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

admin · 2010-11-17T11:50:00+03:00

Инструкция по мержеванию(соединению) панелей от Wilco и визуальных моделей SMS OverlandУв.пользователи на данный момент готовы:А319-100, спасибо VRPА320-214, спасибо ROCK_AVIAА330-200 и А330-300А340-300 и A340-600все остальные только визуальная часть рабочаяНа 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 примеру2. Выбираем папку Model, заходим разумеется и удаляем 2 файла:визуальную модельтекстовый файлДалее 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?! Spoiler 1. Перемещаем/Распаковываем папку с текстурами для модели в нужную директорию(как правило это папка с самим самолетом )2. Открываем aircraft.cfgи на нашем же примере смотрим начиная с верха...исходное значение:[fltsim.0]title=feelThere A330-200 House Coloresim=FeelThere_A330-200sound=GEmodel=texture=panel=checklists=atc_id=F-GZCJatc_airline=Airbus Industriesatc_flight_number=009atc_heavy=1ui_manufacturer=Airbusui_type=A330-200ui_variation=Airbus Industriesvisual_damage=1description=Airbus Series Vol.2nDeveloped by www.feelThere.com nPublished by Wilco Publishing www.wilcopub.comnnSupport at www.wilcopub.comа получить нам нужно вот это:[fltsim.0]title=Airbus A330-200 Air Francesim=FeelThere_A330-200sound=GEmodel=texture=AFRCpanel=checklists=atc_id=F-GZCJatc_airline=Air Franceatc_flight_number=009atc_heavy=1ui_manufacturer=Airbusui_type=A330-200ui_variation=Air Francevisual_damage=1description=Airbus Series Vol.2nDeveloped by www.feelThere.com nPublished by Wilco Publishing www.wilcopub.comnnSupport at www.wilcopub.comскажу 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 реальнуюatc_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 Francesim=FeelThere_A330-200sound=GEmodel=texture=AFRCpanel=checklists=atc_id=F-GZCJatc_airline=Air Franceatc_flight_number=009atc_heavy=1ui_manufacturer=Airbusui_type=A330-200ui_variation=Air Francevisual_damage=1description=Airbus Series Vol.2nDeveloped by www.feelThere.com nPublished by Wilco Publishing www.wilcopub.comnnSupport at www.wilcopub.com[exits]number_of_exits=2exit.0 = 0.25, 78.0, -7.5, 8.5, 0exit.1 = 0.05, -37.0, 7.0, -4.0, 15. Сохраняем.6. Запускаем СИМ и тестим Данные для двигателей CFM/GEAirbus A319 Spoiler [exits]number_of_exits=2exit.0 = 0.25, 35.5, -5.5, 2.8, 0exit.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=landinglight.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=AIRBUSatc_model=A319performance=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, -4.4max_number_of_stations=50station_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= 89500max_gross_weight=167300empty_weight_roll_MOI=1300000empty_weight_pitch_MOI=2000000empty_weight_yaw_MOI=2000000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=30rated_N2_rpm=29920.000000static_thrust=23200.000000afterburner_available=0reverser_available=1[GeneralEngineData]engine_type=1Engine.0= 3.0, -17.5, -2.500000Engine.1= 3.0, 17.5, -2.500000fuel_flow_scalar=1.0000min_throttle_limit=-0.499939max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear[jet_engine]thrust_scalar =1.1[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=13.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=29.0 //ditto to accomodate flap 2flaps-position.5=40.0 //More lift for patched solution to low lift RY[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel]Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000LeftAux= 0.0, -13.0, 0.0, 227.000000, 0.000000RightAux= 0.0, 13.0, 0.0, 227.000000, 0.000000fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=1320.000000wing_span=111.9wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.8723wing_winglets_flag=1wing_sweep=22wing_pos_apex_lon=15.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0max_number_of_points=21static_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 groundgear_system_type=0[brakes]toe_brakes_scale=0.86parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=352.000000max_mach=0.84[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=2[turn_indicators]turn_indicator.0=1,0 Airbus A320 Spoiler [exits]number_of_exits=2exit_rate.0=0.25exit_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=landinglight.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=AIRBUSatc_model=A320performance=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,-4.000000max_number_of_stations=50station_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= 93500max_gross_weight=169800empty_weight_roll_MOI=1700000empty_weight_pitch_MOI=2500000empty_weight_yaw_MOI=2700000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=30rated_N2_rpm=29920.000000static_thrust=26200.000000afterburner_available=0reverser_available=1[GeneralEngineData]engine_type=1Engine.0= -2.25, -18.9, -4.600000Engine.1= -2.25, 18.9, -4.600000fuel_flow_scalar=1.0000min_throttle_limit=-0.499939[jet_engine]thrust_scalar =0.95[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=10.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel]Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000LeftAux= 0.0, -13.0, 0.0, 227.000000, 0.000000RightAux= 0.0, 13.0, 0.0, 227.000000, 0.000000fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=1320.000000wing_span=111.9wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.8wing_winglets_flag=1wing_sweep=22wing_pos_apex_lon=15.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.00point.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, 0.00point.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, 0.00static_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 groundgear_system_type=0[brakes]toe_brakes_scale=0.86parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=352.000000max_mach=0.84[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_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=0.000000gs_proportional_control=19.0gs_integrator_control=0.530gs_derivative_control=0.00gs_integrator_boundary=0.70gs_derivative_boundary=0.00yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=2[turn_indicators]turn_indicator.0=1,0 Airbus A321 Spoiler [exits]number_of_exits=2exit.0 = 0.25, 53.5, -5.5, 2.8, 0exit.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=landinglight.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=AIRBUSatc_model=A321performance=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=50station_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= 106300max_gross_weight=196210empty_weight_roll_MOI=1700000empty_weight_pitch_MOI=2500000empty_weight_yaw_MOI=2700000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=30rated_N2_rpm=29920.000000static_thrust=31400.000000afterburner_available=0reverser_available=1[GeneralEngineData]engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=TurbopropEngine.0=3.25, -18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datumEngine.1=3.25, 18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datumfuel_flow_scalar=1.26 //Scalar for fuel flow efficiencymin_throttle_limit=-0.330000max_contrail_temperature = -30 [jet_engine]thrust_scalar =1.0[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel]Center1= 0.0, 0.0, 0.0, 2118.000000, 0.000000LeftMain= 0.0, -8.0, 0.0, 2001.000000, 0.000000RightMain= 0.0, 8.0, 0.0, 2001.000000, 0.000000fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=1320.000000wing_span=111.9wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.8723wing_winglets_flag=1wing_sweep=22wing_pos_apex_lon=15.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0max_number_of_points=21static_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 groundgear_system_type=0[brakes]toe_brakes_scale=0.86parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=352.000000max_mach=0.84[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=2[turn_indicators]turn_indicator.0=1,0 Airbus A330-200 Spoiler [exits]number_of_exits=2exit.0 = 0.25, 78.0, -7.5, 8.5, 0exit.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=landinglight.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=AIRBUSatc_model=A330-200performance=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, -6.000max_number_of_stations=50station_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= 264875max_gross_weight=507050empty_weight_roll_MOI=21100000empty_weight_pitch_MOI=21400000empty_weight_yaw_MOI=15800000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=55rated_N2_rpm=29920.000000static_thrust=72500.000000 // CF Enginesafterburner_available=0reverser_available=1[GeneralEngineData]engine_type= 1Engine.0= 12.600, -29.900, -6.100Engine.1= 12.600, 29.900, -6.100fuel_flow_scalar= 1.06min_throttle_limit=-0.250000[jet_engine]thrust_scalar =0.96 //300-200 only[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel] Center1= 4.0, 0.0, 0.0, 10980.0, 0.0Center2= -4.0, 0.0, 0.0, 1646.0, 0.0LeftMain= -2.0, -4.0, 0.0, 11095.0, 0.0RightMain= -2.0, 4.0, 0.0, 11095.0, 0.0LeftAux= -7.0, -13.0, 0.0, 964.0, 0.0RightAux= -7.0, 13.0, 0.0, 964.0, 0.0fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=3892wing_span=198wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.8723wing_winglets_flag=1wing_sweep=30wing_pos_apex_lon=35.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000static_pitch= -0.830 static_cg_height= 20.670gear_system_type=0[brakes]toe_brakes_scale=0.66parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=358.000000max_mach=0.865[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=1[turn_indicators]turn_indicator.0=1,0 Airbus A330-300 Spoiler [exits]number_of_exits=2exit.0 = 0.25, 86.0, -7.5, 8.5, 0exit.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=landinglight.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=AIRBUSatc_model=A330-300performance=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, -6.000max_number_of_stations=50station_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= 267000max_gross_weight=509000empty_weight_roll_MOI=21300000empty_weight_pitch_MOI=21900000empty_weight_yaw_MOI=16100000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=55rated_N2_rpm=29920.000000static_thrust=72500.000000afterburner_available=0reverser_available=1[GeneralEngineData]engine_type= 1Engine.0= 10.600, -29.900, -6.100Engine.1= 10.600, 29.900, -6.100fuel_flow_scalar= 0.8900min_throttle_limit=-0.350000[jet_engine]thrust_scalar =0.98[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel] Center1= 4.0, 0.0, 0.0, 0.0, 0.0Center2= -4.0, 0.0, 0.0, 1615.0, 0.0LeftMain= -2.0, -4.0, 0.0, 11025.0, 0.0RightMain= -2.0, 4.0, 0.0, 11025.0, 0.0LeftAux= -7.0, -13.0, 0.0, 974.0, 0.0RightAux= -7.0, 13.0, 0.0, 974.0, 0.0fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=3892wing_span=198wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.892wing_winglets_flag=1wing_sweep=30wing_pos_apex_lon=35.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000static_pitch= -0.830 static_cg_height= 20.670gear_system_type=0[brakes]toe_brakes_scale=0.66parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=358.000000max_mach=0.865[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=1[turn_indicators]turn_indicator.0=1,0 Airbus A340-300 Spoiler [exits]number_of_exits=3exit.0 = 0.25, 86.0, -7.5, 8.5, 0exit.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=landinglight.