;-------------------------------------------------------------------------------

; #alert "alert text goes here - if uncommented, it will be displayed in a pop-up dialog  whever a project using this INI is opened"
; INI date: Feb 10, 2013 11:25PM PT

[MegaTune]
   MTversion      = 2.25 ; MegaTune itself; needs to match exec version.

   versionInfo    = "S"  ; Put this in the title bar.
   queryCommand   = "Q"  ; Verify against signature.
   signature      = "MSII Rev 2.92000   " ; MS-II sends a null at 20th byte.
                   ; 123456789.123456789.
tsWriteBlocks = on

;-------------------------------------------------------------------------------
;
; PREAMBLE
;
; There are several main sections (with brackets around the [section] heading) in this INI file:
;
; - Constants - this is divided into two pages (for recent MS-II code versions, 
;               at least). Page 1 is based on the source code inpram. structure
;               Page 2 is based on the source code in2ram. structure. All of the 
;               values are inputs sent from MegaTune to the MegaSquirt-II
; - Menu (& User Defined) - these define most of the mennus in MegaTune (except 
;                           those that are 'built-in' like the accel wizrd, etc.)
; - Curve Editor and Table Editor
; - Gauge Configuration
; - Front Page & RuntTime & Tuning Config
; - Burst Mode Config
; - Output Channels - this mirrors the outpc. structure from the source code. All 
;                     of the values are sent from MegaSquirt-II to MegaTune on the PC.
; - Datalog - select output channels to log on the PC hard drive
;
; Note: 
;       - To add an input variable to MegaTune, you need to add it to the inpram (or in2ram) 
;         structure in the MegaSquirt source code noting the correct offset (and recompile, 
;         of course), to the Constants section, and to one of the menus.
;       - To add an output variable to MegaTune (for monitoring, logging, or switching purposes),
;         you need to add it to the outpc structure in the source code, to the OuptChannels, and 
;         to the datalog section (and/or the gauge configurations, if you wish to see it directly 
;         in MegaTune). 
;
; In general, the respective notation for variables from the source code to the INI are:
;
;                         signed          unsigned      bytes    bits
;                         ------          --------      -----    ----
;             - char =      S08              U08          1       8
;             - int  =      S16              U16          2       16
;             - long =      S32              U32          4       32
;
; Where the maximum range is:
;
;                         signed           unsigned
;                         ------           --------
;             - char =   -128 to 127       0 to 255
;             - int  =   -32768 to 32767   0 to 65535
;             - long =   -2147483648       0 to 4294967295        
;                         to 2147483647
;
;----------------------------------------------------------------------------
; Temperature Limits and Settings Reference
;----------------------------------------------------------------------------

#unset EXPANDED_CLT_TEMP ; "Expanded Coolant Temperature Range"

; Below is a listing of all of the temperature ranges used throughout the INI for the MegaSquirt II.
;
; CELSIUS (Expanded/Normal):
;     Low limit: -40C/-40C
;     High limit: 300C/150C
;     Low danger: 65C/10C
;     Low warning: 93C/65C
;     High warning: 162C/93C
;     High danger: 176C/104C
;
; FAHRENHEIT (Expanded/Normal):
;     Low Limit: -40F/-40F
;     High limit: 600F/300F
;     Low danger: 150F/50F
;     Low warning: 200F/150F
;     High warning: 325F/200F
;     High danger: 350F/220F
;----------------------------------------------------------------------------

[ReferenceTables]

    tableWriteCommand 	= "t" ; 
    
    referenceTable = mafTableBurner, "Calibrate MAF Table..."
    	;topicHelp = "http://www.megamanual.com/mt29.htm#om"
        tableIdentifier = 003, "MAF Table"
        adcCount 	= 1024 	; length of the table
        bytesPerAdc 	= 2 	; using words
        scale		= 1 ; scale before sending to controller
        ;tableGenerator	= Generator Type, 		Label, xUnits, yUnits,  xLow, xHi,  yLow, yHi ; lows and Hi's are just default values, they will be user editable
    	;tableGenerator	= linearGenerator, "Custom Linear WB", "Volts","AFR",    1,   4,   9.7,  18.7
    	solutionsLabel	= "MAF Sensor"
    	solution	= "Ford Lightning MAF", 	{ table(adcValue, "maffactor_1L3F_Lightning.inc") }
		solution	= "Infiniti Q45 MAF", 		{ table(adcValue, "maffactor_Q45.inc") }
		solution	= "GM LT1/LS1/LS2 MAF", 	{ table(adcValue, "maffactor_lsx.inc") }

    referenceTable = canOutmsgBurner, "Configure CAN Outmsg"
    	;topicHelp = "http://www.megamanual.com/mt29.htm#outmsg"
        tableIdentifier = 010, "outmsg Table"       ; id in octal, 010 = table 8
        adcCount 	= 1024 	; length of the table
        bytesPerAdc 	= 1 	; using bytes
        scale		= 1 ; scale before sending to controller
        ;tableGenerator	= Generator Type, 		Label, xUnits, yUnits,  xLow, xHi,  yLow, yHi ; lows and Hi's are just default values, they will be user editable
    	;tableGenerator	= linearGenerator, "Custom Linear WB", "Volts","AFR",    1,   4,   9.7,  18.7
    	solutionsLabel	= "CAN Outmsg"
    	solution	= "CAN Outmsg", 	{ table(adcValue, "canOutmsg.inc") }


[Constants]

   ;----------------------------------------------------------------------------
   ; Constants Definition
   ; --------------------
   ;
   ; Scalar Values
   ; -------------
   ; The scaling and translation values are used as follows:
   ;    msValue   = userValue / scale - translate
   ;    userValue = (msValue + translate) * scale
   ;
   ; I've got no good way to handle a few of these things yet.
   ;
   ; Temperatures are fine, check out the Fielding IAC example (fastIdleTemp).
   ;
   ; The TPS stuff is a problem, because we have to modify the INI file for
   ; each TPS installation and again whenever we move the TPS...
   ;
   ; Array Values
   ; ------------
   ; Arrays are specified just like scalars, except that they have a "shape"
   ; entry in the fourth parameter.  The shape allows you to define lists or
   ; tables, for example [8] defines a list with eight values and [2x4] defines
   ; a table with eight values (two rows and four columns).  Tables may be
   ; stored in either "X-" or "Y-order."  X-order means that memory is laid
   ; out as follows:
   ;
   ;     [x1,y1] [x2,y1]...[xn,y1] [x1,y2]...
   ;
   ; Y-order would be
   ;
   ;     [x1,y1] [x1,y2]...[x1,yn] [x2,y1]...
   ;
   ; To use the TableEditor, you must define two lists and a table, and
   ; the lengths of the lists must correspond to the shape of the table.
   ;
   ; Bit Fields
   ; ----------
   ; Bits are numbered 0-7, the rightmost being bit zero.  The basic
   ; data word that stores bit fields must be unsigned.
   ;
   ; You need NOT supply the correct number of labels matching the
   ; number of bits you've specified (one bit requires 2 values, two
   ; bits requires 4 values and so on).  If you neglect to supply enough
   ; labels, they will be synthesized using the sequence "1", "2" and so
   ; on based upon their position in the sequence (the cltType and matType
   ; will end up with identical lists).
   ;
   ;----------------------------------------------------------------------------

   pageActivationDelay =  50 ; Milliseconds delay after burn command.
   blockReadTimeout    = 200 ; Milliseconds total timeout for reading page.

   endianness          = big
   nPages              = 2
   pageSize            = 994,            954
   pageIdentifier      = "\x00\x04",     "\x00\x05"
   burnCommand         = "b%2i",         "b%2i"
   pageReadCommand     = "r%2i%2o%2c",   "r%2i%2o%2c"
   pageValueWrite      = "w%2i%2o%2c%v", "w%2i%2o%2c%v"
   pageChunkWrite      = "w%2i%2o%2c%v", "w%2i%2o%2c%v"

   page = 1
   ;  name            = class,  type, offset,      shape,  units,       scale, translate,    lo,      hi, digits
      nCylinders      = bits  ,  U08,      0,      [0:3], "INVALID"                                              ; *
      no_skip_pulses  = scalar,  U08,      1,             "",         1.00000,   0.00000,  1.00,  255.00,      0 ; * (  1 byte)
      ICIgnCapture    = bits  ,  U08,      2,      [0:0], "Falling Edge", "Rising Edge"                          ; *
      ICCrankTrigger  = bits  ,  U08,      2,      [1:2], "Calculated", "Trigger Return", "Trigger Rise",    "INVALID" ; *
      ICIgnOption     = bits  ,  U08,      2,      [4:5], "Standard Coil Charge", "EDIS", "EDIS Multispark", "INVALID" ; *
      spkout_hi_lo    = bits  ,  U08,      3,      [0:0], "Going Low (Normal)", "Going High (Inverted)"          ; *
      max_coil_dur    = scalar,  U08,      4,             "msec",       0.10000,   0.00000,  1.00,    8.00,      1 ; * (  1 byte)
      max_spk_dur     = scalar,  U08,      5,             "msec",       0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte)
      dwellAcc        = scalar,  U08,      6,             "msec",       0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte)
      dwellVolts      = array ,  S08,      7,    [    5], "V",          0.10000,   0.00000,-12.80,   12.70,      1 ; * (  5 bytes)
      dwellDuration   = array ,  S08,     12,    [    5], "msec",       0.10000,   0.00000,-12.80,   12.70,      1 ; * (  5 bytes)
      RevLimOption    = bits  ,  U08,     17,      [0:1], "None", "Spark Retard", "Fuel Cut", "INVALID"          ; * (  1 byte)
      RevLimMaxRtd    = scalar,  U08,     18,             "deg",      0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte)
      PredOpt         = bits  ,  U08,     19,      [0:1], "Last Interval", "Alpha-Beta-Gamma Filter", "INVALID", "INVALID" ; *
      crankingRPM     = scalar,  S16,     20,             "RPM",      1.00000,   0.00000,  0.00,  3000.0,      0 ; * (  2 bytes)
      cold_adv_table  = array ,  S16,     22,    [   10], "deg",      0.10000,   0.00000,-10.00,   10.00,      1 ; * ( 20 bytes)
      triggerOffset   = scalar,  S16,     42,             "deg",      0.10000,   0.00000,-359.0,  359.00,      2 ; * (  2 bytes)
      RevLimRpm1      = scalar,  S16,     44,             "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * (  2 bytes)
      RevLimRpm2      = scalar,  S16,     46,             "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * (  2 bytes)
#if LAMBDA
      afrTable1       = array ,  U08,     48,    [12x12], "Lambda",  0.006803,   0.00000,  0.00,    2.00,      3 ; * (144 bytes)
      afrTable2       = array ,  U08,    192,    [12x12], "Lambda",  0.006803,   0.00000,  0.00,    2.00,      3 ; * (144 bytes)
#else
      afrTable1       = array ,  U08,     48,    [12x12], "AFR",      0.10000,   0.00000,  9.00,   20.00,      1
      afrTable2       = array ,  U08,    192,    [12x12], "AFR",      0.10000,   0.00000,  9.00,   20.00,      1
#endif
      wueBins         = array ,  U08,    336,    [   10], "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * ( 10 bytes)
      taeBins         = array ,  U08,    346,    [    4], "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  4 bytes)
      maeBins         = array ,  U08,    350,    [    4], "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  4 bytes)
      iacstepTable    = array ,  S16,    354,    [   10], "steps",    1.00000,   0.00000,  0.00,  500.00,      0 ; * ( 20 bytes)
      ipwmTable       = array ,  S16,    354,    [   10], "%",        1.00000,   0.00000,  0.00,  100.00,      0
      frpm_table      = array ,  U16,    374,    [   12], "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * ( 24 bytes)
      srpm_table      = array ,  U16,    398,    [   12], "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * ( 24 bytes)
      fmap_table      = array ,  S16,    422,    [   12], "kPa",      0.10000,   0.00000,  0.00,  400.00,      1 ; * ( 24 bytes)
      smap_table      = array ,  S16,    446,    [   12], "kPa",      0.10000,   0.00000,  0.00,  400.00,      1 ; * ( 24 bytes)
#if CELSIUS
  #if EXPANDED_CLT_TEMP
      tempTable       = array ,  S16,    470,    [   10], "°C",       0.05555,  -320.000,-40.00,  300.00,      1 ; * ( 20 bytes) Temperature bins for cranking, cold AE and WUE
  #else  
      tempTable       = array ,  S16,    470,    [   10], "°C",       0.05555,  -320.000,-40.00,  100.00,      1 ; * ( 20 bytes) Temperature bins for cranking, cold AE and WUE
  #endif  
#else
  #if EXPANDED_CLT_TEMP
      tempTable       = array ,  S16,    470,    [   10], "°F",       0.10000,   0.00000,-40.00,  600.00,      1
  #else
      tempTable       = array ,  S16,    470,    [   10], "°F",       0.10000,   0.00000,-40.00,  200.00,      1
  #endif
#endif
      taeRates        = array ,  S16,    490,    [    4], "%/sec",    1.00000,   0.00000,  0.00, 32767.0,      0 ; * (  8 bytes) tpsDot bins used for AE: x for TAE interpolation
      maeRates        = array ,  S16,    498,    [    4], "kPa/sec",  1.00000,   0.00000,  0.00, 32767.0,      0 ; * (  8 bytes) mapDot bins used for AE: x for MAE
      map0            = scalar,  S16,    506,             "kPa",      0.10000,   0.00000, -100.0, 3276.7,      1 ; * (  2 bytes)
      mapmax          = scalar,  S16,    508,             "kPa",      0.10000,   0.00000, -100.0, 3276.7,      1 ; * (  2 bytes)
#if CELSIUS
      clt0            = scalar,  S16,    510,             "°C",       0.05555,  -320.000, -100.0,  500.0,      1 ; * (  2 bytes)
      cltmult         = scalar,  S16,    512,             "%",        1.00000,   0.00000, -200.0,  200.0,      0 ; * (  2 bytes)
      mat0            = scalar,  S16,    514,             "°C",       0.05555,  -320.000, -100.0,  500.0,      1 ; * (  2 bytes)
#else
      clt0            = scalar,  S16,    510,             "°F",       0.10000,   0.00000, -100.0,  500.0,      1
      cltmult         = scalar,  S16,    512,             "%",        1.00000,   0.00000, -200.0,  200.0,      0
      mat0            = scalar,  S16,    514,             "°F",       0.10000,   0.00000, -100.0,  500.0,      1
#endif
      matmult         = scalar,  S16,    516,             "%",        1.00000,   0.00000, -200.0,  200.0,      0 ; * (  2 bytes)
      tpsMin          = scalar,  S16,    518,             "ADC",      1.00000,   0.00000,    0.0, 1023.0,      0 ; * (  2 bytes)
      tpsMax          = scalar,  S16,    520,             "ADC",      1.00000,   0.00000,    0.0, 1023.0,      0 ; * (  2 bytes)
      batt0           = scalar,  S16,    522,             "V",        0.10000,   0.00000,    0.0, 3276.7,      1 ;   (  2 bytes)
      battmax         = scalar,  S16,    524,             "V",        0.10000,   0.00000,-3276.8, 3276.7,      1 ;   (  2 bytes)
      ego0            = scalar,  S16,    526,             "afr",      0.10000,   0.00000,-3276.8, 3276.7,      1 ;   (  2 bytes)
      egomult         = scalar,  S16,    528,             "%",        1.00000,   0.00000, -200.0,  200.0,      0 ;   (  2 bytes)
      baro0           = scalar,  S16,    530,             "kPa",      0.10000,   0.00000,-3276.8, 3276.7,      1 ; * (  2 bytes)
      baromax         = scalar,  S16,    532,             "kPa",      0.10000,   0.00000,-3276.8, 3276.7,      1 ; * (  2 bytes)
      bcor0           = scalar,  S16,    534,             "%",        1.00000,   0.00000,-3276.8, 3276.7,      1 ; * (  2 bytes)
      bcormult        = scalar,  S16,    536,             "%",        1.00000,   0.00000, -200.0,  200.0,      0 ; * (  2 bytes)
      knock0          = scalar,  S16,    538,             "V",        0.01000,   0.00000,    0.0,    5.0,      1 ; * (  2 bytes)
      knockmax        = scalar,  S16,    540,             "V",        0.01000,   0.00000,    0.0,    5.0,      1 ; * (  2 bytes)
      nestINTS        = bits  ,  U08,    542,      [0:0], "Low Speed Comms", "High Speed Comms"                  ; *

