0.00, 9.00, fx_navwhi ,

light.5 = 4, 88.9, 0, 7.3, fx_vclighth

 

 

[General]

atc_type=AIRBUS

atc_model=A330-200

performance=Dimensions: Wing span: 197 ft 10 in \n Length: 188ft 8 in \n Height: 57ft 1 in \n Weights: \n Empty: 274,000 lb \n Max take-off: 513,000 \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Powerplants: Two RR Trent 700 rated at 68,000 lbs (111.2 kN) or Two CF6-80E1 rated at 67.500 lbs. Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position = 0.000, 0.000, -6.000

max_number_of_stations=50

 

station_load.0 = "750, 42.0, 0.0, 0.0, Crew"

station_load.1 = "2000, 37.0, 0.0, 0.0, Galleys"

station_load.2 ="29104, 16.0, 0.0, 0.0, Baggage"

station_load.3 ="23518, 0.0, 0.0, 0.0, Cargo"

station_load.4 ="2480, 26.0, 0.0, 0.0, First"

station_load.5 ="34556, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 264875

max_gross_weight=507050

empty_weight_roll_MOI=21100000

empty_weight_pitch_MOI=21400000

empty_weight_yaw_MOI=15800000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=55

rated_N2_rpm=29920.000000

static_thrust=68600.000000 // CF Engines

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type= 1

Engine.0= 12.600, -29.900, -6.100

Engine.1= 12.600, 29.900, -6.100

fuel_flow_scalar= 1.06

min_throttle_limit=-0.250000

 

[jet_engine]

thrust_scalar =0.96 //300-200 only

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 4.0, 0.0, 0.0, 10980.0, 0.0

Center2= -4.0, 0.0, 0.0, 1646.0, 0.0

LeftMain= -2.0, -4.0, 0.0, 11095.0, 0.0

RightMain= -2.0, 4.0, 0.0, 11095.0, 0.0

LeftAux= -7.0, -13.0, 0.0, 964.0, 0.0

RightAux= -7.0, 13.0, 0.0, 964.0, 0.0

 

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=3892

wing_span=198

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.8723

wing_winglets_flag=1

wing_sweep=30

wing_pos_apex_lon=35.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

 

point.0= 1.000, 75.420, 0.000, -14.220, 1181.100, 0.000, 1.777, 70.000, 0.500, 2.100, 0.814, 11.000, 13.200, 0.000, 0.000, 0.000

point.1= 1.000, -7.200, -15.800, -15.840, 1574.800, 1.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 2.000, 0.000, 0.000

point.2= 1.000, -7.200, 15.800, -15.840, 1574.800, 2.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 3.000, 0.000, 0.000

 

point.3= 2.000, -10.170, -47.330, 0.000, 787.400, 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, -10.170, 47.330, 0.000, 787.400, 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, -83.330, 0.000, 2.500, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

 

 

static_pitch= -0.830

static_cg_height= 20.670

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.66

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=358.000000

max_mach=0.865

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=1

 

 

[turn_indicators]

turn_indicator.0=1,0

 

 

 

Airbus A330-300

 

[exits]

number_of_exits=2

exit.0 = 0.25, 86.0, -7.5, 8.5, 0

exit.1 = 0.05, -42.0, 7.0, -4.0, 1

 

 

[Views]

eyepoint=98.07, -1.80, 5.85

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.1 = 1, 30.66, 0.00, -7.58, fx_beaconb ,

light.2 = 1, 17.40, 0.00, 11.93, fx_beaconh ,

light.3 = 2, -97.42, 0.00, 9.00, fx_strobe ,

light.4 = 3, -97.42, 0.00, 9.00, fx_navwhi ,

light.5 = 4, 88.9, 0, 7.3, fx_vclighth

 

 

[General]

atc_type=AIRBUS

atc_model=A330-300

performance=Dimensions: Wing span: 197 ft 10 in \n Length: 165ft 3 in \n Height: 55ft in \n Weights: \n Empty: 274,000 lb \n Max take-off: 513,000 \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Powerplants: Two RR Trent 700 rated at 68,000 lbs (111.2 kN) or Two CF6-80E1 rated at 72.500 lbs. Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position=0.000, 0.000, -6.000

max_number_of_stations=50

 

station_load.0 = "750, 42.0, 0.0, 0.0, Crew"

station_load.1 = "2000, 37.0, 0.0, 0.0, Galleys"

station_load.2 ="41324, 16.0, 0.0, 0.0, Baggage"

station_load.3 ="35482, 0.0, 0.0, 0.0, Cargo"

station_load.4 ="4960, 26.0, 0.0, 0.0, First"

station_load.5 ="40013, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 267000

max_gross_weight=509000

empty_weight_roll_MOI=21300000

empty_weight_pitch_MOI=21900000

empty_weight_yaw_MOI=16100000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=55

rated_N2_rpm=29920.000000

static_thrust=68600.000000

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type= 1

Engine.0= 10.600, -29.900, -6.100

Engine.1= 10.600, 29.900, -6.100

fuel_flow_scalar= 0.8900

min_throttle_limit=-0.350000

 