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=AIRBUSatc_model=A340-300performance=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, -6.000max_number_of_stations=50station_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= 286150max_gross_weight=573200empty_weight_roll_MOI=33200000empty_weight_pitch_MOI=34400000empty_weight_yaw_MOI=22800000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=57rated_N2_rpm=29920.000000static_thrust=34000.000000 // Trent Engines for A340-600afterburner_available=0reverser_available=1[GeneralEngineData]engine_type= 1Engine.0= -8.420, -63.700, 1.350Engine.1= 12.600, -29.900, -3.100Engine.2= 12.600, 29.900, -3.100Engine.3= -8.420, 63.700, 1.350fuel_flow_scalar= 0.79min_throttle_limit=-0.320000[jet_engine]thrust_scalar =1.5 //340-300 only![EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2lift_scalar=0.77drag_scalar=1.0pitch_scalar=0.0[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.7pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel] Center1= 4.0, 0.0, 0.0, 11207.0, 0.0 // Middle Fuselage Main Centre TankCenter2= -33.0, 0.0, 0.0, 1646.0, 0.0 // Trim Tank in Tail-plane sectinLeftMain= -2.0, -6.0, 0.0, 11301.0, 0.0 // Inner Wing Tank 1 LeftRightMain= -2.0, 6.0, 0.0, 11301.0, 0.0 // Inner Wing Tank 2 RightLeftAux= -6.0, -15.0, 0.0, 964.0, 0.0 // Outer Wing Tank 1 LeftRightAux= -6.0, 15.0, 0.0, 964.0, 0.0 // Outer Wing Tank 2 Rightfuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=3892wing_span=197.85wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.94wing_winglets_flag=1wing_sweep=30wing_pos_apex_lon=38.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000static_pitch= -0.480 static_cg_height= 21.000gear_system_type=0[brakes]toe_brakes_scale=0.78parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=358.000000max_mach=0.865[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_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/IAEAirbus A319 Spoiler [exits]number_of_exits=2exit.0 = 0.25, 35.5, -5.5, 2.8, 0exit.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=landinglight.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=AIRBUSatc_model=A319performance=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, -4.4max_number_of_stations=50station_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= 89500max_gross_weight=167300empty_weight_roll_MOI=1300000empty_weight_pitch_MOI=2000000empty_weight_yaw_MOI=2000000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=30rated_N2_rpm=29920.000000static_thrust=22700.000000afterburner_available=0reverser_available=1[GeneralEngineData]engine_type=1Engine.0= 3.0, -17.5, -2.500000Engine.1= 3.0, 17.5, -2.500000fuel_flow_scalar=1.0000min_throttle_limit=-0.499939max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear[jet_engine]thrust_scalar =1.1[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=13.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=29.0 //ditto to accomodate flap 2flaps-position.5=40.0 //More lift for patched solution to low lift RY[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel]Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000LeftAux= 0.0, -13.0, 0.0, 227.000000, 0.000000RightAux= 0.0, 13.0, 0.0, 227.000000, 0.000000fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=1320.000000wing_span=111.9wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.8723wing_winglets_flag=1wing_sweep=22wing_pos_apex_lon=15.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0max_number_of_points=21static_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 groundgear_system_type=0[brakes]toe_brakes_scale=0.86parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=352.000000max_mach=0.84[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=2[turn_indicators]turn_indicator.0=1,0 Airbus A320 Spoiler [exits]number_of_exits=2exit_rate.0=0.25exit_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=landinglight.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=AIRBUSatc_model=A320performance=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,-4.000000max_number_of_stations=50station_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= 93500max_gross_weight=169800empty_weight_roll_MOI=1700000empty_weight_pitch_MOI=2500000empty_weight_yaw_MOI=2700000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=30rated_N2_rpm=29920.000000static_thrust=27000.000000afterburner_available=0reverser_available=1[GeneralEngineData]engine_type=1Engine.0= -2.25, -18.9, -4.600000Engine.1= -2.25, 18.9, -4.600000fuel_flow_scalar=1.0000min_throttle_limit=-0.499939[jet_engine]thrust_scalar =0.95[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=10.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel]Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000LeftAux= 0.0, -13.0, 0.0, 227.000000, 0.000000RightAux= 0.0, 13.0, 0.0, 227.000000, 0.000000fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=1320.000000wing_span=111.9wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.8wing_winglets_flag=1wing_sweep=22wing_pos_apex_lon=15.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.00point.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, 0.00point.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, 0.00static_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 groundgear_system_type=0[brakes]toe_brakes_scale=0.86parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=352.000000max_mach=0.84[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_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=0.000000gs_proportional_control=19.0gs_integrator_control=0.530gs_derivative_control=0.00gs_integrator_boundary=0.70gs_derivative_boundary=0.00yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=2[turn_indicators]turn_indicator.0=1,0 Airbus A321 Spoiler [exits]number_of_exits=2exit.0 = 0.25, 53.5, -5.5, 2.8, 0exit.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=landinglight.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=AIRBUSatc_model=A321performance=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=50station_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= 106300max_gross_weight=196210empty_weight_roll_MOI=1700000empty_weight_pitch_MOI=2500000empty_weight_yaw_MOI=2700000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=30rated_N2_rpm=29920.000000static_thrust=33000.000000afterburner_available=0reverser_available=1[GeneralEngineData]engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=TurbopropEngine.0=3.25, -18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datumEngine.1=3.25, 18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datumfuel_flow_scalar=1.26 //Scalar for fuel flow efficiencymin_throttle_limit=-0.330000max_contrail_temperature = -30 [jet_engine]thrust_scalar =1.0[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel]Center1= 0.0, 0.0, 0.0, 2118.000000, 0.000000LeftMain= 0.0, -8.0, 0.0, 2001.000000, 0.000000RightMain= 0.0, 8.0, 0.0, 2001.000000, 0.000000fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=1320.000000wing_span=111.9wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.8723wing_winglets_flag=1wing_sweep=22wing_pos_apex_lon=15.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0point.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, 0.0max_number_of_points=21static_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 groundgear_system_type=0[brakes]toe_brakes_scale=0.86parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=352.000000max_mach=0.84[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=2[turn_indicators]turn_indicator.0=1,0 Airbus A330-200 Spoiler [exits]number_of_exits=2exit.0 = 0.25, 78.0, -7.5, 8.5, 0exit.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=landinglight.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=AIRBUSatc_model=A330-200performance=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, -6.000max_number_of_stations=50station_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= 264875max_gross_weight=507050empty_weight_roll_MOI=21100000empty_weight_pitch_MOI=21400000empty_weight_yaw_MOI=15800000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=55rated_N2_rpm=29920.000000static_thrust=71100.000000 // CF Enginesafterburner_available=0reverser_available=1[GeneralEngineData]engine_type= 1Engine.0= 12.600, -29.900, -6.100Engine.1= 12.600, 29.900, -6.100fuel_flow_scalar= 1.06min_throttle_limit=-0.250000[jet_engine]thrust_scalar =0.96 //300-200 only[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel] Center1= 4.0, 0.0, 0.0, 10980.0, 0.0Center2= -4.0, 0.0, 0.0, 1646.0, 0.0LeftMain= -2.0, -4.0, 0.0, 11095.0, 0.0RightMain= -2.0, 4.0, 0.0, 11095.0, 0.0LeftAux= -7.0, -13.0, 0.0, 964.0, 0.0RightAux= -7.0, 13.0, 0.0, 964.0, 0.0fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=3892wing_span=198wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.8723wing_winglets_flag=1wing_sweep=30wing_pos_apex_lon=35.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000static_pitch= -0.830 static_cg_height= 20.670gear_system_type=0[brakes]toe_brakes_scale=0.66parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=358.000000max_mach=0.865[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=1[turn_indicators]turn_indicator.0=1,0 Airbus A330-300 Spoiler [exits]number_of_exits=2exit.0 = 0.25, 86.0, -7.5, 8.5, 0exit.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=landinglight.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=AIRBUSatc_model=A330-300performance=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, -6.000max_number_of_stations=50station_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= 267000max_gross_weight=509000empty_weight_roll_MOI=21300000empty_weight_pitch_MOI=21900000empty_weight_yaw_MOI=16100000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=55rated_N2_rpm=29920.000000static_thrust=71100.000000afterburner_available=0reverser_available=1[GeneralEngineData]engine_type= 1Engine.0= 10.600, -29.900, -6.100Engine.1= 10.600, 29.900, -6.100fuel_flow_scalar= 0.8900min_throttle_limit=-0.350000[jet_engine]thrust_scalar =0.98[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel] Center1= 4.0, 0.0, 0.0, 0.0, 0.0Center2= -4.0, 0.0, 0.0, 1615.0, 0.0LeftMain= -2.0, -4.0, 0.0, 11025.0, 0.0RightMain= -2.0, 4.0, 0.0, 11025.0, 0.0LeftAux= -7.0, -13.0, 0.0, 974.0, 0.0RightAux= -7.0, 13.0, 0.0, 974.0, 0.0fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=3892wing_span=198wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.892wing_winglets_flag=1wing_sweep=30wing_pos_apex_lon=35.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000static_pitch= -0.830 static_cg_height= 20.670gear_system_type=0[brakes]toe_brakes_scale=0.66parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=358.000000max_mach=0.865[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=1[turn_indicators]turn_indicator.0=1,0 Airbus A340-600 Spoiler [exits]number_of_exits=2exit_rate.0=0.25exit_rate.1=0.25[Views]eyepoint=117.02, -1.75, 3.88[LIGHTS]//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landinglight.