      crankTolerance  = scalar,  U08,    544,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      asTolerance     = scalar,  U08,    545,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      pulseTolerance  = scalar,  U08,    546,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      IdleCtl         = bits  ,  U08,    547,      [0:2], "None", "Solenoid", "IAC Stepper Moving Only", "IAC Stepper Always On", "PWM Warmup", "15-Minute IAC", "INVALID", "INVALID" ; *
      IACtstep        = scalar,  U08,    548,             "msec",       0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte)
      IACaccstep      = scalar,  U08,    549,             "msec",       0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte)
      IACminstep      = scalar,  U08,    550,          "steps",       1.00000,   0.00000,  1.00,  255.00,      0 ; * (  1 byte)
      IACpwm_step     = scalar,  U08,    551,             "Hz",      80.00000,   0.00000, 80.00,  800.00,      0 ; * (  1 byte)
      IACStart        = scalar,  S16,    552,             "",         1.00000,   0.00000,  0.00, 4000.00,      0 ; * (  1 byte)
#if CELSIUS
      IdleHyst        = scalar,  S16,    554,             "°C",       0.05555,   0.00000,   0.0,   30.0,       1 ; * (  2 bytes)
#else
      IdleHyst        = scalar,  S16,    554,             "°F",       0.10000,   0.00000,   0.0,   50.0,       1
#endif
      IACcrankpos     = scalar,  S16,    556,             "steps",    1.00000,   0.00000,  0.00, 4000.00,      0 ; * (  2 bytes)
      IACcrankxt      = scalar,  S16,    558,             "sec",      1.00000,   0.00000,  0.00,32767.00,      0 ; * (  2 bytes)
#if CELSIUS
  #if EXPANDED_CLT_TEMP
      IACcoldtmp      = scalar,  S16,    560,             "°C",       0.05555,  -320.000, -40.0,  300.0,       1 ; * (  2 bytes)
  #else
      IACcoldtmp      = scalar,  S16,    560,             "°C",       0.05555,  -320.000, -40.0,  150.0,       1 ; * (  2 bytes)
  #endif
#else
  #if EXPANDED_CLT_TEMP
      IACcoldtmp      = scalar,  S16,    560,             "°F",       0.10000,   0.00000,-40.00,  500.00,      1
  #else
      IACcoldtmp      = scalar,  S16,    560,             "°F",       0.10000,   0.00000,-40.00,  300.00,      1
  #endif
#endif
      IACcoldpos      = scalar,  S16,    562,             "steps",    1.00000,   0.00000,  0.00, 4000.00,      0 ; * (  2 bytes)
      IACcoldxt       = scalar,  S16,    564,             "sec",      1.00000,   0.00000,  0.00,32767.00,      0 ; * (  2 bytes)
      primePulseCold  = scalar,  S16,    566,             "msec",     0.10000,   0.00000,  0.00,   65.00,      1 ; * (  2 bytes)
      primePulseHot   = scalar,  S16,    568,             "msec",     0.10000,   0.00000,  0.00,   65.00,      1 ; * (  2 bytes)
      crankCold       = scalar,  S16,    570,             "msec",     0.10000,   0.00000,  0.00,   65.00,      1 ; * (  1 byte)
      crankHot        = scalar,  S16,    572,             "msec",     0.10000,   0.00000,  0.00,   65.00,      1 ; * (  1 byte)
      asePctCold      = scalar,  S16,    574,             "%",        1.00000,   0.00000,  0.00,  400.00,      0 ; * (  2 bytes)
      asePctHot       = scalar,  S16,    576,             "%",        1.00000,   0.00000,  0.00,  400.00,      0 ; * (  2 bytes)
      aseCountCold    = scalar,  S16,    578,             "cycles",   1.00000,   0.00000,  0.00,32767.00,      0 ; * (  2 bytes)
      aseCountHot     = scalar,  S16,    580,             "cycles",   1.00000,   0.00000,  0.00,32767.00,      0 ; * (  2 bytes)
      taeColdA        = scalar,  U08,    582,             "msec",     0.10000,   0.00000,  0.00,  25.500,      1 ; * (  1 byte)
      taeColdM        = scalar,  U08,    583,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      tpsThresh       = scalar,  U08,    584,             "%/sec",    1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      mapThresh       = scalar,  U08,    585,             "kPa/sec",  1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte) threshold for MAE
      taeTime         = scalar,  U08,    586,             "sec",      0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte)
      tdePct          = scalar,  U08,    587,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      floodClear      = scalar,  S16,    588,             "%",        0.10000,   0.00000,  0.00,  100.00,      1 ; * (  2 bytes)
      TPSOXLimit      = scalar,  S16,    590,             "%",        0.10000,   0.00000,  0.00,  100.00,      1 ; * (  2 bytes)
      tpsProportion   = scalar,  U08,    592,             "%",        1.00000,   0.00000,  0.00,  100.00,      0 ; * (  1 byte)
      baroCorr        = bits  ,  U08,    593,      [0:1], "None", "Initial MAP Reading", "Two Independent Sensors", "INVALID"        ; *
      egoType         = bits  ,  U08,    594,      [0:2], "Disabled", "Narrow Band", "Dual Narrow Band", "Single Wide Band", "Dual Wide Band", "INVALID", "INVALID", "INVALID" ; *
      egoCount        = scalar,  U08,    595,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      egoDelta        = scalar,  U08,    596,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      egoLimit        = scalar,  U08,    597,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
#if   NARROW_BAND_EGO
      egoTarget       = scalar,  U08,    598,             "v",        0.01000,   0.00000,  0.00,    2.00,      4 ; * (  1 byte)
#elif LAMBDA
      AFRTarget       = scalar,  U08,    598,             "Lambda",   0.006803,   0.00000,  0.00,   2.00,      3
#else
      AFRTarget       = scalar,  U08,    598,             "AFR",      0.10000,   0.00000,  0.00,   25.50,      1
#endif
      tempUnits       = bits  ,  U08,    599,      [0:0], "Coolant/IAT Tables in °F", "Coolant/IAT Tables in °C"  ; * (  1 byte)
      MAFOption       = bits  ,  U08,    600,      [0:1], "No MAF",  "MAF Only", "MAF/MAP blend", "MAF Fuel/MAP table index",      ; * 
      MAFpin          = bits  ,  U08,    600,      [4:5], "MAF on MAP pin", "MAF on Baro Pin", "MAF on Knock Pin", "INVALID" ; *
      DualSpkOptn     = bits  ,  U08,    601,      [0:3], "No Dual Spark", "Dual Tach Inputs", "Falling Cam Sync with Tach or Wheel", "Rising Cam Sync with Tach or Wheel", "Single Crank Wheel Input", "Single Cam Wheel Input", "Dual Inputs, Timing from 1 cam tooth", "M-0 Wheel w/ Falling Crank Sync", "M-0 Wheel w/ Rising Crank Sync", "INVALID", "INVALID", "INVALID", "INVALID", "INVALID", "INVALID", "INVALID" ; * (1 byte)
#if CELSIUS
  #if EXPANDED_CLT_TEMP
      fastIdleT       = scalar,  S16,    602,             "°C",       0.05555,  -320.000,-40.00,  300.00,      1 ; * (  2 bytes)
      egoTemp         = scalar,  S16,    604,             "°C",       0.05555,  -320.000,-40.00,  300.00,      1 ; * (  2 bytes)
  #else
      fastIdleT       = scalar,  S16,    602,             "°C",       0.05555,  -320.000,-40.00,  150.00,      1 ; * (  2 bytes)
      egoTemp         = scalar,  S16,    604,             "°C",       0.05555,  -320.000,-40.00,  150.00,      1 ; * (  2 bytes)
  #endif
#else
  #if EXPANDED_CLT_TEMP
      fastIdleT       = scalar,  S16,    602,             "°F",       0.10000,   0.00000,-40.00,  600.00,      1
      egoTemp         = scalar,  S16,    604,             "°F",       0.10000,   0.00000,-40.00,  600.00,      1
  #else
      fastIdleT       = scalar,  S16,    602,             "°F",       0.10000,   0.00000,-40.00,  300.00,      1
      egoTemp         = scalar,  S16,    604,             "°F",       0.10000,   0.00000,-40.00,  300.00,      1
  #endif
#endif
      egoRPM          = scalar,  S16,    606,             "RPM",      1.00000,   0.00000,  0.00, 15000.0,      0 ; * (  2 bytes)
      reqFuel         = scalar,  U16,    608,             "msec",     0.00100,   0.00000,  0.00,  65.536,      2 ; * (  2 bytes)
      divider         = scalar,  U08,    610,             "",         1.00000,   0.00000,  0.00,     255,      0 ; * (  1 byte)
      alternate       = bits,    U08,    611,      [0:0], "Simultaneous", "Alternating"                          ; * (  1 byte)
      injOpen         = scalar,  U08,    612,             "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte)
      injPwmT         = scalar,  U08,    613,             "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte)
      injPwmPd        = scalar,  U08,    614,             "µsec",     1.00000,   0.00000, 40.00,  100.00,      0 ; * (  1 byte)
      injPwmP         = scalar,  U08,    615,             "%",        1.00000,   0.00000,  0.00,  100.00,      0 ; * (  1 byte)
      battFac         = scalar,  U08,    616,             "ms/v",     0.0166667, 0.00000,  0.00,    1.00,      2 ; * (  1 byte)
      twoStroke       = bits,    U08,    617,      [0:0], "Four-stroke",    "Two-stroke"                         ; *
      injType         = bits,    U08,    618,      [0:0], "Port Injection", "Throttle Body"                      ; *
      nInjectors      = bits,    U08,    619,      [0:4], "INVALID"                                              ; *
      OddAng          = scalar,  S16,    620,      "degrees",         0.10000,   0.00000,-350.0,  350.00,      1
      rpmLF           = scalar,  U08,    622,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      mapLF           = scalar,  U08,    623,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      tpsLF           = scalar,  U08,    624,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      egoLF           = scalar,  U08,    625,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      adcLF           = scalar,  U08,    626,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      knkLF           = scalar,  U08,    627,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      AMCOption       = bits,    U08,    628,      [0:1], "Disabled", "RAM Update", "FLASH Update", "INVALID"    ; * (  1 byte)
      dualTable       = bits,    U08,    629,      [0:0], "Single Table", "Dual Table"                           ; *
      algorithm       = bits,    U08,    630,      [0:1], "Speed Density", "Blend SD/AlphaN, PW=--f(tps)xVE(tps,rpm)", "Blend SD/AlphaN, PW=--VE(tps,rpm)", "INVALID" ; *
      alphDir         = bits,    U08,    630,      [4:4],   "Use Above", "Invert Above"                          ; *
      alpha_baro_spkadv = scalar, U08,   631,      "deg/kPa",         0.01000,   0.00000,  0.00,  255.00,      2 ; * (  1 byte)
      AfrAlpha        = scalar,  U08,    632,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; U (  1 byte) UNUSED
      AFRStoich       = scalar,  U08,    633,             "AFR",      0.10000,   0.00000,  0.00,   20.00,      1 ; * (  1 byte)
      AFRStoichWB     = scalar,  U08,    633,             "AFR",      0.10000,   0.00000,  0.00,   20.00,      1 ; * (  1 byte)
      AFRStoichNB     = scalar,  U08,    633,             "Volts",    0.01000,   0.00000,  0.00,    7.00,      3 ; * (1 byte)
      alpha_lorpm     = scalar,  S16,    634,             "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * (  2 bytes)
      alpha_hirpm     = scalar,  S16,    636,             "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * (  2 bytes)
      alphaMAPtable   = array ,  S16,    638,    [ 6x 6], "kPa",      0.10000,   0.00000,  0.00,  200.00,      1 ; * ( 72 bytes)
      amap_tps        = array ,  S16,    710,    [    6], "%",        0.10000,   0.00000,   0.0,  100.00,      1 ; * ( 12 bytes)
      amap_rpm        = array ,  U16,    722,    [    6], "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * ( 12 bytes)
      baud            = scalar,  U32,    734,             "",         1.00000,   0.00000,9600.0,115200.0,      0 ; x (  4 bytes)
      MAPOXLimit      = scalar,  S16,    738,             "kPa",      0.10000,   0.00000,  0.00,  300.00,      2 ; * (  2 bytes)
      board_type      = scalar,  U08,    740,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      mycan_id        = scalar,  U08,    741,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)               
      fet_delay       = scalar,  U08,    742,             "µsec",     1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      vr_delay        = scalar,  U08,    743, "µsec/1000rpm",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)   
      ECUType         = scalar,  U08,    744, "1=MS-II, 2=MicroSquirt",   1.00000,   0.00000,  0.00,    9.00,  0 ; * (  1 byte)

      MapThreshXTD2   = scalar,  U08,    745,    "-kpa/sec",          1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)

#if n2o
      n2oEnrich       = scalar,  U08,    746,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
#else
      pwImpulse       = scalar,  U08,    746,             "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte)
#endif

