//
// TinMouse II Boeing 737-200 Panel
//
// Copyright 2003 - 2006 by the respective authors
//
// Released under the Artistic License v2
//
// Panel by Richard Probst and Bob Scott, et al.
//
// FDE by Gustavo "Omykron" Rodrigues
//
// Sounds by Christoffer Petersen
//
// This configuration for B737-200 models by Terry Gaff and Flight1

[fltsim.0]
title=Boeing 737-200 LAN Chile
sim=737-200adv
model=
panel=
sound=
texture=CVG
kb_checklists=Boeing737-200_check
kb_reference=Boeing737-200_ref
atc_id=CC-CVG
atc_airline=Lan Airlines		
atc_flight_number=291
ui_manufacturer=Boeing
ui_type=737-200 Advanced	
ui_variation=Lan Airlines CC-CVG
description="Boeing 737-247 ADV with JT8D-17R engines rated at 16,400 lbs thrust each\n. Repaint by Franco Zunino S.

[fltsim.1]
title=Boeing 737-200 LAN Argentina
sim=737-200adv
model=
panel=
sound=
texture=BBM
kb_checklists=Boeing737-200_check
kb_reference=Boeing737-200_ref
atc_id=LV-BBM
atc_airline=Lan Airlines		
atc_flight_number=291
ui_manufacturer=Boeing
ui_type=737-200 Advanced	
ui_variation=Lan Airlines LV-BBM
description="Boeing 737-247 ADV with JT8D-17R engines rated at 16,400 lbs thrust each\n. Repaint by Franco Zunino S.

//
// Insert other [Fltsim.xxx] aircraft headers here
//


[General]
atc_type=BOEING 
atc_model=B732 
performance=Cruise Speed\t.72 - .78 MachMaximum Range\t2,100 nmService Ceiling\t35,000 ftMax Takeoff Weight124,000 lbSeating\t\t112 to 118Cargo Capacity\txxxx CU ft 
editable=0 
Category=airplane

[CameraDefinition.0]
Title=Ventanilla del lado derecho
Guid={54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC}
Description=Vista del ala derecha desde la cabina de pasajeros
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=3.2, 1.8, -5
InitialPbh=5, 0, 100
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title=Ventanilla del lado izquierdo
Guid={0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description=Vista del ala izquierda desde la cabina de pasajeros
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=-3.2, 1.8, -5
InitialPbh=5, 0, 260
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title=Tren de aterrizaje
Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description=Vista del tren de aterrizaje y de los flaps internos del ala izquierda
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.52
ShowWeather=Yes
InitialXyz=-3.3, -1.8, -11
InitialPbh=0, 0, 17
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.3]
Title=Cola
Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description=Vista hacia adelante desde la parte posterior del aparato
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.75
ShowWeather=Yes
InitialXyz=0, 6.5, -55.0
InitialPbh=5, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.4]
Title=Ala derecha
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Vista desde el extremo del ala derecha hacia la cabina
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=30.8, 1.6, 4.0
InitialPbh=6, 0, 270
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum

[CameraDefinition.5]
Title=Ala izquierda
Guid={f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description=Vista desde el extremo del ala izquierda hacia la cabina
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=-30.8, 1.6, 4.0
InitialPbh=6, 0, 90
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=No
ClipMode=Minimum

[CameraDefinition.001]
Title=Asiento derecho
Guid={8ff6c134-098d-409f-baec-caba3f683f98}
Origin=Virtual Cockpit
MomentumEffect=YES
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=YES
AllowZoom=TRUE
InitialZoom=.6
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.94, 0.0, 0.0
InitialPbh=2, 0, 0

[CameraDefinition.002]
Title=Consola central
Guid={195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin=Virtual Cockpit
MomentumEffect=No
SnapPbhAdjust=None
SnapPbhReturn=False
PanPbhAdjust=None
PanPbhReturn=False
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.9
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.45, 0.30, -0.15
InitialPbh=84.2, 0, 0

[CameraDefinition.003]
Title=Controles del motor
Guid={a5741a54-ea6d-4580-9709-c99161e38a83}
Origin=Virtual Cockpit
MomentumEffect=No
SnapPbhAdjust=None
SnapPbhReturn=False
PanPbhAdjust=None
PanPbhReturn=False
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.9
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.45, 0.10, 0.35
InitialPbh=85.0, 0, 0

[CameraDefinition.004]
Title=Panel superior
Guid={4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin=Virtual Cockpit
MomentumEffect=No
SnapPbhAdjust=None
SnapPbhReturn=False
PanPbhAdjust=None
PanPbhReturn=False
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.7
SmoothZoomTime=2.0
ZoomPanScalar=1.15
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.47, -0.62, -0.4
InitialPbh=-58.0, 0, 0

