[fltsim.0]
title=Boeing 737-400 Paint4
sim=Boeing737-400
model=
panel=
sound=
texture=AEROPERU
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=N737T
atc_airline=Aeroperu
atc_flight_number=1123
ui_manufacturer=Boeing
ui_type="737-400"
ui_variation=Aeroperu
description="No debería sorprender a nadie que el mayor fabricante mundial de aviones comerciales sea también el productor del reactor de línea aérea más popular. El 737 se convirtió en el reactor comercial más vendido cuando los pedidos llegaron a las 1831 unidades, en junio de 1987 (superando al anterior campeón, el 727, también de Boeing). Sin embargo, no siempre fue así, durante los primeros años de producción Boeing recibió tan pocos pedidos llegó a considerar la cancelación del programa. No lo hicieron, y el avión ha demostrado su valía durante más de tres décadas de servicio."
[General]
atc_type=BOEING
atc_model=B734
editable=0
performance="Velocidad de crucero \n477 nudos 550 mph 885 km\/h\n\nMotores \nCFM56-3C1\n\nAlcance máximo \n2059 mn 2370 mi 3810 km\n\nTecho de servicio \n36089 pies 11000 m\n\nCapacidad de combustible \n5311 galones de EE.UU. 20104 L\n\nPeso en vacío (estándar) \n76180 lb 34550 kg\n\nPeso bruto máximo\n150000 lb 68039 kg\n\nLargo \n120 pies 36,45 m\n\nEnvergadura \n94 pies, 9 pda 25,9 m\n\nAlto \n36,5 pies 11,13 m\n\nPlazas \nAsientos entre 147 y 168\n\nCapacidad de carga \n1373 pies3 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, Piloto" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170.0, 41.0, 1.5, 0.0, Copiloto" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "510.0, 0.0, 0.0, 0.0, Tripulación" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "1360.0, 25.5, 0.0, 0.0, Primera clase" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "8160.0, 11.0, 0.0, 0.0, Turista 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "8160.0, -10.0, 0.0, 0.0, Turista 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "7140.0, -30.5, 0.0, 0.0, Turista 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "10000.0, 20.5, 0.0, 0.0, Equipaje anterior" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "4000.0, -27.5, 0.0, 0.0, Equipaje posterior" //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
