[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