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=AIRBUSatc_model=A340-600performance=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, -4.000empty_weight_CG_position = -4.000, 0.000, 0.000max_number_of_stations=50station_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= 390220max_gross_weight=804675empty_weight_pitch_MOI= 18587807.000empty_weight_roll_MOI = 10295476.000empty_weight_yaw_MOI = 30160328.000empty_weight_coupled_MOI=0.0[pitot_static]vertical_speed_time_constant=999[GROUND_REACTION]MAX_STEERING_ANGLE=75[flight_tuning]cruise_lift_scalar =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=57rated_N2_rpm=29920.000000static_thrust=56000.000000 // Trent Engines for A340-600afterburner_available=0reverser_available=1[GeneralEngineData]engine_type= 1Engine.0= -17.420, -67.700, -5.550Engine.1= 6.600, -31.900, -9.300Engine.2= 6.600, 31.900, -9.300Engine.3= -17.420, 67.700, -5.550fuel_flow_scalar= 0.79min_throttle_limit=-0.250000[jet_engine]thrust_scalar =0.96 //340-600 only[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.5drag_scalar=0.1pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel]Center1= 4.0, 0.0, 0.0, 14521.0, 0.0 // Middle Fuselage Main Centre TankCenter2= -33.0, 0.0, 0.0, 2209.0, 0.0 // Trim Tank in Tail-plane sectinLeftMain= -2.0, -6.0, 0.0, 9182.0, 0.0 // Inner Wing Tank 2 LeftRightMain= -2.0, 6.0, 0.0, 9182.0, 0.0 // Inner Wing Tank 3 RightLeftAux= -6.0, -15.0, 0.0, 6472.0, 0.0 // Inner Wing Tank 1 LeftRightAux= -6.0, 15.0, 0.0, 6472.0, 0.0 // InnerWing Tank 4 RightLeftTip= -12.0, -20.0, 0.0, 1623.0, 0.0 // Outer Tank LeftRightTip= -12.0, 20.0, 0.0 1623.0 0.0 // Outer Tank Rightfuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=4729wing_span=208.1wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.94wing_winglets_flag=1wing_sweep=30wing_pos_apex_lon=38.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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 Gearpoint.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, 300.000point.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, 300.000point.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, 300.000point.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, 300.000point.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, 300.000point.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, 300.000point.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, 300.000point.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, 300.000point.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, 300.000point.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, 300.000point.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// Fuselagepoint.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 // Nosepoint.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 fwdpoint.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 centerpoint.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 aftpoint.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 fwdpoint.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 centerpoint.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 aftpoint.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 ltpoint.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 rtpoint.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 ltpoint.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 rtpoint.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 leftpoint.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 rightpoint.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 aftpoint.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 stabspoint.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 fwdpoint.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 aftpoint.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 ltpoint.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// Wingspoint.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 fwdpoint.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 aftpoint.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 fwdpoint.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 aftpoint.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 fwdpoint.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 aftpoint.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 fwdpoint.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 Enginespoint.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 fwdpoint.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 fwdpoint.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 bottompoint.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 Enginespoint.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 fwdpoint.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 fwdpoint.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 bottompoint.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 bottommax_number_of_points = 50static_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 groundgear_system_type=0 //Hydraulicstatic_pitch=0.0static_cg_height=17.4gear_system_type=0[brakes]toe_brakes_scale=0.78parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=358.000000max_mach=0.865[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1 Данные для двигателей PWAirbus A330-200 Spoiler [exits]number_of_exits=2exit.0 = 0.25, 78.0, -7.5, 8.5, 0exit.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=landinglight.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=AIRBUSatc_model=A330-200performance=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, -6.000max_number_of_stations=50station_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= 264875max_gross_weight=507050empty_weight_roll_MOI=21100000empty_weight_pitch_MOI=21400000empty_weight_yaw_MOI=15800000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=55rated_N2_rpm=29920.000000static_thrust=68600.000000 // CF Enginesafterburner_available=0reverser_available=1[GeneralEngineData]engine_type= 1Engine.0= 12.600, -29.900, -6.100Engine.1= 12.600, 29.900, -6.100fuel_flow_scalar= 1.06min_throttle_limit=-0.250000[jet_engine]thrust_scalar =0.96 //300-200 only[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel] Center1= 4.0, 0.0, 0.0, 10980.0, 0.0Center2= -4.0, 0.0, 0.0, 1646.0, 0.0LeftMain= -2.0, -4.0, 0.0, 11095.0, 0.0RightMain= -2.0, 4.0, 0.0, 11095.0, 0.0LeftAux= -7.0, -13.0, 0.0, 964.0, 0.0RightAux= -7.0, 13.0, 0.0, 964.0, 0.0fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=3892wing_span=198wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.8723wing_winglets_flag=1wing_sweep=30wing_pos_apex_lon=35.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000static_pitch= -0.830 static_cg_height= 20.670gear_system_type=0[brakes]toe_brakes_scale=0.66parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=358.000000max_mach=0.865[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=1[turn_indicators]turn_indicator.0=1,0 Airbus A330-300 Spoiler [exits]number_of_exits=2exit.0 = 0.25, 86.0, -7.5, 8.5, 0exit.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=landinglight.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=AIRBUSatc_model=A330-300performance=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, -6.000max_number_of_stations=50station_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= 267000max_gross_weight=509000empty_weight_roll_MOI=21300000empty_weight_pitch_MOI=21900000empty_weight_yaw_MOI=16100000empty_weight_coupled_MOI=0.0empty_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 =1.000parasite_drag_scalar =1.000induced_drag_scalar =1.1elevator_effectiveness =1.0aileron_effectiveness =1.0rudder_effectiveness =1.0pitch_stability =1.000roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =0.6aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 200electric_always_available = 1flap_motor = 0, 0 , 17.0gear_motor = 0, 0 , 17.0autopilot = 0, 0 , 17.0avionics_bus = 0, 0 , 17.0avionics = 0, 0 , 17.0pitot_heat = 0, 0 , 17.0additional_system = 0, 0 , 17.0marker_beacon = 0, 0 , 17.0gear_warning = 0, 0 , 17.0fuel_pump = 0, 0 , 17.0starter1 = 0, 0 , 17.0starter2 = 0, 0 , 17.0light_nav = 0, 0 , 17.0light_beacon = 0, 0 , 17.0light_landing = 0, 0 , 17.0light_taxi = 0, 0 , 17.0light_strobe = 0, 0 , 17.0light_panel = 0, 0 , 17.0light_cabin = 0, 0 , 17.0auto_brakes = 0, 0 , 17.0standby_vacuum = 0, 0 , 17.0hydraulic_pump = 0, 0 , 17.0fuel_transfer_pump = 0, 0 , 17.0light_recognition = 0, 0 , 17.0light_wing = 0, 0 , 17.0light_logo = 0, 0 , 17.0directional_gyro = 0, 0 , 17.0directional_gyro_slaving = 0, 0 , 17.0[TurbineEngineData]fuel_flow_gain=0.001inlet_area=55rated_N2_rpm=29920.000000static_thrust=68600.000000afterburner_available=0reverser_available=1[GeneralEngineData]engine_type= 1Engine.0= 10.600, -29.900, -6.100Engine.1= 10.600, 29.900, -6.100fuel_flow_scalar= 0.8900min_throttle_limit=-0.350000[jet_engine]thrust_scalar =0.98[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]// Radio Type=availiable, standby frequency, has glide slopeAudio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=0.500000extending-time=20.000000system_type=1flaps-position.0=0.000000,0.000000flaps-position.1=0.0flaps-position.2=15.0 //nominal value should be10 but we need big effect RYflaps-position.3=20.0 //ditto to accomodate flap 2flaps-position.4=26.0 //ditto to accomodate flap 2flaps-position.5=35.0 //ditto to accomodate flap 2[Flaps.1]type=2span-outboard=0.800extending-time=20.000system_type=1damaging-speed=232.000blowout-speed=250.000lift_scalar=0.3drag_scalar=0.2pitch_scalar=0.0flaps-position.0=0flaps-position.1=18.0flaps-position.2=18.0flaps-position.3=22.0flaps-position.4=22.0flaps-position.5=27.0[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[fuel] Center1= 4.0, 0.0, 0.0, 0.0, 0.0Center2= -4.0, 0.0, 0.0, 1615.0, 0.0LeftMain= -2.0, -4.0, 0.0, 11025.0, 0.0RightMain= -2.0, 4.0, 0.0, 11025.0, 0.0LeftAux= -7.0, -13.0, 0.0, 974.0, 0.0RightAux= -7.0, 13.0, 0.0, 974.0, 0.0fuel_type=2.000000number_of_tank_selectors=2electric_pump=1[airplane_geometry]wing_area=3892wing_span=198wing_root_chord=12.000000wing_dihedral=5wing_incidence=1.5wing_twist=1oswald_efficiency_factor=0.892wing_winglets_flag=1wing_sweep=30wing_pos_apex_lon=35.00000wing_pos_apex_vert=0.000000htail_area=328.000000htail_span=40.000000htail_pos_lon=-50.000000htail_pos_vert=0.000000htail_incidence=2.993774htail_sweep=0.000000vtail_area=249.000000vtail_span=17.991665vtail_sweep=0.000000vtail_pos_lon=-50.000000vtail_pos_vert=20.500000elevator_area=70.500000aileron_area=26.800000rudder_area=56.200000elevator_up_limit=28elevator_down_limit=22aileron_up_limit=22aileron_down_limit=20rudder_limit=32elevator_trim_limit=18spoiler_limit=50spoilerons_available=1aileron_to_spoileron_gain=3.000000min_ailerons_for_spoilerons=9.0min_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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000point.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, 0.000static_pitch= -0.830 static_cg_height= 20.670gear_system_type=0[brakes]toe_brakes_scale=0.66parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=10.04[Reference Speeds]flaps_up_stall_speed=180.000000 // at MTWfull_flaps_stall_speed=132.000000// at MTWcruise_speed=320max_indicated_speed=358.000000max_mach=0.865[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800.000000autothrottle_available=1autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=90.000000pitch_takeoff_ga=8.000000max_pitch=10.000000max_pitch_acceleration=0.8max_pitch_velocity_lo_alt=1.0max_pitch_velocity_hi_alt=1.0max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=3.0max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_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

