[fltsim.0]
title=50N Boeing 737-400 KLM
sim=B737-4A00A
model=
panel=
sound=
texture=KLM
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=PHBTF
atc_airline=
atc_flight_number=1123
ui_manufacturer=Boeing FiftyNorth/feelThere
ui_type=737-400
ui_variation=KLM
description=Boeing 737-400 Pilot in Command/FiftyNorth merge. \nVisual model © FiftyNorth Simulation 2004-2005. www.fiftynorth.com \nPanel and flight dynamics developed by www.feelThere.com \nPublished by Wilco Publishing www.wilcopub.com \nPlease set general realism slider to maximum.

[fltsim.1]
title=50N Boeing 737-400 QANTAS
sim=B737-4A00A
model=
panel=
sound=
texture=QANTAS
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=n3pok
atc_airline=QANTAS
atc_flight_number=1123
ui_manufacturer=Boeing FiftyNorth/feelThere
ui_type=737-400
ui_variation=QANTAS
description=Boeing 737-400 Pilot in Command/FiftyNorth merge. \nVisual model © FiftyNorth Simulation 2004-2005. www.fiftynorth.com \nPanel and flight dynamics developed by www.feelThere.com \nPublished by Wilco Publishing www.wilcopub.com \nPlease set general realism slider to maximum.

[fltsim.2]
title=50N Boeing 737-400 Garuda Indonesia
sim=B737-4A00A
model=
panel=
sound=
texture=GARUDA
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=PKGWY
atc_airline=Garuda
atc_flight_number=7125
ui_manufacturer=Boeing FiftyNorth/feelThere
ui_type=737-400
ui_variation=Garuda Indonesia
description=Boeing 737-400 Pilot in Command/FiftyNorth merge. \nVisual model © FiftyNorth Simulation 2004-2005. www.fiftynorth.com \nPanel and flight dynamics developed by www.feelThere.com \nPublished by Wilco Publishing www.wilcopub.com \nPlease set general realism slider to maximum.

[General]
atc_type=BOEING
atc_model=B734
editable=0
performance="MTXW:                150,500 lbs                68,265 kgs\nMTOW:                150,000 lbs                68,038 kgs\nMLDW:                124,000 lbs                56,245 kgs\nMZFW:                117,000 lbs                53070 kgs\nOEW  :                  73,170 lbs                33,189 kgs"

[pitot_static]
vertical_speed_time_constant = 300                //Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]
max_gross_weight = 150000                      // (pounds)
empty_weight = 73170.000                       // (pounds)

reference_datum_position     =  0.0, 0.0, 0.0    // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -1.0, 0.0, 0.0   // (feet) longitudinal, lateral, vertical distance from specified datum
CG_forward_limit= 1.000
CG_aft_limit= 1.000

max_number_of_stations = 50

station_load.0="1000.0,    32.0,  0.0,  0.0, Pilots and Crew"
station_load.1="29000.0,  -0.5,  0.0,  0.0, Pax - Baggage"

//station_load.0 =   "170.0,  41.0, -1.5,	0.0, Pilot"              //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)        
//station_load.1 =   "170.0,  41.0,  1.5,	0.0, Co-Pilot"           //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
//station_load.2 =   "510.0,   0.0,  0.0,	0.0, Crew"               //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
//station_load.3 =  "1360.0,  25.5,  0.0,	0.0, First Class"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
//station_load.4 =  "8160.0,  11.0,  0.0,	0.0, Coach 3-10"         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
//station_load.5 =  "8160.0, -10.0,  0.0,	0.0, Coach 11-18"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
//station_load.6 =  "7140.0, -30.5,  0.0,	0.0, Coach 19-25"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
//station_load.7 = "10000.0,  20.5,  0.0,	0.0, Forward Baggage"    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
//station_load.8 =  "4000.0, -27.5,  0.0,	0.0, Aft Baggage"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

;Moments of Inertia
empty_weight_pitch_MOI  = 2200000
empty_weight_roll_MOI   = 2100000.000
empty_weight_yaw_MOI    = 1800000.000
empty_weight_coupled_MOI = 0.0

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.1
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.1
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 = -4.50, -16.083333,-2.500000          //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -4.50,  16.083333,-2.500000          //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.04                         //Scalar for fuel flow efficiency
min_throttle_limit = -0.29                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature = -30                  //Temperature (deg C) below which contrails may appear

[TurbineEngineData]
fuel_flow_gain = 0.003                          //Gain on fuel flow
inlet_area = 22.0                               //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920                            //RPM, second stage compressor rated value
static_thrust = 23500                           //Lbs, max rated static thrust at Sea Level
afterburner_available = 0                       //Afterburner available?
reverser_available = 1                          //Thrust reverser available?

