[fltsim.0] sim=PSSB773ER-GE // <---dont 4get to do this too model=vc panel=01 [General] visual_damage=1 // 0=off, 1=on atc_type=BOEING atc_model=B773 editable=0 performance=Cruise Speed\tMach .84\nMaximum Range\t5,720 nm\nService Ceiling\t35,000 ft\nMax Takeoff Weight\t660,000 lb\nSeating\t\t336 to 550\nCargo Capacity\t20 standard LD3 containers \n [WEIGHT_AND_BALANCE] max_gross_weight=775000 // (pounds) empty_weight=370000 // (pounds) reference_datum_position = 10.0, 0.0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-12.0, 0.0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0 = "170.0, 86.0, -2.0, 0.0, Pilot" //Weight (lbs), station_load.1 = "170.0, 86.0, 2.0, 0.0, Co-Pilot" //Weight (lbs), station_load.2 = "850.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), station_load.3 = "1920.0, 72.0, 0.0, 0.0, First Class" //Weight (lbs), station_load.4 ="14400.0, 31.0, 0.0, 0.0, Coach 1-9" //Weight (lbs), station_load.5 ="24000.0, -10.0, 0.0, 0.0, Coach 10-25" //Weight (lbs), station_load.6 ="22400.0, -52.5, 0.0, 0.0, Coach 26-40" //Weight (lbs), station_load.6 ="22400.0, -72.5, 0.0, 0.0, Coach 41-55" //Weight (lbs), station_load.7 = "2000.0, 47.0, 0.0, -6.0, Forward Cargo" //Weight (lbs), station_load.8 = "500.0, -67.0, 0.0, -6.0, Aft Cargo" //Weight (lbs), ;Moments of Inertia empty_weight_pitch_MOI=17221604 empty_weight_roll_MOI =7605379 empty_weight_yaw_MOI =18335985 empty_weight_coupled_MOI=0.0 [flight_tuning] cruise_lift_scalar=1.5 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=10.5, -32.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=10.5, 32.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0401 //Scalar for fuel flow efficiency min_throttle_limit=-0.25 [TurbineEngineData] fuel_flow_gain=0.0010 //Gain on fuel flow inlet_area=113.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=11292 //RPM, second stage compressor rated value static_thrust=115300 //GE90-115B 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] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1,1 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 2, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 //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, 90.42, 0.00, -19.55, 1181.1, 0, 4.521, 70.0, 1.23, 2.0, 0.7235, 9.5, 9.7, 0, 260.0, 270.0 point.1=1, -18.50, -17.80, -20.70, 1574.8, 1, 4.521, 0.0, 1.91, 1.85, 0.7470, 11.0, 11.0, 2, 255.0, 278.0 point.2=1, -18.50, 17.80, -20.70, 1574.8, 2, 4.521, 0.0, 1.91, 1.85, 0.7470, 10.0, 10.0, 3, 255.0, 278.0 point.3=2, -10.17, -47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -10.17, 47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -83.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch=-0.45 static_cg_height=19.30 gear_system_type=0 [Views] eyepoint = 103.1, -2.19, 2.15 [Flaps.0] //Inboard Krueger type= 2 span-outboard= 0.100 extending-time= 15.000 system_type= 1 damaging-speed= 270.000 blowout-speed= 275.000 lift_scalar= 0.0 drag_scalar= 0.0000 pitch_scalar= 0.0 flaps-position.0= 0.000, 0.000 flaps-position.1= 30.000, 265.000 [Flaps.1] //Slat type= 2 span-outboard= 0.800 extending-time= 15.000 system_type= 1 damaging-speed= 270.000 blowout-speed= 275.000 lift_scalar= 0.02100 drag_scalar= 0.300 pitch_scalar= 0.00 flaps-position.0= 0.000, 0.000 flaps-position.1= 15.500, 265.000 flaps-position.2= 15.500, 245.000 flaps-position.3= 15.500, 230.000 flaps-position.4= 15.500, 225.000 flaps-position.5= 30.000, 200.000 flaps-position.6= 30.000, 180.000 [Flaps.2] //Inboard Flap type= 1 span-outboard= 0.200 extending-time= 25.000 system_type= 1 damaging-speed= 270.000 blowout-speed= 275.000 lift_scalar= 0.4750 drag_scalar= 0.250 pitch_scalar= 0.00 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.1000, 265.000 flaps-position.2= 5.000, 245.000 flaps-position.3= 15.000, 230.000 flaps-position.4= 20.000, 225.000 flaps-position.5= 25.000, 200.000 flaps-position.6= 30.000, 180.000 [Flaps.3] //Outboard Flap type= 1 span-outboard= 0.600 extending-time= 25.000 