[jet_engine]

thrust_scalar =0.98

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 4.0, 0.0, 0.0, 0.0, 0.0

Center2= -4.0, 0.0, 0.0, 1615.0, 0.0

LeftMain= -2.0, -4.0, 0.0, 11025.0, 0.0

RightMain= -2.0, 4.0, 0.0, 11025.0, 0.0

LeftAux= -7.0, -13.0, 0.0, 974.0, 0.0

RightAux= -7.0, 13.0, 0.0, 974.0, 0.0

 

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=3892

wing_span=198

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.892

wing_winglets_flag=1

wing_sweep=30

wing_pos_apex_lon=35.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

 

point.0= 1.000, 84.420, 0.000, -14.220, 1181.100, 0.000, 1.777, 70.000, 0.500, 2.100, 0.814, 11.000, 13.200, 0.000, 0.000, 0.000

point.1= 1.000, -7.200, -15.800, -15.840, 1574.800, 1.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 2.000, 0.000, 0.000

point.2= 1.000, -7.200, 15.800, -15.840, 1574.800, 2.000, 2.369, 0.000, 1.510, 2.000, 0.747, 9.700, 14.100, 3.000, 0.000, 0.000

 

point.3= 2.000, -10.170, -47.330, 0.000, 787.400, 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, -10.170, 47.330, 0.000, 787.400, 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, -83.330, 0.000, 2.500, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

 

 

static_pitch= -0.830

static_cg_height= 20.670

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.66

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=358.000000

max_mach=0.865

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=1

 

 

[turn_indicators]

turn_indicator.0=1,0

 

 

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Мержи ВК

 

На авсим.коме лежат обновленные текстуры от Pablo Diaz-a, вбиваем в поиске имя и уже 2я ссылка(А340-600 Иберии), выбираем и скачиваем. 26Мб

 

 

1. Открываем папку PANEL

2. Открываем файл PANEL.cfg

3. Листаем почти до самого низа, собственно ищем:

[Vcockpit01]

4. Дальше действуем по прицнипу выше описанному.

Все ниже или заменяем, или стираем и вносим заново...

 

Airbus A330-200 GE

 

[Vcockpit01]

Background_color=0,0,0

size_mm=512

visible=1

pixel_size=512

texture=$g1

 

gauge00=A332GE_feelThere!Standby Airspeed, 5,1,133,123

gauge01=A332GE_feelThere!Standby Altimeter, 143,2,132,124

gauge02=A332GE_feelThere!Standby Attitude VC, 6,132,150,144

gauge03=A332GE_feelThere!Baro, 314,333,98,129

gauge04=A332GE_feelThere!Analog Clock, 278,-1,127,128

gauge05=PAPA330!Engine Start Knob 1, 409,1,48,49

gauge06=PAPA330!Engine Start Knob 2, 462,2,46,48

gauge07=A332GE_feelThere!Chrono, 164,201,65,67

gauge08=A332GE_feelThere!Warnings, 163,130,64,146

gauge09=PAPA330!ABS Aps Window, 47,469,459,40

gauge10=PAPA330!Flight Director Switch, 417,280,41,35

gauge11=PAPA330!Autopilot ILS Switch, 417,318,40,35

gauge12=PAPA330!Autopilot IAS-Mach Switch, 416,356,41,33

gauge13=PAPA330!Autopilot Speed Switch, 417,394,40,34

gauge14=PAPA330!Autopilot Localizer Switch, 417, 431 ,40,33

gauge15=PAPA330!Autopilot Master Switch, 462,280,41,33

gauge16=PAPA330!Autopilot Master Switch, 463,318,40,35

gauge17=PAPA330!Autothrottle Switch, 463,356,41,35

gauge18=PAPA330!Autopilot Altitude Hold Switch, 463,394,40,35

gauge19=A332GE_feelThere!DDRMI, 5,284,138,175

gauge20=PAPA330!Autopilot Approach Switch, 463,431,40,35

gauge21=A332GE_feelThere!Icon Bar, 461,55,41,43

gauge22=simicons!GPS Icon, 464,149,39,40

gauge23=simicons!Map Icon, 415,103,40,41

gauge24=simicons!Kneeboard Icon, 414,56,42,41

gauge25=PAPA330!VC_Autobrakes Switch, 238,133,155,199

gauge26=PAPA330!VC_Anti Ice Eng1 Switch, 151,341,30,28

gauge27=PAPA330!VC_Anti Ice Eng2 Switch, 184,341,30,28

 