      impulseSec      = scalar,  U08,    747,             "sec",      1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      nImpulse        = scalar,  U08,    748,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      mapdotSample    = scalar,  U08,    749,             "msec",     1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      tpsdotSample    = scalar,  U08,    750,             "msec",     1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte) 
      ASEHot          =   bits,  U08,    751,      [0:0], "Disable ASE on Hot Start", "Enable ASE on Hot Start"
      InjStart        = scalar,  U08,    752,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte) 
      MapThreshXTD    = scalar,  U08,    753,             "-kpa/sec", 1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      MapThreshXTA    = scalar,  U08,    754,             "kpa/sec",  1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      trendmapLimit   = scalar,  U08,    755,             "kpa",      1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte)
      ; Port Settings constants
      psEnabled       = array ,  U08,    756,    [    7], "on/off",   1.00000,   0.00000,   0.00,    1.00,     0 ; * (  2 bytes)
      psCondition     = array ,  U08,    763,    [  7x2], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psConnector     = array ,  U08,    777,    [    7], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psInitValue     = array ,  U08,    784,    [    7], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psPortValue     = array ,  U08,    791,    [    7], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psOutSize       = array ,  U08,    798,    [  7x2], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psOutOffset     = array ,  U16,    812,    [  7x2], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psThreshold     = array ,  U16,    840,    [  7x2], "",         1.00000,   0.00000,-32768.0,32767.0,     0 ; * (  4 bytes)
      psHysteresis    = array ,  U16,    868,    [  7x2], "",         1.00000,   0.00000,-32768.0,32767.0,     0 ; * (  4 bytes)
      aeTaperTime     = scalar,  U08,    896,             "sec",        0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte)
      AFRMult         = bits,    U08,    897,      [0:1], "Use Combined VE/AFR table", "Separate VE & AFR table w/ NB EGO", "Separate VE & AFR table w/ WB EGO", "INVALID"  ; * (  1 byte)
      aeEndPW         = scalar,  S16,    898,             "msec",       0.10000,   0.00000,  0.00, 1000.00,      1 ; *
      egoAlgorithm    = bits  ,  U08,    900,      [0:1], "Simple", "Transport Delay", "PID/Smith Predictor", "INVALID" ; * (  1 byte)
      egoKP           = scalar,  U08,    901,             "%",        1.00000,   0.00000,  0.00,  100.00,      0 ; * (  1 byte)
      egoKI           = scalar,  U08,    902,             "%",        1.00000,   0.00000,  0.00,  100.00,      0 ; * (  1 byte)
      egoKD           = scalar,  U08,    903,             "%",        1.00000,   0.00000,  0.00,  100.00,      0 ; * (  1 byte)
      egoKdelay1      = scalar,  U16,    904,             "msec",       1.00000,   0.00000,  0.00,   65535,      0 ; * (  2 bytes)
      egoKdelay2      = scalar,  U16,    906,             "revs",     1.00000,   0.00000,  0.00,   65535,      0 ; * (  2 bytes)
      flexFuel        = bits  ,  U08,    908,      [0:0], "Disabled", "Enabled"                                  ; * (  1 byte)
      prime_delay     = scalar,  U08,    909,             "sec",      1.00000,   0.00000,  0.00,     255,      0 ; * (  1 byte)
      fuelFreq        = array ,  U08,    910,    [    2], "Hz",       1.00000,   0.00000,  0.00,     255,      0 ; * (  2 bytes)
         fuelFreq0    = scalar,  U08,    910,             "Hz",       1.00000,   0.00000,  0.00,     255,      0
         fuelFreq1    = scalar,  U08,    911,             "Hz",       1.00000,   0.00000,  0.00,     255,      0
      fuelCorr        = array ,  U08,    912,    [    2], "%",        1.00000,   0.00000,  0.00,     255,      0 ; * (  2 bytes)
         fuelCorr0    = scalar,  U08,    912,             "%",        1.00000,   0.00000,  0.00,     255,      0
         fuelCorr1    = scalar,  U08,    913,             "%",        1.00000,   0.00000,  0.00,     255,      0
      AMCstep         = scalar,  U08,    914,             "%",        1.00000,   0.00000,  0.00,     255,      0 ; * (  2 bytes)
      AMCdve          = scalar,  U08,    915,             "%",        1.00000,   0.00000,  0.00,     255,      0 ; * (  2 bytes)
      AMCve_rpm       = scalar,  U16,    916,             "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * (  2 bytes)
      AMCve_map       = scalar,  U16,    918,             "kPa",      0.10000,   0.00000,  0.00,  300.00,      2 ; * (  2 bytes)
      AMCramve_dt     = scalar,  U16,    920,             "sec",      1.0,       0.0,      0.0,   300.0,       0 ; * (  2 bytes)
      AMCT_thresh     = scalar,  U16,    922,             "sec",      1.0,       0.0,      0.0,  1800.0,       0 ; * (  2 bytes)
      AMCupdate_thresh= scalar,  U16,    924,             "events",   1.0,       0.0,      0.0, 30000.0,       0 ; * (  2 bytes)
      CWOption        = bits  ,  U08,    926,      [0:0], "Two-Point", "Table"                                   ; * (  1 byte )
      knkOption       = bits  ,  U08,    927,      [0:1], "Disabled", "Safe Mode", "Aggressive Mode", "INVALID"  ; * (  1 byte )
      knkDirection    = bits  ,  U08,    927,      [4:4], "Below threshold", "Above threshold"                   ; *
      knk_maxrtd      = scalar,  U08,    928,             "deg",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_step1       = scalar,  U08,    929,             "deg",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_step2       = scalar,  U08,    930,             "deg",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_trtd        = scalar,  U08,    931,             "sec",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_tadv        = scalar,  U08,    932,             "sec",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_dtble_adv   = scalar,  U08,    933,             "deg",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_ndet        = scalar,  U08,    934,             "knocks",   1.0,       0.0,      0.0,     255,       0 ; * (  1 byte )
     ;pad             = scalar,  U08,    935,
      knk_maxmap      = scalar,  U16,    936,             "kPa",      0.1,       0.0,      0.0,   300.0,       1 ; * (  2 bytes)
      knk_lorpm       = scalar,  U16,    938,             "rpm",      1.0,       0.0,      0.0,   10000,       0 ; * (  2 bytes)
      knk_hirpm       = scalar,  U16,    940,             "rpm",      1.0,       0.0,      0.0,   10000,       0 ; * (  2 bytes)
      knk_rpm         = array ,  U16,    942,    [    6], "rpm",      1.0,       0.0,      0.0,    6000,       0 ; * (  2 bytes)
      knk_thresh      = array ,  U16,    954,    [    6], "v",        0.01,      0.0,      0.0,    5.00,       2 ; * (  2 bytes)
      triggerTeeth    = scalar,  U16,    966,             "teeth",    1.0,       0.0,      0.0,     512,       0 ; * (  2 bytes)
      No_Miss_Teeth   = scalar,  U08,    968,             "teeth",    1.0,       0.0,      0.0,     255,       0 ; * (  1 byte )
      No_Skip_Teeth   = scalar,  U08,    969,             "teeth",    1.0,       0.0,      0.0,     255,       0 ; * (  1 byte )
      Delay_Teeth     = scalar,  U08,    970,             "teeth",    1.0,       0.0,      0.0,     255,       0 ; * (  1 byte )
      ICISR_tmask     = scalar,  U08,    971,             "msec",       0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      ICISR_pmask     = scalar,  U08,    972,             "%",        1.0,       0.0,      0.0,     200,       0 ; * (  1 byte )
      injTestMode     = bits  ,  U08,    973,      [0:1], "Normal Mode", "Test Mode", "Repeat Test", "INVALID"   ;   (  1 byte )
      ae_lorpm        = scalar,  U16,    974,             "rpm",      1.0,       0.0,      0.0,   10000,       0 ; * (  2 bytes)
      ae_hirpm        = scalar,  U16,    976,             "rpm",      1.0,       0.0,      0.0,   10000,       0 ; * (  2 bytes)
      fuelSpkDel      = array ,  S16,    978,    [    2], "deg",      0.10000,   0.00000,-45.00,   45.00,      1 ; * (  4 bytes)
         fuelSpkDel0  = scalar,  S16,    978,             "deg",      0.10000,   0.00000,-45.00,   45.00,      1
         fuelSpkDel1  = scalar,  S16,    980,             "deg",      0.10000,   0.00000,-45.00,   45.00,      1
      injTestSqrts    = scalar,  U16,    982,             "squirts",  1,         0,           0,   65000,      0 ;   (  2 bytes)
      injTestPW       = scalar,  U16,    984,             "msec",     0.001,     0,           0,      65,      3 ;   (  2 bytes)
      injTestOffTime  = scalar,  U16,    986,             "msec",     0.1,       0,           0,    6500,      1 ;   (  2 bytes)
      CID             = scalar,  U16,    988,             "cu.in.",   1,         0,           0,     700,      1 ;   (  2 bytes)         
      alpha           = scalar,  U08,    990,             "%",        1.0,       0.0,        50,     150,      0 ; * (  1 byte ) 
      beta            = scalar,  U08,    991,             "%",        1.0,       0.0,       0.0,     100,      0 ; * (  1 byte )
      gamma           = scalar,  U08,    992,             "%",        1.0,       0.0,       0.0,      50,      0 ; * (  1 byte )
      acc_synchk      = bits,    U08,    993,      [0:1], "Check Only at Steady Speed", "Check Accel and Steady Speed", "Check Decel and Steady Speed", "Check Always" ;  (1 byte)        
  
;     pageSize =  994

;----------------------------------------------------------------------------------------------------------------------------------------

   page = 2
      veTable1        = array ,  U08,      0,    [12x12], "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (144 bytes)
      veTable2        = array ,  U08,    144,    [12x12], "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (144 bytes)
      advanceTable    = array ,  S16,    288,    [12x12], "deg",      0.10000,   0.00000,-10.00,   90.00,      1 ; * (288 bytes)
      AMCNBurns       = scalar,  U16,    576,             "burns",    1,         0,           0,   65000,      0 ; x (  2 bytes)
      primePWTable    = array ,  S16,    578,    [   10], "msec",       0.10000,   0.00000,  0.00,   65.00,      1 ; * ( 20 bytes)
      crankPWTable    = array ,  S16,    598,    [   10], "msec",       0.10000,   0.00000,  0.00,   65.00,      1 ; * ( 20 bytes)
      asePctTable     = array ,  S16,    618,    [   10], "%",        1.00000,   0.00000,  0.00,  400.00,      0 ; * (  2 bytes)
      aseCntTable     = array ,  S16,    638,    [   10], "cycles",   1.00000,   0.00000,  0.00, 2500.00,      0 ; * (  2 bytes)
#if CELSIUS
  #if EXPANDED_CLT_TEMP
      matTemps        = array ,  S16,    658,    [    6], "°C",       0.05555,  -320.000,-40.00,  300.00,      1 ; * ( 12 bytes)
  #else
      matTemps        = array ,  S16,    658,    [    6], "°C",       0.05555,  -320.000,-40.00,  150.00,      1 ; * ( 12 bytes)
  #endif
#else
  #if EXPANDED_CLT_TEMP
      matTemps        = array ,  S16,    658,    [    6], "°F",       0.10000,   0.00000,-40.00,  600.00,      1
  #else
      matTemps        = array ,  S16,    658,    [    6], "°F",       0.10000,   0.00000,-40.00,  300.00,      1
  #endif
#endif
      matRetard       = array ,  U08,    670,    [    6], "deg",      0.10000,   0.00000,  0.00,    25.5,      1 ; * (  6 bytes)
      xTauOption      = bits  ,  U08,    676,      [0:1], "Off", "Accel/Decel Only", "Warm-up + Accel/Decel", "INVALID" ; * (  1 byte )
      spkN2O          = scalar,  U08,    677,             "deg",      0.10000,   0.00000,  0.00,    25.5,      1 ; * (  1 bytes)
      XAccTable       = array,   U16,    678,     [   5], "%",        0.10000,   0.00000,  0.00,      90,      1 ; * ( 10 bytes)
      TauAccTable     = array,   U16,    688,     [   5], "msec",     1.00000,   0.00000,  2.00,   20000,      0 ; * ( 10 bytes)
      XDecTable       = array,   U16,    698,     [   5], "%",        0.10000,   0.00000,  0.00,      90,      1 ; * ( 10 bytes)
      TauDecTable     = array,   U16,    708,     [   5], "msec",     1.00000,   0.00000,  2.00,   20000,      0 ; * ( 10 bytes)
      XTrpms          = array,   U16,    718,     [   5], "rpm",      1.00000,   0.00000,  0.00,   10000,      0 ; * ( 10 bytes)
      XClt            = array,   U16,    728,     [  10], "%",        1.00000,   0.00000,  0.00,     600,      0 ; * ( 20 bytes)
      TauClt          = array,   U16,    748,     [  10], "%",        1.00000,   0.00000,  0.00,     600,      0 ; * ( 20 bytes)
      fRate           = scalar,  U16,    768,             "g/s",      0.00100,   0.00000,  0.00,   60000,      3 ; * ( 2 bytes)
      ipada           = array,   S16,    770,     [   47],"",         1.00000,   0.00000,  0.00,     300,      0 ; * ( 96 bytes)
      ; Supplemental corrections for barometer and IAT.
      baroCorrVals    = array ,  S16,    864,    [    6], "kPa",      0.10000,   0.00000,  80.0,  120.00,      1 ; * ( 24 bytes)
#if CELSIUS
  #if EXPANDED_CLT_TEMP
      matCorrTemps    = array ,  S16,    876,    [    6], "°C",       0.05555,  -320.000,-40.00,  300.00,      1 ; * ( 12 bytes)
  #else
      matCorrTemps    = array ,  S16,    876,    [    6], "°C",       0.05555,  -320.000,-40.00,  150.00,      1 ; * ( 12 bytes)
  #endif
#else
  #if EXPANDED_CLT_TEMP
      matCorrTemps    = array ,  S16,    876,    [    6], "°F",       0.10000,   0.00000,-40.00,  600.00,      1
  #else
      matCorrTemps    = array ,  S16,    876,    [    6], "°F",       0.10000,   0.00000,-40.00,  300.00,      1
  #endif
#endif
      baroCorrDelta   = array ,  S08,    888,    [    6], "%",        1.00000,   0.00000,-100.0,   120.0,      1 ; * (  6 bytes)
      matCorrDelta    = array ,  S08,    894,    [    6], "%",        1.00000,   0.00000,-100.0,   120.0,      1 ; * (  6 bytes)
      MAFFlow         = array ,  U16,    900,    [   12], "gram/sec", 0.01000,   0.00000,  0.00,   650.0,      1 ; * ( 24 bytes)      
      MAFCor          = array ,  U08,    924,    [   12], "%",        1.00000,   0.00000,  0.00,   255.0,      0 ; * ( 12 bytes)   
      MAFRPM1         = scalar,  U16,    936,             "rpm",      1.00000,   0.00000,  0.00,   10000,      0 ; * (  2 bytes)
      MAFRPM2         = scalar,  U16,    938,             "rpm",      1.00000,   0.00000,  0.00,   10000,      0 ; * (  2 bytes)
      MAFDir          = bits  ,  U08,    940,      [0:0], "Use Above", "Invert Above"                             ; * (  1 byte )
      VEIXOptn        = bits  ,  U08,    941,      [0:1], "Use MAP only", "Adjust MAP for Baro", "Use SAE Pid 43 Abs Load", "INVALID"  ; * (  1 byte )
      MatRtdRPMHi     = scalar,  U16,    942,             "rpm",      1.00000,   0.00000,  0.00,   10000,      0 ; * (  2 bytes)  
      MatRtdRPMLo     = scalar,  U16,    944,             "rpm",      1.00000,   0.00000,  0.00,   10000,      0 ; * (  2 bytes)
;      FuelAdj         = scalar,  S16,    946,                "",      1.00000,   0.00000,  0.00,   10000,      0 ; Fuel Adj from MShift - not exposed in menus
;      SpkAdj          = scalar,  S16,    948,                "",      1.00000,   0.00000,  0.00,   10000,      0 ; Spark Adj from MShift - not exposed in menus 
;      IdleAdj         = scalar,  S16,    950,                "",      1.00000,   0.00000,  0.00,   10000,      0 ; Idle Adj from MShift - not exposed in menus 
;      SprAdj          = scalar,  S16,    952,                "",      1.00000,   0.00000,  0.00,   10000,      0 ; Spare Adj from MShift - not exposed in menus 

;     pageSize =  954

;----------------------------------------------------------------------------------------------------------------------------------------

[Menu]

   ;----------------------------------------------------------------------------
   ;  There are five pre-defined values that may be used to define your menus.
   ;  The first four allow access to the "standard" dialog boxes, the last one
   ;  merely draws a separator (horizontal line) in the menu.
   ;
   ;     std_constants
   ;     std_enrichments
   ;     std_realtime
   ;     std_warmup
   ;     std_accel
   ;
   ;     std_separator
   ;
   ;  Additionally, to support MegaSquirt-II firmware, there are two standard
   ;  dialogs to generate its three embedded tables.  The first of these acts
   ;  like Roger Enns' EasyTherm, but only works for MS-II.  The second one
   ;  generates the internal AFR table required for proper closed loop operation
   ;  in MS-II.  Use these without page numbers, as they will just be ignored
   ;  in any case.
   ;
   ;     std_ms2gentherm
   ;     std_ms2geno2
   ;
   ;  If you use any of the std_constants, std_enrichments or std_warmup
   ;  editors, they may be optionally suffixed with a page number (only
   ;  useful for multi-page code variants), which causes them to edit the
   ;  specified page.  If you leave off the page specifier, they edit logical
   ;  page one as specified in the Constants section.
   ;
   ;  There are four special menu names, which when used append to the standard
   ;  menus of the same name instead of creating a new one.  The menu names
   ;  are "File", "Communications", "Tools" and "Help".
   ;
   ;----------------------------------------------------------------------------

   menuDialog = main
      menu = "Fuel &Set-Up"
         subMenu = generalSettings, "&General"
         subMenu = idleControl,     "I&dle Control",                   0,  { ECUType == 1 || ECUType == 2}
         subMenu = std_port_edit,   "Spare &Port Settings",            0,  { ECUType == 1 || ECUType == 2}
         subMenu = std_separator,   ;----------------------------------------------
         subMenu = injChars,        "I&njector Characteristics",       0,  { ECUType == 1 || ECUType == 2}
         subMenu = std_injection,   "Injection &Control",              0,  { ECUType == 1 || ECUType == 2}
         subMenu = revLimiter,      "&Rev Limiter",                    0,  { ECUType == 1 || ECUType == 2}
         subMenu = aseSettings,     "After&Start Enrichment" ,         0,  { ECUType == 1 || ECUType == 2}
         subMenu = accSettings,     "Acce&l Enrichment Config",        0,  { ECUType == 1 || ECUType == 2}
         subMenu = otherFuel,       "&Other Fuel Settings",            0,  { ECUType == 1 || ECUType == 2}
         subMenu = baroCorrection,  "2-Point &Barometric Correction",  0,  { ECUType == 1 || ECUType == 2}
         subMenu = flexFuelSettings,"&Flex Fuel",                      0,  { ECUType == 1 || ECUType == 2}
         subMenu = egoControl,      "&EGO Control",                    0,  { ECUType == 1 || ECUType == 2}
         subMenu = amcSettings,     "Automatic &Mixture Control",      0,  { ECUType == 1 || ECUType == 2}
	 subMenu = std_separator    ;----------------------------------------------
	 subMenu = alphaNOptions,   "&Alpha-N Blending",               0,  { algorithm  > 0 && (ECUType == 1 || ECUType == 2)}
	 subMenu = MAFSettings,     "MAP vrs. MAF &Usage",             0,  { ECUType == 1 || ECUType == 2}

   menuDialog = main
       menu = "&Ignition Set-Up"
         subMenu = ignitionOptions, "&Base Ignition Settings",         0,  { ECUType == 1 || ECUType == 2}
         subMenu = dwellSettings,   "D&well Settings",                 0,  { ECUType == 1 || ECUType == 2}
         subMenu = AdvncdignitionOptions, "&Advanced Ignition Options",0,  { ECUType == 1 || ECUType == 2}
         subMenu = knockSettings,  "&Knock Setup",                     0,  { ECUType == 1 || ECUType == 2}		 
         subMenu = knockThresholdCurve, "K&nock Threshold",            0,  { ECUType == 1 || ECUType == 2} 
   menuDialog = main
      menu = "B&asic Tables"

