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-=ANNIHILATOR=-

Люди, Киньте Плз Aircraft.cfg На 737-400

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Собссно сабж. А то вот заменил, и случайно похерил родной, дефолтовый. Скиньте в мыло, дюже прошу annihilator_@ukr.net

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[fltsim.4]

title=Boeing 737-400 Paint4

sim=Boeing737-400

model=

panel=

sound=

texture=4

kb_checklists=Boeing737-400_check

kb_reference=Boeing737-400_ref

atc_id=N737T

atc_airline=World Travel

atc_flight_number=1123

ui_manufacturer=Boeing

ui_type="737-400"

ui_variation="World Travel Airlines"

description="One should hardly be surprised that the world's most prolific manufacturer of commercial aircraft is also the producer of the world's most popular jetliner. The 737 became the best-selling commercial jetliner worldwide when orders for it hit 1,831 in June 1987 (surpassing Boeing's own 727 as the previous champ). However, it wasn't always that way\s in the first few years of production, there were so few orders that Boeing considered canceling the program. They didn't, and the airplane has more than proven itself in over three decades of service."

 

[General]

atc_type=BOEING

atc_model=B734

editable=0

performance="Cruise Speed \n477 kts 550 mph 885 km\/h\n\nEngines \nCFM56-3C1\n\nMaximum Range \n2,059 nm 2,370 mi 3,810 km\n\nService Ceiling \n36, 089 ft 11,000 m\n\nFuel Capacity \n5,311 U.S. gal 20,104 L\n\nEmpty Weight-Standard \n76,180 lb 34,550 kg\n\nMaximum Gross Weight\n150,000 lb 68,039 kg\n\nLength \n120 ft 36.45 m\n\nWingspan \n94 ft, 9 in 25.9 m\n\nHeight \n36.5 ft 11.13 m\n\nSeating \nSeats 147 to 168\n\nCargo Capacity \n1,373 ft3 38.93 m3\n\n"

 

[pitot_static]

vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI

 

[WEIGHT_AND_BALANCE]

max_gross_weight = 150000 // (pounds)

empty_weight = 74170 // (pounds)

 

reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)

empty_weight_CG_position = -5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum

 

max_number_of_stations = 50

 

station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.3 = "1360.0, 25.5, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.4 = "8160.0, 11.0, 0.0, 0.0, Coach 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.5 = "8160.0, -10.0, 0.0, 0.0, Coach 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.6 = "7140.0, -30.5, 0.0, 0.0, Coach 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

 

;Moments of Inertia

empty_weight_pitch_MOI = 3172439

empty_weight_roll_MOI = 2262183

empty_weight_yaw_MOI = 3337024

empty_weight_coupled_MOI = 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 = 1.0

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

Engine.0 = 4.75, -16.1, -4.5 //(feet) longitudinal, lateral, vertical distance from reference datum

Engine.1 = 4.75, 16.1, -4.5 //(feet) longitudinal, lateral, vertical distance from reference datum

fuel_flow_scalar = 1 //Scalar for fuel flow efficiency

min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser

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

 

[TurbineEngineData]

fuel_flow_gain = 0.002 //Gain on fuel flow

inlet_area = 19.6 //Square Feet, engine nacelle inlet area

rated_N2_rpm = 29920 //RPM, second stage compressor rated value

static_thrust = 23500 //Lbs, max rated static thrust at Sea Level

afterburner_available = 0 //Afterburner available?

reverser_available = 1 //Thrust reverser available?

 

[jet_engine]

thrust_scalar = 1.0

 

[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, 40.00, 0.00, -8.40, 1181.1, 0, 1.442, 55.92, 0.6, 2.5, 0.9, 4.0, 4.0, 0, 220.0, 250.0

point.1=1, -7.75, -8.58, -8.60, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0

point.2=1, -7.75, 8.58, -8.60, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.9, 7.1, 7.1, 3, 220.0, 250.0

 

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=0.04 //degrees, pitch when at rest on the ground (+=Up, -=Dn)

static_cg_height=7.67 //feet, altitude of CG when at rest on the ground

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 = 5.0 //Flap angle that activates warning at idle

flap_limit_power = 25.5 //Flap angle that activates warning at above idle

 

[brakes]

parking_brake = 1 //Parking brake available

toe_brakes_scale = 0.885 //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=43.7, -1.31, 3.7 //(feet) longitudinal, lateral, vertical distance from reference datum

 

[flaps.0] //Trailing Edge Flaps

type = 1 // 1 - tail, 2 - lead

span-outboard = 0.8 // 0.0 .. 1.0

extending-time = 20 // seconds

flaps-position.0 = 0 // degrees

flaps-position.1 = 1 // degrees

flaps-position.2 = 2 // degrees

flaps-position.3 = 5 // degrees

flaps-position.4 = 10 // degrees

flaps-position.5 = 15 // degrees

flaps-position.6 = 25 // degrees

flaps-position.7 = 30 // degrees

flaps-position.8 = 40 // degrees

damaging-speed = 250 // KIAS

blowout-speed = 300 // KIAS

lift_scalar = 1.0

drag_scalar = 1.0

pitch_scalar= 1.0

system_type = 1 //Hydraulic

 