 

// ---------------------------------------------------------

 

[Vcockpit02]

Background_color=0,0,0

size_mm=512

visible=1

pixel_size=512

texture=$ABmain

 

gauge00=A332GE_feelThere!System,0,0,0,0

gauge01=A332GE_feelThere!Primary Flight Display, 6,10,228,208

gauge02=A332GE_feelThere!Navigation Display, 245,5,263,267

gauge03=A332GE_feelThere!Engine/Warning Display, 3,268,233,230

gauge04=A332GE_feelThere!System Display, 248,315,196,187

 

// ---------------------------------------------------------

 

[Default View]

X=0

Y=0

SIZE_X=8192

SIZE_Y=2600

 

Day=255,255,255

Night=255,255,255

Luminous=255,255,255

 

 

 

Airbus A330-200 RR

 

[Vcockpit01]

Background_color=0,0,0

size_mm=512

visible=1

pixel_size=512

texture=$g1

 

gauge00=A332RR_feelThere!Standby Airspeed, 5,1,133,123

gauge01=A332RR_feelThere!Standby Altimeter, 143,2,132,124

gauge02=A332RR_feelThere!Standby Attitude VC, 6,132,150,144

gauge03=A332RR_feelThere!Baro, 314,333,98,129

gauge04=A332RR_feelThere!Analog Clock, 278,-1,127,128

gauge05=PAPA330!Engine Start Knob 1, 409,1,48,49

gauge06=PAPA330!Engine Start Knob 2, 462,2,46,48

gauge07=A332RR_feelThere!Chrono, 164,201,65,67

gauge08=A332RR_feelThere!Warnings, 163,130,64,146

gauge09=PAPA330!ABS Aps Window, 47,469,459,40

gauge10=PAPA330!Flight Director Switch, 417,280,41,35

gauge11=PAPA330!Autopilot ILS Switch, 417,318,40,35

gauge12=PAPA330!Autopilot IAS-Mach Switch, 416,356,41,33

gauge13=PAPA330!Autopilot Speed Switch, 417,394,40,34

gauge14=PAPA330!Autopilot Localizer Switch, 417, 431 ,40,33

gauge15=PAPA330!Autopilot Master Switch, 462,280,41,33

gauge16=PAPA330!Autopilot Master Switch, 463,318,40,35

gauge17=PAPA330!Autothrottle Switch, 463,356,41,35

gauge18=PAPA330!Autopilot Altitude Hold Switch, 463,394,40,35

gauge19=A332RR_feelThere!DDRMI, 5,284,138,175

gauge20=PAPA330!Autopilot Approach Switch, 463,431,40,35

gauge21=A332RR_feelThere!Icon Bar, 461,55,41,43

gauge22=simicons!GPS Icon, 464,149,39,40

gauge23=simicons!Map Icon, 415,103,40,41

gauge24=simicons!Kneeboard Icon, 414,56,42,41

gauge25=PAPA330!VC_Autobrakes Switch, 238,133,155,199

gauge26=PAPA330!VC_Anti Ice Eng1 Switch, 151,341,30,28

gauge27=PAPA330!VC_Anti Ice Eng2 Switch, 184,341,30,28

 

 

// ---------------------------------------------------------

 

[Vcockpit02]

Background_color=0,0,0

size_mm=512

visible=1

pixel_size=512

texture=$ABmain

 

gauge00=A332RR_feelThere!System,0,0,0,0

gauge01=A332RR_FeelThere!Primary Flight Display, 6,10,228,208

gauge02=A332RR_FeelThere!Navigation Display, 245,5,263,267

gauge03=A332RR_FeelThere!Engine/Warning Display, 3,268,233,230

gauge04=A332RR_FeelThere!System Display, 248,315,196,187

 

// ---------------------------------------------------------

 

[Default View]

X=0

Y=0

SIZE_X=8192

SIZE_Y=2600

 

Day=255,255,255

Night=255,255,255

Luminous=255,255,255

 

 

Airbus A330-300 GE

 

[Vcockpit01]

Background_color=0,0,0

size_mm=512

visible=1

pixel_size=512

texture=$g1

 