15.01.2011 в 22:33

Alexuhmm
sim=FeelThere_A321CFM
оставляем

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.

25.01.2011 в 01:19

Версия «Оверленда» играет роль? Насколько мне известно, существуют апдейты, которые также затрагивают и визуальную часть моделей от Оверленда. Или же скрещивать можно и с первоначальной версией?

25.01.2011 в 01:55

2Alexuhmm, я так понял у Вас ФСХ?

2vellit, не играет. Играет роль только модель и aircraft.cfg идущий с ней

Сообщение отредактировал Paha_S7: 28 February 2011 — 13:22

25.01.2011 в 14:08

Т.е. скрещивать можно с первой версией и не париться, да?

25.01.2011 в 15:03

2Alexuhmm, я так понял у Вас ФСХ?

Так точно, FSX

25.01.2011 в 21:47

2vellit, да с любой

хоть с 777 их «производства»

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

25.01.2011 в 22:23

2vellit, да с любой хоть с 777 их «производства»

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.

Вот что у меня в папке. файл model от SMS, остальное не трогал

Прикрепленные файлы

321.jpg 61.17К
33 Количество загрузок:

26.01.2011 в 10:21

Вот что у меня в папке. файл model от SMS, остальное не трогал

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

26.01.2011 в 11:29

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.

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

Spoiler

// feelThere A321 CFM

[fltsim.0]
title=Feelthere A321 CFM Airbus House
sim=FeelThere_A321CFM
sound=
model=
texture=HOUSE
atc_airline=Airbus
panel=
checklists=
atc_id=FGTWW
atc_flight_number=321
atc_heavy=0
ui_manufacturer=Airbus Wilco/SMS
ui_type=A321 CFM
ui_variation=Airbus House
ui_typerole=»Commercial Airliner»
ui_createdby=»feelThere/Wilco»
visual_damage=1
description=Airbus Series Vol.1nDeveloped by http://www.feelThere.com nPublished by Wilco Publishing http://www.wilcopub.comnnSupport at http://www.feelthere.com — http://www.wilcopub.com

[fltsim.1]
title=Feelthere A321 CFM Aeroflot
sim=FeelThere_A321CFM
model=cfm
panel=
sound=
texture=aeroflot
kb_checklists=
kb_reference=a321
atc_id=321
atc_id_color=0xffffffff
atc_airline=AEROFLOT
atc_flight_number=236
ui_manufacturer=Airbus Wilco/SMS
ui_type=Airbus A321
ui_variation=Aeroflot Russian Airlines
description=Overland Co.,Ltd. Products — Airbus A321

[exits]
number_of_exits=2
exit.0 = 0.25, 53.5, -5.5, 2.8, 0
exit.1 = 0.4, -23.5, 5.0, -2.2, 1

[Views]
eyepoint=61.73, -1.65, 5.25

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0= 1, 9.55, 0.0, -4.84, fx_beaconb ,
light.1= 1, 6.32, 0.0, 9.45, fx_beaconh ,
light.2= 2,-75.95, -0.17, 5.19, fx_strobe ,
light.3= 3,-75.95, 0.17, 5.19, fx_navwhi ,
light.4= 4, 60.90, 0.0, 6.70, fx_vclighth //61.73, -1.65, 5.25

[General]
atc_type=AIRBUS
atc_model=A321
performance=Dimensions: Wing span: 111 ft 10 in (33.91 m) n Length: 123 ft 3 in (37.57 m) n Height: 38 ft 9.50 in (11.80 m) n Weights: n Empty: 106,00 lb n Max take-off: 196,000 lb n Performance: Cruise speed: 608 mph (978.48 km/h) n Max Operating altitude: 40,000 ft (12,192 m) n Maximum range: 3,222 miles (5,185 km) n Powerplants: Two IAE V2525-A5 rated at 25,000 lb (111.2 kN) or Two CFM International CFM56-5B4 rated at 32.000 lbs. Hi-bypass Turbofans
Category=airplane

[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
pitot_heat=1.000000

[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
auto_spoiler_available=1
spoiler_extension_time=1.200000
positive_g_limit_flaps_up=2.608974
positive_g_limit_flaps_down=1.709402
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-0.858974

[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
auto_brakes=4

[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
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=2

[turn_indicators]
turn_indicator.0=1,0

[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[deice_system]
structural_deice_type=1

Сообщение отредактировал Jeka_M: 03 June 2011 — 19:33

убрал под спойлер

<div class="post entry-content" itemprop="commentText">
<blockquote class="ipsBlockquote" data-author="'Махони'" data-cid="1719002" data-time="1296022898">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. </blockquote> 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 <div class="bbc_spoiler">
Spoiler <input class="bbc_spoiler_show" type="button" value="Show"/>
<div class="bbc_spoiler_wrapper"><div class="bbc_spoiler_content" style="display:none;"> // feelThere A321 CFM [fltsim.0] title=Feelthere A321 CFM Airbus House sim=FeelThere_A321CFM sound= model= texture=HOUSE atc_airline=Airbus panel= checklists= atc_id=FGTWW atc_flight_number=321 atc_heavy=0 ui_manufacturer=Airbus Wilco/SMS ui_type=A321 CFM ui_variation=Airbus House ui_typerole="Commercial Airliner" ui_createdby="feelThere/Wilco" visual_damage=1 description=Airbus Series Vol.1nDeveloped by www.feelThere.com nPublished by Wilco Publishing www.wilcopub.comnnSupport at www.feelthere.com - www.wilcopub.com [fltsim.1] title=Feelthere A321 CFM Aeroflot sim=FeelThere_A321CFM model=cfm panel= sound= texture=aeroflot kb_checklists= kb_reference=a321 atc_id=321 atc_id_color=0xffffffff atc_airline=AEROFLOT atc_flight_number=236 ui_manufacturer=Airbus Wilco/SMS ui_type=Airbus A321 ui_variation=Aeroflot Russian Airlines description=Overland Co.,Ltd. Products --- Airbus A321 [exits] number_of_exits=2 exit.0 = 0.25, 53.5, -5.5, 2.8, 0 exit.1 = 0.4, -23.5, 5.0, -2.2, 1 [Views] eyepoint=61.73, -1.65, 5.25 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0= 1, 9.55, 0.0, -4.84, fx_beaconb , light.1= 1, 6.32, 0.0, 9.45, fx_beaconh , light.2= 2,-75.95, -0.17, 5.19, fx_strobe , light.3= 3,-75.95, 0.17, 5.19, fx_navwhi , light.4= 4, 60.90, 0.0, 6.70, fx_vclighth //61.73, -1.65, 5.25 [General] atc_type=AIRBUS atc_model=A321 performance=Dimensions: Wing span: 111 ft 10 in (33.91 m) n Length: 123 ft 3 in (37.57 m) n Height: 38 ft 9.50 in (11.80 m) n Weights: n Empty: 106,00 lb n Max take-off: 196,000 lb n Performance: Cruise speed: 608 mph (978.48 km/h) n Max Operating altitude: 40,000 ft (12,192 m) n Maximum range: 3,222 miles (5,185 km) n Powerplants: Two IAE V2525-A5 rated at 25,000 lb (111.2 kN) or Two CFM International CFM56-5B4 rated at 32.000 lbs. Hi-bypass Turbofans Category=airplane [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 pitot_heat=1.000000 [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 auto_spoiler_available=1 spoiler_extension_time=1.200000 positive_g_limit_flaps_up=2.608974 positive_g_limit_flaps_down=1.709402 negative_g_limit_flaps_up=-1.500000 negative_g_limit_flaps_down=-0.858974 [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 auto_brakes=4 [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 stick_shaker=1 [attitude_indicators] attitude_indicator.0=2 [turn_indicators] turn_indicator.0=1,0 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=1 </div></div>
</div>
 

							Сообщение отредактировал Jeka_M: 03 June 2011 - 19:33
							
								 
убрал под спойлер

</div>

29.01.2011 в 14:47

Все заработало! Ошибка была в строке model= файла Aircraft.cfg. Там ничего не должно быть приписано.

Только вот ВК постоянно с черными экранами и вообще в колд-энд-дарке.

29.01.2011 в 15:50

Только вот ВК постоянно с черными экранами и вообще в колд-энд-дарке.

Ну так и будет. Я же говорил, что в Оверлэнде ВК встроена в модель, а не идет отдельным файлом, как у Вилко. Значит поменять получится только 2D панель. А так как все приборы при переустановке получаются вилковские, они тупо не подходят под ВК Оверлэнда, вот и получаются черные квадраты. Для FSX лучше мерж Wilco+PA…

31.01.2011 в 05:52

Ну так и будет. Я же говорил, что в Оверлэнде ВК встроена в модель, а не идет отдельным файлом, как у Вилко. Значит поменять получится только 2D панель. А так как все приборы при переустановке получаются вилковские, они тупо не подходят под ВК Оверлэнда, вот и получаются черные квадраты. Для FSX лучше мерж Wilco+PA…

Вот-вот..вчера потестил — визуалка конечно безусловно хороша, но носовая опора не поворачивается, например((( плюс fmgs не правильно v1, vr, v2 рассчитывает — по данным fmgs отрыв должен был произойти на 156 узлах, а реально отрыв был на 180-ти (!!)…в общем пока остаюсь летать на а319-320 Wilco+PA..

31.01.2011 в 06:28

визуалка конечно безусловно хороша…

Спорный вопрос. Есть моменты, где она проигрывает PA…

16.02.2011 в 21:06

А возможно ли как-то скрестить модели A340-200 и A340-500? Или только осуществимо с -300 и с -600?

