[General]
atc_type=BOEING
atc_model=B744
editable=0
performance=

[pitot_static]
vertical_speed_time_constant = 99


[WEIGHT_AND_BALANCE]
empty_weight        = 394088.0                  // 3-Class
max_gross_weight    = 875000.0                  // 800, 833, 850, 870, 875 x 10^3 lbs [+2000 for max ramp]
max_landing_weight  = 630000.0                  // 574, 630 x 10^3 lbs
max_zerofuel_weight = 542500.0                  // 535, 542.5 x 10^3 lbs
CG_forward_limit=0.130                          // 11% 572000-775000 lbs
CG_aft_limit=0.331
                                                // WARNING : DO NOT EDIT !
reference_datum_position = 112.714, 0.0, 5.502  // (feet) Boeing Section2.0 reference position (RefPos)
empty_weight_CG_position = -97.85, 0, 0         // (feet) from RefPos 19.75% MAC

max_number_of_stations =50


;Moments of Inertia
empty_weight_pitch_MOI   = 17018677.379279
empty_weight_roll_MOI    = 15962454.863936
empty_weight_yaw_MOI     = 16890566.121607
empty_weight_coupled_MOI = 2048.0
station_load.0=1800, -95.55, 0.00, 0.00, First Deck
station_load.1=7560, -97.85, 0.25, 8.00, Upper Deck
station_load.2=6300, -97.85, 0.00, 0.00, Busn Deck
station_load.3=61020, -98.00, -0.53, 0.00, Econ Deck
station_load.4=70000, -97.11, 0.00, -8.00, Cargo Deck

[GeneralEngineData]
engine_type = 1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -107.5, -53.3,  -6.9                 //(feet) from RefPos
Engine.1 =  -76.0, -30.0, -10.4                 //(feet) from RefPos
Engine.2 =  -76.0,  30.0, -10.4                 //(feet) from RefPos
Engine.3 = -107.5,  53.3,  -6.9                 //(feet) from RefPos
fuel_flow_scalar   = 1.07                       // sfc [...]
min_throttle_limit = -0.20                      // reverse

[TurbineEngineData]
//
// Model : CF6-80C2B1F ~58K
//
fuel_flow_gain          = 0.0036                //Gain on fuel flow
inlet_area              = 61.283                //Square Feet, engine nacelle inlet area [d=106 in]
rated_N2_rpm            = 13635.0               //max RPM HPC
static_thrust           = 58000.0               //Lbs, nominal SLS adjusted thru EEC
afterburner_available   = 0                     //Afterburner available?
reverser_available      = 1                     //Thrust reverser available?

[jet_engine]
thrust_scalar = 1.0

[fuel]                                            // Combi/ER + optional stab (Center2)
LeftAux   =  -112.0, -36.5, -3.0,  4482.0, 0.0    // Main 1
LeftMain  =   -96.0, -28.0, -4.0, 12546.0, 0.0    // Main 2
RightMain =   -96.0,  28.0, -4.0, 12546.0, 0.0    // Main 3
RightAux  =  -112.0,  36.5, -3.0,  4482.0, 0.0    // Main 4
LeftTip   =  -130.0, -73.0,  0.0,  1322.0, 0.0    // R2
RightTip  =  -130.0,  73.0,  0.0,  1322.0, 0.0    // R3
Center1   =   -83.5,   0.0, -7.0, 17164.0, 0.0    // CWT
Center2   =  -193.5,   0.0,  6.0,  3300.0, 0.0    // STAB [Optional]
Center3   =   -83.5,   0.0, -7.0,    50.0, 0.0    // Other
fuel_type = 2                                     //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 4                    
electric_pump=0