gauge00=A333GE_feelThere!Standby Airspeed, 5,1,133,123

gauge01=A333GE_feelThere!Standby Altimeter, 143,2,132,124

gauge02=A333GE_feelThere!Standby Attitude VC, 6,132,150,144

gauge03=A333GE_feelThere!Baro, 314,333,98,129

gauge04=A333GE_feelThere!Analog Clock, 278,-1,127,128

gauge05=PAPA330!Engine Start Knob 1, 409,1,48,49

gauge06=PAPA330!Engine Start Knob 2, 462,2,46,48

gauge07=A333GE_feelThere!Chrono, 164,201,65,67

gauge08=A333GE_feelThere!Warnings, 163,130,64,146

gauge09=PAPA330!ABS Aps Window, 47,469,459,40

gauge10=PAPA330!Flight Director Switch, 417,280,41,35

gauge11=PAPA330!Autopilot ILS Switch, 417,318,40,35

gauge12=PAPA330!Autopilot IAS-Mach Switch, 416,356,41,33

gauge13=PAPA330!Autopilot Speed Switch, 417,394,40,34

gauge14=PAPA330!Autopilot Localizer Switch, 417, 431 ,40,33

gauge15=PAPA330!Autopilot Master Switch, 462,280,41,33

gauge16=PAPA330!Autopilot Master Switch, 463,318,40,35

gauge17=PAPA330!Autothrottle Switch, 463,356,41,35

gauge18=PAPA330!Autopilot Altitude Hold Switch, 463,394,40,35

gauge19=A333GE_feelThere!DDRMI, 5,284,138,175

gauge20=PAPA330!Autopilot Approach Switch, 463,431,40,35

gauge21=A333GE_feelThere!Icon Bar, 461,55,41,43

gauge22=simicons!GPS Icon, 464,149,39,40

gauge23=simicons!Map Icon, 415,103,40,41

gauge24=simicons!Kneeboard Icon, 414,56,42,41

gauge25=PAPA330!VC_Autobrakes Switch, 238,133,155,199

gauge26=PAPA330!VC_Anti Ice Eng1 Switch, 151,341,30,28

gauge27=PAPA330!VC_Anti Ice Eng2 Switch, 184,341,30,28

 

 

// ---------------------------------------------------------

 

[Vcockpit02]

Background_color=0,0,0

size_mm=512

visible=1

pixel_size=512

texture=$ABmain

 

gauge00=A333GE_feelThere!System,0,0,0,0

gauge01=A333GE_FeelThere!Primary Flight Display, 6,10,228,208

gauge02=A333GE_FeelThere!Navigation Display, 245,5,263,267

gauge03=A333GE_FeelThere!Engine/Warning Display, 3,268,233,230

gauge04=A333GE_FeelThere!System Display, 248,315,196,187

 

// ---------------------------------------------------------

 

[Default View]

X=0

Y=0

SIZE_X=8192

SIZE_Y=3072

 

Day=255,255,255

Night=255,255,255

Luminous=255,255,255

 

 

Airbus A330-300 RR

 

[Vcockpit01]

Background_color=0,0,0

size_mm=512

visible=1

pixel_size=512

texture=$g1

 

gauge00=A333RR_feelThere!Standby Airspeed, 5,1,133,123

gauge01=A333RR_feelThere!Standby Altimeter, 143,2,132,124

gauge02=A333RR_feelThere!Standby Attitude VC, 6,132,150,144

gauge03=A333RR_feelThere!Baro, 314,333,98,129

gauge04=A333RR_feelThere!Analog Clock, 278,-1,127,128

gauge05=PAPA330!Engine Start Knob 1, 409,1,48,49

gauge06=PAPA330!Engine Start Knob 2, 462,2,46,48

gauge07=A333RR_feelThere!Chrono, 164,201,65,67

gauge08=A333RR_feelThere!Warnings, 163,130,64,146

gauge09=PAPA330!ABS Aps Window, 47,469,459,40

gauge10=PAPA330!Flight Director Switch, 417,280,41,35

gauge11=PAPA330!Autopilot ILS Switch, 417,318,40,35

gauge12=PAPA330!Autopilot IAS-Mach Switch, 416,356,41,33

gauge13=PAPA330!Autopilot Speed Switch, 417,394,40,34

gauge14=PAPA330!Autopilot Localizer Switch, 417, 431 ,40,33

gauge15=PAPA330!Autopilot Master Switch, 462,280,41,33

gauge16=PAPA330!Autopilot Master Switch, 463,318,40,35

gauge17=PAPA330!Autothrottle Switch, 463,356,41,35

gauge18=PAPA330!Autopilot Altitude Hold Switch, 463,394,40,35

gauge19=A333RR_feelThere!DDRMI, 5,284,138,175

gauge20=PAPA330!Autopilot Approach Switch, 463,431,40,35

gauge21=A333RR_feelThere!Icon Bar, 461,55,41,43

gauge22=simicons!GPS Icon, 464,149,39,40

gauge23=simicons!Map Icon, 415,103,40,41

gauge24=simicons!Kneeboard Icon, 414,56,42,41

gauge25=PAPA330!VC_Autobrakes Switch, 238,133,155,199

gauge26=PAPA330!VC_Anti Ice Eng1 Switch, 151,341,30,28

gauge27=PAPA330!VC_Anti Ice Eng2 Switch, 184,341,30,28

 

 

// ---------------------------------------------------------

 