[flaps.1] //Inboard Leading Edge Flaps

type = 2 // 1 - tail, 2 - lead

span-outboard = 0.8 // 0.0 .. 1.0

extending-time = 2 // seconds

flaps-position.0 = 0 //

flaps-position.1 = 1.0 //

damaging-speed = 250 // KIAS

blowout-speed = 300 // KIAS

lift_scalar = 1.0

drag_scalar = 1.0

pitch_scalar= 1.0

system_type = 1 //Hydraulic

 

 

[flaps.2] //Outboard Leading Edge Slat

type = 2 // 1 - tail, 2 - lead

span-outboard = 0.8 // 0.0 .. 1.0

extending-time = 3 // seconds

flaps-position.0 = 0 //

flaps-position.1 = 0.5 //

flaps-position.4 = 1.0 //

damaging-speed = 250 // KIAS

blowout-speed = 300 // KIAS

lift_scalar = 1.0

drag_scalar = 1.0

pitch_scalar= 1.0

system_type = 1 //Hydraulic

 

[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

 

[LIGHTS]

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

light.0 = 3, -19.14, -47.24, 1.38, fx_navredm ,

light.1 = 3, -19.14, 47.24, 1.38, fx_navgrem ,

light.2 = 3, -64.32, 0.00, 4.92, fx_navwhih ,

light.3 = 2, -18.22, -47.08, 1.38, fx_strobeh ,

light.4 = 2, -18.22, 47.08, 1.38, fx_strobeh ,

light.5 = 2, -2.65, 0.00, -4.60, fx_beaconb ,

light.6 = 1, 2.20, 0.00, 8.30, fx_beaconh ,

light.7 = 4, 44.41, 0.00, 3.50, fx_vclighth ,

 

[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=0,0

 

[exits]

number_of_exits = 2

exit_rate.0 = 0.4 ;Percent per second

exit_rate.1 = 0.4 ;Percent per second

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_max_rpm = 90

autothrottle_takeoff_ga=1

pitch_takeoff_ga = 8;

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=12.00

nav_integrator_control=0.25

nav_derivative_control=0.00

nav_integrator_boundary=2.50

nav_derivative_boundary=0.00

gs_proportional_control=25.0

gs_integrator_control=0.53

gs_derivative_control=0.00

gs_integrator_boundary=0.70

gs_derivative_boundary=0.00

yaw_damper_gain = 1.0

 

[fuel]

Center1 = 0, 0, 0, 2313, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

LeftMain = -3, -19, 0, 1500, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

RightMain = -3, 19, 0, 1500, 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=0

 

[airplane_geometry]

wing_area = 1137.0 //Square feet

wing_span = 94.75 //Feet

wing_root_chord = 18.0 //Feet

wing_dihedral = 6.2 //Degrees

wing_incidence = 1.0 //Degrees

wing_twist = -0.5 //Degrees

oswald_efficiency_factor= 0.75 //Measure of lift effeciency of wing

wing_winglets_flag = 0 //Are winglets available?

wing_sweep = 25.0 //Degrees, wing leading edge

wing_pos_apex_lon = 8.0 //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 = 338.0 //Square feet

htail_span = 41.7 //Feet

htail_pos_lon = -35.0 //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 = 0.0 //Degrees

htail_sweep = 30.0 //Degrees, horizontal tail leading edge

vtail_area = 224.0 //Square feet

vtail_span = 20.0 //Feet, tip to body

vtail_sweep = 35.0 //Degrees, vertical tail leading edge

vtail_pos_lon = -35.8 //Feet, longitudinal distance from reference point, negative going aft

vtail_pos_vert = 5.8 //Feet, vertical distance from reference point, positive going up

elevator_area = 70.5 //Square feet

aileron_area = 26.9 //Square feet

rudder_area = 56.2 //Square feet

elevator_up_limit = 22.5 //Degrees

elevator_down_limit = 19.5 //Degrees

aileron_up_limit = 20.0 //Degrees

aileron_down_limit = 20.0 //Degrees

rudder_limit = 26.0 //Degrees

elevator_trim_limit = 20.0 //Degrees

spoiler_limit = 60.0 //Degrees

spoilerons_available = 1 //Spoilerons Available?

aileron_to_spoileron_gain = 3 //Aileron to spoileron gain

min_ailerons_for_spoilerons = 10 //Degrees

min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate

 

[Reference Speeds]

flaps_up_stall_speed = 142.0 //Knots True (KTAS)

full_flaps_stall_speed = 113.0 //Knots True (KTAS)

cruise_speed = 477.0 //Knots True (KTAS)

max_mach = 0.82

max_indicated_speed = 340 //Red line (KIAS)

 

[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

 

[stall_warning]

type=2

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Более чем пренадглобально благодарствую.

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