2. То, что самолеты стоят на стоянках и не летают, это только означает одно — кривой флайт план (хотя, может у них расписание такое).

Предлагаю, в файле флайтплана выбрать любой понравившийся рейс.
Направится за 10 минут до отлета на место вылета, и проследить что там происходит.
Если рейс выполняется по расписанию, значит это такое расписание.

Иногда, авторы флайт планов для сима специально вводят в расписание стощие (реальные) на стоянках самолеты, которые уже давно никуда не летают, но они есть! Так вот, для того что бы в симе увидеть эти борта, для них создается отдельная строка в которой создается полет на 5! минут.
Только из-за того, что нельзя принудительно указывать стоянку на аэродроме где он стоит, эти самолеты оказываются на любых стоянках, в том числе и у гейтов .

P.S. У меня много флайт планов установлено, в которых некоторые рейсы выполняют один рейс в неделю, или парочку….
Из-за этого может сложится впечатление, что в аэропорту столпотворение никуда не летающих самолетов, но на самом деле, все работает, все летают!

P.S. Сегодня, заходил на промежуточную посадку где-то в Мексике (забыл название крупного аэродрома). Высота над уровнем моря более 11 тыс. футов. У меня все нормально получилось, а вот параллельно со мной на параллельную полосу заходил В757-200, так его пилотов не слабо колбасило, заходили ступеньками. В итоге торец ВПП они прошли на 2000ф. выше, чем надо, но полоса длинная и уже на середине ВПП они благополучно и очень жестко плюхнулись. Следом за мной шел A320-200, и тоже по аналогичной методике.
Я проверил FP, с эшелонами там все в порядке, и расстояние большое между п. вылета и п. назначения.
Значит, на таких высотных аэродромах не очень корректно трафик в симе работает.
И еще, с этого аэродрома, весьма бодро трафик набирает высоту.. Как правило 2 мин. и он уже на 31000 ф. А вот мой PT — 154 как и положено, еле ноги унес от туда.

Как мне кажется, проблема не в динамике и даже не в инсталлере МРАИ, а в… тебе. Прочти же наконец инструкцию к TrafficViewBoard.

Можно исправить это дело и если да, то подскажите пожалуйста, как?

[General]
atc_type=BEECHCRAFT
atc_model=BE20
editable=1
performance=»AI Aircraft»

[WEIGHT_AND_BALANCE]
max_gross_weight = 16000 // (pounds)
empty_weight = 10000 // (pounds)

reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 2.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 2

station_load.0 = «170, 5.0, -2.0, 0.0, Pilot» //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = «170, 5.0, 2.0, 0.0, Co-Pilot» //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI = 50000
empty_weight_roll_MOI = 48200
empty_weight_yaw_MOI = 46500
empty_weight_coupled_MOI= 0.0

[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.5
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0

[GeneralEngineData]
engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 7.3, -8.8, 0.7 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 7.3, 8.8, 0.7 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser

[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter = 8.8 //Propeller Diameter, (feet)
propeller_blades = 4 //Number of propeller blades
propeller_moi = 24 //Propeller moment of inertia
beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min = 15.2 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm = 25520 //Miminum governed RPM
prop_tc = 0.004 //Prop time-constant
gear_reduction_ratio = 17.6 //Propeller gear reduction ratio
fixed_pitch_beta = 0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit = 80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available = 1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available = 1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather = 700 //Minimum RPM for prop feathering
beta_feather = 79.3 //Feathering pitch angle (degrees)
power_absorbed_cf = 0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta = 1.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta = -14.0 //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain = 0.011 //Gain on fuel flow
inlet_area = 1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 158 //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar = 1.0 //Scalar on Turboprop power
maximum_torque = 3270 //Maximum torque available (ft-lbs)

[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0

//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)

[contact_points]
point.0=1, 13.00, 0.00, -4.65, 1181, 0, 0.600, 60.0, 0.500, 1.0, 0.900, 5.8, 5.8, 0, 0.0, 0.0
point.1=1, -2.10, -9.70, -4.40, 1574, 1, 0.600, 0.0, 0.500, 2.5, 0.800, 5.2, 5.2, 2, 0.0, 0.0
point.2=1, -2.10, 9.70, -4.40, 1574, 2, 0.600, 0.0, 0.500, 2.5, 0.800, 4.8, 4.8, 3, 0.0, 0.0

static_pitch = -0.6
static_cg_height = 4.2
gear_system_type=1 //Hydraulic

[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.2 //Brake scalar

[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2

[Views]
eyepoint = 4.54, -1.20, 3.25

[flaps.0]
type = 1 // 1 — tail, 2 — lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 20 // degrees
flaps-position.2 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS

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

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 0.00, -27.20, 2.00, fx_navred ,
light.1 = 3, 0.00, 27.20, 2.00, fx_navgre ,
light.2 = 3, -30.00, 0.00, 10.60, fx_navwhi ,
light.3 = 2, -0.05, -27.30, 2.00, fx_strobeh ,
light.4 = 2, -0.05, 27.30, 2.00, fx_strobeh ,
light.5 = 1, -25.40, 0.00, 11.00, fx_beaconb ,
light.6 = 1, -5.80, 0.00, -1.45, fx_beaconb ,

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

[fuel]
LeftMain = 0.0, -14.5, -1.0, 190.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = 0.0, -6.0, -1.5, 79.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0.0, 14.5, -1.0, 190.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = 0.0, 6.0, -1.5, 79.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1

[airplane_geometry]
wing_area = 320.0 //Square feet
wing_span = 47.2 //Feet
wing_root_chord = 5.4 //Feet
wing_dihedral = 6.0 //Degrees
wing_incidence = 1.0 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.7 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 1.0 //Degrees, wing leading edge
wing_pos_apex_lon = 2.1 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 67.0 //Square feet
htail_span = 17.2 //Feet
htail_pos_lon = -22.6 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.5 //Degrees
htail_sweep = 20.0 //Degrees, horizontal tail leading edge
vtail_area = 42.0 //Square feet
vtail_span = 7.4 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -20.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 4.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 17.0 //Square feet
aileron_area = 13.5 //Square feet
rudder_area = 7.3 //Square feet
elevator_up_limit = 17.0 //Degrees
elevator_down_limit = 15.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed = 96.0 //Knots True (KTAS)
full_flaps_stall_speed = 76.8 //Knots True (KTAS)
cruise_speed = 300.0 //Knots True (KTAS)
max_mach = 0.58
max_indicated_speed = 263 //Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[forcefeedback]

[stall_warning]
type=2