[Vcockpit02]

Background_color=0,0,0

size_mm=512

visible=1

pixel_size=512

texture=$ABmain

 

gauge00=A333RR_feelThere!System,0,0,0,0

gauge01=A333RR_FeelThere!Primary Flight Display, 6,10,228,208

gauge02=A333RR_FeelThere!Navigation Display, 245,5,263,267

gauge03=A333RR_FeelThere!Engine/Warning Display, 3,268,233,230

gauge04=A333RR_FeelThere!System Display, 248,315,196,187

 

// ---------------------------------------------------------

 

[Default View]

X=0

Y=0

SIZE_X=8192

SIZE_Y=3072

 

Day=255,255,255

Night=255,255,255

Luminous=255,255,255

 

 

Airbus A340-300 CFM

 

[Vcockpit01]

Background_color=0,0,0

size_mm=512

visible=1

pixel_size=512

texture=$g1

 

gauge00=A343CFM_feelThere!Standby Airspeed, 5,1,133,123

gauge01=A343CFM_feelThere!Standby Altimeter, 143,2,132,124

gauge02=A343CFM_feelThere!Standby Attitude VC, 6,132,150,144

gauge03=A343CFM_feelThere!Baro, 314,333,98,129

gauge04=A343CFM_feelThere!Analog Clock, 278,-1,127,128

gauge05=PAPA330!Engine Start Knob 1, 409,1,48,49

gauge06=PAPA330!Engine Start Knob 2, 462,2,46,48

gauge07=A343CFM_feelThere!Chrono, 164,201,65,67

gauge08=A343CFM_feelThere!Warnings, 163,130,64,146

gauge09=PAPA330!ABS Aps Window, 47,469,459,40

gauge10=PAPA330!Flight Director Switch, 417,280,41,35

gauge11=PAPA330!Autopilot ILS Switch, 417,318,40,35

gauge12=PAPA330!Autopilot IAS-Mach Switch, 416,356,41,33

gauge13=PAPA330!Autopilot Speed Switch, 417,394,40,34

gauge14=PAPA330!Autopilot Localizer Switch, 417, 431 ,40,33

gauge15=PAPA330!Autopilot Master Switch, 462,280,41,33

gauge16=PAPA330!Autopilot Master Switch, 463,318,40,35

gauge17=PAPA330!Autothrottle Switch, 463,356,41,35

gauge18=PAPA330!Autopilot Altitude Hold Switch, 463,394,40,35

gauge19=A343CFM_feelThere!DDRMI, 5,284,138,175

gauge20=PAPA330!Autopilot Approach Switch, 463,431,40,35

gauge21=A343CFM_feelThere!Icon Bar, 461,55,41,43

gauge22=simicons!GPS Icon, 464,149,39,40

gauge23=simicons!Map Icon, 415,103,40,41

gauge24=simicons!Kneeboard Icon, 414,56,42,41

gauge25=PAPA330!VC_Autobrakes Switch, 238,133,155,199

gauge26=PAPA330!VC_Anti Ice Eng1 Switch, 151,341,30,28

gauge27=PAPA330!VC_Anti Ice Eng2 Switch, 184,341,30,28

 

 

// ---------------------------------------------------------

 

[Vcockpit02]

Background_color=0,0,0

size_mm=512

visible=1

pixel_size=512

texture=$ABmain

 

gauge00=A343CFM_feelThere!System,0,0,0,0

gauge01=A343CFM_FeelThere!Primary Flight Display, 6,10,228,208

gauge02=A343CFM_FeelThere!Navigation Display, 245,5,263,267

gauge03=A343CFM_FeelThere!Engine/Warning Display, 3,268,233,230

gauge04=A343CFM_FeelThere!System Display, 248,315,196,187

 

// ---------------------------------------------------------

 

[Default View]

X=0

Y=0

SIZE_X=8192

SIZE_Y=2600

 

Day=255,255,255

Night=255,255,255

Luminous=255,255,255

 

 

Airbus A340-600 RR

 

 

 

 

Скриншоты на примере А340-300 Air France(3шт) и А330-300 Cathay Pacific

 

 

2aa7b35b9b5c.jpg

 

ad06b624f32b.jpg

 

7d225ef1789b.jpg

 

fc1e3589efeb.jpg

 

106b8d8dd452.jpg

 

 

 

За основу(процентов эдак 90) спасибо Frontx, все остальное только замена гаугов одного ВС на другое

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Резерв для ВК и боковых видов

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резерв для чего другого...

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Спасибо, давно хотел скрестить А330.

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Павел! Спасибо!

p.s сам буду ждать A319 ( точнее метод скрещевания ), могу потестировать, найду глюки, обязательно отпишу!