system_type= 1 damaging-speed= 270.000 blowout-speed= 275.000 lift_scalar= 0.4750 drag_scalar= 0.300 pitch_scalar= 0.00 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.10, 265.000 flaps-position.2= 5.000, 245.000 flaps-position.3= 15.000, 230.000 flaps-position.4= 20.000, 225.000 flaps-position.5= 25.000, 200.000 flaps-position.6= 30.000, 180.000 [Radios] Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 1 Adf.1=1,1 Adf.2=1,1 Transponder.1=1 Marker.1=1 [keyboard_response] elevator=150, 250 aileron=150, 250 rudder=150, 250 [direction_indicators] direction_indicator.0=3,0 [LIGHTS] light.1 = 2, -127.10, 0.00, 5.30, fx_shockwave_strobe_l_2 , light.2 = 1, -1.70, -0.01, -11.65, fx_shockwave_beaconb , light.3 = 1, 68.90, -0.01, 9.95, fx_shockwave_beaconh , light.4 = 3, -126.80, 0.00, 1.30, fx_shockwave_navwhi_l_nl , light.5 = 4, 104, 0, 3.4, fx_shockwave_vclight_l light.6 = 5, 23.80, 12.36, -5.0, fx_shockwave_landing_light_narrow, light.7 = 5, 23.80, -12.36, -5.0, fx_shockwave_landing_light_narrow , light.8 = 6, 94.00, 0, -10.90, fx_shockwave_landing_light_double_small, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 startup = fx_pss_startup windshield_rain_effect_available = 1 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [fuel] Center1 = 0.0, 0.0, -4.0, 20550, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -6.0, -30.0, 0.0, 9300.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -6.0, 30.0, 0.0, 9300.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux = -9, -49, 0.0, 4370, 0 RightAux = -9, 49, 0.0, 4370, 0 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 4 electric_pump=1 [airplane_geometry] wing_area=4605.0 //Square feet wing_span=199.92 //Feet wing_root_chord=23.0 //Feet wing_dihedral=6.2 //Degrees wing_incidence=1.0 //Degrees wing_twist=-0.5 //Degrees oswald_efficiency_factor=0.86367 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=32.0 //Degrees, wing leading edge wing_pos_apex_lon=26.1 //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=1090.0 //Square feet htail_span=70.7 //Feet htail_pos_lon=-84.0 //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=40.0 //Degrees, horizontal tail leading edge vtail_area=573.0 //Square feet vtail_span=27.3 //Feet, tip to body vtail_sweep=35.0 //Degrees, vertical tail leading edge vtail_pos_lon=-93.3 //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=137.0 //Square feet aileron_area=68.0 //Square feet rudder_area=232.0 //Square feet elevator_up_limit=30.0 //Degrees elevator_down_limit=30.0 //Degrees aileron_up_limit=30.0 //Degrees aileron_down_limit=15.0 //Degrees rudder_limit=25.0 //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=150.0 //Knots True (KTAS) full_flaps_stall_speed=120.0 //Knots True (KTAS) cruise_speed=482.0 //Knots True (KTAS) max_mach = 0.90 max_indicated_speed = 330 //Red line (KIAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required= 1 autothrottle_max_rpm = 108.5 autothrottle_takeoff_ga= 1 pitch_takeoff_ga=8 ; max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=0.7 max_pitch_velocity_hi_alt=0.4 max_pitch_velocity_lo_alt_breakpoint=11000.0 max_pitch_velocity_hi_alt_breakpoint=25000.0 max_bank=25.0 max_bank_acceleration=1.4 max_bank_velocity=2.8 max_throttle_rate=0.08 nav_proportional_control=11.00 nav_integrator_control=0.17 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=19.0 gs_integrator_control=0.530 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [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=0.7 parking_brake=1 differential_braking_scale = 1.0 [gear_warning_system] gear_warning_available = 0 //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 [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 1 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [stall_warning] type=2 [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=1,0 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 ;Percent per second [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0.0