17.02.2011 в 13:51

1officer, разумеется можно =)
делаете так.
берете 2 aircraft.cfg первый от SMS, второй от WILCO. Затем в конфиге из конфига от SMS копируете секции:
contact points
lights
exit
smokesystem
general engine data
и заменяете ими данные в конфиге от WILCO, данные полученные выложите здесь под спойлер. мы проверим, и если они верны то добавим в шапку

23.02.2011 в 19:51

Paha_S7, спасибо за консультацию! Решил поискать информацию на зарубежных сайтах, там совету.т в любых сборках менять вот эти секции:
exits
views
lightsl
contact points
folding wings
tail hook

А также строку reference_datum_position в секции Weight and balance.

Сделал в соответствии с рекомендациями сборку A340-500 Wilco + Overland. Самолет протестировал по маршруту WSSS — LSZH, 14 часов без нареканий. Результат под спойлером:

Spoiler

// FeelThere A340-600

[fltsim.0]
title=FSPAP A340-500 Air Canada (No VC)
sim=FeelThere_A340-600
model=
panel=
sound=
texture=ACA
atc_id=C-GKOL
atc_airline=Air Canada
atc_flight_number=51
atc_heavy=1
ui_manufacturer=Simmer’s Sky
ui_type=Airbus A340-500
ui_variation=AIR CANADA (No VC)
description=Overland Co.,Ltd. Products — Airbus A340-500nnL1 Cabin Door [Shift+E] then [1]nCargo Door Operate with Door Display GaugenL2 Cabin Door Operate with Door Display Gauge

[fltsim.1]
title=FSPAP A340-500 Singapore Airlines
sim=FeelThere_A340-600
model=
panel=
sound=
texture=SIA
atc_id=9V-SGE
atc_airline=Singapore
atc_flight_number=51
atc_heavy=1
ui_manufacturer=Simmer’s Sky
ui_type=Airbus A340-500
ui_variation=SINGAPORE AIRLINES (No VC)
description=Overland Co.,Ltd. Products — Airbus A340-500nnL1 Cabin Door [Shift+E] then [1]nCargo Door Operate with Door Display GaugenL2 Cabin Door Operate with Door Display Gauge

[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second

[Views]
eyepoint=99.62, -1.75, 3.85

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1 = 1, 28.40, -0.01, -9.95, fx_beaconb ,
light.2 = 1, 11.10, -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=2.00000,0.000000,-4.000000
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 =»4534, 16.0, 0.0, 0.0, Baggage»
station_load.3 =»8972, 0.0, 0.0, 0.0, Cargo»
station_load.4 =»5952, 26.0, 0.0, 0.0, First»
station_load.5 =»59358, 0.0, 0.0, 0.0, Coach»

empty_weight= 390220
max_gross_weight=804675
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=56000.000000 // Trent Engines for A340-600
afterburner_available=0
reverser_available=1

[GeneralEngineData]
engine_type=1
Engine.0= 0.0, -30.0, -2.500000
Engine.1= -10.0, -68.0, -2.500000
Engine.2= 0.00, 30.0, -2.500000
Engine.3= -10.0, 68.0, -2.500000
fuel_flow_scalar=0.73
min_throttle_limit=-0.7

[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]
point.0=1, 86.42, 0.00, -16.62, 1181.1, 0, 3.554, 60.0, 1.03, 1.7, 0.7235, 8.0, 10.2, 0, 0.0, 0.0 //nose
point.1=1, -6.50, -19.80, -18.04, 1574.8, 1, 4.737, 0.0, 1.71, 2.0, 0.7470, 9.7, 14.1, 2, 0.0, 0.0 //left main
point.2=1, -6.50, 19.80, -18.04, 1574.8, 2, 4.737, 0.0, 1.71, 2.0, 0.7470, 9.7, 14.1, 3, 0.0, 0.0 //right main
point.3=1, -8.75, 0.00, -18.00, 1574.8, 0, 4.737, 0.0, 1.71, 2.0, 0.7470, 9.7, 14.1, 0,185.0,250.0 //center main

point.4=2, -10.17, -47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.5=2, -10.17, 47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.6=2, -83.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0

static_pitch=-0.83
static_cg_height=20.570
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=1

[turn_indicators]
turn_indicator.0=1,0

[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=100,100 ;Percent per second

[TailHook]
tailhook_length=4 ;(feet)
tailhook_position=0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.0

<div class="post entry-content" itemprop="commentText">
Paha_S7, спасибо за консультацию! Решил поискать информацию на зарубежных сайтах, там совету.т в любых сборках менять вот эти секции: 
exits 
views 
lightsl 
contact points 
folding wings 
tail hook 
 
А также строку reference_datum_position в секции Weight and balance. 
 
Сделал в соответствии с рекомендациями сборку A340-500 Wilco + Overland. Самолет протестировал по маршруту WSSS - LSZH, 14 часов без нареканий. Результат под спойлером: 
 
<div class="bbc_spoiler">
Spoiler <input class="bbc_spoiler_show" type="button" value="Show"/>
<div class="bbc_spoiler_wrapper"><div class="bbc_spoiler_content" style="display:none;"> 
// FeelThere A340-600 
 
 
[fltsim.0] 
title=FSPAP A340-500 Air Canada (No VC) 
sim=FeelThere_A340-600 
model= 
panel= 
sound= 
texture=ACA 
atc_id=C-GKOL 
atc_airline=Air Canada 
atc_flight_number=51 
atc_heavy=1 
ui_manufacturer=Simmer's Sky 
ui_type=Airbus A340-500 
ui_variation=AIR CANADA (No VC) 
description=Overland Co.,Ltd. Products --- Airbus A340-500nnL1 Cabin Door 	[Shift+E] then [1]nCargo Door 	Operate with Door Display GaugenL2 Cabin Door Operate with Door Display Gauge 
 
[fltsim.1] 
title=FSPAP A340-500 Singapore Airlines 
sim=FeelThere_A340-600 
model= 
panel= 
sound= 
texture=SIA 
atc_id=9V-SGE 
atc_airline=Singapore 
atc_flight_number=51 
atc_heavy=1 
ui_manufacturer=Simmer's Sky 
ui_type=Airbus A340-500 
ui_variation=SINGAPORE AIRLINES (No VC) 
description=Overland Co.,Ltd. Products --- Airbus A340-500nnL1 Cabin Door 	[Shift+E] then [1]nCargo Door 	Operate with Door Display GaugenL2 Cabin Door Operate with Door Display Gauge 
 
[exits] 
number_of_exits=2 
exit_rate.0=0.4 			;Percent per second 
exit_rate.1=0.4 			;Percent per second 
 
[Views] 
eyepoint=99.62, -1.75, 3.85 
 
[LIGHTS] 	 
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 
light.1 = 1, 28.40, -0.01, -9.95, fx_beaconb , 
light.2 = 1, 11.10, -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=2.00000,0.000000,-4.000000 
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 ="4534, 16.0, 0.0, 0.0, Baggage" 
station_load.3 ="8972, 0.0, 0.0, 0.0, Cargo" 	 
station_load.4 ="5952, 26.0, 0.0, 0.0, First" 
station_load.5 ="59358, 0.0, 0.0, 0.0, Coach" 
 
empty_weight= 390220 
max_gross_weight=804675 
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=56000.000000 // Trent Engines for A340-600 
afterburner_available=0 
reverser_available=1 
 
[GeneralEngineData] 
engine_type=1 
Engine.0= 0.0, -30.0, -2.500000 
Engine.1= -10.0, -68.0, -2.500000 
Engine.2= 0.00, 30.0, -2.500000 
Engine.3= -10.0, 68.0, -2.500000 
fuel_flow_scalar=0.73 
min_throttle_limit=-0.7 
 
[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] 
point.0=1, 86.42, 0.00, -16.62, 1181.1, 0, 3.554, 60.0, 1.03, 1.7, 0.7235, 8.0, 10.2, 0, 0.0, 0.0 //nose 
point.1=1, -6.50, -19.80, -18.04, 1574.8, 1, 4.737, 0.0, 1.71, 2.0, 0.7470, 9.7, 14.1, 2, 0.0, 0.0 //left main 
point.2=1, -6.50, 19.80, -18.04, 1574.8, 2, 4.737, 0.0, 1.71, 2.0, 0.7470, 9.7, 14.1, 3, 0.0, 0.0 //right main 
point.3=1, -8.75, 0.00, -18.00, 1574.8, 0, 4.737, 0.0, 1.71, 2.0, 0.7470, 9.7, 14.1, 0,185.0,250.0 	//center main 
 
point.4=2, -10.17, -47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 
point.5=2, -10.17, 47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 
point.6=2, -83.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 
point.7=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 
 
static_pitch=-0.83 
static_cg_height=20.570 
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=1 
 
 
[turn_indicators] 
turn_indicator.0=1,0 
 
[folding_wings] 
wing_fold_system_type=4 ;0=None 
fold_rates=100,100 ;Percent per second 
 
[TailHook] 
tailhook_length=4 ;(feet) 
tailhook_position=0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum 
cable_force_adjust=0.0 
</div></div>
</div>

</div>

28.02.2011 в 09:20

Stakan, установи гауги от Overlenda =) должно помочь, если не поможет то себе поставлю мерж и отпишусь…

11.10.2011 в 08:17

он есть надо только точку обзора на место поставить. А у меня нет особо времени сидеть подгонять