#if MAPbaro
	 subMenu = std_separator    ;----------------------------------------------
         subMenu = veTable1Tbl,     "&VE Table 1 (MAP/Baro)",         0,  { (MAFOption == 0 || MAFOption == 2) && VEIXOptn == 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = afrTable1Tbl,    "&AFR Table 1 (MAP/Baro)",        0,  { VEIXOptn == 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = veTable2Tbl,     "V&E Table 2 (MAP/baro)",         0,  { (MAFOption == 0 || MAFOption == 2) && dualTable && VEIXOptn == 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = afrTable2Tbl,    "AFR &Table 2 (MAP/Baro)",        0,  { dualTable && VEIXOptn == 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = ignitionTbl,     "&Spark Advance Table (MAP/Baro)",0,  { VEIXOptn == 1  && (ECUType == 1 || ECUType == 2)}

#else
         subMenu = veTable1Tbl,     "VE Table &1 (MAP or PID43)",              0,  { (MAFOption == 0 || MAFOption == 2) && VEIXOptn != 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = afrTable1Tbl,    "A&FR Table 1 (MAP or PID43)",             0,  { VEIXOptn != 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = veTable2Tbl,     "VE Table &2 (MAP or PID43)",              0,  { (MAFOption == 0 || MAFOption == 2) && dualTable && VEIXOptn != 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = afrTable2Tbl,    "AF&R Table 2 (MAP or PID43)",             0,  { dualTable && VEIXOptn != 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = ignitionTbl,     "S&park Advance Table (MAP or PID43)",     0,  { VEIXOptn != 1  && (ECUType == 1 || ECUType == 2)}
#endif
  
     menuDialog = main
      menu = "Othe&r Tables" 
         subMenu = tempTableBins,   "&Temperature Table Values",      0,  { ECUType == 1 || ECUType == 2}
         subMenu = alphaMAPTbl,     "&Alpha-N MAP Table",             0, { algorithm > 0 && (ECUType == 1 || ECUType == 2)}
         subMenu = barometerCorr,   "Barometric &Correction",         0, { (ECUType == 1 || ECUType == 2)}
         subMenu = std_separator    ;----------------------------------------------   
         subMenu = primingPW,       "Pri&ming Pulse",                 0, { CWOption > 0  && (ECUType == 1 || ECUType == 2)}
         subMenu = crankingPW,      "Cra&nking Pulse",                0, { CWOption > 0  && (ECUType == 1 || ECUType == 2)}
         subMenu = asePct,          "A&SE Percentage",                0, { CWOption > 0  && (ECUType == 1 || ECUType == 2)}
         subMenu = aseTaper,        "AS&E Taper",                     0, { CWOption > 0  && (ECUType == 1 || ECUType == 2)}

   menuDialog = veTable1Tbl
      menu = "&Edit Bins"
	 subMenu = fmapTableBins,      "Edit Fuel &MAP Bins"
	 subMenu = frpmTableBins,      "Edit Fuel &RPM Bins"

   menuDialog = veTable2Tbl
      menu = "&Edit Bins"
	 subMenu = fmapTableBins,      "Edit Fuel &MAP Bins"
	 subMenu = frpmTableBins,      "Edit Fuel &RPM Bins"


   menuDialog = ignitionTbl
      menu = "&Edit Bins"
	 subMenu = smapTableBins,      "Edit Spark &MAP Bins"
	 subMenu = srpmTableBins,      "Edit Spark &RPM Bins"		 

   menuDialog = main
      menu = "&Tuning"
         subMenu = std_realtime,    "&Realtime Display",              0,  { ECUType == 1 || ECUType == 2}

#if MAPbaro
         subMenu = std_separator    ;----------------------------------------------
         subMenu = veTable1Map,     "VE &Table 1 (MAP/Baro)",         0, { (MAFOption == 0 || MAFOption == 2) && VEIXOptn == 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = veTable2Map,     "VE T&able 2 (MAP/Baro)",         0, { (MAFOption == 0 || MAFOption == 2) && dualTable && VEIXOptn == 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = afrTable1Map,    "A&FR Ta&ble 1 (MAP/Baro)",       0, { VEIXOptn == 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = afrTable2Map,    "A&FR Tabl&e 2 (MAP/Baro)",       0, { dualTable && VEIXOptn == 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = ignitionMap,     "I&gnition Advance Table (MAP/Baro)",    0, { VEIXOptn == 1 && (ECUType == 1 || ECUType == 2)}

#else
         subMenu = std_separator    ;----------------------------------------------
         subMenu = veTable1Map,     "VE Table &1 (MAP or PID43)",              0, { (MAFOption == 0 || MAFOption == 2) && VEIXOptn != 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = veTable2Map,     "VE Table &2 (MAP or PID43)",              0, { (MAFOption == 0 || MAFOption == 2) && VEIXOptn != 1 && dualTable && (ECUType == 1 || ECUType == 2)}
         subMenu = afrTable1Map,    "A&FR Table 1 (MAP or PID43)",             0, { VEIXOptn != 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = afrTable2Map,    "AF&R Table 2 (MAP or PID43)",             0, { dualTable && VEIXOptn != 1 && (ECUType == 1 || ECUType == 2)}
         subMenu = ignitionMap,     "&Spark Advance Table (MAP or PID43)",     0, { VEIXOptn != 1 && (ECUType == 1 || ECUType == 2)}
#endif

         subMenu = std_separator    ;----------------------------------------------
         subMenu = std_warmup,      "&Warmup Wizard",                 0,  { ECUType == 1 || ECUType == 2}
         subMenu = std_accel,       "Acce&leration Wizard",           0,  { ECUType == 1 || ECUType == 2}       

   menuDialog = main
       menu = "X-Ta&u Tuning"
         subMenu = XAccTable,       "Puddling Factors (&accel)",      0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
         subMenu = XDecTable,       "Puddling Factors (&decel)",      0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
         subMenu = TauAccTable,     "Time Factors (a&ccel)",          0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
         subMenu = TauDecTable,     "Time Factors (d&ecel)",          0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
         subMenu = XCltTable,       "&X (Puddling) Temp. Corrections",0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}    
         subMenu = TCltTable,       "&Tau (Time) Temp. Corrections",  0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
         subMenu = std_separator    ;---------------------------------------------- 
         subMenu = xTauSettings,    "&MAPdot Settings",               0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}    
         subMenu = XTrpmsdial,      "&RPM Values",                    0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}

   menuDialog = main
       menu = "Oth&er Tuning"
         subMenu = coldAdvance,     "&Cold Advance",                  0,  { ECUType == 1 || ECUType == 2}
         subMenu = std_separator    ;----------------------------------------------
         subMenu = manifoldTempCorr,"I&AT-Based Fuel Correction",     0,  { ECUType == 1 || ECUType == 2}
         subMenu = matBasedRetard,  "IAT-&Based Timing Retard",       0,  { ECUType == 1 || ECUType == 2}
         subMenu = std_separator    ;----------------------------------------------	
         subMenu = iacSteps,        "I&dle Steps",                    0, { IdleCtl == 2 || IdleCtl == 3 || IdleCtl == 5 && (ECUType == 1 || ECUType == 2)}
         subMenu = ipwBins,         "Idle &PWM Dutycycle",            0, { IdleCtl == 4 }	
         subMenu = std_separator    ;----------------------------------------------
         subMenu = alphaMAPMap,     "Alpha-&N MAP Table",             0, { algorithm > 0 && (ECUType == 1 || ECUType == 2)} 
         subMenu = std_separator    ;----------------------------------------------
         subMenu = MAFtable1,       "&MAF Correction Table",          0, { MAFOption > 0 && (ECUType == 1 || ECUType == 2)}
 
   menuDialog = main
      menu = "Tools"
         subMenu = std_ms2gentherm, "Calibrate T&hermistor Tables...",0,  { ECUType == 1 || ECUType == 2}
         subMenu = std_ms2geno2,    "Calibrate &AFR Table...",        0,  { ECUType == 1 || ECUType == 2}
         subMenu = mafTableBurner,  "Calibrate &MAF Table...",        0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}         
         subMenu = sensorCal,       "&Sensor Calibration...",         0,  { ECUType == 1 || ECUType == 2}
         subMenu = std_trigwiz,     "Tri&gger Wizard...",             0,  { ECUType == 1 || ECUType == 2}
	     subMenu = injector_test,   "&Injector Test Mode",            0,  { ECUType == 1 || ECUType == 2}
         subMenu = canOutmsgBurner, "Configure CAN Outmsg",           0,  { ECUType == 1 || ECUType == 2 || ECUType == 3} 		 

   menu = "Help"
         subMenu = helpGeneral,     "&MS-II Info"
         subMenu = sensorHelp,      "&Sensor Calibration"
         subMenu = burnHelp,        "&Burning Values to ECU"

;-------------------------------------------------------------------------------

[UserDefined]

   dialog = generalSettings, "General Settings"
      topicHelp = "http://www.megamanual.com/mt29.htm#sg"
      field = "ECU Type",                 ECUType
      field = "!MUST set ECU Type before editting other values."
      field = "Engine displacement",      CID,                 { ECUType == 1 || ECUType == 2}
      field = "Injector Flow Rate",       fRate,
      field = "Injection Timing Delay",   InjStart,            { ECUType == 1 || ECUType == 2}
;     field = "#System"
;     field = "Temperature Units",        tempUnits,           { ECUType == 1 || ECUType == 2}
      field = "Dual Table Use",           dualTable,           { ECUType == 1 || ECUType == 2}
      field = "Barometric Correction",    baroCorr,            { ECUType == 1 || ECUType == 2}
      #  set X_TAU_VISIBLE
      #if X_TAU_VISIBLE
      field = "X-Tau Usage",            xTauOption,            { ECUType == 1 || ECUType == 2}
      #endif
      field = "Prime, ASE, WUE & Baro Tables", CWOption,       { ECUType == 1 || ECUType == 2}

   field = "#Input Smoothing Factors"
      field = "MAP/MAF Averaging Lag Factor", mapLF,           { ECUType == 1 || ECUType == 2}
      field = "RPM Averaging Lag Factor",    rpmLF,            { ECUType == 1 || ECUType == 2}
      field = "TPS Averaging Lag Factor",    tpsLF,            { ECUType == 1 || ECUType == 2}
      field = "Lambda Averaging Lag Factor", egoLF,            { ECUType == 1 || ECUType == 2}
      field = "CLT/IAT/Battery Lag Factor",  adcLF,            { ECUType == 1 || ECUType == 2}
      field = "Knock Averaging Lag Factor",  knkLF,            { ECUType == 1 || ECUType == 2}

   field = "#Sampling Rates"
      field = "TPS Sample Rate",             tpsdotSample,     { ECUType == 1 || ECUType == 2}
      field = "MAP Sample Rate",             mapdotSample,     { ECUType == 1 || ECUType == 2}

   dialog = revLimiter, "Rev Limiter"
      topicHelp = "http://www.megamanual.com/mt29.htm#sr"
      field = "Algorithm",                   RevLimOption
      field = "Maximum Retard",              RevLimMaxRtd, { RevLimOption == 1 }
      field = "Lower Rev Limit",             RevLimRpm1
      field = "Upper Rev Limit",             RevLimRpm2

   dialog = flexFuelSettings, "Flex Fuel Settings"
      topicHelp = "http://www.megamanual.com/mt29.htm#sf"
      field = "Flex Fuel Sensor",           flexFuel
      field = "Frequency (low)",            fuelFreq0,   { flexFuel > 0 }
      field = "Fuel Correction (low)",      fuelCorr0,   { flexFuel > 0 }
      field = "Timing Correction (low)",    fuelSpkDel0, { flexFuel > 0 }
      field = "Frequency (high)",           fuelFreq1,   { flexFuel > 0 }
      field = "Fuel Correction (high)",     fuelCorr1,   { flexFuel > 0 }
      field = "Timing Correction (high)",   fuelSpkDel1, { flexFuel > 0 }

   dialog = otherFuel, "Other Fuel Settings"
      topicHelp = "http://www.megamanual.com/mt29.htm#so"	  
      field = "#Engine Start Up"
      field = "Max. Cranking Speed",        crankingRPM,      { 1 }
	  field = "TPS for Flood Clear Mode",   floodClear
      field = "#VE Table Adjustments"
      field = "(May have to save MSQ and reload to get to stick)"
      field = "VE/SPK/AFR table index",    VEIXOptn,         { 1 }
      field = "    - For MAP/Baro also set/unset MAPbaro in Properties -"
      field = "    - Must use PID43 for MAF only -"
      field = "AFR Table Fuel Calc Usage",  AFRMult,          { 1 }
      field = "AFR Stioch. Ratio",          AFRStoichNB,      { AFRMult == 1 }
      field = "AFR Stioch. Ratio",          AFRStoichWB,      { AFRMult == 2 }
      field = "#Two-Point Prime"
      field = "Prime Pulse Cold PW",        primePulseCold,   { CWOption == 0 }
      field = "Prime Pulse Hot PW",         primePulseHot,    { CWOption == 0 }
      field = "Prime Delay", prime_delay
      field = "#Additional Fuel (switched by E0 low or cyclic)"

#if n2o
      field = "Nitrous Oxide Enrichment",   n2oEnrich
	  field = "Spark Retard When N2O Active", spkN2O
#else 
      field = "Fuel Added to Base PW",      pwImpulse
      field = "#Additional Fuel (cyclic only)"
      field = "Time Between Added Fuel",    impulseSec
      field = "Number of Cycles",           nImpulse
#endif
   
  dialog = aseSettings, "AfterStart Enrichment Settings"
      topicHelp = "http://www.megamanual.com/mt29.htm#ss"    
      field = "#Hot AfterStart Enrichment"
      field = "ASE Hot Start Enable",    ASEHot

      field = "#Two-Point AfterStart Enrich"
      field = "ASE Cold Percent",        asePctCold,    { CWOption == 0 }
      field = "ASE Hot Percent",         asePctHot,     { CWOption == 0 }
      field = "ASE Cold Count",          aseCountCold,  { CWOption == 0 }
      field = "ASE Hot Count",           aseCountHot,   { CWOption == 0 }
  
  dialog = accSettings, "Accel Enrichment Configuration"
      topicHelp = "http://www.megamanual.com/mt29.htm#sl"
      field = "#AE RPM Scaling (for non-XTau accel)"
      field = "Low RPM Threshold",       ae_lorpm,
      field = "High RPM Threshold",      ae_hirpm,
  
   dialog = baroCorrection, "2-Point Barometric Correction"
      topicHelp = "http://www.megamanual.com/mt29.htm#sb"
      field = "#Barometric Correction"
      field =    "At total vacuum ",     bcor0
      field =    "Rate",                 bcormult

   dialog = xTauSettings, "X-Tau MAPdot Settings"
      topicHelp = "http://www.megamanual.com/mt29.htm#um"
      field = "#MAPdot Thresholds for transition to X, Tau Decel Tables"
      field = "Start Transition",  MapThreshXTD
      field = "Finish Transition",  MapThreshXTD2      
      field = "#"
      field = "#MAPdot trending threshhold is the start of"
      field = "#Map Trending for faster AE/ XTau enrichment"
      field = "MAPdot Trending Threshhold",        MapThreshXTA
      field = "Max. MAP added per sample",         trendmapLimit
	  
   dialog = injChars, "Injector Characteristics"
      topicHelp = "http://www.megamanual.com/mt29.htm#sn"
      field = "Injector Open Time",         injOpen
      field = "Battery Voltage Correction", battFac
      field = "PWM Current Limit",          injPwmP
      field = "PWM Time Threshold",         injPwmT
      field = "!Injector PWM Period",       injPwmPd ; !
      field = "!Red settings require an MS-II reboot!"