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Anikron, A319 выложил, но есть проблемы:

та же самая что и при мерже WILCO+PA, ВС на малом газу по глиссаде разгоняется. Я пробую исправить

также есть проблемы с креном при изменении курса, задает слишком большой, что влияет на вертикальную скорость

 

ну и разумеется если что еще найдете пишите :pilotfly:

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Anikron, A319 выложил, но есть проблемы:

та же самая что и при мерже WILCO+PA, ВС на малом газу по глиссаде разгоняется. Я пробую исправить

также есть проблемы с креном при изменении курса, задает слишком большой, что влияет на вертикальную скорость

 

Ок, на выходных попробую потестировать, спасибо Вам за Ваш труд!

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Paha_S7, Вы конечно молодец, очень удобно всё оформили, но, Вы хотя бы полётом по кругу тестируете свои сборки? К А330/340 вопросов нет, с ними всё просто и ясно - заменил в Вилковском конфиге пару секций Оверлэндовскими (можно и наоборот) и всё ОК. А вот лёгкая серия А319/321, по вашему летабельными получились? Взять к примеру А320, при V2 = 149 и 2/UP1.5 самолёт нехотя начинает отрыв после 160 узлов и при этом джой нужно тянуть на себя так, что рукоять "трещит". Про выравнивание и автолэнд я вообще молчу... Уже столько раз обсуждалось, что недостаточно для "лёгкой" серии того принципа, которым скрещивается "тяжёлая" серия и РА, а Вы всех под одну гребёнку. Оверлэндовские А319/321 имеют смещёную центровку (не путать с TO CG), заточенную под Оверлэндовскую динамику. А Вилковская динамика заточена под Вилковские же модели с нулевой центровкой. Вот в этом, собственно и вся проблема. Если не обнулить центровку (Reference_Datum_Position), то нормально взлетать и садиться Оверлэндовские А319/321 с Вилковской динамикой НЕ БУДУТ! И тупым перемешиванием Aircraft.cfg это НЕ РЕШАЕТСЯ.

post-44591-0-93273600-1290158606_thumb.jpg

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ROCK_AVIA да, знаю про центровку. Я не сказал что представленные мною решения верные 100%. Буду рад Вашей и любой другой помощи в данном вопросе.

в ответном сообщении для Anikron-а мною было написано, что я пытаюсь исправить сие недоразумение.

 

А по сути, да. Для легкой серии пока не совсем верные мержи. Взлет и посадка как Вы сами сказали это адские игрушки

 

Стоит отметить это в 1м посте :pilotfly:

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Вот, парни, попробуйте мой конфиг A319CFM. (Отдельное спасибо ROCKAVIA за предоставленную информацию!) Вроде летает более-менее похоже на A319, только при посадке Landing Lights светят почему-то в левую сторону, не знаю - это где-то моя ошибка или какой-то глюк. Кто знает что к чему, пожалуйста, отпишитесь.

 

 

[exits]

number_of_exits=2

exit.0 = 0.25, 35.5, -5.5, 2.8, 0

exit.1 = 0.4, -18.5, 5.0, -2.2, 1

 

[Views]

eyepoint=43.13, -1.85, 5.19

 

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0=3, -5.81, -54.7, 3.49, fx_navred ,

light.1=3, -5.81, 54.7, 3.49, fx_navgre ,

light.2=2, -6.42, -55.3, 3.59, fx_strobe ,

light.3=2, -6.42, 55.3, 3.59, fx_strobe ,

light.4=1, 14.15, 0.0, -4.90, fx_beaconh ,

light.5=1, 11.52, 0.0, 9.55, fx_beaconh ,

light.6=2,-54.23, 0.17, 5.19, fx_strobe ,

light.7=3,-54.23, -0.17, 5.19, fx_navwhi ,

light.8 = 4, 39, 0, 5.7, fx_vclighth

 

[General]

atc_type=AIRBUS

atc_model=A319

performance=Dimensions: Wing span: 111 ft 10 in (33.91 m) \n Length: 111 ft 0 in (33.84 m) \n Height: 38 ft 7 in (11.76 m) \n Weights: \n Empty: 89,000 lb \n Max take-off: 166,000 lb \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Maximum range: 3,700 miles (6,800 km) \n Powerplants: Two IAE V2525-A5 rated at 23.500 lbs (111.2 kN) or Two CFM International CFM56-5B4 rated at 22.000 lbs. Hi-bypass Turbofans

 

 

 

[WEIGHT_AND_BALANCE]

reference_datum_position=0, 0, -4.4

max_number_of_stations=50

 

station_load.0 = "450, 42.0, 0.0, 0.0, Crew"

station_load.1 = "1000, 37.0, 0.0, 0.0, Galleys"

station_load.2 = "4000, 16.0, 0.0, 0.0, Baggage"

station_load.3 = "7000, 0.0, 0.0, 0.0, Cargo"

station_load.4 = "6200, 26.0, 0.0, 0.0, First"

station_load.5 = "17000, 0.0, 0.0, 0.0, Coach"

