[fltsim.0]
title=Boeing 747-258F EL AL Cargo 4X-AXK
sim=747-200B-PW-JT9D-7R4G2.air
model=
panel=
sound=
texture=axk
checklists=

atc_airline=EL AL
atc_id=4X-AXK
atc_flight_number=2376
atc_heavy=1

ui_manufacturer=Boeing
ui_type=747-258F
ui_variation=EL AL Cargo 4X-AXK
visual_damage=1


description=Project Opensky \nBoeing 747-258F\nVersion 2002.3.1\n\nEngine Type PW-JT9D-7R4G2\n\n747-200 Cargo Version \nRepainted for Virtual EL AL Airlines with additional textures\nby Tony Radmilovich\n\n\nModel Designers\n   Mitsushi Yutaka\n   Hiroshi Igami  \n\nFlight Dynamics Designer\n   Warren C. Daniel\n\nTechnical Resource\n   Simon Ng\n   Shigeo Kitaguchi\n\nTest Pilots\n   Project Opensky Members\n\nMaximun Range: 6,370 nm\n\nFor proper operation: See B747 manual at: \n  www.project-opensky.com

[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

[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                //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=0.000000,0.000000,0.000000,0.000000
empty_weight=538340.000000
empty_weight_roll_MOI=11331310.000
empty_weight_pitch_MOI=36732189.000
empty_weight_yaw_MOI=32844259.000
empty_weight_coupled_MOI=1000.000
max_gross_weight=833000.00
CG_forward_limit=0.000
CG_aft_limit=1.000

[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=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=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=13.751
elevator_down_limit=10.313
aileron_up_limit=31.513
aileron_down_limit=31.513
rudder_limit=17.189
elevator_trim_limit=9.167
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, 1181.102, 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, 1574.803, 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, 1574.803, 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, -14.167, -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.4=2.000, -14.167, 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.5=2.000, -132.667, 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.6=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.7=2.000, -14.167, -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.8=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
static_pitch=-1.000
static_cg_height=13.625

// Nose gear
//point.0=1.000, 67.333, -1.500, -14.333, 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, -14.333, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -15.833, 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, -14.167, -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.19=2.000, -14.167, 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.20=2.000, -132.667, 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.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, -14.167, -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.23=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
//
//static_pitch=-1.000
//static_cg_height=13.625

[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=0.8676

[TurbineEngineData]
bypass_ratio=4.970000
fuel_flow_gain=0.001000
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=424.337

[keyboard_response]
elevator=100.000, 200.000
aileron=100.000, 200.000
rudder=150.000, 250.000

[Views]
eyepoint=77.330, -1.487, 20.005

[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: GE CF6-50E2\nTO Thrust: 52,500 lb x 4\n\nMax Fuel Cap.: 52,410 US Gal.\nMaxTOW: 833,000 lbs\nMLW: 630,000 lbs\nZFW: 538,340 lbs\nOEW: 388,010 lbs\n\nMax Range: 6,370  nm\nTypical Cruise Speed \n   @ FL350: M.84

atc_type=BOEING AIRCRAFT
atc_model=B742
editable=0


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=105.000
pitch_takeoff_ga=8.000
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.

[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=0.7
drag_scalar=1.0
pitch_scalar=0.9
system_type=1                                         //Hydraulic

[flaps.1]
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=0.3
drag_scalar=1.0
pitch_scalar=0.1
system_type=1                                         //Hydraulic



[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

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[direction_indicators]
direction_indicator.0=3,0



[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