   dialog = egoControl, "EGO Control"
      topicHelp = "http://www.megamanual.com/mt29.htm#se"
      field = "EGO Sensor Type",           egoType
   #if   NARROW_BAND_EGO
      field = "NB Voltage Target",         egoTarget,    { egoType == 1 || egoType == 2}
   #elif LAMBDA
      field = "NB Lambda Target",          AFRTarget,    { egoType == 1 || egoType == 2}
   #else
      field = "NB AFR Target",             AFRTarget,    { egoType == 1 || egoType == 2}
   #endif
      field = "Ignition Events per Step",  egoCount,     { egoType == 1 || egoType == 2 ||  egoType >  2  && egoAlgorithm == 0}

      field = "Controller Step Size",      egoDelta,     { egoType == 1 || egoType == 2}
      field = "Controller Authority ±",    egoLimit,     { egoType >  0 }
      field = "Active Above Coolant Temp", egoTemp,      { egoType >  0 }
      field = "Active Above RPM",          egoRPM,       { egoType >  0 }
      field = "Active Below TPS",          TPSOXLimit,   { egoType >  0 }
      field = "Active Below MAP",          MAPOXLimit,   { egoType >  0 }

   field = "#WB Controller Settings"
      field = "Algorithm",                 egoAlgorithm, { egoType >  2 }
      field = "PID Proportional Gain",     egoKP,        { egoType >  2 }
      field = "Transport Delay 1",         egoKdelay1,   { egoType >  2 && egoAlgorithm > 0 }
      field = "Transport Delay 2",         egoKdelay2,   { egoType >  2 && egoAlgorithm > 0 }
      field = "PID Integral",              egoKI,        { egoType >  2 && egoAlgorithm > 1 }
      field = "PID Derivative",            egoKD,        { egoType >  2 && egoAlgorithm > 1 }
      field = "#" 
      field = "#To stop Closed Loop but not sensor "
      field = "#readings, set 'Active Below MAP' to 0"

   dialog = amcSettings, "Automatic Mixture Control"
      topicHelp = "http://www.megamanual.com/mt29.htm#sm"
      field = "!Must have EGO correction enabled for AMC to operate!"
      field = "Automatic Mixture Control", AMCOption,    { egoType   > 0 }
      field = "Step size",                 AMCstep,      { AMCOption > 0 }
      field = "Minimum VE Change",         AMCdve,       { AMCOption > 0 }
      field = "Vertex Tolerance",          AMCve_rpm,    { AMCOption > 0 }
      field = "Vertex Tolerance",          AMCve_map,    { AMCOption > 0 }
      field = "Table Change Interval",     AMCramve_dt,  { AMCOption > 0 }
      field = "Flash Update Interval",     AMCT_thresh,  { AMCOption > 1 }
      field = "Update After",              AMCupdate_thresh, { AMCOption > 1 }
   
   dialog = alphaNOptions, "Alpha-N Blending"
      topicHelp = "http://www.megamanual.com/mt29.htm#sa"
      field = "Low RPM Blend Threshold - AlphaN below",  alpha_lorpm
      field = "High RPM Blend Threshold - SD above",     alpha_hirpm
      field = "Invert above AlphaN/SD blend logic",      alphDir
      field = "Baro Spark Advance (deg/kPa below 100)",  alpha_baro_spkadv

   dialog = ignitionOptions, "Base Ignition Settings"
      topicHelp = "http://www.megamanual.com/mt29.htm#ib"
      field = "#General Ignition"
      field = "Trigger Offset",            triggerOffset
      field = "Skip Pulses",               no_skip_pulses
      field = "#Prediction Settings",      
      field = "Predictor Algorithm",       PredOpt
      field = "Alpha",                     alpha,           { PredOpt == 1 }
      field = "Beta",                      beta,            { PredOpt == 1 }
      field = "Gamma",                     gamma,           { PredOpt == 1 }
      field = "#Tach Signal Masking" 
      field = "Time Mask",                 ICISR_tmask
      field = "Percentage Mask",           ICISR_pmask
      field = "#Next-Pulse Tolerance"
      field = "   Cranking",               crankTolerance
      field = "   After-start",            asTolerance
      field = "   Normal Running",         pulseTolerance
      field = "Check Tach Sync Options",   acc_synchk,      { triggerTeeth == 0 }
      field = "!Ignition Input Capture",   ICIgnCapture,    { ICIgnOption != 2 && ICIgnOption != 3 } ; !
      field = "!Cranking Trigger",         ICCrankTrigger,  { ICIgnOption != 2 && ICIgnOption != 3 } ; !
      field = "!Coil Charging Scheme",     ICIgnOption  ; !
      field = "!Spark Output",             spkout_hi_lo ; !

 
   dialog = AdvncdignitionOptions, "Advanced Ignition Options"
      topicHelp = "http://www.megamanual.com/mt29.htm#ia"
      field = "#Trigger Wheel Only (0 is no trigger wheel)"
      field = "#Set only with ENGINE OFF"
      field = "!Trigger Wheel Teeth",          triggerTeeth
      field = "!Missing Teeth",                No_Miss_Teeth,  { triggerTeeth > 0 }
      field = "!Skip Teeth",                   No_Skip_Teeth,  { triggerTeeth > 0 }
      field = "!Delay Teeth",                  Delay_Teeth,    { triggerTeeth > 0 }
      field = "#Dual Spark Ignition Options"
      field = "!Dual Spark Options",            DualSpkOptn
      field = "Offset (advance) for Output #2", OddAng
      field = "#IAT-based Spark Retard Limiting Options"
      field = "Start IAT Retard ",              MatRtdRPMLo
      field = "Full IAT Retard ",               MatRtdRPMHi
      field = "#Signal Delay Parameters"
      field = "FET Ouput Delay",                fet_delay
      field = "VR Input Delay",                 vr_delay     
      field = "!Red settings require an MS-II reboot!"

   dialog = dwellSettings, "Dwell Settings"
      topicHelp = "http://www.megamanual.com/mt29.htm#iw"
      field = "Maximum Dwell Duration",        max_coil_dur
      field = "Maximum Spark Duration",        max_spk_dur
      field = "Acceleration Compensation",     dwellAcc
      field = "#Battery Voltage Compensation"
      ; Make this an array2D when available.
      array1D   = "", "Voltage  %INDEX% ", dwellVolts
      array1D   = "", "Duration at Voltage %INDEX% ", dwellDuration

   dialog = idleControl, "Idle Control"
      topicHelp = "http://www.megamanual.com/mt29.htm#sd"
      field = "Algorithm",                     IdleCtl
      field = "Fast Idle Temperature",         fastIdleT,    { IdleCtl == 1 }
      field = "Time Step Size",                IACtstep,     { IdleCtl == 2 || IdleCtl == 3 || IdleCtl == 5 }
      field = "Acceleration Step Size",        IACaccstep,   { IdleCtl == 2 || IdleCtl == 3 || IdleCtl == 5 }
      field = "Minimum # steps to move",       IACminstep,   { IdleCtl == 2 || IdleCtl == 3 || IdleCtl == 5 }
      field = "!PWM Frequency",                IACpwm_step,  { IdleCtl == 4 }
      field = "!Start Value (retract)",        IACStart,     { IdleCtl > 1 } ; !
      field = "Cranking Position (extend)",    IACcrankpos,  { IdleCtl > 1 }
      field = "Crank-to-Run Taper Time",       IACcrankxt,   { IdleCtl > 1 }
      field = "Hysteresis",                    IdleHyst,     { IdleCtl >= 1 }
      field = "#Time-Based After Start (extended warm-up)"
      field = "   Cold Temperature",           IACcoldtmp,   { IdleCtl > 1 }
      field = "   Cold Position",              IACcoldpos,   { IdleCtl > 1 }
      field = "   Cold Taper Time",            IACcoldxt,    { IdleCtl > 1 }

   dialog = sensorCal, "Sensor Calibration"
      topicHelp = sensorHelp
      field = "#MAP Sensor (F1 for common values)"
      field =    "Value at 0.0 volts",   map0
      field =    "Value at 5.0 volts",   mapmax
      field = "#Barometer Sensor (usually identical to MAP)"
      field =    "Value at 0.0 volts",   baro0
      field =    "Value at 5.0 volts",   baromax

   dialog = knockSettings, "Knock Sensor Settings"
      topicHelp = "http://www.megamanual.com/mt29.htm#ik"
      field = "Knock Control",        knkOption
      field = "#Detection"
      field = "Threshold Direction",  knkDirection,   { knkOption > 0 }
      field = "knock value at 0V",    knock0
      field = "knock value at 5V",    knockmax
      field = "Knock Count",          knk_ndet,       { knkOption > 0 }
      field = "No Knock Above MAP",   knk_maxmap,     { knkOption > 0 }
      field = "No Knock Below RPM",   knk_lorpm,      { knkOption > 0 }
      field = "No Knock Above RPM",   knk_hirpm,      { knkOption > 0 }
      field = "#Retarding"
      field = "Maximum Retard",       knk_maxrtd,     { knkOption > 0 }
      field = "Retard Check Time",    knk_trtd,       { knkOption > 0 }
      field = "Retard Step Size",     knk_step1,      { knkOption > 0 }
      field = "#Recovery"
      field = "Advance Check Time",   knk_tadv,       { knkOption > 0 }
      field = "Advance Step Size",    knk_step2,      { knkOption > 0 }
      field = "Recovery Advance",     knk_dtble_adv,  { knkOption > 1 }

   dialog = injector_test, "Injector Test Mode"
      topicHelp = "http://www.megamanual.com/mt29.htm#oi"
      field = "!Injector test mode",  injTestMode ; !
      field = "Injector test squirts",  injTestSqrts,    { injTestMode > 0 }
      field = "Injector test PW",  injTestPW,            { injTestMode > 0 }
      field = "Injector test offtime",  injTestOffTime,  { injTestMode > 0 }
      field = "!Reboot to test, set to 'Normal Mode' to reset"

   dialog = frpmTableBins, "RPM Table Bins for Fuel Tables"
      topicHelp="http://www.megamanual.com/mt29.htm#"
      array1D   = "", "Fuel RPM  %INDEX% ", frpm_table
      field = "#Close and re-open Table(s) to see changes"

   dialog = fmapTableBins, "MAP Table Bins for Fuel Table(s)"
      topicHelp="http://www.megamanual.com/mt29.htm#"
      array1D   = "", "Fuel MAP  %INDEX% ", fmap_table
      field = "#Close and re-open Table(s) to see changes"

   dialog = srpmTableBins, "RPM Table Bins for Spark Table"
      topicHelp="http://www.megamanual.com/mt29.htm#"
      array1D   = "", "Spark RPM  %INDEX% ", srpm_table
      field = "#Close and re-open Table(s) to see changes"

   dialog = smapTableBins, "MAP Table Bins for Spark Table"
      topicHelp="http://www.megamanual.com/mt29.htm#"
      array1D   = "", "Spark MAP  %INDEX% ", smap_table
      field = "#Close and re-open Table(s) to see changes"

   dialog = tempTableBins, "Temperature Table Values"
      topicHelp="http://www.megamanual.com/mt29.htm#at"
      array1D   = "", "Temperature  %INDEX% ", tempTable
      
   dialog = XtempTableBins, "X Temperature Correction Values"
      topicHelp="http://www.megamanual.com/mt29.htm#at"
      field = "#Temperature Correction for X Enrichments"
      array1D   = "", "Correction  %INDEX% ", XClt
  
   dialog = TtempTableBins, "Tau Temperature Correction Values"
      topicHelp="http://www.megamanual.com/mt29.htm#at"
      array1D   = "", "Correction  %INDEX% ", TauClt
 
   dialog = XTrpmsdial, "X-Tau RPM Values"
      topicHelp="http://www.megamanual.com/mt29.htm#ur"
      field = "#RPM Bins for X-Tau Enrichments"                                                    
      array1D   = "", "X-Tau RPM  %INDEX% ", XTrpms

   dialog = MAFSettings, "MAF vrs. MAP Usage"
      topicHelp = "http://www.megamanual.com/mt29.htm#su"
      field = "#See Tables for MAF flow setting"
      field = "Enable MAF Use",             MAFOption
      field = "MAF Hardware Configuration", MAFpin,   { MAFOption > 0 }
      field = "Note: MAF must NOT be on MAP pin for MAF/MAP blend."
      field = "#MAP MAF Blend Settings"
      field = "MAP Only Below RPM",         MAFRPM1,  { MAFOption == 2 }
      field = "MAF Only Above RPM",         MAFRPM2,  { MAFOption == 2 }
      field = "Invert above MAP/MAF settings",       MAFDir,  { MAFOption == 2 }
      field = "#Viewing MAF in Real Time"
      field = "You can set one of the gauges on the front page to mafGauge"
      field = "to see the MAF in real time. Right click on any gauge and"
      field = "select mafGuage "
	  
   help = burnHelp, "Burning Values to ECU"
      webHelp = "http://www.megamanual.com/mt29.htm"
      text = "Occassionally, you may have trouble getting values to 'stick'"
      text = "in MegaTune. There are a few things you can try if this happens:<br><br>"
      text = "\tHit TAB after entering the value. This forces MegaTune to" 
      text = "recognize the changed value.<br>" 
      text = "\tThen 'Burn to ECU'<br><br>"	
      text = "If that doesn't work:<br><br>"	
      text = "\tChange the value (as above) and immediately save the MSQ file ('File/Save').<br>"
      text = "\tThen reload the file you just saved, and burn it when prompted.<br><br>"
      text = "This forces all the values to be burned to both flash and RAM memory, and"
      text = "should solve the problem."	
   
   help = sensorHelp, "Sensor Calibration"
      webHelp = "http://www.megamanual.com/mt29.htm#os"
      text = "MAP Sensor Calibration<br>"
      text = "<br>"
      text = "For the\tMPX4115   use\t10.6 and \t121.7<br>"
      text = "\tMPX4250\t\t10.0\t260.0<br>"
      text = "\tMPXH6300\t1.1\t315.5<br>"
      text = "\tGM 3-BAR\t1.1\t315.5<br>"
      text = "\tMPXH6400\t3.5\t416.5<br>"
      text = "<br>"
      text = "(GM 3-bar data from Dave Hartnell, http://www.not2fast.com/electronics/component_docs/MAP_12223861.pdf)<br>"
      text = "<br>"
      text = "\tSensor type\tvLo\tpLo\tvHi\tpHi\tvRef<br>"
      text = "\tMPX4115 \t0.204 v\t15 kPa\t4.794 v\t115 kPa\t5.100 v<br>"
      text = "\tMPX4250 \t0.204 v\t20 kPa\t4.896 v\t250 kPa\t5.100 v<br>"
      text = "\tMPXH6300\t0.306 v\t20 kPa\t4.913 v\t304 kPa\t5.100 v<br>"
      text = "\tGM 3-BAR\t0.631 v\t40 kPa\t4.914 v\t304 kPa\t5.100 v<br>"
      text = "\tMPXH6400\t0.200 v\t20 kPa\t4.800 v\t400 kPa\t5.000 v<br>"
      text = "<br>"
      text = "In general, use values derived from these equations:<br>"
      text = "<br>"
      text = "\tm = (pHi-pLo)/(vHi-vLo)<br>"
      text = "\tpv1 = pLo - m * vLo<br>"
      text = "\tpv2 = pv1 + m * vRef<br>"
      text = "<br>"
      text = "References:<br>"
      text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPX4115A.pdf<br>"
      text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPX4250A.pdf<br>"
      text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPXH6300A.pdf<br>"
      text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPXH6400A.pdf<br>"
      text = "<br>"
      text = "Barometer Sensor Calibration<br>"
      text = "<br>"
      text = "If your system has an external barometer sensor, separate from the MAP"
      text = "sensor, then use these values to calibrate it properly.  If you have"
      text = "a standard MS installation, then copy your MAP sensor values here.<br>"
      text = "<br>"
      text = "Barometric Correction Calibration<br>"
      text = "<br>"
      text = "Correction for barometric effects is performed using the linear function below.<br>"
      text = "<br>"
      text = "\tcorrection = correction_0 + (rate * barometer) / 100<br>"
      text = "<br>"
      text = "'At total vacuum' contains the total correction at a barometer reading"
      text = "of 0 kPa (you are on the moon).  The 'Rate' contains the percentage per 100"
      text = "kPa to scale the barometer value.  Using the default values of 147 and -47,"
      text = "we see that for a barometer of 100 kPa, we have 100% correction.<br>"
      text = "<br>"
      text = "\tcorrection = 147 + (-47*100) / 100 = 100%"


   help = helpGeneral, "MS-II General Info"
      webHelp = "http://www.megamanual.com/mt29.htm"
      text = "Al Grippo and Bruce Bowling have created MegaSquirt-II, which"
      text = "is a plug-in daughter card that replaces the 8-bit MC68HC908GP32"
      text = "with a 16-bit MC9S12C64 processor."
      text = "<br>"
      text = "It is basically a plug-in processor card that has the MC9S12C64"
      text = "processor plus support hardware as well as a stepper motor chip,"
      text = "and an ignition module controller.  The embedded code is written"
      text = "in C, rather than assembly language, so it should be more accessible"
      text = "to more programmers (Stephane Carrez has ported GCC to the HC12"
      text = "processor so, although it doesn't use the full 9S12 instruction"
      text = "set, we are able to use his version to write code for the MS-II).<br>"
      text = "<br>"
      text = "For current documentation, click the Web Help button below, or for"
      text = "support questions visit http://www.msefi.com/."

