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 — AircraftfeelThere 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_A330-200model.GE1. Получается с визуальной частью мы процентов на 80 разобрались. Остальные 20% это наши текстуры.
А как устанавливать текстуры?!
)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.2nDeveloped by www.feelThere.com nPublished by Wilco Publishing www.wilcopub.comnnSupport 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.2nDeveloped by www.feelThere.com nPublished by Wilco Publishing www.wilcopub.comnnSupport 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 — бн 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.2nDeveloped by www.feelThere.com nPublished by Wilco Publishing www.wilcopub.comnnSupport 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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
Сообщение отредактировал Paha_S7: 20 February 2011 — 23:38
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
Airbus A330-200 RR
Airbus A330-300 GE
Airbus A330-300 RR
Airbus A340-300 CFM
Airbus A340-600 RR
Скриншоты на примере А340-300 Air France(3шт) и А330-300 Cathay Pacific
[size=»2″]За основу(процентов эдак 90) спасибо [b][size=»5″]Frontx-у, все остальное только замена гаугов одного ВС на другое
Сообщение отредактировал Paha_S7: 19 December 2010 — 14:13
p.s сам буду ждать A319 ( точнее метод скрещевания ), могу потестировать, найду глюки, обязательно отпишу!
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
Сообщение отредактировал Paha_S7: 28 February 2011 — 14:24
Ок, на выходных попробую потестировать, спасибо Вам за Ваш труд!
Прикрепленные изображения
Сообщение отредактировал ROCK_AVIA: 19 November 2010 — 14:08
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
Сообщение отредактировал Paha_S7: 28 February 2011 — 14:25
Сообщение отредактировал AirArt: 28 November 2010 — 18:37
Убрал конфиг в спойлер
Странно… Почему у меня все в порядке..? Может у нас симы разные? У меня девятка.
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?
Сообщение отредактировал ROCK_AVIA: 28 November 2010 — 17:25
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.
VRP добавил Ваш конфиг в шапку
Сообщение отредактировал Paha_S7: 28 February 2011 — 14:26
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.
Сообщение отредактировал Paha_S7: 28 February 2011 — 14:26
Спасибочки…а на 319-320 будут????
upd: добавил скриншоты ВК в соотв пост
Сообщение отредактировал Paha_S7: 28 February 2011 — 14:27
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:27
под спойлером А340-600 RR ничего
Добавьте пожалуйста. Пытаюсь скрестить именно этот крафт.
Да это понятно….Я уже сделал,хотел просто проверить,может что забыл.И может кто-то,когда-то переделает текстуры ВК.
поставите на место буду благодарен
Сообщение отредактировал Paha_S7: 06 December 2010 — 17:06
Paha_7 Я тупо скопировал строчки Vcockpit-а с Overlanda в Wilco,ВК появилась….,но наверно это не правильно…
Сообщение отредактировал dacool: 06 December 2010 — 18:41
В мерже рабочие тублеры всех огней, NAV, Beacon, Strobe, Taxi, T.O., VC Lights, также рабочие кнопки Anti Ice, Pito Heat. CDU кликабельна 100% и функциональна примерно на 70% если брать за 100% родную от WILCO, но менять режимы не получится.
Ну и основное, это шасси, спойлеры, закрылки все вертится и крутится.
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:27
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:27
Сообщение отредактировал Jeka_M: 03 June 2011 — 19:36
убрал под спойлер
stinger1968 уберите конфиг под спойлер
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:21
А где в конфиге прописана центровка? Вообще на эшелоне и автоленде всё нормально, только вот при взлёте проблема, а вообще контакт и другие параметры взяты из оригинального Overland 320
Сообщение отредактировал stinger1968: 13 December 2010 — 18:50
Внимательно прочитайте первую страницу этой ветки и все вопросы отпадут
. Да и для чего Вы изобретаете велосипед, если он уже изобретён? Вам же подсказали — поставьте конфиг из спойлера в первом посте.
Да попробовал конфиг из первого поста, отлично всё работает…Спасибо!!!
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:22
я включаю свет панели и регулирую яркость,но подсветка работает только на правой стороны,а как быть с левой стороной?
у меня вопрос как у других пользователей Wilco с освещением в кабине,реализована ли световая подстветка левой панели приборов?
всем спасибо
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:22
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:22
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:22
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:22
P.S.Вопрос снят,ВК есть.Теперь осталось дисплеи заставить работать.
Сообщение отредактировал Adrenaline: 10 January 2011 — 21:17
В Большинстве летаю в России поэтому пользуюсь вот этим сайтом маршрутов http://intinfo.matfm…tme/routes.htme
Некоторые точки ввожу по типу:Трасса-и к какой точке по этой трассе следовать.
Иногда компьютер мне отвечает AWY/WPT MISMATCH
Подскажите что это?
И как с этим бороться?
Летаю на А-320v1 Fs9
Сообщение отредактировал Bulka92: 14 January 2011 — 21:25
я еще на всякий случай переименовал все bmp файлы вк текстур, в названии которых есть a340, в а330
Сообщение отредактировал Jeka_M: 03 June 2011 — 19:35
убрал под спойлер
sim=FeelThere_A321CFM
оставляем
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:22
поменял секцию, все равно не пашет(( Может я что-то перепутал когда папки переносил? Оверлендовский Файл model я перенес в соответствующую папку взамен стертого model от вилковского эрбаса. В той же папке осталось нетронутыми 2 файла MDL файла. А текстового файла никакого не было.
2vellit, не играет. Играет роль только модель и aircraft.cfg идущий с ней
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:22
Так точно, FSX
2Alexuhmm, с постройкой модели в FSX не знаком, хотя что-то подсказывает, что в папке один файл отвечает за ВК, другой за модель, меняйте модель и пробуйте.
Сообщение отредактировал Paha_S7: 28 February 2011 — 13:23
Вот что у меня в папке. файл model от SMS, остальное не трогал
Прикрепленные файлы
321.jpg 61.17К
33 Количество загрузок:
1) Файл 321cfm_interior.MDL можете смело убрать из папки, ибо он отвечает за вилковский ВК, а у SMS ВК впаяна в модель и не идет отдельным файлом.
2) файл 321cfm.MDL -вот он и должен быть от Оверлэнда. При переносе имя файла оставить (переименовать) вилковское, то есть 321cfm.MDL
3) Текстовый файл model открывается блокнотом и там должны быть следующие строчки:
[models]
normal=321cfm
Строчку interior=321cfm_interior убрать.
Сообщение отредактировал Махони: 26 January 2011 — 10:26
Получилось, но не то)) В общем мерж отражается в симе в меню выбора самолетов, но в заводской ливрее, а после выбора ее — самолет загружается, но полностью черный какой-то. По папке model сделал как написано Вами было.
Ну и aircraft.CFG
Сообщение отредактировал Jeka_M: 03 June 2011 — 19:33
убрал под спойлер