[fltsim.0]
title=737-300
sim=Boeing737-400
model=
panel=
sound=
texture=KLM
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=
atc_airline=
atc_flight_number=
ui_manufacturer=Boeing
ui_type=
ui_variation=KLM
description=From the most successful family of jetliners ever built comes the 737-400. This can be your entry into virtual airline flying. Whether you're making short-haul or longer domestic flights, the 737-400 is a versatile and efficient airplane. See the Aircraft Information section of Help for tips on flying this aircraft.

[fltsim.1]
title=Boeing 737-300 Transaero
sim=Boeing737-400
model=
panel=
sound=
texture=transaero
visual_damage=1
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=EI-CXN
atc_airline=Transaero
atc_flight_number=
ui_manufacturer=Boeing
ui_type=737-300
ui_variation=Transaero
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.

[fltsim.2]
title=Boeing 737-300 KLD
sim=Boeing737-400
model=
panel=
sound=
texture=KLD
visual_damage=1
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=LE-O
atc_airline=KLD
atc_flight_number=
ui_manufacturer=Boeing
ui_type=737-300
ui_variation=KLD
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.

[General]
atc_type=
atc_model=
editable=1
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 Takeoff Weight\n138,500 lb         62,800 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=1.50                //Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]
max_gross_weight=138325                 // (pounds)
empty_weight=102640	                // (pounds)

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

max_number_of_stations=50

station_load.0=0.000000,0.000000,0.000000,0.000000

;Moments of Inertia
empty_weight_pitch_MOI=3500000
empty_weight_roll_MOI=2262183
empty_weight_yaw_MOI=837024
empty_weight_coupled_MOI=0

[flight_tuning]
cruise_lift_scalar=0.70
parasite_drag_scalar=0.20
induced_drag_scalar=1.10

ELEVATOR_EFFECTIVENESS=3.0 // ADJUST THIS VALUE TO MEET PITCHCRITERIA
AILERON_EFFECTIVENESS=3.0  // ADJUST THIS VALUE TO MEET ROLLCRITERIA

rudder_effectiveness=1.0
pitch_stability=2.0
roll_stability=1.5
yaw_stability=0.7
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=4.75, -16.1, -2.5 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=4.75,  16.1, -2.5 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.59      //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000

[TurbineEngineData]
fuel_flow_gain=0.002                          //Gain on fuel flow
inlet_area=19.6                               //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                            //RPM, second stage compressor rated value
static_thrust=22000                           //Lbs, max rated static thrust at Sea Level
afterburner_available=0                       //Afterburner available?
reverser_available=1                          //Thrust reverser available?

[jet_engine]
thrust_scalar=0.87

[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, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 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

//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]
point.0= 1.000, 31.729, 0.735, -8.800, 1181.100, 0.000, 1.070, 35.920, 0.800, 2.500, 0.900, 7.000, 7.000, 0.000, 0.000, 0.000 
point.1= 1.000, 31.729, -0.735, -8.800, 1181.100, 0.000, 1.070, 35.920, 0.800, 2.500, 0.900, 7.000, 7.000, 0.000, 0.000, 0.000 

point.2= 1.000, -7.933, -9.970, -9.800, 1574.800, 1.000, 1.640, 0.200, 1.000, 2.500, 0.900, 8.000, 8.000, 2.000, 0.000, 0.000 
point.3= 1.000, -7.933, 7.864, -9.800, 1574.800, 2.000, 1.640, 0.200, 1.000, 2.500, 0.900, 8.000, 8.000, 3.000, 0.000, 0.000 
point.4= 1.000, -7.933, -7.864, -9.800, 1574.800, 1.000, 1.640, 0.200, 1.000, 2.500, 0.900, 8.000, 8.000, 3.000, 0.000, 0.000 
point.5= 1.000, -7.933, 9.970, -9.800, 1574.800, 2.000, 1.640, 0.200, 1.000, 2.500, 0.900, 8.000, 8.000, 3.000, 0.000, 0.000

point.6= 2.000, 46.187, 0.000, 1.634, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 
point.7= 2.000, -53.635, 0.000, 7.877, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 
point.8= 2.000, 46.545, 0.000, 4.137, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000

max_number_of_points=21

static_pitch=0.62       //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.66   //feet, altitude of CG when at rest on the ground
gear_system_type=0

[Views]
eyepoint=38.5461192,-1.509168,5.8988784

[flaps.0] 	          //Trailing Edge Flaps
type=1                    // 1 - tail, 2 - lead
span-outboard=0.8         // 0.0 .. 1.0
extending-time=30         // seconds
flaps-position.0=0        // degrees
flaps-position.1=1        // degrees
flaps-position.2=2        // degrees
flaps-position.3=5        // degrees
flaps-position.4=11       // degrees
flaps-position.5=17       // degrees
flaps-position.6=25       // degrees
flaps-position.7=32       // degrees
flaps-position.8=40       // degrees
damaging-speed=250        // KIAS
blowout-speed=300         // KIAS
lift_scalar=1.3095
drag_scalar=-0.900
pitch_scalar=1.0
system_type=1             // Hydraulic

[flaps.1]                 // Flaps 15 adjustment
type=2                    // 1 - tail, 2 - lead
span-outboard=0.325         // 0.0 .. 1.0
extending-time=10          // seconds
flaps-position.0=0.0      // 
flaps-position.1=0.5      //
flaps-position.4=1.0      // 
damaging-speed=250        // KIAS
blowout-speed=300         // KIAS
lift_scalar=0.750
drag_scalar=-0.400
pitch_scalar=1.0
system_type=1             // Hydraulic

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1
// Com.2=1
Nav.1=1
Nav.2=1
Adf.1=1
Transponder.1=1
Marker.1=1

[LIGHTS] 
light.0 =3, -8.54, -49.74, 1.90, fx_navred , 
light.1 =3, -8.54, 49.74, 1.90, fx_navgre , 
light.2 =3, -8.94, -49.74, 1.90, fx_navred , 
light.3 =3, -8.94, 49.74, 1.90, fx_navgre , 
light.4 =3, -53.12, 0.00, 6.30, fx_navwhih , 
light.5 =2, -10.14, -49.84, 1.90, fx_strobe , 
light.6 =2, -10.14, 49.84, 1.90, fx_strobe , 
light.7 =1, 2.20, 0.00, 10.30, fx_beaconh ,
light.8 =3, -13.60, -49.22, 1.90, fx_navwhi , 
light.9 =3, -13.60, 49.22, 1.90, fx_navwhi , 

[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

[exits]
number_of_exits = 4
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.2                              ;Percent per second
exit_rate.2 = 0.4                               ;Percent per second
exit_rate.3 = 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=800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=94
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
use_no_default_pitch=1
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
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=0.100000
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
yaw_damper_gain=1.000000

[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=13.0                  //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=156.0                 //Knots True (KTAS)
full_flaps_stall_speed=110.0                 //Knots True (KTAS)
cruise_speed=477.0                 //Knots True (KTAS)
max_indicated_speed=340.000000
max_mach=0.820020

[folding_wings]
wing_fold_system_type = 4                       ;0=None
fold_rates = 0.12,0.11                          ;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
[brakes]
toe_brakes_scale=0.885037
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0