;-------------------------------------------------------------------------------

[CurveEditor]
   curve = coldAdvance, "Cold Ignition Advance Offset"
      topicHelp   = "http://www.megamanual.com/mt29.htm#ec"
      columnLabel = "Coolant", "Offset"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif 
      yAxis       = -10,  10, 5
      xBins       = tempTable, coolant
      yBins       = cold_adv_table
      gauge       = cltGauge

   curve = iacSteps, "IAC Steps"
      topicHelp   = "http://www.megamanual.com/mt29.htm#ed"
      columnLabel = "Coolant", "IAC Steps"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0, 300, 7
      xBins       = tempTable, coolant
      yBins       = iacstepTable
      gauge       = cltGauge

   curve = ipwBins, "PWM Idle Duty Cycle"
      topicHelp   = "http://www.megamanual.com/mt29.htm#ep"
      columnLabel = "Coolant", "Idle PWM"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0, 100, 6
      xBins       = tempTable, coolant
      yBins       = ipwmTable
      gauge       = cltGauge

   curve = primingPW, "Priming Pulsewidth"
     topicHelp   = "http://www.megamanual.com/mt29.htm#rm"
      columnLabel = "Coolant", "Prime PW"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0,  20, 5
      xBins       = tempTable, coolant
      yBins       = primePWTable
      gauge       = cltGauge

   curve = crankingPW, "Cranking Pulsewidth"
     topicHelp   = "http://www.megamanual.com/mt29.htm#rn"
      columnLabel = "Coolant", "Cranking PW"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0,  20, 5
      xBins       = tempTable, coolant
      yBins       = crankPWTable
      gauge       = cltGauge

   curve = asePct, "Afterstart Enrichment Percentage"
     topicHelp   = "http://www.megamanual.com/mt29.htm#rs"
      columnLabel = "Coolant", "Afterstart"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0, 100, 6
      xBins       = tempTable, coolant
      yBins       = asePctTable
      gauge       = cltGauge

   curve = aseTaper, "Afterstart Enrichment Taper"
     topicHelp   = "http://www.megamanual.com/mt29.htm#re"
      columnLabel = "Coolant", "Taper"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0, 500, 6
      xBins       = tempTable, coolant
      yBins       = aseCntTable
      gauge       = cltGauge

   curve = matBasedRetard, "IAT-Based Spark Timing Retard"
     topicHelp   = "http://www.megamanual.com/mt29.htm#eb"
      columnLabel = "IAT", "Retard"
      xAxis       = 100, 300, 9
      yAxis       =   0,  15, 7
      xBins       = matTemps, mat
      yBins       = matRetard
      gauge       = matGauge

   curve = knockThresholdCurve, "Knock Threshold"
     topicHelp   = "http://www.megamanual.com/mt29.htm#ik"
      columnLabel = "RPM", "Threshold"
      xAxis       =   0, 6000, 7
      yAxis       =   0,  5.0, 6
      xBins       = knk_rpm, rpm
      yBins       = knk_thresh
      gauge       = tachometer

   curve = barometerCorr, "Non-Linear Barometric Correction"
     topicHelp   = "http://www.megamanual.com/mt29.htm#rc"
      columnLabel = "Barometer", "Correction"
      xAxis       =  60, 120, 7
      yAxis       = -30,  30, 7
      xBins       = baroCorrVals, barometer
      yBins       = baroCorrDelta
      gauge       = barometerGauge

   curve = manifoldTempCorr, "Non-Linear IAT (intake air temperature) Fuel Correction"
     topicHelp   = "http://www.megamanual.com/mt29.htm#ea"
      columnLabel = "IAT", "Correction"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =  -30,  30, 7
      xBins       = matCorrTemps, mat
      yBins       = matCorrDelta
      gauge       = matGauge
   
   curve = XAccTable, "X Accel Fuel Correction"
     topicHelp   = "http://www.megamanual.com/mt29.htm#ua"
      columnLabel = "RPM", "Correction"
      xAxis       =    0,  8000, 4
      yAxis       =    0,   120, 4
      xBins       = XTrpms, rpm
      yBins       = XAccTable
      gauge       = xTauGauge1
        
   curve = XDecTable, "X Decel Fuel Correction"
     topicHelp   = "http://www.megamanual.com/mt29.htm#ud"
      columnLabel = "RPM", "Correction"
      xAxis       =    0,  8000, 9
      yAxis       =    0,   120, 9
      xBins       = XTrpms, rpm
      yBins       = XDecTable
      gauge       = xTauGauge1
       
   curve = TauAccTable, "Tau Accel Fuel Correction"
     topicHelp   = "http://www.megamanual.com/mt29.htm#uc"
      columnLabel = "RPM", "time"
      xAxis       =    0,  8000, 9
      yAxis       =    0,  1000, 9
      xBins       = XTrpms, rpm
      yBins       = TauAccTable
      gauge       = xTauGauge1
 
   curve = TauDecTable, "Tau Decel Correction"
     topicHelp   = "http://www.megamanual.com/mt29.htm#ue"
      columnLabel = "RPM", "time"
      xAxis       =    0,  8000, 9
      yAxis       =    0,  1000, 9
      xBins       = XTrpms, rpm
      yBins       = TauDecTable
      gauge       = xTauGauge1 
      
   curve = XCltTable, "X (Puddling) Temp. Correction Factors"
     topicHelp   = "http://www.megamanual.com/mt29.htm#ux"
      columnLabel = "Temperature", "Correction"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =    0,   600, 9
      xBins       = tempTable
      yBins       = XClt
      gauge       = cltGauge 
      
   curve = TCltTable, "Tau (Time) Temp. Correction Factors"
     topicHelp   = "http://www.megamanual.com/mt29.htm#ut"
      columnLabel = "Temperature", "time"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =    0,   600, 9
      xBins       = tempTable
      yBins       = TauClt
      gauge       = cltGauge                 

	  
   curve = MAFtable1, "MAF Correction Table (to alter default MAF curve)"
     topicHelp   = "http://www.megamanual.com/mt29.htm#em"
      columnLabel = "MAF Flow", "Correction"
      xAxis       =  0, 300, 11
      yAxis       =  0, 255, 11
      xBins       = MAFFlow, maf
      yBins       = MAFCor
      gauge       = mafGauge
	  
	  
[TableEditor]

#if MAPbaro

   table = veTable1Tbl, veTable1Map, "VE Table 1 (MAP/baro)", 2
     topicHelp   = "http://www.megamanual.com/mt29.htm#a1"
      ;             constant,   variable
      xBins       = frpm_table, rpm,   readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = veTable1

      upDownLabel = "RICHER", "LEANER"
      gridHeight  = 2.0
      gridOrient  = 250,   0, 340 ; Space 123 rotation of grid in degrees.

   table = veTable2Tbl, veTable2Map, "VE Table 2", 2
     topicHelp   = "http://www.megamanual.com/mt29.htm#a1"
      xBins       = frpm_table, rpm,   readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = veTable2

      upDownLabel = "RICHER", "LEANER"
      gridHeight  = 2.0
      gridOrient  = 250,   0, 340


#else

   ;       table_id,    map3d_id,    "title",      page
   table = veTable1Tbl, veTable1Map, "VE Table 1 (MAP)", 2
     topicHelp   = "http://www.megamanual.com/mt29.htm#a1"
      ;             constant,   variable
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = veTable1

      upDownLabel = "RICHER", "LEANER"
      gridHeight  = 2.0
      gridOrient  = 250,   0, 340 ; Space 123 rotation of grid in degrees.


   table = veTable2Tbl, veTable2Map, "VE Table 2", 2
     topicHelp   = "http://www.megamanual.com/mt29.htm#a1"
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = veTable2

      upDownLabel = "RICHER", "LEANER"
      gridHeight  = 2.0
      gridOrient  = 250,   0, 340

#endif

#if LAMBDA
   table = afrTable1Tbl, afrTable1Map, "Lambda Table 1", 1
      gridHeight  = 3.0
#else
   table = afrTable1Tbl, afrTable1Map, "AFR Table 1", 1
      gridHeight  = 1.0
#endif
     topicHelp   = "http://www.megamanual.com/mt29.htm#af"
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = afrTable1
      upDownLabel = "LEANER", "RICHER"
      gridOrient  = 250,   0, 340

#if LAMBDA
   table = afrTable1Tblix, afrTable1MapIX, "Lambda Table 1", 1
      gridHeight  = 3.0
#else
   table = afrTable1Tblix, afrTable1MapIX, "AFR Table 1", 1
      gridHeight  = 1.0
#endif
     topicHelp   = "http://www.megamanual.com/mt29.htm#af"
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix,   readonly
      zBins       = afrTable1
      upDownLabel = "LEANER", "RICHER"
      gridOrient  = 250,   0, 340

#if LAMBDA
   table = afrTable2Tbl, afrTable2Map, "Lambda Table 2", 1
      gridHeight  = 3.0
#else
   table = afrTable2Tbl, afrTable2Map, "AFR Table 2", 1
      gridHeight  = 1.0
#endif
     topicHelp   = "http://www.megamanual.com/mt29.htm#af"
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = afrTable2
      upDownLabel = "LEANER", "RICHER"
      gridOrient  = 250,   0, 340

#if LAMBDA
   table = afrTable2Tblix, afrTable2MapIX, "Lambda Table 2", 1
      gridHeight  = 3.0
#else
   table = afrTable2Tblix, afrTable2MapIX, "AFR Table 2", 1
      gridHeight  = 1.0
#endif
     topicHelp   = "http://www.megamanual.com/mt29.htm#af"
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix,   readonly
      zBins       = afrTable2
      upDownLabel = "LEANER", "RICHER"
      gridOrient  = 250,   0, 340

   table = ignitionTbl, ignitionMap, "Spark Advance Table", 2
     topicHelp   = "http://www.megamanual.com/mt29.htm#ap"
      xBins       = srpm_table, rpm, readonly
      yBins       = smap_table, kpaix, readonly
      zBins       = advanceTable
      upDownLabel = "ADVANCING", "RETARDING"
      gridHeight  = 3.0
      gridOrient  = 250,   0, 340

   table = alphaMAPTbl, alphaMAPMap, "Alpha-N MAP Table", 1
     topicHelp   = "http://www.megamanual.com/mt29.htm#en"
      xBins       = amap_rpm, rpm
      yBins       = amap_tps, tps
      zBins       = alphaMAPtable
      upDownLabel = "UP", "DOWN"
      gridHeight  = 2.0
      gridOrient  = 250,   0, 340


;-------------------------------------------------------------------------------

[GaugeConfigurations]

   ;-------------------------------------------------------------------------------
   ;  Notes on some of the gauges.
   ;
   ;  The accelEnrichGauge is now a composite of both acceleration enrichment
   ;  and deceleration enleanment numbers.  See the definition of the variable
   ;  accDecEnrich in the OutputChannels section.
   ;
   ;  David Hooke contributed the lambda gauge and associated transfer
   ;  function files.
   ;
   ;  The lambda gauge is the best way (my opinion) to report data from a
   ;  wide band EGO gauge, it standardizes the output irrespective of fuel
   ;  or mix of fuels, so you needn't do any brainwork to know if your 75%
   ;  gasoline and 25% methanol is rich at 10:1 or not.
   ;
   ;  Use the file WBlambda100AVR.inc, if using a standard ADC (e.g., AVR cpu).
   ;  Use the file WBlambda100MOT.inc, if using a biased ADC (e.g., MOT cpu).
   ;-------------------------------------------------------------------------------
   ; Define a gauge's characteristics here, then go to a specific layout
   ; block (Tuning or FrontPage) and use the name you've defined here to
   ; display that gauge in a particular position.
   ;
   ; Name  = Case-sensitive, user-defined name for this gauge configuration.
   ; Var   = Case-sensitive name of variable to be displayed, see the
   ;         OutputChannels block in this file for possible values.
   ; Title = Title displayed at the top of the gauge.
   ; Units = Units displayed below value on gauge.
   ; Lo    = Lower scale limit of gauge.
   ; Hi    = Upper scale limit of gauge.
   ; LoD   = Lower limit at which danger color is used for gauge background.
   ; LoW   = Lower limit at which warning color is used.
   ; HiW   = Upper limit at which warning color is used.
   ; HiD   = Upper limit at which danger color is used.
   ; vd    = Decimal places in displayed value
   ; ld    = Label decimal places for display of Lo and Hi, above.

