[fltsim.0] title=Orient Thai 747-306M sim=B747341combigmax model= panel= sound= texture=ox checklists= atc_airline=Orient Thai atc_flight_number=1997 ui_manufacturer=Boeing ui_type=747-306M ui_variation=Orient Thai Airlines visual_damage=1 atc_heavy=1 atc_id=HS-UTK atc_parking_types=GATE atc_parking_codes=OX description=Project Opensky - 747-300 Gmax\nOrient Thai HS-UTK \n\nModel Designers \n Chang Yeon, Vicent Cho\nPainter\n Olve Askim \n\nFlight Dynamics Designer\n Warren C. Daniel\n Nick Peterson\n ver 2002.5.3.3\n \nTest Pilot\n Luiz Antonio Perina\n\nTechnical Resource\n Shigeo Kitaguchi\n Nick Peterson\n\n\nMaximun Range: 7220 nm\n\n copyright by: Project Opensky\n www.project-opensky.com [General] performance=Passengers\nFirst Class (P): 12 pax\nExec Class(C): 61 pax\nEcon Class(Y):188 pax \n\nCargo\nTotal lower hold volume:\n 5,497 ft3 (155.6 m3)\n 7 palletes at the Cabin no.5 \n\nCity Pairs:\nSAO-LAX-TYO\nSAO-NYC\nSAO-MIA\n\nEngines: GE CF6-80C2B1\nTO Thrust: 54,750 lb x 4\n\nMax Fuel Cap.: 57,065 US Gal.\nMaxTOW: 870,000 lbs\nMLW: 630,000 lbs\nZFW: 545,965 lbs\nOEW: 407,107 lbs\n\nMax Range: 7220 nm \nTypical Cruise Speed \n @ FL350: M.86 atc_type=BOEING atc_model=B743 editable=1 [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 = 1.4 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 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 [pitot_static] vertical_speed_time_constant=999 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 empty_weight=446847 empty_weight_roll_MOI= 13155743.000 empty_weight_pitch_MOI= 22600873.000 empty_weight_yaw_MOI= 25151035.000 empty_weight_coupled_MOI= 1000.000 max_gross_weight=833000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 station_load.0=0.000000,0.000000,0.000000,0.000000 [fuel] Center1 =0.000, 0.0, -4.0, 19431.0, 3.0 LeftMain =-5.0, -35.0, -4.0, 16660.0, 3.0 LeftAux =-11.5, -52.0, -3.0, 500.0, 3.0 RightMain =-5.0, 35.0, -4.0, 16660.0, 3.0 RightAux =-11.5, 52.0, -3.0, 500.0, 3.0 fuel_type = 2 number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area= 5500.000 wing_span= 196.000 wing_root_chord= 23.000 wing_dihedral= 6.998 wing_incidence= 2.000 wing_twist= -0.994 oswald_efficiency_factor= 0.830 wing_winglets_flag= 0 wing_sweep= 37.500 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 1470.000 htail_span= 72.750 htail_pos_lon= -17.167 htail_pos_vert= 0.000 htail_incidence= -4.000 htail_sweep= 37.500 vtail_area= 1060.000 vtail_span= 37.121 vtail_sweep= 45.000 vtail_pos_lon= -16.500 vtail_pos_vert= 6.083 elevator_area= 326.800 aileron_area= 225.200 rudder_area= 229.900 elevator_up_limit= 20.751 elevator_down_limit= 15.313 aileron_up_limit= 31.513 aileron_down_limit= 31.513 rudder_limit= 17.189 elevator_trim_limit= 19.167 spoiler_limit= 25.783 spoilerons_available= 0 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 11.459 min_flaps_for_spoilerons= 0.000 [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 = 1.000, 67.333, 0.000, -13.850, 2181.102, 0.000, 5.812, 78.480, 0.859, 0.500, 0.518, 9.000, 8.000, 0.000, 0.000, 0.000 point.1 = 1.000, -12.583, -18.000, -13.833, 2574.803, 1.000, 5.812, 0.000, 0.602, 0.500, 0.551, 9.500, 8.000, 2.000, 0.000, 0.000 point.2 = 1.000, -12.583, 18.000, -13.833, 2574.803, 2.000, 5.812, 0.000, 0.602, 0.500, 0.551, 9.500, 8.000, 3.000, 0.000, 0.000 point.3 = 2.000, -49.000, -102.900, 7.000, 787.402, 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, -49.000, 102.900, 7.000, 787.402, 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, -92.667, 0.000, -2.000, 787.402, 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, 88.167, 0.000, -5.750, 787.402, 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,-132.667, 0.000, 55.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 point.8 = 2.000, -14.917, -69.500, -7.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.9 = 2.000, 14.917, -39.167, -11.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.10= 2.000, 14.917, 39.167, -11.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.11= 2.000, -14.917, 69.500, -7.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 static_pitch= -1.000 static_cg_height= 13.125 gear_system_type=0 [SMOKESYSTEM] smoke.0=7, -44.967, -69.467, fx_posky743_vortex.fx smoke.1=7, -44.967, 69.467, fx_posky743_vortex.fx [GeneralEngineData] engine_type=1 Engine.0=-14.916667,-69.500000,0.000000 Engine.1=14.916667,-39.166667,-7.000000 Engine.2=14.916667,39.166667,-7.000000 Engine.3=-14.916667,69.500000,0.000000 fuel_flow_scalar=1.15 min_throttle_limit=-0.379944 [TurbineEngineData] bypass_ratio=4.970000 fuel_flow_gain=0.002000 inlet_area=37.558941 rated_N2_rpm=26928.000000 static_thrust=52500.000000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed= 150.000 full_flaps_stall_speed= 126.000 cruise_speed= 524.337 max_indicated_speed=350.000000 