[pitot_static]
vertical_speed_time_constant=999
pitot_heat=1.000000

[weight_and_balance]
max_gross_weight = 117000
empty_weight = 61890
reference_datum_position = 0.0, 0.0, 0.0
empty_weight_CG_position = 1.20, 0, 0
empty_weight_pitch_MOI = 571131
empty_weight_roll_MOI = 384600
empty_weight_yaw_MOI = 930732
empty_weight_coupled_MOI = 24000
max_number_of_stations = 30

station_load.0 = 165, 43.5, -1.36, 5.5, Captain
station_load.1 = 165, 43.5, 1.361, 5.5, First Officer
station_load.2 = 165, 36, -3, 4, Flight Attendant
station_load.3 = 165, 36, -1.44, 4, Flight Attendant
station_load.4 = 660, 30, 0, 4, 1A to 1F  //6 seats per row  660 = 4 of 6 occupied per row x 165
station_load.5 = 660, 27, 0, 4, 2A to 2F
station_load.6 = 660, 24, 0, 4, 3A to 3F
station_load.7 = 660, 21, 0, 4, 4A to 4F
station_load.8 = 660, 18, 0, 4, 5A to 5F
station_load.9 = 660, 15, 0, 4, 6A to 6F
station_load.10 = 660, 12, 0, 4, 7A to 7F
station_load.11 = 660, 9, 0, 4, 8A to 8F
station_load.12 = 660, 6, 0, 4, 9A to 9F
station_load.13 = 660, 2, 0, 4, 10A to 10F
station_load.14 = 660, -1, 0, 4, 11A to 11F
station_load.15 = 660, -4, 0, 4, 12A to 12F
station_load.16 = 660, -7, 0, 4, 13A to 13F
station_load.17 = 660, -10, 0, 4, 14A to 14F
station_load.18 = 660, -13, 0, 4, 15A to 15F
station_load.19 = 660, -16, 0, 4, 16A to 16F
station_load.20 = 660, -19, 0, 4, 17A to 17F
station_load.21 = 660, -22, 0, 4, 18A to 18F
station_load.22 = 660, -25, 0, 4, 19A to 19F
station_load.23 = 660, -28, 0, 4, 20A to 20F
station_load.24 = 165, -33, -3, 4, Flight Attendant
station_load.25 = 165, -33, -1.44, 4, Flight Attendant
station_load.26 = 1200, 27, 0, -0.98, Cargo Hold 1FWD //Maximum 2146 lbs
station_load.27 = 2000, 18, 0, -0.98, Cargo Hold 2FWD //Maximum 3340 lbs
station_load.28 = 1700, -7, 0, -0.98, Cargo Hold 1AFT //Maximum 4040 lbs
station_load.29 = 1500, -16, 0, -0.98, Cargo Hold 2AFT //Maximum 3459


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 1,    8.3558,    0.0000,   9.4058, fx_beacon,
light.1 = 1,   11.3558,    0.0000,  -3.9672, fx_beacon,
light.2 = 3,  -13.1086,  -46.3622,   2.5446, fx_navred ,
light.3 = 3,  -13.1086,   46.3622,   2.5446, fx_navgre ,
light.4 = 3,  -48.5807,    0.0000,   7.1568, fx_navwhi ,
light.5 = 3,  -17.3041,  -46.1595,   2.3199, fx_navwhi ,
light.6 = 3,  -17.3041,   46.1595,   2.3199, fx_navwhi ,
light.7 = 2,  -12.5919,  -46.2687,   2.5669, fx_strobeh,
light.8 = 2,  -12.5919,   46.2687,   2.5669, fx_strobeh,


[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.64
engine.0 = 0, -17, -2.5
engine.1 = 0, 17, -2.5
min_throttle_limit=-0.25

[smokesystem]
// lon/vert/lat
smoke.0 = -16.5, -2.5, -17, fx_smoke_JT8D.fx
smoke.1 = -16.5, -2.5,  17, fx_smoke_JT8D.fx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
contrail = fx_contrail_l

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1

Center1 = 6.25, 0, -0.2, 2303.7, 0      // 15433 lbs max
LeftMain = 1.5, -9.6, -0.2, 1428.15, 0  //  9567 lbs max
RightMain = 1.5, 9., -0.2, 1428.15, 0 
electric_pump=0


[contact_points]
//static_pitch = -0.4
//static_cg_height = 8.00 
//max_number_of_points = 8