   ;Name               Var            Title                 Units     Lo     Hi     LoD    LoW   HiW   HiD vd ld

   advBucketGauge    = veTuneValue,   "Advance Bucket",     "degrees", 0,    55,    -1,     -1,  999,  999, 1, 1
   advdegGauge       = advance,       "Ignition Advance",   "degrees", 5,    50,    -1,     -1,  999,  999, 1, 1
   IACgauge          = iacstep,       "IAC position",       "steps",   0,   255,    -1,     -1,  999,  999, 0, 0
   dwellGauge        = dwell,         "Dwell",              "mSec",    0,    10,   0.5,    1.0,  6.0,  8.0, 1, 1
   PWMIdlegauge      = idleDC,        "Idle PWM%",          "%",       0,   100,    -1,     -1,  999,   90, 0, 0
   accelEnrichGauge  = accDecEnrich,  "Accel Enrich",       "%",       0,   300,   -999,  -999,  999,  999, 0, 0
   accelEnrichPcnt   = accEnrichPcnt, "Accel Enrich",       "%",      50,   150,     -1,    -1,  999,  999, 0, 0
   accelEnrichMS     = accEnrichMS,   "Accel Enrich",    "msec",       0,  25.5,     -1,    -1,  999,  999, 1, 1
   decelEnrichPcnt   = decEnrichPcnt, "Decel Enrich",       "%",      50,   150,     -1,    -1,  999,  999, 0, 0
   decelEnrichMS     = decEnrichMS,   "Decel Enrich",    "msec",   -25.5,   0.0,    -25,   -25,    1,    1, 1, 1
   afr1Gauge         = afr1,          "Air:Fuel Ratio",     "",       10,  19.4,     12,    13,   15,   16, 2, 2
   afr2Gauge         = afr2,          "Air:Fuel Ratio 2",   "",       10,  19.4,     12,    13,   15,   16, 2, 2
   clockGauge        = seconds,       "Clock",              "Seconds", 0,   255,     10,    10,  245,  245, 0, 0
   dutyCycle1Gauge   = dutyCycle1,    "Duty Cycle 1",       "%",       0,   100,     -1,    -1,   85,   90, 1, 1
   dutyCycle2Gauge   = dutyCycle2,    "Duty Cycle 2",       "%",       0,   100,     -1,    -1,   85,   90, 1, 1
   egoCorrGauge      = egoCorrection, "EGO Correction",     "%",      50,   150,     90,    99,  101,  110, 0, 0
   egoCorrGauge1     = egoCorrection1,"EGO Correction 1",   "%",      50,   150,     90,    99,  101,  110, 0, 0
   egoCorrGauge2     = egoCorrection2,"EGO Correction 2",   "%",      50,   150,     90,    99,  101,  110, 0, 0
   egoGauge          = egoVoltage,    "Exhaust Gas Oxygen", "volts",   0,   1.0,    0.2,   0.3,  0.7,  0.8, 2, 2
   kpaixGauge        = kpaix,         "Table Load Index",   "kPa",     0,   255,      0,    20,  200,  245, 1, 0
   knockGauge        = knockRetard    "Knock Retard",       "deg",     0,  25.0,     -1,    -1,  5.0, 10.0, 1, 1
   lambda1Gauge      = lambda1,       "Lambda",             "",      0.5,   1.5,    0.5,   0.7,    2,  1.1, 2, 2
   lambda2Gauge      = lambda2,       "Lambda",             "",      0.5,   1.5,    0.5,   0.7,    2,  1.1, 2, 2
   gammaEnrichGauge  = gammaEnrich,   "Gamma Enrichment",   "%",      50,   150,     -1,    -1,  151,  151, 0, 0
   mapGauge          = map,           "Engine MAP",         "kPa",     0,   255,      0,    20,  200,  245, 1, 0
   mafGauge          = maf,           "MAF Air flow",       "g/sec",   0,   650,      0,   200,  480,  550, 2, 0
   barometerGauge    = barometer,     "Barometer",          "kPa",    60,   120,      0,    20,  200,  245, 1, 0
   calcMapGauge      = kpa,           "calcMAP",            "kPa",     0,   255,      0,    20,  200,  245, 1, 0
   pulseWidth1Gauge  = pulseWidth1,   "Pulse Width 1",      "mSec",    0,  25.5,    1.0,   1.2,   20,   25, 3, 1
   pulseWidth2Gauge  = pulseWidth2,   "Pulse Width 2",      "mSec",    0,  25.5,    1.0,   1.2,   20,   25, 3, 1
   tachometer        = rpm,           "Engine Speed",       "RPM",     0,  8000,    300,   500, 5000, 6000, 0, 0
   throttleGauge     = throttle,      "Throttle Position",  "%",       0,   100,     -1,     1,   90,  100, 0, 0
   deltaTGauge       = deltaT,        "Timing Delta",       "uS",      0, 25000,      0,     0,25000, 25000, 0, 0 
   veBucketGauge     = veTuneValue,   "VE Value",           "%",       0,   120,     -1,    -1,  999,  999, 0, 0
   veGauge           = veCurr1,       "VE Current",         "%",       0,   120,     -1,    -1,  999,  999, 0, 0
   voltMeter         = batteryVoltage, "Battery Voltage",    "volts",   7,    21,     9,    10,   16,   17, 2, 2
   warmupEnrichGauge = warmupEnrich,  "Warmup Enrichment",  "%",     100,   150,     -1,    -1,  101,  105, 0, 0
   xTauGauge1        = xTauFuelCorr1, "X-Tau Correction1",   "%",      0,   200,     40,    70,  130,  160, 0, 0
   xTauGauge2        = xTauFuelCorr2, "X-Tau Correction2",   "%",      0,   200,     40,    70,  130,  160, 0, 0
#if CELSIUS
  #if EXPANDED_CLT_TEMP
   cltGauge          = coolant,       "Coolant Temp",       "C",     -40,   600,     65,    93,  162,  176, 0, 0
   matGauge          = mat,           "Intake Air Temp",    "C",     -40,   110,    -15,     0,   95,  100, 0, 0
  #else
   cltGauge          = coolant,       "Coolant Temp",       "C",     -40,   120,    -15,     0,   95,  105, 0, 0
   matGauge          = mat,           "Intake Air Temp",    "C",     -40,   110,    -15,     0,   95,  100, 0, 0
  #endif
#else
  #if EXPANDED_CLT_TEMP
   cltGauge          = coolant,       "Coolant Temp",       "°F",    -40,   600,    150,   200,  325,  350, 0, 0
   matGauge          = mat,           "Intake Air Temp",    "°F",    -40,   215,      0,    30,  200,  210, 0, 0
  #else
   cltGauge          = coolant,       "Coolant Temp",       "°F",    -40,   250,      0,    30,  200,  220, 0, 0
   matGauge          = mat,           "Intake Air Temp",    "°F",    -40,   215,      0,    30,  200,  210, 0, 0
  #endif
#endif
   e85Gauge          = fuelCorrection,"E85 Fuel Correction", "%",    100,   200,     99,    99,  164,  170, 0, 0 
   ethanolGas        = fuelComposition, "Ethanol Percentage","%",      0,   100,     -1,    -1,   85,  101, 0, 0
   triggers±         = trig_fix,      "Triggers add/sub",     "",   -200,   200,   -100,   -10,   10,  100, 0, 0
   Synch Stat        = synch,          "Synch Status",        "",      0,     5,      0,     0,    5,    5, 0, 0
   tachCount         = tachCount,     "Number Tach Pulses",   "",      0,  1000,     -1,    -1, 1000, 1000, 0, 0   

;-------------------------------------------------------------------------------

[FrontPage]
#if   NARROW_BAND_EGO
   egoLEDs         =  0.0, 1.0,  0.5 ; Voltage settings.
#elif LAMBDA
   egoLEDs         =  1.5, 0.5,  1.0 ; Lambda settings.
#else
   egoLEDs         = 19.7, 9.7, 14.7 ; Afr settings.
#endif

   ; Gauges are numbered left to right, top to bottom.
   ;
   ;    1  2  3  4
   ;    5  6  7  8

   gauge1 = tachometer
   gauge2 = throttleGauge
   gauge3 = pulseWidth1Gauge
#if   NARROW_BAND_EGO
   gauge4 = egoGauge
#elif LAMBDA
   gauge4 = lambda1Gauge
#else
   gauge4 = afr1Gauge
#endif
   gauge5 = mapGauge
#if IAC_GAUGE
   gauge6 = IACgauge
#elif PWM_GAUGE
   gauge6 = PWMIdlegauge
#else
   gauge6 = matGauge
#endif
   gauge7 = advdegGauge
   gauge8 = dwellGauge


   ;----------------------------------------------------------------------------
   ; Indicators
   ;               expr         off-label          on-label, off-bg, off-fg, on-bg, on-fg
   ;   indicator = { tpsaen }, "Not Accelerating", "AE",     cyan,   white,  red,   black
   ;
   ; Look in the new colorScheme.ini for the basic ones, add more or tell me what to add.

   indicator = { ECUType == 1 || ECUType == 2 }, "SET ECU!!",    "ECU Set",  red, black, white, green
   indicator = { crank              }, "Not Cranking", "Cranking",    white, black, black, white
   indicator = { startw             }, "ASE off",      "ASE ON",         white, black, cyan,   black
   indicator = { warmup             }, "WUE off",      "WUE ON",         white, black, blue, white
   indicator = { tpsaen             }, "Accel Enrich",   "Accel Enrich",   white, black, green, black
   indicator = { tpsden             }, "Decel Cut",      "Decel Cut", white, black, green, black
   indicator = { tps > floodClear && crank }, "Flood clear off", "FLOOD CLEAR ON", white, black, red, black
   indicator = { batteryVoltage < 10.5 }, "Battery OK",  "Battery LOW", green, black, red,   black
   indicator = { port0              },  "Port 0 Off",  "Port 0 On",   white, black, red,   black

;-------------------------------------------------------------------------------

[RunTime]
   barHysteresis = 2.5 ; Seconds
#if CELSIUS
  #if EXPANDED_CLT_TEMP
   coolantBar    = -40,  300
   matBar        = -40,  100
  #else
   coolantBar    = -40,  100
   matBar        = -40,  100
  #endif
#else
  #if EXPANDED_CLT_TEMP
   coolantBar    = -40,  600
   matBar        = -40,  215
  #else
   coolantBar    = -40,  215
   matBar        = -40,  215
  #endif
#endif
   batteryBar    =   6,   15
   dutyCycleBar  =   0,  100
#if   NARROW_BAND_EGO
   egoBar        = 0.0 ,  1.0
#elif LAMBDA
   egoBar        = 0.5,   1.5
#else
   egoBar        = 9.7,  19.7
#endif
   gammaEBar     =   0,  200
   mapBar        =   0,  255
   pulseWidthBar =   0, 25.5
   rpmBar        =   0, 8000
   throttleBar   =   0,  100
   egoCorrBar    =   0,  200
   baroCorrBar   =   0,  200
   warmupCorrBar =   0,  200
   airdenCorrBar =   0,  200
   veCorrBar     =   0,  200
   accCorrBar    =   0,  100

;-------------------------------------------------------------------------------

[Tuning]
#if   NARROW_BAND_EGO
   egoLEDs         =  0.0, 1.0,  0.5 ; Voltage settings.
#elif LAMBDA
   egoLEDs         =  1.5, 0.5,  1.0 ; Lambda settings.
#else
   egoLEDs         = 19.7, 9.7, 14.7 ; Afr settings.
#endif

;  font            = "Lucida Console", 12
;  font            = "Courier", 14
   spotDepth       =   2 ; 0 = no indicators, 1 = Z only, 2 = XYZ indicators.
   cursorDepth     =   2 ; Same as spot depth.

   ; The four radio buttons on the tuning screen select a "page" of six
   ; gauges.  The gauge numbering is the same as the front page, across
   ; then down.
   ;             1  2
   ;             3  4
   ;             5  6
   ;
   ; gaugeColumns allows you to hide or show gauges in column 2 (i.e.,
   ; gauges 2, 4 and 6).

   gaugeColumns = 2 ; Only 1 or 2 are valid.

   ;              Page 1            Page 2             Page 3            Page 4
   pageButtons  = "&EGO",           "&WUE",            "PW&1",           "PW&2"
   gauge1       = tachometer,       tachometer,        tachometer,       tachometer
   gauge2       = mapGauge,         mapGauge,          mapGauge,         mapGauge
#if   NARROW_BAND_EGO
   gauge3       = egoGauge,         egoGauge,          egoGauge,         egoGauge
#elif LAMBDA
   gauge3       = lambda1Gauge,     lambda1Gauge,      lambda1Gauge,     lambda1Gauge
#else
   gauge3       = afr1Gauge,        afr1Gauge,         afr1Gauge,        afr1Gauge
#endif
   gauge4       = egoCorrGauge,     warmupEnrichGauge, pulseWidth1Gauge, pulseWidth2Gauge
   gauge5       = veBucketGauge,    veBucketGauge,     veBucketGauge,    veBucketGauge
   gauge6       = accelEnrichGauge, accelEnrichGauge,  dutyCycle1Gauge,  dutyCycle2Gauge

;-------------------------------------------------------------------------------

[AccelerationWizard]
   tpsDotBar = 0, 100
   mapDotBar = 0, 200

;-------------------------------------------------------------------------------

[BurstMode]
   getCommand       = "a\x00\x06"

[OutputChannels]
   deadValue        = { 0 } ; Convenient unchanging value.

   ochBlockSize     = 112
   ochGetCommand    = "a\x00\x06" ; Lower case so we don't get confused.

   seconds          = scalar, U16,    0, "s",     1.000, 0.0
   secl = { seconds % 256 }, "s" ; For runtime screen.
   pulseWidth1      = scalar, U16,    2, "s",     0.001, 0.0
   pulseWidth2      = scalar, U16,    4, "s",     0.001, 0.0
   pulseWidth       = { pulseWidth1 }, "s" ; For runtime screen.

   rpm              = scalar, U16,    6, "RPM",   1.000, 0.0
   advance          = scalar, S16,    8, "deg",   0.100, 0.0

   ; unsigned char squirt,engine,afrtgt1,afrtgt2;    // afrtgt in afr x 10
   squirt           = scalar, U08,   10, "bit", 1.000, 0.0
   ; Squirt Event Scheduling Variables - bit fields for "squirt" variable above
   ; inj1:    equ    3       ; 0 = no squirt         1 = squirt
   ; inj2:    equ    5       ; 0 = no squirt         1 = squirt
   ; sched1:  equ    2       ; 0 = nothing scheduled 1 = scheduled to squirt
   ; firing1: equ    0       ; 0 = not squirting     1 = squirting
   ; sched2:  equ    4
   ; firing2: equ    1
   firing1          = bits,   U08,   10, [0:0]
   firing2          = bits,   U08,   10, [1:1]
   sched1           = bits,   U08,   10, [2:2]
   inj1             = bits,   U08,   10, [3:3]
   sched2           = bits,   U08,   10, [4:4]
   inj2             = bits,   U08,   10, [5:5]

   engine           = scalar, U08,   11, "bit",   1.000, 0.0
   ; Engine Operating/Status variables - bit fields for "engine" variable above
   ; ready:  equ     0       ; 0 = engine not ready 1 = ready to run
   ; crank:  equ     1       ; 0 = engine not cranking 1 = engine cranking
   ; startw: equ     2       ; 0 = not in startup warmup 1 = in warmup enrichment
   ; warmup: equ     3       ; 0 = not in warmup 1 = in warmup
   ; tpsaen: equ     4       ; 0 = not in TPS acceleration mode 1 = TPS acceleration mode
   ; tpsden: equ     5       ; 0 = not in deacceleration mode 1 = in deacceleration mode
   ; mapaen: equ     6       ; 0 = not in MAP acceleration mode 1 = MAP deaceeleration mode; not implemented
   ready            = bits,   U08,   11, [0:0]
   crank            = bits,   U08,   11, [1:1]
   startw           = bits,   U08,   11, [2:2]
   warmup           = bits,   U08,   11, [3:3]
   tpsaen           = bits,   U08,   11, [4:4]
   tpsden           = bits,   U08,   11, [5:5]
   mapaen           = bits,   U08,   11, [6:6]

   afrtgt1          = scalar, U08,   12, "AFR",   0.100, 0.0
   afrtgt2          = scalar, U08,   13, "AFR",   0.100, 0.0

   ; unsigned char wbo2_en1,wbo2_en2; // from wbo2 - indicates whether wb afr valid
   wbo2_en1         = scalar, U08,   14, "",      1.000, 0.0
   wbo2_en2         = scalar, U08,   15, "",      1.000, 0.0

   ; int baro,map,mat,clt,tps,batt,ego1,ego2,knock, // baro   - kpa x 10
   ;                                                // map    - kpa x 10
   ;                                                // mat, clt deg(C/F)x 10
   ;                                                // tps    - % x 10
   ;                                                // batt   - vlts x 10
   ;                                                // ego1,2 - afr x 10
   ;                                                // knock  - volts x 100
   barometer        = scalar, S16,   16, "kPa",   0.100, 0.0
   map              = scalar, S16,   18, "kPa",   0.100, 0.0
#if CELSIUS
   mat              = scalar, S16,   20, "°C",   0.05555, -320.0
   coolant          = scalar, S16,   22, "°C",   0.05555, -320.0
#else
   mat              = scalar, S16,   20, "°F",    0.100, 0.0
   coolant          = scalar, S16,   22, "°F",    0.100, 0.0
#endif
   tps              = scalar, S16,   24, "%",     0.100, 0.0
   tpsADC           = { tps*10.23 }, "ADC" ; Fake for calibrator and file indexing.
   throttle         = { tps }, "%"
   batteryVoltage   = scalar, S16,   26, "v",     0.100, 0.0
   afr1             = scalar, S16,   28, "AFR",   0.100, 0.0
   afr2             = scalar, S16,   30, "AFR",   0.100, 0.0
   lambda1          = { afr1 / 14.7 }, "Lambda"
   lambda2          = { afr2 / 14.7 }, "Lambda"
   knock            = scalar, S16,   32, "v",     0.010, 0.0