[airplane_geometry]
wing_area               = 5825.0                //Square feet
wing_span               = 211.4                 //Feet       [Jig Position (213.0 at full weight)]
wing_root_chord         = 47.298                //Feet
wing_dihedral           = 7.0                   //Degrees
wing_incidence          = 0.0                   //Degrees    [Inop in FS9]
wing_twist              = 0.0                   //Degrees    [Inop in FS9]
oswald_efficiency_factor = 0.504                //[...]
wing_winglets_flag      = 1                     //Winglet flag [0:false/1:true]
wing_sweep              = 37.5                  //Degrees at 25% MAC
wing_pos_apex_lon       = -60.606               //Feet from RefPos
wing_pos_apex_vert      = 0.0                   //Feet from RefPos
htail_area              = 1470.0                //Square feet
htail_span              = 75.75                 //Feet
htail_pos_lon           = -210.0                //Feet, from RefPos
htail_pos_vert          = 7.32                  //Feet, from RefPos
htail_incidence         = 0.0                   //Degrees    [Inop in FS9]
htail_sweep             = 37.5                  //Degrees, horizontal tail leading edge
vtail_area              = 1060.0                //Square feet
vtail_span              = 37.1                  //Feet, tip to body
vtail_sweep             = 45.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -198.5                //Feet from RefPos
vtail_pos_vert          = 26.1                  //Feet from RefPos
elevator_area           = 342.0                 //Square feet
aileron_area            = 225.0                 //Square feet
rudder_area             = 230.0                 //Square feet
elevator_up_limit       = 28.0                  //Degrees
elevator_down_limit     = 20.0                  //Degrees
aileron_up_limit        = 29.5                  //Degrees
aileron_down_limit      = 27.5                  //Degrees
rudder_limit            = 31.5                  //Degrees
elevator_trim_limit     = 20.0                  //Degrees
spoiler_limit           = 70.0                  //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 3.2                 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 4.0               //Degrees
min_flaps_for_spoilerons = 0.0                  //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed    = 174.55                //Stall clean KTAS @450,000 lbs
full_flaps_stall_speed  = 122.0                 //Stall flaps KTAS
cruise_speed            = 485.0                 //Cruise      KTAS
max_mach                = 0.920                 //Barber pole MACH
max_indicated_speed     = 372.0                 //            KIAS / modified provision for CAS->KIAS

[flaps.0]
type             = 1                                    // Trailing edge
span-outboard    = 0.7                                  // 0.0 .. 1.0
extending-time   = 60                                   // seconds
flaps-position.0 = 0                                    // pseudo-degrees
flaps-position.1 = 0.00,280                             // 1 - no TE
flaps-position.2 = 25.0,260                             // 5
flaps-position.3 = 27.5,240                             // 10
flaps-position.4 = 30.0,230                             // 20
flaps-position.5 = 31.5,205                             // 25
flaps-position.6 = 33.0,180                             // 30
lift_scalar = 1.0
drag_scalar = 0.1
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[flaps.1]
type             = 2                                    // Inboard/midboard leading edge
span-outboard    = 0.53333                              // 0.0 .. 1.0
extending-time   = 12                                   // seconds
flaps-position.0 = 0                                    // pseudo-degrees
flaps-position.1 = 1.0                                  // 1
damaging-speed   = 275                                  // KIAS
blowout-speed    = 280                                  // KIAS
lift_scalar = 0.88
drag_scalar = 1.54
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[flaps.2]
type             = 2                                    // Outboard leading edge
span-outboard    = 0.2666                               // 0.0 .. 1.0
extending-time   = 10                                   // seconds
flaps-position.0 = 0                                    // pseudo-degrees
flaps-position.1 = 0.0                                  // 1 - no effect
flaps-position.2 = 5.0                                  // 5
damaging-speed   = 255                                  // KIAS
blowout-speed    = 260                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[flaps.3]
type             = 2                                    // Correct 5-30 / TE LIFT
span-outboard    = 0.7                                  // 0.0 .. 1.0
extending-time   = 50                                   // seconds
flaps-position.0 = 0                                    // pseudo-degrees
flaps-position.1 = 0.00
flaps-position.2 = 25.0
flaps-position.3 = 21.0
flaps-position.4 = 16.1
flaps-position.5 = 8.7
flaps-position.6 = 4.7
lift_scalar  = -1.22
drag_scalar  =  0.00
pitch_scalar = -0.12
system_type  = 1                                         //Hydraulic

[flaps.4]
type             = 2                                    // Correct 10 / TE DRAG
span-outboard    = 0.7                                  // 0.0 .. 1.0
extending-time   = 60                                   // seconds
flaps-position.0 = 0                                    // pseudo-degrees
flaps-position.1 = 0.0
flaps-position.2 = 0.0
flaps-position.3 = 1.0
flaps-position.4 = 0.1
flaps-position.5 = 3.0
lift_scalar  =  0.00
drag_scalar  = -1.00
pitch_scalar =  0.00
system_type = 1                                         //Hydraulic

