[fltsim.0]
title=Boeing 737-300 Conviasa YV2556
sim=Boeing737-400
model=
panel=
sound=
texture=
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=
atc_airline=Conviasa
atc_flight_number=2105
ui_manufacturer=Boeing
ui_type=737-300
ui_variation=Conviasa
description=Boeing 737-300 Conviasa YV2556
[General]
atc_type=boeing 737-300
atc_model=boeing
editable=1
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 Takeoff Weight\n138,500 lb 62,800 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
Category=airplane
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[WEIGHT_AND_BALANCE]
max_gross_weight = 134500
empty_weight = 72360
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 3.280, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0=0.000000,0.000000,0.000000,0.000000
station_load.1 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.2 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.3 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.4 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
;Moments of Inertia
empty_weight_pitch_MOI= 3172439
//3172439
empty_weight_roll_MOI= 2262183
empty_weight_yaw_MOI= 3337024
empty_weight_coupled_MOI = 0
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar=0.70
parasite_drag_scalar=0.20
induced_drag_scalar=1.10
ELEVATOR_EFFECTIVENESS=3.0 // ADJUST THIS VALUE TO MEET PITCHCRITERIA
AILERON_EFFECTIVENESS=3.0 // ADJUST THIS VALUE TO MEET ROLLCRITERIA
rudder_effectiveness=1.0
pitch_stability=2.0
roll_stability=1.5
yaw_stability=0.7
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, -2.5 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=4.75, 16.1, -2.5 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.59 //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000
//Based on APB TARGET SPDS, ALT, N1, EGT, N2 and FF_FU
//into consideration, the 327 setting for fuel flow produces accurate
//FF at FL310 but WRONG fuel burn/hr therefore FF data is suspect
[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=22000 //Lbs, max rated static thrust at Sea Level
afterburner_available=0 //Afterburner available?
reverser_available=1 //Thrust reverser available?
[jet_engine]
thrust_scalar =0.87
[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, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 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= 1.000, 31.729, 0.735, -8.800, 1181.100, 0.000, 1.070, 35.920, 0.800, 2.500, 0.900, 7.000, 7.000, 0.000, 0.000, 0.000
point.1= 1.000, 31.729, -0.735, -8.800, 1181.100, 0.000, 1.070, 35.920, 0.800, 2.500, 0.900, 7.000, 7.000, 0.000, 0.000, 0.000
point.2= 1.000, -7.933, -9.970, -9.800, 1574.800, 1.000, 1.640, 0.200, 1.000, 2.500, 0.900, 8.000, 8.000, 2.000, 0.000, 0.000
point.3= 1.000, -7.933, 7.864, -9.800, 1574.800, 2.000, 1.640, 0.200, 1.000, 2.500, 0.900, 8.000, 8.000, 3.000, 0.000, 0.000
point.4= 1.000, -7.933, -7.864, -9.800, 1574.800, 1.000, 1.640, 0.200, 1.000, 2.500, 0.900, 8.000, 8.000, 3.000, 0.000, 0.000
point.5= 1.000, -7.933, 9.970, -9.800, 1574.800, 2.000, 1.640, 0.200, 1.000, 2.500, 0.900, 8.000, 8.000, 3.000, 0.000, 0.000
point.6= 2.000, 46.187, 0.000, 1.634, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, -53.635, 0.000, 7.877, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.8= 2.000, 46.545, 0.000, 4.137, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
max_number_of_points=21
static_pitch=0.62 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.66 //feet, altitude of CG when at rest on the ground
gear_system_type=0
[Views]
eyepoint=38.5461192,-1.509168,5.8988784
[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=.577
drag_scalar=2.730
pitch_scalar=6.333
system_type=1 // Hydraulic
[flaps.1] // Inboard Leading Edge Flaps 15 adjustment
type=2 // 1 - tail, 2 - lead
span-outboard=0.8 // 0.0 .. 1.0
extending-time=5.0 // seconds
flaps-position.0=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 Flaps 30 adjustment
type=2 // 1 - tail, 2 - lead
span-outboard=0.8 // 0.0 .. 1.0
extending-time=6.0 // seconds
flaps-position.0=0.0 //
flaps-position.1=0.5 //
flaps-position.4=1.0 //
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS
lift_scalar= 1.00.770
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
// Com.2=1
Nav.1=1
Nav.2=1
Adf.1=1
Transponder.1=1
Marker.1=1
[LIGHTS]
light.0 =3, -8.54, -49.74, 1.90, fx_navred ,
light.1 =3, -8.54, 49.74, 1.90, fx_navgre ,
light.2 =3, -8.94, -49.74, 1.90, fx_navred ,
light.3 =3, -8.94, 49.74, 1.90, fx_navgre ,
light.4 =3, -53.12, 0.00, 6.30, fx_navwhih ,
light.5 =2, -10.14, -49.84, 1.90, fx_strobe ,
light.6 =2, -10.14, 49.84, 1.90, fx_strobe ,
light.7 =1, 2.20, 0.00, 10.30, fx_beaconh ,
light.8 =3, -13.60, -49.22, 1.90, fx_navwhi ,
light.9 =3, -13.60, 49.22, 1.90, fx_navwhi ,
[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
[exits]
number_of_exits = 3
exit_rate.0 = 0.10 ;Percent per second
