[fltsim.8] title=737 VARIG sim=Boeing737-400 model= panel= sound= texture=8 kb_checklists=Boeing737-400_check kb_reference=Boeing737-400_ref atc_id=PTDLB atc_airline=VARIG atc_flight_number= ui_manufacturer=Boeing ui_type=737-400 visual_damage=1 ui_variation=VARIG description=Boeing 737-400 da VARIG do Brasil.\nProduzido, pintado e testado pelo Cmte. MARCOS KONDE (PT-MAV) (V-717).\nDa família mais próspera de aviões a jato já construída, este é o 737-400.\nSe você gosta de voos curtos ou vôos domésticos mais longos, \no 737-400 é um avião versátil e eficiente. atc_heavy=0 [General] atc_type=BOEING AIRCRAFT atc_model=B734 editable=0 performance=Velocidade de Cruzeiro \n477 kts 550 mph 885 km\/h\n\nMotores \nCFM56-3C1\n\nAlcance Máximo \n2,059 nm 2,370 mi 3,810 km\n\nAltitude máx. de voo \n36, 089 ft 11,000 m\n\nCapacidade de Combustível \n5,311 U.S. gal 20,104 L\n\nPeso Vazio \n76,180 lb 34,550 kg\n\nPeso Máximo Cheio\n138,500 lb 62,800 kg\n\nComprimento \n120 ft 36.45 m\n\nExtensão das asas \n94 ft, 9 in 25.9 m\n\nAltura \n36.5 ft 11.13 m\n\nLugares(passageiros) \nAssentos 147 to 168\n\nCapacidade de carga \n1,373 ft3 38.93 m3\n\n [SMOKESYSTEM] smoke.1=-18.00,-10.00,16.00, fx_smoke_w.fx smoke.2=-18.00,-10.00,-16.00, fx_smoke_w.fx [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 = 138500.000 empty_weight = 100792.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 max_number_of_stations =50 station_load.0 =0.000000,0.000000,0.000000,0.000000 ;Moments of Inertia empty_weight_pitch_MOI = 3172439.000 empty_weight_roll_MOI = 2262183.000 empty_weight_yaw_MOI = 3337024.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [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 Engine.0 = 4.750, -16.100, -2.500 Engine.1 = 4.750, 16.100, -2.500 fuel_flow_scalar = 1.000 [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 19.600 rated_N2_rpm = 29920.000 static_thrust = 23500.000 afterburner_available = 0 reverser_available = 1 [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, 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, 40.000, 0.000, -8.100, 1181.100, 0.000, 1.442, 55.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000 point.1= 1.000, -7.750, -8.580, -8.680, 1574.800, 1.000, 1.442, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000 point.2= 1.000, -7.750, 8.580, -8.680, 1574.800, 2.000, 1.442, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000 point.3= 2.000, -14.170, -47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -14.170, 47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -54.000, 0.000, 2.830, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points = 21 static_pitch= 0.620 static_cg_height= 7.660 [Views] eyepoint=43.7, -1.31, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum [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=1, 44.81, 0.00, 3.40, fx_vclighth , light.8=4, 45.34, -1.30, 3.39, fx_vcfloodltm , light.9=4, 45.34, 1.30, 3.39, fx_vcfloodltm , [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 = 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] use_no_default_bank=1 autoland_available=0 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; [fuel] Center1 = 0.000, 0.000, 0.000, 2313.000, 0.000 LeftMain = -3.000, -19.000, 0.000, 1500.000, 0.000 RightMain = -3.000, 19.000, 0.000, 1500.000, 0.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 [airplane_geometry] wing_area = 1137.000 wing_span = 94.750 wing_root_chord = 18.000 wing_dihedral = 6.200 wing_incidence = 1.000 wing_twist = -0.500 oswald_efficiency_factor= 0.750 wing_winglets_flag = 0 wing_sweep = 25.000 wing_pos_apex_lon = 8.000 wing_pos_apex_vert = 0.000 htail_area = 338.000 htail_span = 41.700 htail_pos_lon = -35.000 htail_pos_vert = 0.000 htail_incidence = 0.000 htail_sweep = 30.000 vtail_area = 224.000 vtail_span = 20.000 vtail_sweep = 35.000 vtail_pos_lon = -35.800 vtail_pos_vert = 5.800 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 = 10.000 min_flaps_for_spoilerons = 0.000 [Reference Speeds] flaps_up_stall_speed = 142.000 full_flaps_stall_speed = 113.000 cruise_speed = 477.000 [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 [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 20.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 2.000, 0.000 flaps-position.3= 5.000, 0.000 flaps-position.4= 10.000, 0.000 flaps-position.5= 15.000, 0.000 flaps-position.6= 25.000, 0.000 flaps-position.7= 30.000, 0.000 flaps-position.8= 40.000, 0.000 [Flaps.1] type= 2 span-outboard= 0.800 extending-time= 2.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 [Flaps.2] type= 2 span-outboard= 0.800 extending-time= 3.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.500, 0.000 flaps-position.2= 1.000, 0.000