 

empty_weight= 89500

max_gross_weight=167300

empty_weight_roll_MOI=1300000

empty_weight_pitch_MOI=2000000

empty_weight_yaw_MOI=2000000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000, 0.000, 0.000

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[flight_tuning]

cruise_lift_scalar =1.000

parasite_drag_scalar =1.000

induced_drag_scalar =1.1

elevator_effectiveness =1.0

aileron_effectiveness =1.0

rudder_effectiveness =1.0

pitch_stability =1.000

roll_stability =1.000

yaw_stability =1.000

elevator_trim_effectiveness =0.6

aileron_trim_effectiveness =1.000

rudder_trim_effectiveness =1.000

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available = 1

flap_motor = 0, 0 , 17.0

gear_motor = 0, 0 , 17.0

autopilot = 0, 0 , 17.0

avionics_bus = 0, 0 , 17.0

avionics = 0, 0 , 17.0

pitot_heat = 0, 0 , 17.0

additional_system = 0, 0 , 17.0

marker_beacon = 0, 0 , 17.0

gear_warning = 0, 0 , 17.0

fuel_pump = 0, 0 , 17.0

starter1 = 0, 0 , 17.0

starter2 = 0, 0 , 17.0

light_nav = 0, 0 , 17.0

light_beacon = 0, 0 , 17.0

light_landing = 0, 0 , 17.0

light_taxi = 0, 0 , 17.0

light_strobe = 0, 0 , 17.0

light_panel = 0, 0 , 17.0

light_cabin = 0, 0 , 17.0

auto_brakes = 0, 0 , 17.0

standby_vacuum = 0, 0 , 17.0

hydraulic_pump = 0, 0 , 17.0

fuel_transfer_pump = 0, 0 , 17.0

light_recognition = 0, 0 , 17.0

light_wing = 0, 0 , 17.0

light_logo = 0, 0 , 17.0

directional_gyro = 0, 0 , 17.0

directional_gyro_slaving = 0, 0 , 17.0

 

[TurbineEngineData]

fuel_flow_gain=0.001

inlet_area=30

rated_N2_rpm=29920.000000

static_thrust=22000.000000

afterburner_available=0

reverser_available=1

 

[GeneralEngineData]

engine_type=1

Engine.0= 3.0, -17.5, -2.500000

Engine.1= 3.0, 17.5, -2.500000

fuel_flow_scalar=1.0000

min_throttle_limit=-0.499939

max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear

 

[jet_engine]

thrust_scalar =1.1

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[Radios]

// Radio Type=availiable, standby frequency, has glide slope

Audio.1=1

Com.1=1, 1

Com.2=1, 1

Nav.1=1, 1, 1

Nav.2=1, 1, 0

Adf.1=1

Transponder.1=1

Marker.1=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=13.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=29.0 //ditto to accomodate flap 2

flaps-position.5=40.0 //More lift for patched solution to low lift RY

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.2

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[forcefeedback]

gear_bump_nose_magnitude=3000 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=2700 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=2700 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=1300 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=200 ; 0 - 10000

ground_bumps_angle2=09100 ; 0 - 35999 degrees

ground_bumps_intercept2=1.075

ground_bumps_slope2=0.035

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

 

 

 

 

[fuel]

Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000

LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000

RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000

LeftAux= 0.0, -13.0, 0.0, 227.000000, 0.000000

RightAux= 0.0, 13.0, 0.0, 227.000000, 0.000000

 

fuel_type=2.000000

number_of_tank_selectors=2

electric_pump=1

 

[airplane_geometry]

wing_area=1320.000000

wing_span=111.9

wing_root_chord=12.000000

wing_dihedral=5

wing_incidence=1.5

wing_twist=1

oswald_efficiency_factor=0.8723

wing_winglets_flag=1

wing_sweep=22

wing_pos_apex_lon=15.00000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=28

elevator_down_limit=22

aileron_up_limit=22

aileron_down_limit=20

rudder_limit=32

elevator_trim_limit=18

spoiler_limit=50

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.0

min_flaps_for_spoilerons=0.000000

 

 

[contact_points]

point.0=1, 35.80, 0.00, -10.56, 1500, 0, 1.25, 60.12, 0.38, 2.4, 0.5135, 7.0, 8.2, 0, 0.0, 0.0

point.1=1, -4.25, -11.58, -11.06, 2200, 1, 2.15, 0.00, 1.11, 2.0, 0.5470, 9.7, 14.1, 2, 0.0, 0.0

point.2=1, -4.25, 11.58, -11.06, 2200, 2, 2.15, 0.00, 1.11, 2.0, 0.5470, 9.7, 14.1, 3, 0.0, 0.0