Spoiler

[Vcockpit01]
Background_color=0,0,0
size_mm=512
visible=1
pixel_size=512
texture=$g1

gauge00=A346RR_feelThere!Standby Airspeed, 5,1,133,123
gauge01=A346RR_feelThere!Standby Altimeter, 143,2,132,124
gauge02=A346RR_feelThere!Standby Attitude VC, 6,132,150,144
gauge03=A346RR_feelThere!Baro, 314,333,98,129
gauge04=A346RR_feelThere!Analog Clock, 278,-1,127,128
gauge05=PAPA330!Engine Start Knob 1, 409,1,48,49
gauge06=PAPA330!Engine Start Knob 2, 462,2,46,48
gauge07=A346RR_feelThere!Chrono, 164,201,65,67
gauge08=A346RR_feelThere!Warnings, 163,130,64,146
gauge09=PAPA330!ABS Aps Window, 47,469,459,40
gauge10=PAPA330!Flight Director Switch, 417,280,41,35
gauge11=PAPA330!Autopilot ILS Switch, 417,318,40,35
gauge12=PAPA330!Autopilot IAS-Mach Switch, 416,356,41,33
gauge13=PAPA330!Autopilot Speed Switch, 417,394,40,34
gauge14=PAPA330!Autopilot Localizer Switch, 417, 431 ,40,33
gauge15=PAPA330!Autopilot Master Switch, 462,280,41,33
gauge16=PAPA330!Autopilot Master Switch, 463,318,40,35
gauge17=PAPA330!Autothrottle Switch, 463,356,41,35
gauge18=PAPA330!Autopilot Altitude Hold Switch, 463,394,40,35
gauge19=A346RR_feelThere!DDRMI, 5,284,138,175
gauge20=PAPA330!Autopilot Approach Switch, 463,431,40,35
gauge21=A346RR_feelThere!Icon Bar, 461,55,41,43
gauge22=simicons!GPS Icon, 464,149,39,40
gauge23=simicons!Map Icon, 415,103,40,41
gauge24=simicons!Kneeboard Icon, 414,56,42,41
gauge25=PAPA330!VC_Autobrakes Switch, 238,133,155,199
gauge26=PAPA330!VC_Anti Ice Eng1 Switch, 151,341,30,28
gauge27=PAPA330!VC_Anti Ice Eng2 Switch, 184,341,30,28

// ———————————————————

[Vcockpit02]
Background_color=0,0,0
size_mm=512
visible=1
pixel_size=512
texture=$ABmain

gauge00=A346RR_feelThere!System,0,0,0,0
gauge01=A346RR_FeelThere!Primary Flight Display, 6,10,228,208
gauge02=A346RR_FeelThere!Navigation Display, 245,5,263,267
gauge03=A346RR_FeelThere!Engine/Warning Display, 3,268,233,230
gauge04=A346RR_FeelThere!System Display, 248,315,196,187

// ———————————————————

[Default View]
X=0
Y=0
SIZE_X=8192
SIZE_Y=2600

[Color]
Day=255,255,255
Night=255,255,255
Luminous=255,255,255

поставите на место буду благодарен

скажите, какой параметр отвечает за точку обзора в ВК ?

<div class="post entry-content" itemprop="commentText">
<blockquote class="ipsBlockquote" data-author="Paha_S7" data-cid="1662458" data-time="1291640625">он есть <img alt=":)" class="bbc_emoticon" src="https://www.avsim.su/wp-content/themes/avia/img/smile.png"/> надо только точку обзора на место поставить. А у меня нет особо времени сидеть подгонять <div class="bbc_spoiler">
Spoiler <input class="bbc_spoiler_show" type="button" value="Show"/>
<div class="bbc_spoiler_wrapper"><div class="bbc_spoiler_content" style="display:none;">[Vcockpit01] Background_color=0,0,0 size_mm=512 visible=1 pixel_size=512 texture=$g1 gauge00=A346RR_feelThere!Standby Airspeed, 5,1,133,123 gauge01=A346RR_feelThere!Standby Altimeter, 143,2,132,124 gauge02=A346RR_feelThere!Standby Attitude VC, 6,132,150,144 gauge03=A346RR_feelThere!Baro, 314,333,98,129 gauge04=A346RR_feelThere!Analog Clock, 278,-1,127,128 gauge05=PAPA330!Engine Start Knob 1, 409,1,48,49 gauge06=PAPA330!Engine Start Knob 2, 462,2,46,48 gauge07=A346RR_feelThere!Chrono, 164,201,65,67 gauge08=A346RR_feelThere!Warnings, 163,130,64,146 gauge09=PAPA330!ABS Aps Window, 47,469,459,40 gauge10=PAPA330!Flight Director Switch, 417,280,41,35 gauge11=PAPA330!Autopilot ILS Switch, 417,318,40,35 gauge12=PAPA330!Autopilot IAS-Mach Switch, 416,356,41,33 gauge13=PAPA330!Autopilot Speed Switch, 417,394,40,34 gauge14=PAPA330!Autopilot Localizer Switch, 417, 431 ,40,33 gauge15=PAPA330!Autopilot Master Switch, 462,280,41,33 gauge16=PAPA330!Autopilot Master Switch, 463,318,40,35 gauge17=PAPA330!Autothrottle Switch, 463,356,41,35 gauge18=PAPA330!Autopilot Altitude Hold Switch, 463,394,40,35 gauge19=A346RR_feelThere!DDRMI, 5,284,138,175 gauge20=PAPA330!Autopilot Approach Switch, 463,431,40,35 gauge21=A346RR_feelThere!Icon Bar, 461,55,41,43 gauge22=simicons!GPS Icon, 464,149,39,40 gauge23=simicons!Map Icon, 415,103,40,41 gauge24=simicons!Kneeboard Icon, 414,56,42,41 gauge25=PAPA330!VC_Autobrakes Switch, 238,133,155,199 gauge26=PAPA330!VC_Anti Ice Eng1 Switch, 151,341,30,28 gauge27=PAPA330!VC_Anti Ice Eng2 Switch, 184,341,30,28 // --------------------------------------------------------- [Vcockpit02] Background_color=0,0,0 size_mm=512 visible=1 pixel_size=512 texture=$ABmain gauge00=A346RR_feelThere!System,0,0,0,0 gauge01=A346RR_FeelThere!Primary Flight Display, 6,10,228,208 gauge02=A346RR_FeelThere!Navigation Display, 245,5,263,267 gauge03=A346RR_FeelThere!Engine/Warning Display, 3,268,233,230 gauge04=A346RR_FeelThere!System Display, 248,315,196,187 // --------------------------------------------------------- [Default View] X=0 Y=0 SIZE_X=8192 SIZE_Y=2600 [Color] Day=255,255,255 Night=255,255,255 Luminous=255,255,255</div></div>
</div> поставите на место буду благодарен </blockquote> скажите, какой параметр отвечает за точку обзора в ВК ?
					
					 
</div>

28.10.2011 в 08:06

Sataroth, [views] :wink:

20.08.2013 в 13:59

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

Spoiler

[exits]
number_of_exits=2
exit.0 = 0.25, 35.5, -5.5, 2.8, 0
exit.1 = 0.4, -18.5, 5.0, -2.2, 1

[Views]
eyepoint=43.13, -1.85, 5.19

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -5.81, -54.7, 3.49, fx_navred ,
light.1=3, -5.81, 54.7, 3.49, fx_navgre ,
light.2=2, -6.42, -55.3, 3.59, fx_strobe ,
light.3=2, -6.42, 55.3, 3.59, fx_strobe ,
light.4=1, 14.15, 0.0, -4.90, fx_beaconh ,
light.5=1, 11.52, 0.0, 9.55, fx_beaconh ,
light.6=2,-54.23, 0.17, 5.19, fx_strobe ,
light.7=3,-54.23, -0.17, 5.19, fx_navwhi ,
light.8 = 4, 39, 0, 5.7, fx_vclighth

[General]
atc_type=AIRBUS
atc_model=A319
performance=Dimensions: Wing span: 111 ft 10 in (33.91 m) n Length: 111 ft 0 in (33.84 m) n Height: 38 ft 7 in (11.76 m) n Weights: n Empty: 89,000 lb n Max take-off: 166,000 lb n Performance: Cruise speed: 608 mph (978.48 km/h) n Max Operating altitude: 40,000 ft (12,192 m) n Maximum range: 3,700 miles (6,800 km) n Powerplants: Two IAE V2525-A5 rated at 23.500 lbs (111.2 kN) or Two CFM International CFM56-5B4 rated at 22.000 lbs. Hi-bypass Turbofans

[WEIGHT_AND_BALANCE]
reference_datum_position=0, 0, -4.4
max_number_of_stations=50

station_load.0 = «450, 42.0, 0.0, 0.0, Crew»
station_load.1 = «1000, 37.0, 0.0, 0.0, Galleys»
station_load.2 = «4000, 16.0, 0.0, 0.0, Baggage»
station_load.3 = «7000, 0.0, 0.0, 0.0, Cargo»
station_load.4 = «6200, 26.0, 0.0, 0.0, First»
station_load.5 = «17000, 0.0, 0.0, 0.0, Coach»

empty_weight= 89500
max_gross_weight=167300
empty_weight_roll_MOI=1300000
empty_weight_pitch_MOI=2000000
empty_weight_yaw_MOI=2000000
empty_weight_coupled_MOI=0.0
empty_weight_CG_position=0.000, 0.000, 0.000

[pitot_static]
vertical_speed_time_constant=999

[GROUND_REACTION]
MAX_STEERING_ANGLE=75

[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.1
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.0
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.6
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 200
electric_always_available = 1
flap_motor = 0, 0 , 17.0
gear_motor = 0, 0 , 17.0
autopilot = 0, 0 , 17.0
avionics_bus = 0, 0 , 17.0
avionics = 0, 0 , 17.0
pitot_heat = 0, 0 , 17.0
additional_system = 0, 0 , 17.0
marker_beacon = 0, 0 , 17.0
gear_warning = 0, 0 , 17.0
fuel_pump = 0, 0 , 17.0
starter1 = 0, 0 , 17.0
starter2 = 0, 0 , 17.0
light_nav = 0, 0 , 17.0
light_beacon = 0, 0 , 17.0
light_landing = 0, 0 , 17.0
light_taxi = 0, 0 , 17.0
light_strobe = 0, 0 , 17.0
light_panel = 0, 0 , 17.0
light_cabin = 0, 0 , 17.0
auto_brakes = 0, 0 , 17.0
standby_vacuum = 0, 0 , 17.0
hydraulic_pump = 0, 0 , 17.0
fuel_transfer_pump = 0, 0 , 17.0
light_recognition = 0, 0 , 17.0
light_wing = 0, 0 , 17.0
light_logo = 0, 0 , 17.0
directional_gyro = 0, 0 , 17.0
directional_gyro_slaving = 0, 0 , 17.0