max_mach=0.900000 [keyboard_response] elevator= 100.000, 200.000 aileron= 100.000, 200.000 rudder= 150.000, 250.000 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.000 autothrottle_available= 1 autothrottle_arming_required= 1 autothrottle_takeoff_ga= 1 autothrottle_max_rpm= 105.000 pitch_takeoff_ga= 14.000 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=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [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 = 0.28 drag_scalar = 0.40 pitch_scalar= 0.40 system_type = 1 //Hydraulic [flaps.1] 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 = 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 = 0.28 drag_scalar = 0.40 pitch_scalar= 0.40 system_type = 1 //Hydraulic [flaps.2] type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 12 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 5 // degrees flaps-position.2 = 10 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.28 drag_scalar = 0.40 pitch_scalar= 0.40 system_type = 1 [stored information] cargo_config=auto cargo_container_type= cargo1=0 cargo2=0 cargo3=0 cargo4=0 cargo5=0 cargo6=0 cargo7=0 cargo8=0 cargo9=0 cargo10=0 cargo11=0 cargo12=0 cargo13=0 cargo14=0 cargo15=0 cargo16=0 cargo17=0 cargo18=0 cargo19=0 cargo20=0 cargo21=0 cargo22=0 cargo23=0 cargo24=0 cargo25=0 cargo26=0 cargo27=0 cargo28=0 cargo29=0 cargo30=0 cargo_bulk=0 main_deck_cargo=0 main_deck_cargo_type= per_pax_weight=42 forward_cargo=0 aft_cargo=0 total_passengers=301 pax_config=simple pax_upper=0 pax1=0 pax2=0 pax3=0 pax4=0 pax5=0 pax6=0 aircraft_type=747-200 seating_type=Basic Mixed-Class [default information] empty_weight=439520 max_gross_weight=820000 Center1=0.000, 0.0, -4.0, 17153.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-5.0, -35.0, -4.0, 12538.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux=-11.5, -52.0, -3.0, 5761.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-5.0, 35.0, -4.0, 12538.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux=-11.5, 52.0, -3.0, 5761.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) station_load.0=0.000000,0.000000,0.000000,0.000000 [exits] number_of_exits = 2 exit_rate.0 = 0.15 ;Percent per second exit_rate.1 = 0.15 ;Percent per second [TailHook] // shift+C For opening cargo door. tailhook_length=4 ;(feet) tailhook_position = -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust = 1.0 [folding_wings] // CapsLock For opening main cabin cargo door wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [Views] eyepoint=83.000, -2.000, 14.800 // 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) flap_motor = 1, 0 , 1.0 gear_motor = 0, 5 , 17.0 avionics_bus = 0, 0 , 1.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 0 , 1.0 additional_system = 0, 0 , 1.0 marker_beacon = 1, 2 , 17.0 gear_warning = 7, 0 , 99.0 gear_motor = 4, 0 , 1.0 fuel_pump = 0, 0 , 1.0 fuel_transfer_pump = 0, 0 , 1.0 starter1 = 0, 20, 17.0 starter2 = 0, 0 , 1.0 light_nav = 0, 0 , 1.0 light_beacon = 0, 0 , 1.0 light_landing = 0, 0 , 1.0 light_taxi = 0, 0 , 1.0 light_strobe = 0, 0 , 1.0 light_panel = 0, 7 , 99.0 light_recognition = 0, 0 , 1.0 light_wing = 0, 0 , 1.0 marker_beacon = 0, 0 , 1.0 standby_vacuum = 0, 0 , 1.0 auto_brakes = 0, 0 , 1.0 hydraulic_pump = 0, 0 , 1.0 propeller_device = 0, 0 , 1.0 [Radios] // Radio Type = available, 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 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=Opensky_sparks, 1 touchdown=fx_tchdwn, 1 [SMOKESYSTEM] //Aileron tip vortecies smoke.0=0, -30.167, -86.167, Opensky_vortex smoke.1=0, -30.167, 86.167, Opensky_vortex //Wing condensation smoke.2=0, -08.917, -39.167, Opensky_conden smoke.3=0, -08.917, 39.167, Opensky_conden [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 1, 65.000, 0.600, 19.210, Opensky_beacon , light.1 = 1, 13.600, 0.000, -7.380, Opensky_beacon , //light.2 = 2, -49.000, -102.900, 13.150, fx_strobeh , //light.3 = 2, -49.000, 102.900, 13.150, fx_strobeh , light.4 = 3, -122.300, -0.250, 12.300, fx_navwhi , light.5 = 3, -122.300, 0.250, 12.300, fx_navwhi , light.6 = 2, -121.900, 0.000, 11.450, fx_strobeh , light.7 = 4, 85.330, 0.000, 19.005, Opensky_747_vclight , light.8 = 5, -117.500, -3.500, 40.750, Opensky_logo_light , light.9 = 5, -117.500, 3.500, 40.750, Opensky_logo_light , light.10= 5, 18.700, -29.200, -2.000, Opensky_nacelle_refl , light.11= 5, 18.700, 29.200, -2.000, Opensky_nacelle_refl , light.12= 5, 44.500, -11.700, 0.000, Opensky_wing_light , light.13= 5, 44.500, 11.700, 0.000, Opensky_wing_light , light.14= 5, 57.500, -13.700, 1.900, Opensky_wing_light , light.15= 5, 57.500, 13.700, 1.900, Opensky_wing_light , light.16= 5, 83.333, 0.000, -2.000, Opensky_wing_light , [brakes] toe_brakes_scale=0.756859 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0