[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