[fltsim.0]
title=Boeing 737-500 Alania
sim=B737_500
model=
panel=
sound=
texture=AL
visual_damage=1
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=42338
atc_airline=ALANIA
atc_flight_number=42338
ui_manufacturer=Boeing
ui_type=737-500
ui_variation=ALANIA
description=One should hardly be surprised that the world's most prolific manufacturer of commercial aircraft is also the producer of the world's most popular jetliner. The 737 became the best-selling commercial jetliner worldwide when orders for it hit 1,831 in June 1987 (surpassing Boeing's own 727 as the previous champ). However, it wasn't always that way\s in the first few years of production, there were so few orders that Boeing considered canceling the program. They didn't, and the airplane has more than proven itself in over three decades of service.


[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -12.5, -50.8, 1.9, fx_navred
light.1 = 3, -12.9, -50.8, 1.9, fx_navred
light.2 = 3, -12.5, 50.8, 1.9, fx_navgre
light.3 = 3, -12.9, 50.8, 1.9, fx_navgre
light.4 = 3, -17.2, 50.65, 1.9, fx_navwhi
light.5 = 3, -17.2, -50.65, 1.9, fx_navwhi
light.6 = 2, -13, -50.8, 1.9, fx_strobe
light.7 = 2, -13, 50.8, 1.9, fx_strobe
light.8 = 2, -52, 0, 6.4, fx_strobe
light.9 = 3, -52, 0, 6.4, fx_navwhi
light.10 = 1, 7.1, 0, 9.6, fx_beaconb
light.11 = 1, 5.50, 0.00, -4.90, fx_beaconh,
light.12 = 4, 44.0000, 0.00, 2.2, fx_vclighth ,



[contact_points]
point.0=1.000, 36.137, 0.000, -8.832, 1181.1, 0, 1.442, 78.0, 0.6, 1.372, 0.9, 4.0, 4.0, 0, 220.0, 250.0
point.1=1.000, -9.410, -9.919, -9.827, 1574.8, 1, 1.442,  0.00, 1.0, 1.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0
point.2=1.000, -9.410, 9.919 -9.827, 1574.8, 2, 1.442,  0.00, 1.0, 1.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0

point.3=2.000, 42.747, 0.000, 4.243, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //Nose scrape
point.4=2.000, -33.316, 0.000, 2.421, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //Tail scrape
point.5=2.000, -13.585, -50.333, 2.08, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Left wing scrape
point.6=2.000, -13.585, 50.333, 2.08, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Right wing scrape

static_pitch=-0.900000
static_cg_height=9.919
gear_system_type=0

[Views]
eyepoint=34.129659,-1.307210,3.614050

[exits]
number_of_exits=2
exit_rate.0 = 0.28
exit_rate.1 = 0.28

[TailHook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=0.7

[folding_wings]
wing_fold_system_type=4
fold_rates=0.12,0.11

////////////////////////////////

[GeneralEngineData]
engine_type = 1
Engine.0 = 4.75, -16.1, -4.5
Engine.1 = 4.75,  16.1, -4.5
fuel_flow_scalar = 1
min_throttle_limit = -0.25
max_contrail_temperature = -30

[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 19.6
rated_N2_rpm = 29920
static_thrust = 18920	/CFM56-3C1 @ 20,000
afterburner_available = 0
reverser_available = 1

[jet_engine]
thrust_scalar = 1.0

////////////////////////////////

[General]
atc_type=BOEING
atc_model=B734
editable=0
performance="Cruise Speed        \n477 kts              550 mph         885 km\/h\n\nEngines     \nCFM56-3C1\n\nMaximum Range    \n2,059 nm          2,370 mi          3,810 km\n\nService Ceiling     \n36, 089 ft         11,000 m\n\nFuel Capacity       \n5,311 U.S. gal     20,104 L\n\nEmpty Weight-Standard       \n76,180 lb           34,550 kg\n\nMaximum Gross Weight\n150,000 lb         68,039 kg\n\nLength     \n120 ft                 36.45 m\n\nWingspan     \n94 ft, 9 in           25.9 m\n\nHeight        \n36.5 ft               11.13 m\n\nSeating      \nSeats 147 to 168\n\nCargo Capacity    \n1,373 ft3            38.93 m3\n\n"

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]
max_gross_weight = 150000                      // (pounds)
empty_weight = 74170                           // (pounds)

reference_datum_position     =  0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -5, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

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  = 3172439
empty_weight_roll_MOI   = 2262183
empty_weight_yaw_MOI    = 3337024
empty_weight_coupled_MOI = 0

[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

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5,  17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2,  17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 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

[gear_warning_system]
gear_warning_available = 1
pct_throttle_limit =  0.1
flap_limit_idle    =  5.0
flap_limit_power   = 25.5

[brakes]
parking_brake = 1
toe_brakes_scale = 0.885

[hydraulic_system]
normal_pressure = 3000.0
electric_pumps  = 0
engine_map      = 1,1,0,0

[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 20                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 1                                    // degrees
flaps-position.2 = 2                                    // degrees
flaps-position.3 = 5                                    // degrees
flaps-position.4 = 10                                   // degrees
flaps-position.5 = 15                                   // degrees
flaps-position.6 = 25                                   // degrees
flaps-position.7 = 30                                   // degrees
flaps-position.8 = 40                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[flaps.1]       //Inboard Leading Edge Flaps
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 2                                    // seconds
flaps-position.0 = 0                                    // 
flaps-position.1 = 1.0                                  // 
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic


[flaps.2]       //Outboard Leading Edge Slat
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 3                                    // seconds
flaps-position.0 = 0                                    // 
flaps-position.1 = 0.5                                  // 
flaps-position.4 = 1.0                                  // 
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
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

[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

[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 = 1 

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

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

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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 90
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=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[fuel]
Center1    = 0,   0, 0, 2313, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  = -3, -19, 0, 1500, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3,  19, 0, 1500, 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=0

[airplane_geometry]
wing_area               = 1137.0                //Square feet
wing_span               = 94.75                 //Feet
wing_root_chord         = 18.0                  //Feet
wing_dihedral           = 6.2                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -0.5                  //Degrees
oswald_efficiency_factor= 0.75                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 25.0                  //Degrees, wing leading edge
wing_pos_apex_lon       = 8.0                   //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              = 338.0                 //Square feet
htail_span              = 41.7                  //Feet
htail_pos_lon           = -35.0                 //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             = 30.0                  //Degrees, horizontal tail leading edge
vtail_area              = 224.0                 //Square feet
vtail_span              = 20.0                  //Feet, tip to body
vtail_sweep             = 35.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -35.8                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 5.8                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 70.5                  //Square feet
aileron_area            = 26.9                  //Square feet
rudder_area             = 56.2                  //Square feet
elevator_up_limit       = 22.5                  //Degrees
elevator_down_limit     = 19.5                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 20.0                  //Degrees
rudder_limit            = 26.0                  //Degrees
elevator_trim_limit     = 20.0                  //Degrees
spoiler_limit           = 60.0                  //Degrees
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

[Reference Speeds]
flaps_up_stall_speed    = 142.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 113.0                 //Knots True (KTAS)
cruise_speed            = 477.0                 //Knots True (KTAS)
max_mach                = 0.82
max_indicated_speed     = 340                   //Red line (KIAS)

[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