[fltsim.0]
title=Atlas Air NC B747-47UF(SCD)
sim=747-400F-GE-CF6-80C2B5F
model=
panel=
sound=
texture=
checklists=

atc_airline=SPEED BIRD
atc_id=N499MC
atc_flight_number=9336
atc_heavy=1

ui_manufacturer=Boeing
ui_type=747-400F
ui_variation=Atlas Air New Colours
visual_damage=1

description=Project Opensky - 747-400F\nVersion 2002.4.1\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-----\nCrew: 4 \nPassengers: 0\nCrew Station: 4 seats, 2 rest bunks\nLavatory: 1\nGalley: 1\n\nEngines: GE CF6-80C2B15F2\nTO Thrust: 62,100 lb x 4\n\nTypical Cruise Speed \n   @ FL350: M.84\n\nFor proper operation, see B747\nmanual at: project-opensky.com

[General]
performance=Cargo\nAft Bulk: 520 ft3 (9,720 lb)  \nLower Deck Aft: 2800 ft3 (57,500 lb)\nLower Deck Fwd: 2800 ft3 (61,000 lb)\nMain Deck: 21,117 (load dependant)\n\nDimensions\nSpan 211 ft 5 in (213 ft -- fueled)\nLength 231 ft 10 in\nHeight 63 ft 5 in\n\nMax Fuel Cap.: 53,644 US Gal.\nMax Gross Taxi Weight: 877,000 lb\nMax Gross TOW: 875,000 lb\nMLW: 666,000 lb\nMZFW: 610,000 lb\nOEW: 363,473 lb\n\nWheels\/Brakes: BF Goodrich\/Carbon Brakes\nNoise Compliance: Stage III\nApproach Category: CAT IIIB
atc_type=BOEING AIRCRAFT
atc_model=B744

[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=363473.000
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=877000.000
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=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=0.7
drag_scalar=0.9
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=0.1
pitch_scalar=0.1
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=0.3230

[TurbineEngineData]
bypass_ratio=4.800000
fuel_flow_gain=0.001
inlet_area=48.150
rated_N2_rpm=179520.000
static_thrust=62100.000
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)

// 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 (lef)
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

[Views]
eyepoint=77.330422,-1.486631,20.005434   // 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)
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0


[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

//[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing                   
//light.0=3, -150.30, -102.56,   3.22, fx_navredh ,
//light.1=3, -150.30,  102.56,   3.22, fx_navgreh ,
//light.2=3, -223.85,    0.00,   8.85, fx_navwhih ,
//light.3=2, -150.30, -102.56,   3.22, fx_strobeh ,
//light.4=2, -150.30,  102.56,   3.22, fx_strobeh ,
//light.5=2, -228.97,    0.00,  44.62, fx_strobeh ,
//light.6=1,  -45.05,    0.00,  14.65, fx_beaconh ,
//light.7=1,  -80.22,    0.00, -12.05, fx_beaconb ,
//light.8=4,  -16.24,    0.00,   9.19, fx_vclighth,

[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

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

[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