//point.0 = 1,  37.94,  0.00, -7.95, 1574.80, 0, 1.216, 70.0, 0.55, 2.5, 0.639, 6.1, 6.3, 0, 180, 250
//point.1 = 1,  -1.81, -10.0, -8.85, 1574.80, 1, 1.5371, 0.0, 0.55 , 2.5, 0.639, 6.3, 6.7, 2, 180, 250
//point.2 = 1,  -1.81,  10.0, -8.85, 1574.80, 2, 1.5371, 0.0, 0.55 , 2.5, 0.639, 6.2, 6.6, 3, 180, 250
//point.3 = 2,   5.66, -48.45, 3.00, 787.80, 0. 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0, 0
//point.4 = 2,   5.66, 48.45, 3.00, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0, 0
//point.5 = 2, -44.66, 0.00, 7.60, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0, 0
//point.6 = 2,  58.94, 0.00, 1.75, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0, 0
//point.7 = 2, -15.76, 0.00, -2.30, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0, 0

//gear_system_type=0

static_pitch = -0.4
static_cg_height = 7.45
max_number_of_points = 8
point.0 = 1.000,   37.94,   0.0000,  -7.6000,  900.00, 0.000,  1.000, 78.000, 0.3047, 1.900, 0.867, 4.600, 4.5, 0, 285, 310
point.1 = 1.000,   -1.81,  -9.8248,  -9.5892, 1500.00, 1.000,  3.333,  0.000, 1.9410, 1.000, 0.879, 5.500, 5.9, 2, 285, 310
point.2 = 1.000,   -1.81,   9.8248,  -9.5892, 1500.00, 2.000,  3.333,  0.000, 1.9410, 1.000, 0.879, 5.500, 5.9, 3, 285, 310
point.3 = 2.000,    5.66, -48.4500,   3.0000,  787.80, 0. 0.0, 0.000,  0.000, 0.0000, 0.000, 0.000, 0.000, 5.0, 0, 0
point.4 = 2.000,    5.66,  48.4500,   3.0000,  787.80, 0, 0.0, 0.000,  0.000, 0.0000, 0.000, 0.000, 0.000, 6.0, 0, 0
point.5 = 2.000,  -44.66,   0.0000,   7.6000,  787.80, 0, 0.0, 0.000,  0.000, 0.0000, 0.000, 0.000, 0.000, 9.0, 0, 0
point.6 = 2.000,   58.94,   0.0000,   1.7500,  787.80, 0, 0.0, 0.000,  0.000, 0.0000, 0.000, 0.000, 0.000, 4.0, 0, 0
point.7 = 2.000,  -15.76,   0.0000,  -2.3000,  787.80, 0, 0.0, 0.000,  0.000, 0.0000, 0.000, 0.000, 0.000, 4.0, 0, 0
gear_system_type=0

[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
wing_area = 980.000
wing_span = 93.000
wing_root_chord = 10.54
wing_dihedral = 0.000
wing_incidence = 1
wing_twist = 0
oswald_efficiency_factor = 0.77
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 4.6376
wing_pos_apex_vert = 0
htail_area = 312.00
htail_span = 30.000
htail_pos_lon = -40.0
htail_pos_vert = 7.112
htail_incidence = 1.50
htail_sweep = 35.000
vtail_area = 224.000
vtail_span = 22.5
vtail_sweep = 0.000
vtail_pos_lon = -37
vtail_pos_vert = 9.25
elevator_area = 70.46
aileron_area = 13.4
rudder_area = 56.2
elevator_up_limit = 22.00
elevator_down_limit = 18.00
aileron_up_limit = 30.000
aileron_down_limit = 20.000
rudder_limit = 40.000
elevator_trim_limit = 17.000
spoiler_limit = 60.000
aileron_to_spoileron_gain = 3.00
min_ailerons_for_spoilerons = 12.50
min_flaps_for_spoilerons = 0.0000
spoilerons_available = 1
auto_spoiler_available=1
spoiler_extension_time=1.500000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000

[electrical]
max_battery_voltage = 28
generator_alternator_voltage = 28
max_generator_alternator_amps = 400
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 0, 5, 17
pitot_heat = 0, 2, 17
additional_system = 1, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 2, 20, 17
starter2 = 2, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[flight_tuning]
cruise_lift_scalar=1.00 
parasite_drag_scalar=1.00 
induced_drag_scalar=1.00 
elevator_effectiveness=1.00 
aileron_effectiveness=1.000 
rudder_effectiveness=1.000 
pitch_stability=1.0 
roll_stability=1.500 
yaw_stability=1.000 
elevator_trim_effectiveness=1.00 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 

[gear_warning_system]
gear_warning_available=1	//Normal
pct_throttle_limit=0.1		//Percent throttle that activates warning
flap_limit_idle=1.0		//Flap angle that activates warning at idle
flap_limit_power=15.0		//Flap angle that activates warning at above idle