[TurbineEngineData]
fuel_flow_gain=0.001
inlet_area=30
rated_N2_rpm=29920.000000
static_thrust=22000.000000
afterburner_available=0
reverser_available=1

[GeneralEngineData]
engine_type=1
Engine.0= 3.0, -17.5, -2.500000
Engine.1= 3.0, 17.5, -2.500000
fuel_flow_scalar=1.0000
min_throttle_limit=-0.499939
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear

[jet_engine]
thrust_scalar =1.1

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[direction_indicators]
direction_indicator.0=3,0

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

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=20.000000
system_type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=0.0
flaps-position.2=13.0 //nominal value should be10 but we need big effect RY
flaps-position.3=20.0 //ditto to accomodate flap 2
flaps-position.4=29.0 //ditto to accomodate flap 2
flaps-position.5=40.0 //More lift for patched solution to low lift RY

[Flaps.1]
type=2
span-outboard=0.800
extending-time=20.000
system_type=1
damaging-speed=232.000
blowout-speed=250.000
lift_scalar=0.3
drag_scalar=0.2
pitch_scalar=0.0
flaps-position.0=0
flaps-position.1=18.0
flaps-position.2=18.0
flaps-position.3=22.0
flaps-position.4=22.0
flaps-position.5=27.0

[forcefeedback]
gear_bump_nose_magnitude=3000 ; 0 — 10000
gear_bump_nose_direction=18000 ; 0 — 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 — 10000
gear_bump_left_direction=35500 ; 0 — 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 — 10000
gear_bump_right_direction=00500 ; 0 — 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 — 10000
ground_bumps_angle1=08900 ; 0 — 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 — 10000
ground_bumps_angle2=09100 ; 0 — 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000 ; 0 — 10000
crash_direction1=01000 ; 0 — 35999 degrees
crash_magnitude2=10000 ; 0 — 10000
crash_direction2=9000 ; 0 — 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=2500000 ; in microseconds

[fuel]
Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000
LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000
RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000
LeftAux= 0.0, -13.0, 0.0, 227.000000, 0.000000
RightAux= 0.0, 13.0, 0.0, 227.000000, 0.000000

fuel_type=2.000000
number_of_tank_selectors=2
electric_pump=1

[airplane_geometry]
wing_area=1320.000000
wing_span=111.9
wing_root_chord=12.000000
wing_dihedral=5
wing_incidence=1.5
wing_twist=1
oswald_efficiency_factor=0.8723
wing_winglets_flag=1
wing_sweep=22
wing_pos_apex_lon=15.00000
wing_pos_apex_vert=0.000000
htail_area=328.000000
htail_span=40.000000
htail_pos_lon=-50.000000
htail_pos_vert=0.000000
htail_incidence=2.993774
htail_sweep=0.000000
vtail_area=249.000000
vtail_span=17.991665
vtail_sweep=0.000000
vtail_pos_lon=-50.000000
vtail_pos_vert=20.500000
elevator_area=70.500000
aileron_area=26.800000
rudder_area=56.200000
elevator_up_limit=28
elevator_down_limit=22
aileron_up_limit=22
aileron_down_limit=20
rudder_limit=32
elevator_trim_limit=18
spoiler_limit=50
spoilerons_available=1
aileron_to_spoileron_gain=3.000000
min_ailerons_for_spoilerons=9.0
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1, 35.80, 0.00, -10.56, 1500, 0, 1.25, 60.12, 0.38, 2.4, 0.5135, 7.0, 8.2, 0, 0.0, 0.0
point.1=1, -4.25, -11.58, -11.06, 2200, 1, 2.15, 0.00, 1.11, 2.0, 0.5470, 9.7, 14.1, 2, 0.0, 0.0
point.2=1, -4.25, 11.58, -11.06, 2200, 2, 2.15, 0.00, 1.11, 2.0, 0.5470, 9.7, 14.1, 3, 0.0, 0.0

point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0

max_number_of_points=21

static_pitch= -0.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=14.26 //feet, altitude of CG when at rest on the ground
gear_system_type=0

[brakes]
toe_brakes_scale=0.86
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=10.04

[Reference Speeds]
flaps_up_stall_speed=180.000000 // at MTW
full_flaps_stall_speed=132.000000// at MTW
cruise_speed=320
max_indicated_speed=352.000000
max_mach=0.84

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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=0.8
max_pitch_velocity_lo_alt=1.0
max_pitch_velocity_hi_alt=1.0
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=3.0
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=2