[jet_engine]
thrust_scalar = 1.0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 200
electric_always_available = 1

                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 0 , 17.0
gear_motor         = 0, 0 , 17.0
autopilot          = 0, 0 , 17.0
avionics_bus       = 0, 0 , 17.0
avionics           = 0, 0 , 17.0
pitot_heat         = 0, 0 , 17.0
additional_system  = 0, 0 , 17.0
marker_beacon      = 0, 0 , 17.0
gear_warning       = 0, 0 , 17.0
fuel_pump          = 0, 0 , 17.0
starter1           = 0, 0 , 17.0
starter2           = 0, 0 , 17.0
light_nav          = 0, 0 , 17.0
light_beacon       = 0, 0 , 17.0
light_landing      = 0, 0 , 17.0
light_taxi         = 0, 0 , 17.0
light_strobe       = 0, 0 , 17.0
light_panel        = 0, 0 , 17.0
light_cabin        = 0, 0 , 17.0
auto_brakes        = 0, 0 , 17.0
standby_vacuum     = 0, 0 , 17.0
hydraulic_pump     = 0, 0 , 17.0
fuel_transfer_pump = 0, 0 , 17.0
light_recognition  = 0, 0 , 17.0
light_wing         = 0, 0 , 17.0
light_logo         = 0, 0 , 17.0
directional_gyro   = 0, 0 , 17.0
directional_gyro_slaving = 0, 0 , 17.0

        //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)

[contact_points]
//------0-----1--------2--------3----------4---5---6-------7-----8-----9----10----11---12--13----14-----15--
point.0=1,  40.00,    0.0000, -7.5500, 2574.8, 0, 1.095, 55.00, 0.10, 5.20, 0.60, 8.0, 8.0, 0, 220.0, 280.0
point.1=1,  -6.8470, -8.5800, -7.8500, 3574.8, 1, 1.650,  0.00, 0.60, 0.60, 0.60, 6.9, 7.9, 2, 220.0, 280.0
point.2=1,  -6.8470,  8.5800, -7.8500, 3574.8, 2, 1.650,  0.00, 0.60, 0.60, 0.60, 7.5, 7.1, 3, 220.0, 280.0

point.3=2, -14.17, -47.33,  0.00,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -14.17,  47.33,  0.00,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -54.00,   0.00,  2.83,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2,  42.67,   0.00, -3.75,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0

max_number_of_points = 21

static_pitch = -0.10      //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height = 7.8    //feet, altitude of CG when at rest on the ground
gear_system_type=1        //Hydraulic	

[gear_warning_system]
gear_warning_available = 0        //Normal
pct_throttle_limit =  0.099976    //Percent throttle that activates warning
flap_limit_idle    =  0.974028    //Flap angle that activates warning at idle
flap_limit_power   = 24.637185    //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1         //Parking brake available
toe_brakes_scale = 0.50   //Brake scalar

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

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1=    0.5,   0.0, 0.0, 2311.0, 0.0
LeftMain=  -1.5, -11.0, 0.0, 1500.0, 0.0
RightMain= -1.5,  11.0, 0.0, 1500.0, 0.0
fuel_type=2                                 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=2
electric_pump=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, 1
Adf.1         = 1
Adf.2         = 1
Transponder.1 = 1
Marker.1      = 1

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -18.011664, -47.3237064,  3.215184, fx_navred ,
light.1 = 3, -18.011664, 47.3237064,  3.215184, fx_navgre ,
light.2 = 2, -62.3581656,   0.00,  7.4506968, fx_strobeh ,
light.3 = 2, -17.3193432, -47.3695088,  3.1954992, fx_strobeh ,
light.4 = 2, -17.3193432,  47.3695088,  3.1954992, fx_strobeh ,
light.5 = 2,  7.00,   0.00, -4.10, fx_beaconb ,
light.6 = 1,  4.1,   0.00,  9.9, fx_beaconh ,
light.7 = 4,  44.41,   0.00,  3.50, fx_vclighth ,
light.8 = 3,   -22.20, -46.97,3.175, fx_navwhi
light.9 = 3,   -22.20,  46.97,3.175, fx_navwhi

[autopilot]
autopilot_available=1 // A/p is all custom and implemented outside this file...but DO NOT change these settings
flight_director_available=0
autothrottle_available=0
yaw_damper_gain=0.0
default_vertical_speed=1800.000000
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.08
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000

