[fltsim.0] title=HSST AI TRAFFIC CLI sim=hsst-ai-traffic model=hsst-ai-traffic panel= sound= texture=CLI atc_id= atc_airline=CALIFORNIAN atc_flight_number= atc_heavy=1 ui_manufacturer=HSST ui_type=HSST-500 ui_variation=Californian Airlines HSST For AI Traffic description=HSST-500 - ! AI Traffic Version !\n\nBy UranusJay - Jan Martin\nhttp:\/\/www.geocities.com\/uranusjay\/\nuranusjay03@gmx.net\n\n! Not For Commercial Use ! visual_damage=0 atc_parking_types=GATE atc_parking_codes=CLI,USDM,NARG [General] atc_type=SUPER_CRUISER atc_model=H500 editable=1 performance= // Do not remove or edit this section. // This section is for PAI Installer information and will not interfere with aircraft behaviour [Project AI] Version=5acof // FDE Revision by Jan Martin // // End of Project AI specific settings [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -194.00, -103.25, 5.75, fx_navredm , light.1=3, -194.10, -103.35, 5.75, fx_navredh , light.2=2, -197.00, -103.00, 5.35, fx_strobeh , light.3=3, -193.00, 103.25, 5.75, fx_navgrem , light.4=3, -193.10, 103.35, 5.75, fx_navgreh , light.5=2, -197.00, 103.00, 5.35, fx_strobeh , light.6=1, -96.65, 0.00, 15.55, fx_beaconh , light.7=1, -109.30, 0.00, -6.30, fx_beaconh , light.8=2, -227.00, 0.00, 37.50, fx_strobeh , light.9=2, -243.10, 0.00, 10.00, fx_strobeh , [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=-183.0, -33.5, -7.4 Engine.1=-183.0, 33.5, -7.4 fuel_flow_scalar=0.3000 min_throttle_limit=-0.05 max_contrail_temperature=-30.0 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=11.0 rated_N2_rpm=29920 static_thrust=180000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=160 full_flaps_stall_speed=130 cruise_speed=1150 max_indicated_speed=590 max_mach=2.430000 [WEIGHT_AND_BALANCE] max_gross_weight=630000 // (pounds) empty_weight=395000 // (pounds) reference_datum_position=115.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-115, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 ;Moments of Inertia empty_weight_pitch_MOI=18000000 empty_weight_roll_MOI=5500000 empty_weight_yaw_MOI=16300000 empty_weight_coupled_MOI=0.0 [contact_points] point.0=1, -65.0, 0.0, -17.60, 2000.0, 0, 2.0, 60.0, 0.8, 2.5, 0.300, 8.0, 8.0, 0, 220, 250 point.1=1, -154.0, -19.0, -18.75, 2000.0, 1, 2.0, 0.0, 0.8, 2.5, 0.300, 11.0, 11.0, 2, 220, 250 point.2=1, -154.0, 19.0, -18.75, 2000.0, 2, 2.0, 0.0, 0.8, 2.5, 0.300, 11.0, 11.0, 3, 220, 250 point.3=2, -14.17, -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, -14.17, 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=0.10 static_cg_height=17.56 gear_system_type=1 //Hydraulic [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 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, 5 , 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 2 , 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 [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=1.0 //Brake scalar [hydraulic_system] normal_pressure=3000.0 //PSI electric_pumps=0 //no electric pumps engine_map=1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=90.0, -2.65, 8.89 [flaps.0] //Inboard Trailing Edge type=1 // 1 - tail, 2 - lead span-outboard=0.2 // 0.0 .. 1.0 extending-time=25 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=5 // degrees flaps-position.3=15 // degrees flaps-position.4=20 // degrees flaps-position.5=25 // degrees flaps-position.6=30 // degrees damaging-speed=260 // KIAS blowout-speed=300 // KIAS lift_scalar=0.55 drag_scalar=0.55 pitch_scalar=0.55 system_type=1 //Hydraulic [flaps.1] //Outboard Trailing Edge type=1 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=23 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=5 // degrees flaps-position.3=15 // degrees flaps-position.4=20 // degrees flaps-position.5=25 // degrees flaps-position.6=30 // degrees damaging-speed=260 // KIAS blowout-speed=300 // KIAS lift_scalar=0.35 drag_scalar=0.35 pitch_scalar=0.35 system_type=1 //Hydraulic [flaps.2] //Inboard Leading Edge Slats type=2 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=4 // seconds flaps-position.0=0 // degrees flaps-position.1=0.5 // degrees flaps-position.2=0.5 // degrees flaps-position.3=0.5 // degrees flaps-position.4=0.5 // degrees flaps-position.5=1.0 // degrees flaps-position.6=1.0 // degrees damaging-speed=260 // KIAS blowout-speed=300 // KIAS lift_scalar=0.05 drag_scalar=0.05 pitch_scalar=0.05 system_type=1 //Hydraulic [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 [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 [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 [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, 26100.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-7.0, -35.0, 0.0, 9300.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-7.0, 35.0, 0.0, 9300.0, 3.0 //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=4605.0 //Square feet wing_span=200.0 //Feet wing_root_chord=42.0 //Feet wing_dihedral=6.2 //Degrees wing_incidence=1.0 //Degrees wing_twist=-0.5 //Degrees oswald_efficiency_factor=0.6 //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=20.0 //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=-100.0 //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=-108.3 //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 [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=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 [stall_warning] type=2