[turn_indicators]
turn_indicator.0=1,0

хороший конфиг

<div class="post entry-content" itemprop="commentText">
<blockquote class="ipsBlockquote" data-author="VRP" data-cid="1652476" data-time="1290881693">
<div>
Вот, парни, попробуйте мой конфиг A319CFM. (Отдельное спасибо ROCKAVIA за предоставленную информацию!) Вроде летает более-менее похоже на A319, только при посадке Landing Lights светят почему-то в левую сторону, не знаю - это где-то моя ошибка или какой-то глюк. Кто знает что к чему, пожалуйста, отпишитесь. 
<div class="bbc_spoiler">
Spoiler <input class="bbc_spoiler_show" type="button" value="Show"/>
<div class="bbc_spoiler_wrapper"><div class="bbc_spoiler_content" style="display:none;">[exits] 
number_of_exits=2 
exit.0 = 0.25, 35.5, -5.5, 2.8, 0 
exit.1 = 0.4, -18.5, 5.0, -2.2, 1 
[Views] 
eyepoint=43.13, -1.85, 5.19 
[LIGHTS] 
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 
light.0=3, -5.81, -54.7, 3.49, fx_navred , 
light.1=3, -5.81, 54.7, 3.49, fx_navgre , 
light.2=2, -6.42, -55.3, 3.59, fx_strobe , 
light.3=2, -6.42, 55.3, 3.59, fx_strobe , 
light.4=1, 14.15, 0.0, -4.90, fx_beaconh , 
light.5=1, 11.52, 0.0, 9.55, fx_beaconh , 
light.6=2,-54.23, 0.17, 5.19, fx_strobe , 
light.7=3,-54.23, -0.17, 5.19, fx_navwhi , 
light.8 = 4, 39, 0, 5.7, fx_vclighth 
[General] 
atc_type=AIRBUS 
atc_model=A319 
performance=Dimensions: Wing span: 111 ft 10 in (33.91 m) n Length: 111 ft 0 in (33.84 m) n Height: 38 ft 7 in (11.76 m) n Weights: n Empty: 89,000 lb n Max take-off: 166,000 lb n Performance: Cruise speed: 608 mph (978.48 km/h) n Max Operating altitude: 40,000 ft (12,192 m) n Maximum range: 3,700 miles (6,800 km) n Powerplants: Two IAE V2525-A5 rated at 23.500 lbs (111.2 kN) or Two CFM International CFM56-5B4 rated at 22.000 lbs. Hi-bypass Turbofans 
[WEIGHT_AND_BALANCE] 
reference_datum_position=0, 0, -4.4 
max_number_of_stations=50 
station_load.0 = "450, 42.0, 0.0, 0.0, Crew" 
station_load.1 = "1000, 37.0, 0.0, 0.0, Galleys" 
station_load.2 = "4000, 16.0, 0.0, 0.0, Baggage" 
station_load.3 = "7000, 0.0, 0.0, 0.0, Cargo" 
station_load.4 = "6200, 26.0, 0.0, 0.0, First" 
station_load.5 = "17000, 0.0, 0.0, 0.0, Coach" 
empty_weight= 89500 
max_gross_weight=167300 
empty_weight_roll_MOI=1300000 
empty_weight_pitch_MOI=2000000 
empty_weight_yaw_MOI=2000000 
empty_weight_coupled_MOI=0.0 
empty_weight_CG_position=0.000, 0.000, 0.000 
[pitot_static] 
vertical_speed_time_constant=999 
[GROUND_REACTION] 
MAX_STEERING_ANGLE=75 
[flight_tuning] 
cruise_lift_scalar =1.000 
parasite_drag_scalar =1.000 
induced_drag_scalar =1.1 
elevator_effectiveness =1.0 
aileron_effectiveness =1.0 
rudder_effectiveness =1.0 
pitch_stability =1.000 
roll_stability =1.000 
yaw_stability =1.000 
elevator_trim_effectiveness =0.6 
aileron_trim_effectiveness =1.000 
rudder_trim_effectiveness =1.000 
[electrical] 
max_battery_voltage = 24 
generator_alternator_voltage = 28 
max_generator_alternator_amps = 200 
electric_always_available = 1 
flap_motor = 0, 0 , 17.0 
gear_motor = 0, 0 , 17.0 
autopilot = 0, 0 , 17.0 
avionics_bus = 0, 0 , 17.0 
avionics = 0, 0 , 17.0 
pitot_heat = 0, 0 , 17.0 
additional_system = 0, 0 , 17.0 
marker_beacon = 0, 0 , 17.0 
gear_warning = 0, 0 , 17.0 
fuel_pump = 0, 0 , 17.0 
starter1 = 0, 0 , 17.0 
starter2 = 0, 0 , 17.0 
light_nav = 0, 0 , 17.0 
light_beacon = 0, 0 , 17.0 
light_landing = 0, 0 , 17.0 
light_taxi = 0, 0 , 17.0 
light_strobe = 0, 0 , 17.0 
light_panel = 0, 0 , 17.0 
light_cabin = 0, 0 , 17.0 
auto_brakes = 0, 0 , 17.0 
standby_vacuum = 0, 0 , 17.0 
hydraulic_pump = 0, 0 , 17.0 
fuel_transfer_pump = 0, 0 , 17.0 
light_recognition = 0, 0 , 17.0 
light_wing = 0, 0 , 17.0 
light_logo = 0, 0 , 17.0 
directional_gyro = 0, 0 , 17.0 
directional_gyro_slaving = 0, 0 , 17.0 
[TurbineEngineData] 
fuel_flow_gain=0.001 
inlet_area=30 
rated_N2_rpm=29920.000000 
static_thrust=22000.000000 
afterburner_available=0 
reverser_available=1 
[GeneralEngineData] 
engine_type=1 
Engine.0= 3.0, -17.5, -2.500000 
Engine.1= 3.0, 17.5, -2.500000 
fuel_flow_scalar=1.0000 
min_throttle_limit=-0.499939 
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear 
[jet_engine] 
thrust_scalar =1.1 
[EFFECTS] 
wake=fx_wake 
water=fx_spray 
dirt=fx_tchdrt 
concrete=fx_sparks 
touchdown=fx_tchdwn, 1 
[direction_indicators] 
direction_indicator.0=3,0 
[Radios] 
// Radio Type=availiable, standby frequency, has glide slope 
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 1, 1 
Nav.2=1, 1, 0 
Adf.1=1 
Transponder.1=1 
Marker.1=1 
[Flaps.0] 
type=1 
span-outboard=0.500000 
extending-time=20.000000 
system_type=1 
flaps-position.0=0.000000,0.000000 
flaps-position.1=0.0 
flaps-position.2=13.0 //nominal value should be10 but we need big effect RY 
flaps-position.3=20.0 //ditto to accomodate flap 2 
flaps-position.4=29.0 //ditto to accomodate flap 2 
flaps-position.5=40.0 //More lift for patched solution to low lift RY 
[Flaps.1] 
type=2 
span-outboard=0.800 
extending-time=20.000 
system_type=1 
damaging-speed=232.000 
blowout-speed=250.000 
lift_scalar=0.3 
drag_scalar=0.2 
pitch_scalar=0.0 
flaps-position.0=0 
flaps-position.1=18.0 
flaps-position.2=18.0 
flaps-position.3=22.0 
flaps-position.4=22.0 
flaps-position.5=27.0 
[forcefeedback] 
gear_bump_nose_magnitude=3000 ; 0 - 10000 
gear_bump_nose_direction=18000 ; 0 - 35999 degrees 
gear_bump_nose_duration=250000 ; in microseconds 
gear_bump_left_magnitude=2700 ; 0 - 10000 
gear_bump_left_direction=35500 ; 0 - 35999 degrees 
gear_bump_left_duration=250000 ; in microseconds 
gear_bump_right_magnitude=2700 ; 0 - 10000 
gear_bump_right_direction=00500 ; 0 - 35999 degrees 
gear_bump_right_duration=250000 ; in microseconds 
ground_bumps_magnitude1=1300 ; 0 - 10000 
ground_bumps_angle1=08900 ; 0 - 35999 degrees 
ground_bumps_intercept1=3.0 
ground_bumps_slope1=0.20 
ground_bumps_magnitude2=200 ; 0 - 10000 
ground_bumps_angle2=09100 ; 0 - 35999 degrees 
ground_bumps_intercept2=1.075 
ground_bumps_slope2=0.035 
crash_magnitude1=10000 ; 0 - 10000 
crash_direction1=01000 ; 0 - 35999 degrees 
crash_magnitude2=10000 ; 0 - 10000 
crash_direction2=9000 ; 0 - 35999 degrees 
crash_period2=75000 ; in microseconds 
crash_duration2=2500000 ; in microseconds 
[fuel] 
Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000 
LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000 
RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000 
LeftAux= 0.0, -13.0, 0.0, 227.000000, 0.000000 
RightAux= 0.0, 13.0, 0.0, 227.000000, 0.000000 
fuel_type=2.000000 
number_of_tank_selectors=2 
electric_pump=1 
[airplane_geometry] 
wing_area=1320.000000 
wing_span=111.9 
wing_root_chord=12.000000 
wing_dihedral=5 
wing_incidence=1.5 
wing_twist=1 
oswald_efficiency_factor=0.8723 
wing_winglets_flag=1 
wing_sweep=22 
wing_pos_apex_lon=15.00000 
wing_pos_apex_vert=0.000000 
htail_area=328.000000 
htail_span=40.000000 
htail_pos_lon=-50.000000 
htail_pos_vert=0.000000 
htail_incidence=2.993774 
htail_sweep=0.000000 
vtail_area=249.000000 
vtail_span=17.991665 
vtail_sweep=0.000000 
vtail_pos_lon=-50.000000 
vtail_pos_vert=20.500000 
elevator_area=70.500000 
aileron_area=26.800000 
rudder_area=56.200000 
elevator_up_limit=28 
elevator_down_limit=22 
aileron_up_limit=22 
aileron_down_limit=20 
rudder_limit=32 
elevator_trim_limit=18 
spoiler_limit=50 
spoilerons_available=1 
aileron_to_spoileron_gain=3.000000 
min_ailerons_for_spoilerons=9.0 
min_flaps_for_spoilerons=0.000000 
[contact_points] 
point.0=1, 35.80, 0.00, -10.56, 1500, 0, 1.25, 60.12, 0.38, 2.4, 0.5135, 7.0, 8.2, 0, 0.0, 0.0 
point.1=1, -4.25, -11.58, -11.06, 2200, 1, 2.15, 0.00, 1.11, 2.0, 0.5470, 9.7, 14.1, 2, 0.0, 0.0 
point.2=1, -4.25, 11.58, -11.06, 2200, 2, 2.15, 0.00, 1.11, 2.0, 0.5470, 9.7, 14.1, 3, 0.0, 0.0 
point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 
point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 
point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 
point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 
max_number_of_points=21 
static_pitch= -0.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn) 
static_cg_height=14.26 //feet, altitude of CG when at rest on the ground 
gear_system_type=0 
[brakes] 
toe_brakes_scale=0.86 
parking_brake=1 
[gear_warning_system] 
gear_warning_available=0 
pct_throttle_limit=0.099976 
flap_limit_power=25.496622 
flap_limit_idle=10.04 
[Reference Speeds] 
flaps_up_stall_speed=180.000000 // at MTW 
full_flaps_stall_speed=132.000000// at MTW 
cruise_speed=320 
max_indicated_speed=352.000000 
max_mach=0.84 
[keyboard_response] 
elevator=150.000000,250.000000 
aileron=150.000000,250.000000 
rudder=150.000000,250.000000 
[autopilot] 
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800.000000 
autothrottle_available=1 
autothrottle_arming_required=1 
autothrottle_takeoff_ga=1 
autothrottle_max_rpm=90.000000 
pitch_takeoff_ga=8.000000 
max_pitch=10.000000 
max_pitch_acceleration=0.8 
max_pitch_velocity_lo_alt=1.0 
max_pitch_velocity_hi_alt=1.0 
max_pitch_velocity_lo_alt_breakpoint=20000.000000 
max_pitch_velocity_hi_alt_breakpoint=28000.000000 
max_bank=25.000000 
max_bank_acceleration=3.0 
max_bank_velocity=3.000000 
max_throttle_rate=0.100000 
nav_proportional_control=9.000000 
nav_integrator_control=0.250000 
nav_derivative_control=0.000000 
nav_integrator_boundary=2.500000 
nav_derivative_boundary=0.000000 
gs_proportional_control=9.520000 
gs_integrator_control=0.260000 
gs_derivative_control=0.000000 
gs_integrator_boundary=0.700000 
gs_derivative_boundary=0.000000 
yaw_damper_gain=0.000000 
[hydraulic_system] 
electric_pumps=0 
engine_map=1,1,0,0 
normal_pressure=3000.000000 
[stall_warning] 
type=1 
[attitude_indicators] 
attitude_indicator.0=2 
[turn_indicators] 
turn_indicator.0=1,0 </div></div>
</div>
</div>
</blockquote>
 
 
хороший конфиг
 
</div>

12.12.2014 в 14:23

здравствуйте !! люди добрые у меня тут проблема с Simmer’s sky Overland , Элероны направление застревали в мертвом положение на A340-500 , A340-600 A380-800 . остальные работают
фото:
http://scr.hu/2mb/rgzn9

http://scr.hu/2mb/t9rct

http://scr.hu/2mb/cymv0

помогите устранить проблему !!!

25.04.2016 в 05:32

Есть ли возможность скорректировать эффективность «speed brake» и закрылки 1.

А330-300 overland/wilco масса 170 тонн скорость 220 узлов снижение вертикальная 1200 выпустил закрылки 1, как летел на 220 узлах так и идет дальше даже не шелохнулся…так и с тормозом что выпускашь что нет…эффект минимальный

25.04.2016 в 20:29

Есть ли возможность скорректировать эффективность «speed brake» и закрылки 1.
А330-300 overland/wilco масса 170 тонн скорость 220 узлов снижение вертикальная 1200 выпустил закрылки 1, как летел на 220 узлах так и идет дальше даже не шелохнулся…так и с тормозом что выпускашь что нет…эффект минимальный

Надо ковырять динамику. Если умеете это делать — флаг вам в руки и вперёд.

26.04.2016 в 06:05

Надо ковырять динамику. Если умеете это делать — флаг вам в руки и вперёд.

Ох, если бы умел не спрашивал бы точно)))

31.05.2016 в 18:02

Господа,есть у кого-то A320/321 с ВК на 9-ку..? Эйрсиммер + Вилко уродливый уж больно,да и взлетает как коров. Если есть — поделитесь,пожалуйста

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