[flaps.5]
type             = 2                                    // Correct 30 / TE DRAG
span-outboard    = 0.7                                  // 0.0 .. 1.0
extending-time   = 60                                   // seconds
flaps-position.0 = 0                                    // pseudo-degrees
flaps-position.1 = 0.0
flaps-position.2 = 0.0
flaps-position.3 = 0.0
flaps-position.4 = 0.0
flaps-position.5 = 0.0
flaps-position.6 = 6.5
lift_scalar  = 0.00
drag_scalar  = 1.00
pitch_scalar = 0.00
system_type = 1                                         //Hydraulic

[flaps.6]
type             = 1                                    // Model
span-outboard    = 0.7
extending-time   = 60 
flaps-position.0 = 0.0
flaps-position.1 = 1.0
flaps-position.2 = 5.0
flaps-position.3 = 10.0
flaps-position.4 = 20.0
flaps-position.5 = 25.0
flaps-position.6 = 30.0
lift_scalar =  0.0
drag_scalar =  0.0
pitch_scalar=  0.0
system_type = 1

[autopilot]
autopilot_available = 0
autothrottle_available = 0
default_pitch_mode=0
default_bank_mode=0

//Do Not Alter the following line or your 747-400 may cease operating.
[AFDSAuth]
---BEGIN SHA1---
D8A506E2E1987CCB2A2E73848A051AD4E7C74639
---END SHA1---
// Do Not Alter the above lines.

[contact_points]
//
point.0 = 1,  -24.194,    0.000, -17.546, 1500.0, 0, 1.932, 56.0, 1.45, 0.128, 0.780,  9.0, 12.0, 0, 270, 320
point.1 = 1, -102.496,  -16.009, -18.941, 1500.0, 1, 1.932,  0.0, 1.54, 1.171, 0.880, 16.0, 21.0, 2, 270, 320
point.2 = 1, -102.496,   16.009, -18.941, 1500.0, 2, 1.932,  0.0, 1.54, 1.171, 0.880, 15.0, 20.0, 3, 270, 320
point.3 = 1, -115.277,   -4.253, -18.598, 1700.0, 1, 1.932,  0.0, 1.50, 1.203, 0.820, 15.0, 18.0, 2, 270, 320
point.4 = 1, -115.277,    4.253, -18.598, 1700.0, 1, 1.932,  0.0, 1.50, 1.203, 0.820, 15.0, 18.0, 2, 270, 320
//
point.5 = 2, -153.600, -103.500,   3.000, 1250.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 5,   0,   0
point.6 = 2, -153.600,  103.500,   3.000, 1250.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 6,   0,   0
point.7 = 2,   -2.945,    0.000,  -3.312, 1500.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 9,   0,   0
point.8 = 2, -156.766,    0.000,  -9.961, 1500.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0

static_pitch = -0.29
static_cg_height = 12.09
gear_system_type=0

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  5.0     //Flap angle that activates warning at idle
flap_limit_power   = 31.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 0.78  //Brake scalar

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,1,1   //pumps on Eng1,2,3,4

[Views]
eyepoint = -19.100, -1.312, 11.122              ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
//eyepoint= -18.848, -1.312, 11.122

[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, 5 , 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
Adf.2         = 1
Transponder.1 = 1
Marker.1      = 1

[LIGHTS]
light.0 = 3, -225.500,  -0.50,     4.745,   fx_navwhih,      		//Position Aft
light.1 = 2, -225.500,   0.50,     4.745,   fx_strobeh,       		//Strobe Aft
light.2 = 1,  -33.596,   0.00,    14.868,   fx_pmdg744_beacon,       	//Beacon Top
light.3 = 1,  -86.149,   0.00,   -11.735,   fx_pmdg744_beacon,       	//Beacon Bottom
light.4 = 9, -210.149,   8.00,    35.117,   fx_pmdg744_logo,  		//Logo Right
light.5 = 9, -210.149,  -8.00,    35.117,   fx_pmdg744_logo,  		//Logo Left
light.6 = 8,  -77.000,  26.00,    -4.000,   fx_pmdgwinglight, 		//Wing Right
light.7 = 8,  -77.000, -26.00,    -4.000,   fx_pmdgwinglight, 		//Wing Left

[SMOKESYSTEM]
smoke.0 = 0.00, -20.5, 0.00, fx_pmdg744_cockpit,

[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

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2 
attitude_indicator.1 = 1 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0

[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 = 150, 250
aileron  = 150, 250
rudder   = 150, 250

[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

[stall_warning]
type=2