[brakes]
parking_brake=1		//Parking brake available
toe_brakes_scale=0.645	//Brake scalar
auto_brakes=4

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

[Views]
eyepoint=44.45, -2.25, 6.25   //(feet) longitudinal, lateral, vertical distance from reference datum

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1 
Com.1=1, 0 
Com.2=1, 0 
Nav.1=1, 0, 1 
Nav.2=1, 0, 0 
Adf.1=1 
Adf.2=1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
direction_indicator.0=3,0 //Electric-Mag gyros 

[attitude_indicators]
attitude_indicator.0=2,2

[turn_indicators]
turn_indicator.0=1,0

[Airspeed_indicators]
airspeed_indicator.0=0.9826, 0.0 //Calibrates IAS to CAS

[exits]			//Exits
number_of_exits=2
exit_rate.0=0.2                               ;Percent per second
exit_rate.1=0.2                               ;Percent per second

[TailHook]		//Leading Flaps Landing Lights
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=0.7

[folding_wings]		//Ground Spoilers
wing_fold_system_type = 4                       ;0=None
fold_rates = 3.0,3.0                            ;Percent per second

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=2500 
autothrottle_available=1 
autothrottle_arming_required=0
autothrottle_max_rpm=100
autothrottle_takeoff_ga=1
pitch_takeoff_ga=12 
max_pitch=10.0
max_pitch_acceleration=2.0
max_pitch_velocity_lo_alt=3.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=15000.0
max_pitch_velocity_hi_alt_breakpoint=25000.0
max_bank=32.0
max_bank_acceleration=2.0
max_bank_velocity=3.0
max_throttle_rate=5.0
nav_proportional_control=10.00
nav_integrator_control=0.0 //0.1
nav_derivative_control=0.0
nav_integrator_boundary=0.50
nav_derivative_boundary=0.00
gs_proportional_control=25.00
gs_integrator_control=1.00
gs_derivative_control=0.00
gs_integrator_boundary=0.50
gs_derivative_boundary=0.00
yaw_damper_gain=1.0
use_no_default_pitch=1
default_bank_mode=2
default_pitch_mode=0

[Reference Speeds]
flaps_up_stall_speed=175.000 
full_flaps_stall_speed=140.000 
cruise_speed=430.000 
max_mach=0.84
max_indicated_speed=350				//Red line (KIAS)

[stall_warning]
type=1
stick_shaker=1


[Flaps.0]   // trailing edge flaps - Inboard flaps between root chord wing and turbine
type=1
span-outboard=0.800
extending-time=40.000
system_type=1
damaging-speed=250.000
blowout-speed=280.000
lift_scalar=0.40
drag_scalar=0.25
pitch_scalar=1.250
flaps-position.0=0.000
flaps-position.1=1.000
flaps-position.2=2.000
flaps-position.3=5.000
flaps-position.4=10.000
flaps-position.5=15.000
flaps-position.6=25.000
flaps-position.7=30.000
flaps-position.8=40.000

[Flaps.1]   // trailing edge flaps - outboard flaps between turbine and tip chord wing
type=1
span-outboard=0.800
extending-time=40.000
system_type=1
damaging-speed=250.000
blowout-speed=280.000
lift_scalar=0.50
drag_scalar=0.25
pitch_scalar=1.450
flaps-position.0=0.000
flaps-position.1=1.000
flaps-position.2=2.000
flaps-position.3=5.000
flaps-position.4=10.000
flaps-position.5=15.000
flaps-position.6=25.000
flaps-position.7=30.000
flaps-position.8=40.000

[Flaps.2] // leading edge Slats setting - Inboard flaps between root chord wing and turbine
type= 2
span-outboard= 0.800
extending-time=15.000
system_type= 1
damaging-speed= 280.000
blowout-speed= 320.000
lift_scalar= 0.50
drag_scalar= 0.10
pitch_scalar=0.10
flaps-position.0= 0.000
flaps-position.1= 0.500
flaps-position.4= 1.000

[Flaps.3] // leading edge flap setting - outboard devices between turbine and tip chord wing
type= 2
span-outboard= 0.800
extending-time=5.000
system_type= 1
damaging-speed= 280.000
blowout-speed= 320.000
lift_scalar= 0.50
drag_scalar= 0.20
pitch_scalar=0.500
flaps-position.0= 0.000
flaps-position.1= 1

[TurbineEngineData]
fuel_flow_gain=0.002 
inlet_area=9.850 
rated_N2_rpm=12250  //HPC maximum RPM
static_thrust=17000  //Static Thrust for JT8D-17 
afterburner_available=0 
reverser_available=1 

[jet_engine]
thrust_scalar=1 

[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0