[fltsim.0] title=Boeing 747-400 sim=Boeing747-400 model= panel= sound= texture= kb_checklists=Boeing747-400_check kb_reference=Boeing747-400_ref atc_id=N747 atc_airline=Global Freightways atc_flight_number=1489AD atc_heavy=1 atc_parking_types=CARGO ui_manufacturer=Boeing ui_type="747-400" ui_variation="Da Vinci" description="Da Vinci Code, right ? Fly it and spot Tom Hanks face turning negative when the sunlight shines on it and negative again when the light shines away from it. So much for the Da Vinci code... this effect is much more impressive, I think !! As for the B747-400, more than 30 years ago, the 747 made its first trip from New York to London. Since then, it's become the standard by which other large passenger jets are judged. Its size, range, speed and capacity were then, and are now, the best in its class." [General] atc_type=BOEING atc_model=B744 editable=0 performance="Cruise Speed\n0.85 Mach 565 mph 910 km\/h\n\nEngine options\nPratt & Whitney PW4062\nRolls-Royce RB211-524H\nGeneral Electric CF6-80C2B5F\n\nMaximum Range\n7,325 nm 13,570 km\n\nMaximum Certified Operating Altitude 45,100 ft 13,747 m\n\nFuel Capacity\n57,285 gal 216,840 L\n\nBasic Empty Weight\n394,088 lb 178,755 kg\n\nMax Gross Weight 875,000 lb 396,893 kg\n\nLength\n231 ft, 10 in 70.6 m\n\nWingspan\n211 ft, 5 in 64.4 m\n\nHeight\n63 ft, 8 in 19.4 m\n\nSeating Typical 3-class configuration - 416\nTypical 2-class configuration - 524" [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 = 875000 // (pounds) empty_weight = 394088 // (pounds) reference_datum_position = 83.5, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -90.5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "170.0, -19.0, -2.0, 8.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "170.0, -19.0, 2.0, 8.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "1700.0, -83.5, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "5440.0, -27.0, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "5780.0, -65.0, 0.0, 0.0, Business Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = "7140.0, -50.0, 0.0, 8.0, Upper Deck" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "10710.0, -91.0, 0.0, 0.0, Coach 1-7" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = "18020.0, -119.0, 0.0, 0.0, Coach 8-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8 = "23800.0, -160.0, 0.0, 0.0, Coach 19-34" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.9 = "18000.0, -52.0, 0.0, -6.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.10 = "6000.0, -123.0, 0.0, -6.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_roll_MOI = 13352310 empty_weight_pitch_MOI = 24223159 empty_weight_yaw_MOI = 39531785 empty_weight_coupled_MOI = 0 [fuel] LeftMain = -96.0, -28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -96.0, 28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux = -112.0, -36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux = -112.0, 36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftTip = -130.0, -73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightTip = -130.0, 73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center1 = -83.5, 0.0, -7.0, 17164.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2 = -193.5, 0.0, 6.0, 3300.0, 0.0 //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 = 5825.0 //Square feet wing_span = 211.4 //Feet wing_root_chord = 48.8 //Feet wing_dihedral = 7.0 //Degrees wing_incidence = 2.0 //Degrees wing_twist = -1.0 //Degrees oswald_efficiency_factor= 0.68 //Measure of lift effeciency of wing wing_winglets_flag = 1 //Are winglets available? wing_sweep = 37.5 //Degrees, wing leading edge wing_pos_apex_lon = -58.2 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 0 //Feet, vertical distance from reference point, positive going up htail_area = 1470 //Square feet htail_span = 72.8 //Feet htail_pos_lon = -210.0 //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 = 37.5 //Degrees, horizontal tail leading edge vtail_area = 1060 //Square feet vtail_span = 37.1 //Feet, tip to body vtail_sweep = 45.0 //Degrees, vertical tail leading edge vtail_pos_lon = -198.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 26.1 //Feet, vertical distance from reference point, positive going up elevator_area = 327 //Square feet aileron_area = 225 //Square feet rudder_area = 230 //Square feet elevator_up_limit = 25 //Degrees elevator_down_limit = 15 //Degrees aileron_up_limit = 25 //Degrees aileron_down_limit = 15 //Degrees rudder_limit = 31.5 //Degrees elevator_trim_limit = 20 //Degrees spoiler_limit = 45 //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 = 140.0 //Knots True (KTAS) full_flaps_stall_speed = 112.0 //Knots True (KTAS) cruise_speed = 505.0 //Knots True (KTAS) max_mach = 0.92 max_indicated_speed = 365.0 //Red line (KIAS) [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 25 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 1 // degrees flaps-position.2 = 5 // degrees flaps-position.3 = 10 // degrees flaps-position.4 = 20 // degrees flaps-position.5 = 25 // degrees flaps-position.6 = 30 // degrees damaging-speed = 200 // KIAS blowout-speed = 250 // KIAS lift_scalar = 0.7 drag_scalar = 0.9 pitch_scalar= 0.9 system_type = 1 //Hydraulic [flaps.1] type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 2 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 1.0 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.3 drag_scalar = 0.1 pitch_scalar= 0.1 system_type = 1 //Hydraulic [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 = -107.5, -69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -76.0, -38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.2 = -76.0, 38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.3 = -107.5, 69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency min_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser [TurbineEngineData] fuel_flow_gain = 0.002 //Gain on fuel flow inlet_area = 60.0 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 56750 //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 [autopilot] autopilot_available = 1 flight_director_available = 1 default_vertical_speed = 1800.0 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=16.00 nav_integrator_control=0.17 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control = 18.0 gs_integrator_control = 0.33 gs_derivative_control = 0.00 gs_integrator_boundary = 0.70 gs_derivative_boundary = 0.00 yaw_damper_gain = 1.0 [contact_points] //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) point.0 = 1, -25.0, 0.0, -17.5, 1000.0, 0, 2.0, 70.0, 0.5, 3.5, 0.900, 9.0, 8.0, 0, 220, 250 point.1 = 1, -114.0, -18.0, -21.3, 2000.0, 1, 2.0, 13.0, 3.0, 2.5, 0.900, 11.0, 9.0, 2, 220, 250 point.2 = 1, -114.0, 18.0, -21.3, 2000.0, 2, 2.0, 13.0, 3.0, 2.5, 0.900, 11.0, 9.0, 3, 220, 250 point.3 = 2, -152.6, -103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0 point.4 = 2, -152.6, 103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0 point.5 = 2, 3.0, 0.0, 0.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0 point.6 = 2, -222.7, 0.0, 4.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 static_pitch = -1.5 static_cg_height = 18.6 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 = 1.24 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,1,1 //pumps on Eng1,2,3,4 [Views] eyepoint = -19.05, -1.97, 9.7 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 5 , 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 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 [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, -150.30, -102.56, 3.22, fx_navredh , light.1 = 3, -150.30, 102.56, 3.22, fx_navgreh , light.2 = 3, -223.85, 0.00, 8.85, fx_navwhih , light.3 = 2, -150.30, -102.56, 3.22, fx_strobeh , light.4 = 2, -150.30, 102.56, 3.22, fx_strobeh , light.5 = 2, -228.97, 0.00, 44.62, fx_strobeh , light.6 = 1, -45.05, 0.00, 14.65, fx_beaconh , light.7 = 1, -80.22, 0.00, -12.05, fx_beaconb , light.8 = 4, -16.24, 0.00, 9.19, fx_vclighth, [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 = 2 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;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 [stall_warning] type=2