 

point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0

point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0

point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0

point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0

 

max_number_of_points=21

 

static_pitch= -0.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn)

static_cg_height=14.26 //feet, altitude of CG when at rest on the ground

gear_system_type=0

 

 

[brakes]

toe_brakes_scale=0.86

parking_brake=1

 

 

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=10.04

 

 

[Reference Speeds]

flaps_up_stall_speed=180.000000 // at MTW

full_flaps_stall_speed=132.000000// at MTW

cruise_speed=320

max_indicated_speed=352.000000

max_mach=0.84

 

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

 

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.000000

max_bank_acceleration=3.0

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

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,1,0,0

normal_pressure=3000.000000

 

 

[stall_warning]

type=1

 

 

[attitude_indicators]

attitude_indicator.0=2

 

 

[turn_indicators]

turn_indicator.0=1,0

 

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абсолютно кривая сборка,не ставьте, :hmm1: начиная от автоленда ,заканчивая проваливанем колёс,задиранием носа :sarcastic: всем кому нужен мерж смс+вилки сюдасюда

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абсолютно кривая сборка,не ставьте, :help: начиная от автоленда ,заканчивая проваливанем колёс,задиранием носа :help: всем кому нужен мерж смс+вилки сюдасюда

 

Странно... Почему у меня все в порядке..? Может у нас симы разные? У меня девятка.

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абсолютно кривая сборка,не ставьте, :diablo: начиная от автоленда ,заканчивая проваливанем колёс,задиранием носа :diablo: всем кому нужен мерж смс+вилки сюдасюда

 

Хоть и не использую А319, но предложенный VRP конфиг проверил - подтверждаю, всё отлично! Ничего никуда не проваливается, LIGHTS корректно подогнаны и с автолэндом полный порядок! tupol154b2, а Вы случаем с А320 не перепутали? Ведь Вы ссылаетесь на тему с вариантами конфигов для А320.

 

P.S. VRP, ну а с посадочным светом...даже не знаю, у меня всё в порядке. Видимо у Вас глюк какой-то, т.к. правкой Aircraft.cfg изменить его Вы не могли (фары и свет "зашиты" в модели). Может какие-либо эффекты света фар устанавливали и в них проблема?

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Хоть и не использую А319, но предложенный VRP конфиг проверил - подтверждаю, всё отлично! Ничего никуда не проваливается, LIGHTS корректно подогнаны и с автолэндом полный порядок! tupol154b2, а Вы случаем с А320 не перепутали? Ведь Вы ссылаетесь на тему с вариантами конфигов для А320.

 

P.S. VRP, ну а с посадочным светом...даже не знаю, у меня всё в порядке. Видимо у Вас глюк какой-то, т.к. правкой Aircraft.cfg изменить его Вы не могли (фары и свет "зашиты" в модели). Может какие-либо эффекты света фар устанавливали и в них проблема?

 

Я тоже думаю что глюк. Эффектов никаких не ставил. Да, и Taxi Lights появляется только после повторного включения (это тоже после посадки). Ну ничего, будем искать...

Кстати, на A320 все в порядке.

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VRP, ROCK_AVIA спасибо за тестирование. Я также потестил и на ура :rolleyes:

 

VRP добавил Ваш конфиг в шапку :blink:

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VRP, ROCK_AVIA спасибо за тестирование. Я также потестил и на ура :rolleyes:

 

VRP добавил Ваш конфиг в шапку :blink:

 

Спасибо! Приятно что могу быть чем-нибудь полезен для адептов авиации!

P.S. А со светом разобрался. Просто в конфиге самоля по-умолчанию были назначены точно такие же комбинации клавиш, как на поворот фары в симе. Короче, конфликт.

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Приветствую. Заполнил секции ВК для А330-200/300, А340-300, А340-600

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Приветствую. Заполнил секции ВК для А330-200/300, А340-300, А340-600

 

Спасибочки...а на 319-320 будут????

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dacool, там текстуры мягко говоря отбивают все желание делать ее...

 

 

upd: добавил скриншоты ВК в соотв пост

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Приветствую. Заполнил секции ВК для А330-200/300, А340-300, А340-600

под спойлером А340-600 RR ничего :) Добавьте пожалуйста. Пытаюсь скрестить именно этот крафт.

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dacool, там текстуры мягко говоря отбивают все желание делать ее...

 

 

upd: добавил скриншоты ВК в соотв пост

 

Да это понятно....Я уже сделал,хотел просто проверить,может что забыл.И может кто-то,когда-то переделает текстуры ВК.

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dacool сделали уже?? делитесь с авсимовцами, проверим, поправим и поможем :)

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Paha_S7, ну так как, будет информация по мержу ВК для 340-600 RR?

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