[fltsim.0]
title=747-400
sim=747-400-GE-CF6-80C2B1
model=400
panel=
sound=
texture=400_Domestic
checklists=
atc_airline=Lynx Airways
atc_flight_number=LYX
ui_manufacturer=Lynx Airways Worldwide
ui_type=747-400 Passenger
ui_variation=Domestic/International
visual_damage=1
atc_heavy=1
atc_id=L07113D
description=Project Opensky Boeing 747-400 Version 2002.5.6C Model Designer: Chang Yeon, Vincent Cho Flight Dynamics Designer: Warren C. Daniel Senior QC & Adviso: Simon Ng Test Pilots: Project Opensky Members. For proper operation: See B747 manual at: www.project-opensky.com. Repaint was completed by our very own Media Division Officer, Yoshi. Lynx Airways Worldwide has been given permission by MelJet to repaint their aircraft. We at Lynx thank MelJet, their staff, and designers for the oportunity to fly their aircraft as part of our fleet.
[General]
performance=Passengers\n3-class conf: 524 \n2-class conf: 416 \n1-class conf: N\/A\n\nCargo\nTotal lower hold volume:\n 5,497 ft3 (155.6 m3) \n\nDimensions\nSpan 211 ft 5 in (213 ft -- fueled)\nLength 231 ft 10 in\nHeight 63 ft 5 in\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: 7305 mi \nTypical Cruise Speed \n @ FL350: M.85
atc_type=BOEING
atc_model=B744
editable=0
[pitot_static]
vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI
[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
//station_load.0 = 9720,-100.0, 0.0, -11.0 //Aft Bulk - Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.1 = 57500, 80.0, 0.0, 0.0 //LD aft - Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.2 = 61000, -80.0, 0.0, 0.0 //LD fwd - Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.3 =118307, 0.0, 0.0, 0.0 //Main Dk - Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.4 = 2640, 47.0, 0.0, 20.005434 //Upper Dk - Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight= 545965.000
empty_weight_roll_MOI= 9857983.000
empty_weight_pitch_MOI= 20732658.000
empty_weight_yaw_MOI= 31205473.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 928300.489
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, 17153.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = -193.5, 0.0, 6.0, 3298.0, 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)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[airplane_geometry]
wing_area= 5650.000
wing_span= 211.000
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= 1
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= 0.000
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= 24.000
elevator_down_limit= 18.000
aileron_up_limit= 20.000
aileron_down_limit= 20.000
rudder_limit= 30.000
elevator_trim_limit= 9.167
spoiler_limit= 45.000
spoilerons_available= 0
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 11.459
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed = 150.0 //Knots True (KTAS)
full_flaps_stall_speed = 126.0 //Knots True (KTAS)
cruise_speed = 495.0 //Knots True (KTAS)
[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 = 5 // degrees
flaps-position.2 = 10 // degrees
flaps-position.3 = 15 // 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 = 5 // degrees
flaps-position.2 = 10 // degrees
flaps-position.3 = 15 // 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 = 20.0 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.40
system_type = 1 //Hydraulic
[flaps.3]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 12 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 20 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.40
system_type = 1 //Hydraulic
[flaps.4]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.2 // 0.0 .. 1.0
extending-time = 12 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 10 // degrees
flaps-position.2 = 20.0 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.40
system_type = 1 //Hydraulic
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 2.0
aileron_effectiveness = 2.0
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= -14.917, -69.500, 0.000
Engine.1= 14.917, -39.167, -7.000
Engine.2= 14.917, 39.167, -7.000
Engine.3= -14.917, 69.500, 0.000
fuel_flow_scalar= 0.9676
[TurbineEngineData]
bypass_ratio=4.800000
fuel_flow_gain= 0.001
inlet_area= 48.150
rated_N2_rpm= 29992.000
static_thrust= 54750.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar = 1.0
[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=8.000000
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
[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, 11.000, 11.000, 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, 14.900, 14.900, 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, 17.100, 17.100, 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
// Nose gear
//point.0= 1.000, 67.333, -1.500, -15.333, 1181.102, 0.000, 2.000, 70.000, 1.859, 2.500, 0.518, 9.000, 11.000, 0.000, 240.000, 280.000
//point.1= 1.000, 67.333, 1.500, -15.333, 1181.102, 0.000, 2.000, 70.000, 1.859, 2.500, 0.518, 9.000, 11.000, 0.000, 240.000, 280.000
//
// Main Wing Gear (left)
//point.2= 1.000, -7.583, -18.000, -17.133, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//point.3= 1.000, -7.583, -14.000, -17.133, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//point.4= 1.000, -2.583, -18.000, -17.133, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//point.5= 1.000, -2.583, -14.000, -17.133, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//
// Main Wing Gear (right)
//point.6= 1.000, -7.583, 18.000, -17.133, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000
//point.7= 1.000, -7.583, 14.000, -17.133, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000
//point.8= 1.000, -2.583, 18.000, -17.133, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000
//point.9= 1.000, -2.583, 14.000, -17.133, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000
//
// Main Center Gear (left)
//point.10= 1.000, -18.583, -8.000, -17.133, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//point.11= 1.000, -18.583, -4.000, -17.133, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//point.12= 1.000, -12.583, -8.000, -17.133, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//point.13= 1.000, -12.583, -4.000, -17.133, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//
// Main Center Gear (right)
//point.14= 1.000, -18.583, 8.000, -17.133, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//point.15= 1.000, -18.583, 4.000, -17.133, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//point.16= 1.000, -12.583, 8.000, -17.133, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//point.17= 1.000, -12.583, 4.000, -17.133, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//
//Scrape points
//point.18= 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.19= 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.20= 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.21= 2.000, 88.167, 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.22= 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.23= 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.24= 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.25= 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.26= 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= 13.625
[TailHook] // For opening cargo door.
tailhook_length=1 ;(feet)
tailhook_position = 0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum
[folding_wings] // For opening main deck cargo door.
wing_fold_system_type = 4 ;0=None
fold_rates = 0.05,0.05 ;Percent per second
cable_force_adjust = 1.0
[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 = 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
[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
[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 = 100, 200
aileron = 100, 200
rudder = 100, 200
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[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
[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, 65.200, 0.600, 19.100, Opensky_beacon ,
light.1 = 1, 13.500, 0.000, -7.080, 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, -122.700, -0.250, 12.300, Opensky_nav_yellow ,
light.5 = 3, -122.700, 0.250, 12.300, Opensky_nav_yellow ,
light.6 = 2, -121.900, 0.000, 11.450, fx_strobeh ,
light.7 = 3, 84.850, 0.000, 14.850, fx_vclighth ,
light.8 = 3, -111.500, -4.500, 43.750, Opensky_wing_light ,
light.9 = 3, -111.500, 4.500, 43.750, Opensky_wing_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, 51.500, -11.700, 0.000, Opensky_nacelle_refl ,
light.13= 5, 51.500, 11.700, 0.000, Opensky_nacelle_refl ,
light.14= 5, 57.500, -13.700, 1.900, Opensky_nacelle_refl ,
light.15= 5, 57.500, 13.700, 1.900, Opensky_nacelle_refl ,
light.16= 5, 83.333, 0.000, -2.000, Opensky_nacelle_refl ,
light.17= 3, 72.300, -6.500, 6.000, Opensky_nacelle_refl ,
light.18= 3, 45.610, -4.500, 6.000, Opensky_nacelle_refl ,
light.19= 3, -47.510, 0.000, -3.000, Opensky_wing_light ,
