//// FAIB 747-400D GE FSX Aircraft.cfg version 1.0 + HotFix1  FDE: Erez Werber////
//// FLTSIM Sections go here ////

[General]
atc_type=BOEING
atc_model=B744
editable=0
performance="Out of this world!"
Category = airplane

[contact_points]
// FAIB B747-400 Contact Points
point.0 = 1,  -4.4,  0.0, -15.55, 1600, 0, 2.1, 70.0, 1.55 , 1.3419, 0.900,  9.0,  8.0, 0, 220, 250
point.1 = 1, -95.0, -17.7, -16.3 , 1600, 1, 2.16, 0.0 , 1.8  , 1.2777, 0.900, 11.0,  9.0, 2, 220, 250
point.2 = 1, -95.0,  17.7, -16.3 , 1600, 2, 2.16, 0.0 , 1.8  , 1.2777, 0.900, 11.0,  9.0, 3, 220, 250
point.3 = 2, -152.6,  -103.5,   3.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 5,   0,   0
point.4 = 2, -152.6,   103.5,   3.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 6,   0,   0
point.5 = 2,    3.0,     0.0,   0.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 9,   0,   0
point.6 = 2, -222.7,     0.0,   4.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0    
                                 
static_pitch = -0.35
static_cg_height = 14.75
gear_system_type=1      //Hydraulic

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing   
// FAIB B747-400D Lights                
light.1 = 3, -203.3,    0.00,   10.35, fx_navwhi
light.2 = 1,  -18.7,    0.00,  19.0, fx_beacon
light.3 = 1,  -67.5,    0.00, -7.66, fx_beacon
// If using the NWF models remove the "//" from the beginings of the next lines
//light.4 = 3, -124.73, -96.63, 6.16, fx_navred
//light.5 = 3, -124.73,  96.63, 6.16, fx_navgre
//light.6 = 2, -123.88, -96.46, 6.16, fx_strobe
//light.7 = 2, -123.88,  96.46, 6.16, fx_strobe
//light.8 = 2, -202.7,    0.00,  9.4, fx_strobe
//If you have Shockwave lights you can enable them by removing the "//" from the beginings of the next lines
//light.9 = 5, -65.05, 18.45, -0.6,  fx_Shockwave_landing_light_747_rw
//light.10 = 5, -65.05, -18.45, -0.6,  fx_Shockwave_landing_light_747_lw

[exits]
// FAIB B747-400 Exits
number_of_exits = 2
exit.0 = 0.4, -10.0 ,  -9.8,  5.2, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1 = 0.4, -126.4,   8.0, -4.3, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0    //Scalar on heat effectiveness, 0 = not available

[WEIGHT_AND_BALANCE]
max_gross_weight = 875000                       // (pounds)
empty_weight = 600088                           // (pounds)

reference_datum_position     =  83.5, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -70.5, 0, 0     // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

;Moments of Inertia
empty_weight_roll_MOI    = 13352310
empty_weight_pitch_MOI   = 24223159
empty_weight_yaw_MOI     = 39531785
empty_weight_coupled_MOI = 0


[fuel]
LeftMain  =   -96.0, -28.0, -4.0, 300.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 
RightMain =   -96.0,  28.0, -4.0, 300.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 

fuel_type = 2                                     //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1
fuel_dump_rate = 0.0167                        //Percent of max quantity per second, i.e. about 1 minute for full fuel

[airplane_geometry]
wing_area               = 5500.0                //Square feet
wing_span               = 195.7                 //Feet
wing_root_chord         = 48.8                  //Feet
wing_dihedral           = 7.0                   //Degrees
wing_incidence          = 2.0                   //Degrees
wing_twist              = -1.0                  //Degrees
oswald_efficiency_factor= 0.68                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 37.5                  //Degrees, wing leading edge
wing_pos_apex_lon       = -58.2                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 3.8                     //Feet, vertical distance from reference point, positive going up
htail_area              = 1470                  //Square feet
htail_span              = 72.8                  //Feet
htail_pos_lon           = -210.0                //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.0                   //Degrees
htail_sweep             = 37.5                  //Degrees, horizontal tail leading edge
vtail_area              = 1060                  //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, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 26.1                  //Feet, vertical distance from reference point, positive going up
elevator_area           = 327                   //Square feet
aileron_area            = 225                   //Square feet
rudder_area             = 230                   //Square feet
elevator_up_limit       = 25                    //Degrees
elevator_down_limit     = 15                    //Degrees
aileron_up_limit        = 25                    //Degrees
aileron_down_limit      = 15                    //Degrees
rudder_limit            = 31.5                  //Degrees
elevator_trim_limit     = 20                    //Degrees
spoiler_limit           = 45                    //Degrees
spoiler_extension_time  = 2.0			//Seconds
spoilerons_available    = 1                     //Spoilerons Available?
aileron_to_spoileron_gain = 3                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10                //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate
auto_spoiler_available   = 1
positive_g_limit_flaps_up  =  4.0               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=  3.0               //Design G load tolerance (positive, flaps down) 
negative_g_limit_flaps_up  = -3.0               //Design G load tolerance (negative, flaps up) 
negative_g_limit_flaps_down= -2.0               //Design G load tolerance (negative, flaps down) 
load_safety_factor         =  1.5               //Design G load safety factor 

[Reference Speeds]
flaps_up_stall_speed    = 140.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 112.0                 //Knots True (KTAS)
cruise_speed            = 505.0                 //Knots True (KTAS)
max_mach                = 0.92
max_indicated_speed     = 278.0                 //Red line (KIAS)

[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   = 2                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 1.0                                  // 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 = 1.0
aileron_effectiveness  = 1.0
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                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -107.5, -69.5,  -6.9                 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -76.0, -38.9, -10.4                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = -76.0,  38.9, -10.4                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 = -107.5,  69.5,  -6.9                 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar        = 1.0                   //Scalar for fuel flow efficiency
min_throttle_limit = -0.25;                     //Minimum percent throttle.  Generally negative for turbine reverser

[TurbineEngineData]
fuel_flow_gain          = 0.002                 //Gain on fuel flow
inlet_area              = 60.0                  //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 29920                 //RPM, second stage compressor rated value
static_thrust           = 56750                 //Lbs, max rated static thrust at Sea Level
afterburner_available   = 0                     //Afterburner available?
reverser_available      = 1                     //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.40

[jet_engine]
thrust_scalar = 1.0

[autopilot]
autopilot_available             = 1
flight_director_available       = 1
default_vertical_speed          = 1800.0
autothrottle_available          = 1
autothrottle_arming_required    = 1
autothrottle_max_rpm            = 99
autothrottle_takeoff_ga         = 1
pitch_takeoff_ga                = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.05
nav_proportional_control=16.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control  = 18.0 
gs_integrator_control    = 0.33
gs_derivative_control    = 0.00
gs_integrator_boundary   = 0.70
gs_derivative_boundary   = 0.00
yaw_damper_gain = 1.0

[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   = 25.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 1.0  //Brake scalar
auto_brakes = 4
hydraulic_system_scalar = 1  //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure

[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 = -18.55, -2.0, 11.0              ; 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, 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
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

[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1

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

[altimeters]
altimeter.0=1
altimeter.1=1

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

[vacuum_system]
//Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
max_pressure=5.150000
vacuum_type=2

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[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

[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
stick_shaker=1

[deice_system]
structural_deice_type=1     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots




