[General]
performance=Passengers\n3-class conf: 366 \n2-class conf: 452 \n1-class conf: N\/A\n\nCargo\nTotal lower hold volume:\n 5,497 ft3 (155.6 m3) \n\nDimensions\nSpan 195 ft 8 in\nLength 231 ft 10 in\nHeight 63 ft 5 in\n\nEngines: PW JT9D-7R4G2\nTO Thrust: 54,750 lb x 4\n\nMax Fuel Cap.: 52,410 US Gal.\nMaxTOW: 833,000 lbs\nMLW: 630,000 lbs\nZFW: 460,340 lbs\nOEW: 388,010 lbs\n\nMax Range: 5,650 nm\nTypical Cruise Speed \n @ FL350: M.84
atc_type=BOEING
atc_model=B742
[fltsim.0]
title=B747-206B
sim=747-100PW
model=
panel=
sound=
texture=
checklists=
atc_airline=Boeing
atc_flight_number=001
ui_manufacturer=Boeing
ui_type=747-206B
ui_variation=KLM
visual_damage=1
atc_heavy=1
atc_id=PH-BUB
atc_type=BOEING AIRCRAFT
atc_model=B742
editable=0
description=Project Opensky - 747-100/200\nVersion 2004.1.0\n\nB747-206B cn19923/118 registration PH-BUB\n\nEngine Type PW JT9D7GR4\n\nModel Designers\n Vincent Cho\n Yosuke Ube\n\nRepaint\n Tijn Mar\n\nFlight Dynamics Designer\n Nick Peterson\n Based on original by Warren Daniel\n\nTechnical Resource\n Simon Ng\n Shigeo Kitaguchi\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 7220 nm\n\nFor proper operation: See B747 manual at: \n www.project-opensky.com
atc_parking_types=gate,ramp,ga
atc_parking_codes=KL
[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
[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= 88.000, 0.000, 0.000
empty_weight_CG_position= -105.000, 0.000, 0.000
empty_weight=386850
empty_weight_roll_MOI= 18155743.000
empty_weight_pitch_MOI= 17600873.000
empty_weight_yaw_MOI= 19151035.000
empty_weight_coupled_MOI= 0.000
max_gross_weight=833000
max_number_of_stations= 6
station_load.0 = "3060.0, -19.0, 0.0, 2.0, 1stClass 17Pax"
station_load.1 = "2800.0, -48.00, 0.0,14.0, Upp Deck 42Pax"
station_load.2 = "7020.0, -83.0, 0.0, 2.0, Bus Class 39Pax"
station_load.3 = "50040.0, -118.0, 0.0, 2.0, Coach 278Pax"
station_load.4 = "18000.0, -63.0, 0.0,-2.0, Forward Cargo"
station_load.5 = "16000.0, -120, 0.0,-2.0, Aft Cargo"
[fuel]
Center1 = -88.0, 0.0, -4.0, 19431.0, 3.0
LeftMain =-102.0, -35.0, -4.0, 16660.0, 3.0
LeftAux =-109.5, -52.0, -3.0, 500.0, 3.0
RightMain =-102.0, 35.0, -4.0, 16660.0, 3.0
RightAux =-109.5, 52.0, -3.0, 500.0, 3.0
fuel_type =2.000000
electric_pump=1
number_of_tank_selectors=1
[airplane_geometry]
wing_area= 5500.000
wing_span= 196.000
wing_root_chord= 53.000
wing_dihedral= 3.998
wing_incidence= 3.500
wing_twist= -0.194
oswald_efficiency_factor= 0.730
wing_winglets_flag= 0
wing_sweep= 37.500
wing_pos_apex_lon= -78.000
wing_pos_apex_vert= 0.000
htail_area= 1470.000
htail_span= 72.750
htail_pos_lon= -204.167
htail_pos_vert= 7.000
htail_incidence= 0.000
htail_sweep= 37.500
vtail_area= 1060.000
vtail_span= 37.121
vtail_sweep= 45.000
vtail_pos_lon= -204.500
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]
point.0= 1.000, -21.333, 0.00, -14.853, 1181.102, 0.000, 2.000, 70.000, 1.129, 1.100, 0.98, 9.000, 11.000,0.000, 240.000, 280.000
point.1= 1.000, -99.583, -16.000, -15.403, 1574.803, 1.000, 2.000, 0.000, 1.62, 1.15, 0.741, 12.900, 14.900, 2.000, 240.000, 280.000
point.2= 1.000, -99.583, 16.000, -15.403, 1574.803, 2.000, 2.000, 0.000, 1.62, 1.15, 0.741, 13.100, 15.400, 3.000, 240.000, 280.000
point.3= 1.000, -109.583, -6.000, -15.403, 1574.803, 1.000, 2.000, 13.000, 1.62, 1.15, 0.741, 13.400, 14.900, 2.000, 240.000, 280.000
point.4= 1.000, -109.583, 6.000, -15.403, 1574.803,2.000, 2.000, 13.000,1.62, 1.15, 0.741, 12.500, 13.500, 3.000, 240.000, 280.000