exit_rate.1 = 0.12 ;Percent per second
exit_rate.2 = 0.12 ;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=800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
use_no_default_pitch=1
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=12.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=25.0000
gs_integrator_control=0.53
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=1.000000
[fuel]
Center1 = 6.562, 0, 0, 2313.000, 0 //source Boeing Tank Capacity Manual page 15.20.04 / Nov 13/91 // Modified
LeftMain = 3.562, -19.000, 0.000, 1499.000, 0.000 //source Boeing Tank Capacity Manual page 15.20.04 / Nov 13/91 // Modified
RightMain = 3.562, 19.000, 0.000, 1499.000, 0.000 //source Boeing Tank Capacity Manual page 15.20.04 / Nov 13/91 // Modified
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2 // Modified
electric_pump=0
//Note: Number of tank selectors is used at 2 for
//the TCAS II and ADV panels from Ariane.
//If you use anyone else's panels, please consult their docs
//Ariane TCAS II Series correctly 'scavenges' from the Center Tank
//to the #1 tank accurately so 'tank balancing' is necessary.
[CameraDefinition.0]
Title = "Right Wing"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Right Wing Engine View
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .50
ShowWeather = Yes
InitialXyz = 1, 1, 5
InitialPbh = 0, 0, 120
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Left Wing"
Guid = {0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description = View of the left wing Engine from the passenger cabin
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -1, 1, 5
InitialPbh = 0, 0, 240
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Right rear Wing"
Guid = {54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC}
Description = View of the rear right wing from the passenger cabin
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 1, 1, -3
InitialPbh = 0, 0, 80
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[CameraDefinition.3]
Title = "Left Rear Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = Left rear wing view
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .50
ShowWeather = Yes
InitialXyz = -1, 1, -3
InitialPbh = 0, 0, 280
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.4]
Title = "Landing Gear"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = Landing gear
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .50
ShowWeather = Yes
InitialXyz = 0, -2, -7
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[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=0
[airplane_geometry]
wing_area = 1135.000 // Modified
wing_span = 94.900 // Modified
wing_root_chord = 15.500 // Modified
wing_dihedral = 6.200
wing_incidence = 1.000
wing_twist = -0.500
oswald_efficiency_factor= 0.800820
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 8.000
wing_pos_apex_vert = 0.000
htail_area = 338.000
htail_span = 41.700
htail_pos_lon = -52.162
htail_pos_vert = 5.577
htail_incidence = 0.000
htail_sweep = 30.000
vtail_area = 249.000
vtail_span = 20.000
vtail_sweep = 35.000
vtail_pos_lon = -48.133
vtail_pos_vert = 9.843
elevator_area = 70.500
aileron_area = 26.900
rudder_area = 56.200
elevator_up_limit = 22.500
elevator_down_limit = 19.500
aileron_up_limit = 20.000
aileron_down_limit = 20.000
rudder_limit = 26.000
elevator_trim_limit = 20.000
spoiler_limit = 60.000
spoilerons_available = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 7.700
min_flaps_for_spoilerons = 0.000
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
//CAUTION! Below speeds are based on CANNED flap speeds and not "speed card"
//the aircraft is designed to fly within the required envelope for these
//in conditions such as a rudder "hard-over".
//Gross weight is a factor and is weighed at less than 117,000.
//There are a number of exceptions where you might go slower than these //speeds.
[Reference Speeds]
flaps_up_stall_speed=156.0 //Knots True (KTAS)
full_flaps_stall_speed=110.0 //Knots True (KTAS)
cruise_speed=477.0 //Knots True (KTAS)
max_indicated_speed=340.000000
max_mach=0.820020
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.12,0.11 ;Percent per second
[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
[brakes]
toe_brakes_scale=0.885037
parking_brake=1
auto_brakes=4
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[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=1
[turn_indicators]
turn_indicator.0=1,0
[SMOKESYSTEM]
smoke.0=-2.50,0.25,-16.1, fx_smoke_rx // Modified
smoke.1=-2.50,0.25,16.1, fx_smoke_rx // Modified
//The CFM engines do not smoke; characteristicly,
//but it adds an added dimension in the effect on approach
//and was a requested addition by a number of customers
[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
[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=0
