[fltsim.0]
title=Project Opensky - Boeing 747-400 Paint3
sim=747-400-GE-CF6-80C2B1
model=
panel=
sound=
texture=
checklists=

atc_airline=----
atc_flight_number=314

ui_manufacturer=Project Opensky
ui_type=747-400
ui_variation=British Airways
visual_damage=1

atc_heavy=1
atc_id=1

description=    My first repaint.  Hope you enjoy!!!  The rest of the credit goes to Project Opensky \nBoeing 747-400\nVersion 2002.5.6C\n\nEngine Type GE CF6-80C2B1\n\n747-400 Commercial Version \n\nModel Designer\n   Chang Yeon, Vincent Cho  \n\nFlight Dynamics Designer\n   Warren C. Daniel\n\nSenior QC & Advisor\n   Simon Ng\n\nTest Pilots\n   Project Opensky Members\n\nMaximun Range: 7305 nm\n\nFor proper operation: See B747 manual at: \n  www.project-opensky.com

[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 ,