point.5= 2.000, -102.167, -96.167, 0.000, 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.6= 2.000, -102.167, 96.167, 0.000, 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.7= 2.000, -220.667, 0.000, 2.500, 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.8= 2.000, 0.0, 0.000, -3.750, 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.9= 2.000, -102.167, -96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.10= 2.000, -220.667, 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
static_pitch= -.300
static_cg_height= 13.625
gear_system_type=0
[GeneralEngineData]
engine_type=1
Engine.0=-109.916667,-69.500000,0.000000
Engine.1=-86.916667,-39.166667,-7.000000
Engine.2=-86.916667,39.166667,-7.000000
Engine.3=-109.916667,69.500000,0.000000
fuel_flow_scalar=1.04
min_throttle_limit=-0.399902
[TurbineEngineData]
bypass_ratio=4.970000
fuel_flow_gain=0.002000
inlet_area=37.558941
rated_N2_rpm=29920.000000
static_thrust=54750.000000
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
[Views]
eyepoint=-35.000, -2.000, 14.800
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=105.000000
pitch_takeoff_ga=14.000000
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Def
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=1.000000
[flaps.0]
type = 1 span-outboard = 0.4 extending-time = 25
flaps-position.0 = 0
flaps-position.1 = 5
flaps-position.2 = 10
flaps-position.3 = 15
flaps-position.4 = 20
flaps-position.5 = 25
flaps-position.6 = 30
damaging-speed = 200
blowout-speed = 250
lift_scalar = 1.00
drag_scalar = .67
pitch_scalar= 0.3
system_type = 1
[flaps.1]
type = 1
span-outboard = 0.4
extending-time = 25
flaps-position.0 = 0
flaps-position.1 = 5
flaps-position.2 = 10
flaps-position.3 = 15
flaps-position.4 = 20
flaps-position.5 = 25
flaps-position.6 = 30
damaging-speed = 200
blowout-speed = 250
lift_scalar = 1.00
drag_scalar = .67
pitch_scalar= 0.3
system_type = 1
[flaps.2]
type = 2
span-outboard = 0.8
extending-time = 12
flaps-position.0 = 0
flaps-position.1 = 20.0
damaging-speed = 250
blowout-speed = 300
lift_scalar = 0.67
drag_scalar = .4
pitch_scalar= 0.1
system_type = 1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[direction_indicators]
direction_indicator.0=3,0
[folding_wings] // For opening main deck cargo door.
wing_fold_system_type = 4 ;0=None
fold_rates = 0.070, 0.070 ;Percent per second
cable_force_adjust = 1.0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1 = 0.4
[TailHook] // For opening cargo door.
tailhook_length=1 ;(feet)
tailhook_position = 0.0, 0.0, 0.0 fold_rates = .070, .07
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1, -22.95, 0.600, 19.100, Opensky_beacon ,
light.1 = 1, -74.500, 0.000, -7.080, Opensky_beacon ,
light.2 = 2, -130.00, -95.000, 8.80, fx_strobeh ,
light.3 = 2, -130.00, 95.000, 8.80, fx_strobeh ,
light.4 = 3, -210.700, -0.250, 12.300, Opensky_nav_yellow ,
light.5 = 3, -210.700, 0.250, 12.300, Opensky_nav_yellow ,
light.6 = 2, -210.900, 0.000, 11.450, fx_strobeh ,
light.7 = 3, -4.850, 0.000, 14.850, fx_vclighth ,
light.8 = 3, -199.500, -4.500, 43.750, Opensky_wing_light ,
light.9 = 3, -199.500, 4.500, 43.750,
Opensky_wing_light ,
light.10= 5, -70.700, -29.200, 0.000, Opensky_nacelle_refl ,
light.11= 5, -70.700, 29.200, 0.000, Opensky_nacelle_refl ,
light.12= 5, -37.500, -11.700, 2.000, Opensky_nacelle_refl ,
light.13= 5, -37.500, 11.700, 2.000, Opensky_nacelle_refl ,
light.14= 5, -31.500, -13.700, 3.900, Opensky_nacelle_refl ,
light.15= 5, -31.500, 13.700, 3.900, Opensky_nacelle_refl ,
light.16= 5, -5.333, 0.000, -2.000, Opensky_nacelle_refl ,
light.17= 3, -9.300, -6.500, 6.000, Opensky_nacelle_refl ,
light.18= 3, -43.610, -4.500, 6.000, Opensky_nacelle_refl ,
light.19= 3, -135.510, 0.000, -3.000, Opensky_wing_light ,
[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
[brakes]
toe_brakes_scale=.90555
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