[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

[airplane_geometry]
wing_area               = 1137.0                //Square feet
wing_span               = 94.75                 //Feet
wing_root_chord         = 11.250000             //Feet
wing_dihedral           = 6.218262              //Degrees
wing_incidence          = -2.8                  //Degrees
wing_twist              = -1.999512             //Degrees
oswald_efficiency_factor= 1.089813              //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 25.000000             //Degrees, wing leading edge
wing_pos_apex_lon       = 13                    //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 337.000000            //Square feet
htail_span              = 41.750000             //Feet
htail_pos_lon           = -91.162000            //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 5.5770000             //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.000000              //Degrees
htail_sweep             = 30.000000             //Degrees, horizontal tail leading edge
vtail_area              = 249.000000            //Square feet
vtail_span              = 17.991665             //Feet, tip to body
vtail_sweep             = 0.000000              //Degrees, vertical tail leading edge
vtail_pos_lon           = -48.13333             //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 9.843                 //Feet, vertical distance from reference point, positive going up
elevator_area           = 70.500000             //Square feet
aileron_area            = 26.800000             //Square feet
rudder_area             = 56.200000             //Square feet
elevator_up_limit       = 27                    //Degrees
elevator_down_limit     = 22                    //Degrees
aileron_up_limit        = 19.480565             //Degrees //by50N
aileron_down_limit      = 14.896903             //Degrees
rudder_limit            = 26                    //Degrees
elevator_trim_limit     = 19                    //Degrees
spoiler_limit           = 58                    //Degrees
spoilerons_available    = 1                     //Spoilerons Available?
aileron_to_spoileron_gain = 2.00                //Aileron to spoileron gain
min_ailerons_for_spoilerons = 6.00              //Degrees
min_flaps_for_spoilerons = 0.0                  //Minimum flap handle position when spoilerons activate

[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

[flaps.0]       //Trailing Edge Flaps (dummy - no visual - tune here)
type=1                                    // 1 - trailing, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=35                                  // seconds
flaps-position.0=0.000, 0.000                      // degrees
flaps-position.1=1.000, 0.000                      // degrees
flaps-position.2=2.000, 0.000                      // degrees
flaps-position.3=5.000, 0.000                      // degrees
flaps-position.4=10.000, 0.000                     // degrees
flaps-position.5=15.000, 0.000                     // degrees
flaps-position.6=25.000, 0.000                     // degrees
flaps-position.7=30.000, 0.000                     // degrees
flaps-position.8=40.000, 0.000                     // degrees
damaging-speed=260                                 // KIAS
blowout-speed=320                                  // KIAS
lift_scalar=1.1
drag_scalar=1.0
pitch_scalar=1.0
system_type=1

[flaps.1]       //Trailing Edge Flaps (outboard - visual effect only)
type=1                                    // 1 - trailing, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=35                                  // seconds
flaps-position.0=0                                 // degrees
flaps-position.1=3                                 // degrees
flaps-position.2=8                                 // degrees
flaps-position.3=13                                // degrees
flaps-position.4=18                                // degrees
flaps-position.5=22                                // degrees
flaps-position.6=28                                // degrees
flaps-position.7=33                                // degrees
flaps-position.8=40                                // degrees
damaging-speed=260                                 // KIAS
blowout-speed=320                                  // KIAS
lift_scalar=0.0
drag_scalar=0.0
pitch_scalar=0.0
system_type=1                                       //Hydraulic

[flaps.2]       //Inboard Leading Edge Flaps
type=2                                    // 1 - trailing, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=2.000                               // seconds
system_type=1                                      //Hydraulic
damaging-speed=250                                 // KIAS
blowout-speed=300                                  // KIAS
flaps-position.0=0.000, 0.000                      // degrees
flaps-position.1=1.000, 0.000                      // degrees

[flaps.3]       //Outboard Leading Edge Slat
type=2                                    // 1 - trailing, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=4.000                               // seconds
system_type=1                                      //Hydraulic
damaging-speed= 250.000                            // KIAS
blowout-speed= 300.000                             // KIAS
//Slats are animated incorrectly on 50N model, here's a workaround
flaps-position.0=0.000, 0.000                      // flaps up
flaps-position.1=0.500, 0.000                      // flaps 1
flaps-position.2=0.500, 0.000                      // flaps 2
flaps-position.3=0.500, 0.000                      // flaps 5
flaps-position.4=1.000, 0.000                      // flaps 10

[Reference Speeds]
flaps_up_stall_speed    = 153.000000            //Knots True (KTAS)
full_flaps_stall_speed  = 122.400000            //Knots True (KTAS)
cruise_speed            = 428.0                 //Knots True (KTAS)
max_mach                = 0.825000
max_indicated_speed     = 345.000000            //Red line (KIAS)

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.1                               ;Percent per second

[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.12,0.11  

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

[Views]
//eyepoint=43.8, -2.0, 6.2   // feelThere settings
eyepoint=43.7, -1.31, 3.55   //(feet) longitudinal, lateral, vertical distance from reference datum

[stall_warning]
type=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=2,0

[airspeed_indicators]                //IAS adjustmet parameters
airspeed_indicator.0 = 0.9826, 0.0   //Appropriate values for Jet AC

[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