   ; egocor1,egocor2,aircor,warmcor,     // all in %
   egoCorrection1   = scalar, S16,   34, "%",     1.000, 0.0
   egoCorrection    = { ( egoCorrection1 + egoCorrection2) / 2 }, "%" ; Alias for old gauges.
   egoCorrection2   = scalar, S16,   36, "%",     1.000, 0.0
   airCorrection    = scalar, S16,   38, "%",     1.000, 0.0
   warmupEnrich     = scalar, S16,   40, "%",     1.000, 0.0

   fuelComposition  = { (fuelCorrection - 100)*1.587 }, % ; works with default sensor values

   ; tpsaccel,tpsfuelcut,barocor,gammae, // tpsaccel - acc enrich(.1 ms units)
   ;                                     // tpsfuelcut - %
   ;                                     // barcor,gammae - %
   accelEnrich      = scalar, S16,   42, "msec",    0.100, 0.0
   tpsfuelcut       = scalar, S16,   44, "%",     1.000, 0.0
   baroCorrection   = scalar, S16,   46, "%",     1.000, 0.0
   gammaEnrich      = scalar, S16,   48, "%",     1.000, 0.0

   ;  vecurr1,vecurr2,iacstep,cold_adv_deg;           // vecurr - %
   ;                                                  // iacstep - steps
   ;                                                  // cold_adv_deg - deg x 10
   veCurr1          = scalar, S16,   50, "%",     1.000, 0.0
   veCurr2          = scalar, S16,   52, "%",     1.000, 0.0
   veCurr           = { veCurr1 }, "%" ; For runtime display.
   iacstep          = scalar, S16,   54, "",      1.000, 0.0
   idleDC           = { iacstep } ; Close enough.
   coldAdvDeg       = scalar, S16,   56, "deg",   0.100, 0.0
   tpsDOT           = scalar, S16,   58, "%/sec",   1.000, 0.0
   mapDOT           = scalar, S16,   60, "kPa/sec", 1.000, 0.0
   dwell            = scalar, S16,   62, "msec",    0.100, 0.0
   maf              = scalar, S16,   64, "g/sec", 0.010, 0.0
   kpa              = scalar, S16,   66, "kPa",   0.100, 0.0 ; Blend of MAP, MAFMAP and TPS, depends on algorithm
   fuelCorrection   = scalar, S16,   68, "%",     1.000, 0.0 ; Percent alcohol in fuel.

   portStatus       = scalar, U08,   70, "bit",   1.000, 0.0 ; Spare port status bits
   port0            = bits,   U08,   70, [0:0]
   port1            = bits,   U08,   70, [1:1]
   port2            = bits,   U08,   70, [2:2]
   port3            = bits,   U08,   70, [3:3]
   port4            = bits,   U08,   70, [4:4]
   port5            = bits,   U08,   70, [5:5]
   port6            = bits,   U08,   70, [6:6]

   knockRetard      = scalar, U08,   71, "deg",   0.100, 0.0
   xTauFuelCorr1    = scalar, S16,   72, "%",     1.000, 0.0
   egoV1            = scalar, S16,   74, "Volts", 0.010, 0.0
   egoV2            = scalar, S16,   76, "Volts", 0.010, 0.0
   amcUpdates       = scalar, S16,   78,  "",     1.000, 0.0
   kpaix            = scalar, S16,   80,  "kPa",  0.100, 0.0
   xTauFuelCorr2    = scalar, S16,   82, "%",     1.000, 0.0
   synch            = scalar, U08,   84,  "",     1.000, 0.0 
   cspare           = scalar, U08,   85,  "",     1.000, 0.0 
   spare1           = scalar, S16,   86,  "",     1.000, 0.0
   spare2           = scalar, S16,   88,  "",     1.000, 0.0
   trig_fix         = scalar, S16,   90,  "",     1.000, 0.0
   spare4           = scalar, S16,   92,  "",     1.000, 0.0
   spare5           = scalar, S16,   94,  "",     1.000, 0.0
   spare6           = scalar, S16,   96,  "",     1.000, 0.0
   spare7           = scalar, S16,   98,  "",     1.000, 0.0
   spare8           = scalar, S16,  100,  "",     1.000, 0.0
   spare9           = scalar, S16,  102,  "",     1.000, 0.0
   tachCount        = scalar, U16,  104,  "",     1.000, 0.0
   ospare           = scalar, U08,  106,  "",     1.000, 0.0
   cksum            = scalar, U08,  107,  "",     1.000, 0.0
   deltaT           = scalar, U32,  108,  "uS",   1.000, 0.0 ; Normalized time between trigger pulses,
                                                             ; "fills in" missing teeth.


   accDecEnrich     = { ((accEnrichMS + decEnrichMS)/pulseWidth1*100) + 100 }, "%"
   accDecEnrichPcnt = { accelEnrich/pulseWidth1 + (tpsden ? tpsfuelcut : accelEnrich/pulseWidth1*100)      }, "%"
   accEnrichPcnt    = { 100 + (accelEnrich/pulseWidth1*100)  }, "%"
   accEnrichMS      = { accelEnrich                  }, "msec"
   decEnrichPcnt    = { (tpsden ? tpsfuelcut : 100)  }, "%"
   decEnrichMS      = { (tpsfuelcut/100*pulseWidth1)-pulseWidth1   }, "msec"
    
   time             = { timeNow                                        }, "s"
   rpm100           = { rpm / 100.0                                    }

   altDiv1          = { alternate ? 2 : 1                              }
   altDiv2          = { alternate ? 2 : 1                              }

   cycleTime1       = { 60000.0 / rpm * (2.0-twoStroke)                }, "ms"
   cycleTime2       = { 60000.0 / rpm * (2.0-twoStroke)                }, "ms"
   nSquirts1        = { nCylinders/divider                             }

#if MS2_SEQ
   dutyCycle1       = { (100.0 * pulseWidth1) / (cycleTime1 / (2.0-ignmode)) }, "%"
   dutyCycle2       = { (100.0 * pulseWidth2) / (cycleTime2 / (2.0-ignmode)) }, "%"
#else 
   nSquirts1        = { nCylinders/divider                             }
   nSquirts2        = { nCylinders/divider                             }
   dutyCycle1       = { 100.0*nSquirts1/altDiv1*pulseWidth1/cycleTime1 }, "%"
   dutyCycle2       = { 100.0*nSquirts2/altDiv2*pulseWidth2/cycleTime2 }, "%"
#endif

#if   NARROW_BAND_EGO
   egoVoltage = { egoV1            }, "V"      ; For LED bars...
#elif LAMBDA
   egoVoltage = { lambda1          }, "Lambda" ; For LED bars...
#else
   egoVoltage = { afr1             }, "AFR"    ; For LED bars...
#endif
;     pageSize =  130

;-------------------------------------------------------------------------------
;--  The entries are saved in the datalog file in the order in which they     --
;--  appear in the list below.                                                --
;--                                                                           --
;--   Channel - Case sensitive name of output channel to be logged.           --
;--   Label   - String written to header line of log.  Be careful             --
;--             about changing these, as programs like MSLVV and              --
;--             MSTweak key off specific column names.                        --
;--   Type    - Data type of output, converted before writing.                --
;--   Format  - C-style output format of data.                                --

[Datalog]
   ;       Channel          Label          Type    Format
   ;       --------------   ----------     -----   ------
   entry = time,            "Time",        float,  "%.3f"
   entry = seconds,         "SecL",        int,    "%d"
   entry = rpm,             "RPM",         int,    "%d"
   entry = map,             "MAP",         float,  "%.1f"
   entry = kpaix,           "Tbl Indx",    float,  "%.1f"
   entry = maf,             "MAF",         float,  "%.2f"
   entry = throttle,        "TP",          float,  "%.1f"
   entry = batteryVoltage,  "vBatt",       float,  "%.2f"
#if   NARROW_BAND_EGO
   entry = egoVoltage,      "O2",          float,  "%.3f"
#elif LAMBDA
   entry = lambda1,         "Lambda",      float,  "%.3f"
#else
   entry = afr1,            "AFR",         float,  "%.2f"
#endif
   entry = mat,             "IAT",         float,  "%.1f"
   entry = coolant,         "CLT",         float,  "%.1f"
   entry = engine,          "Engine",      int,    "%d"
   entry = egoCorrection,   "Gego",        int,    "%d"
   entry = airCorrection,   "Gair",        int,    "%d"
   entry = warmupEnrich,    "Gwarm",       int,    "%d"
   entry = baroCorrection,  "Gbaro",       int,    "%d"
   entry = gammaEnrich,     "Gammae",      int,    "%d"
   entry = accDecEnrich,    "AccelEnrich", int,    "%d"
   entry = veCurr1,         "Gve",         int,    "%d"
   entry = pulseWidth1,     "PW",          float,  "%.3f"
   entry = dutyCycle1,      "DutyCycle1",  float,  "%.1f"
   entry = veCurr2,         "Gve2",        int,    "%d"
   entry = pulseWidth2,     "PW2",         float,  "%.3f"
   entry = dutyCycle2,      "DutyCycle2",  float,  "%.1f"
   entry = advance,         "SparkAdv",    float,  "%.1f"
   entry = knockRetard,     "knockRet",    float,  "%.1f"
   entry = coldAdvDeg,      "ColdAdv",     float,  "%.1f"
   entry = dwell,           "Dwell",       float,  "%.2f"
   entry = tpsDOT,          "tpsDOT",      int,    "%d"
   entry = mapDOT,          "mapDOT",      int,    "%d"
   entry = iacstep,         "IAC",         int,    "%d"
   entry = deltaT,          "deltaT",      float,  "%.0f"
   entry = trig_fix,        "Trigger±",    int,    "%d"
   entry = synch,           "Sync Stat",   int,    "%d"
   entry = tachCount,       "tachCount",   int,    "%d"
   entry = xTauFuelCorr1    "XTau1",       int,    "%d"
   entry = xTauFuelCorr2    "XTau2",       int,    "%d"
   entry = afrtgt1,         "AFRtrgt1",    float,  "%.2f"
   entry = knock,           "knck-V",      float,  "%.2f"
   
;-------------------------------------------------------------------------------

[SettingContextHelp]

; constantName  = "Help Text"

      nCylinders       = "The number of cylinders in your engine."  
      no_skip_pulses   = "Skip at least this number of tach pulses at startup."
      ICIgnCapture     = "For tach/crank singal, use Falling Edge or Rising Edge"
      ICCrankTrigger   = "While cranking, for spark advance use Calculated or Trigger Return or Trigger Rise"
      ICIgnOption      = "For coil, use Standard Coil Charge or EDIS or EDIS Multispark"
      spkout_hi_lo     = "Spark when Going Low (Normal) or Going High (Inverted) - be sure to read documentation carefully on this!!!"
      max_coil_dur     = "Maximun dwell time for the coil while runnning with nominal voltage (12V)."
      max_spk_dur      = "Time to allow between dwell periods, if enough time is available."
      dwellAcc         = "Dwell increase while accelerating."
      dwellVolts       = "Dwell battery voltage compensation table voltage bins."
      dwellDuration    = "Dwell battery voltage compensation additional dwell time table."
      RevLimOption     = "For rev limiting, use None or Spark Retard or Fuel Cut"
      RevLimMaxRtd     = "If using spark retard for rev limiing, the maximum amount of reatrad applied."
      PredOpt          = "Last Interval or Alpha-Beta-Gamma Filter"
      crankingRPM      = "RPM below which the cranking algorithm is used, above this rpm, the engine is considered to be running."
      cold_adv_table   = "Timing advance adjustment for cold coolant tempratures."
      triggerOffset    = "The number of degrees between the tach trigger signal and TDC."
      RevLimRpm1       = "Retard: RPM to satrt retarding spark. Fuel Cut: RPM to restore fuel."
      RevLimRpm2       = "Retard: RPM for full spark retard. Fuel Cut: RPM to cut fuel."
      afrTable1        = "Air/Fuel ratio table 1 for EGO feedback (and fuel calc if enabled)."
      afrTable2        = "Air/Fuel ratio table 2 for EGO feedback (and fuel calc if enabled)."
      wueBins          = "Percentage enrichment versus coolant temperature."
      taeBins          = "Accel enrichment added to pulse width versus change in TPS."
      maeBins          = "Accel enrichment added to pulse width versus change in MAP."
      iacstepTable     = "Idle speed controller steps (if stepper) or percent (if PWM) vs temperature."
      ipwmTable        = "Idle speed controller steps (if stepper) or percent (if PWM) vs temperature."
      frpm_table       = "Fuel (VE) table RPM bins."
      srpm_table       = "Spark advance table RPM bins."
      fmap_table       = "Fuel (VE) table MAP bins."
      smap_table       = "Spark advance table MAP bins."
      tempTable        = "Temperature bins for cranking, cold AE and WUE"
      taeRates         = "TPSdot bins used for Accel Enrichment"
      maeRates         = "MAPdot bins used for Accel Enrichment"
      map0             = "MAP value (kPa) at 0 ADC count."
      mapmax           = "MAP value (kPa) at 1023 ADC counts."
      clt0             = "CLT value (kPa) at 0 ADC counts."
      cltmult          = "CLT multiplier value (for cltfactor table)."
      mat0             = "MAT value (kPa) at 0 ADC counts."
      matmult          = "MAT multiplier value (for matfactor table)."
      tpsMin           = "TPS value (kPa) at 0 ADC count."
      tpsMax           = "TPS value (kPa) at 1023 ADC counts"
      batt0            = "vBatt value (kPa) at 0 ADC count."
      battmax          = "vBatt value (kPa) at 1023 ADC counts."
      ego0             = "EGO value (kPa) at 0 ADC counts."
      egomult          = "EGO multiplier value (for egofactor table)."
      baro0            = "Barometric value (kPa) at 0 ADC counts."
      baromax          = "Barometric value (kPa) at 1023 ADC counts."
      bcor0            = "Barometric correction at 0 kPa."
      bcormult         = "Barometric correction slope."
      knock0           = "Knock value (kPa) at 0 ADC counts."
      knockmax         = "Knock value (kPa) at 1023 ADC counts."
      crankTolerance   = "Percentage tolerance for next input pulse while cranking."
      asTolerance      = "Percentage tolerance for next input pulse during after start period."
      pulseTolerance   = "Percentage tolerance for next input pulse while running."
      IdleCtl          = "Idle speed controller type: None or Solenoid or IAC Stepper Moving Only or IAC Stepper Always On or PWM Warmup or 15-Minute IAC"
      IACtstep         = "IAC stepper motor nominal time between steps."
      IACaccstep       = "IAC stepper motor accel/decel step time."
      IACminstep       = "IAC stepper motor minimum step size to move. Must be at least 1."
      IACpwm_step      = "Sets frequency for PWM FIdle solenoid."
      IACStart         = "Number of steps to send at startup to put stepper motor at reference (wide open) position."
      IdleHyst         = "Amount the coolant temperature must move before idle position is changed."
      IACcrankpos      = "IAC position must be open at least this much (steps) while cranking."
      IACcrankxt       = "Number of seconds from end of cranking for IAC pos to blend into coolant dependent position."
      IACcoldtmp       = "When below this temperature, set IAC to IAC cold position."
      IACcoldpos       = "The psoition to set the IAC to when below the Cold temperature."
      IACcoldxt        = "The time over which to interpolate between the Cold Position and the table based values."
      primePulseCold   = "Priming pulse width at minimum temperature in temperature table; 2pt prime."
	  primePulseHot    = "Priming pulse width at maximum temperature in temperature table; 2pt prime."
      crankCold        = "Cranking pulse width at minimum temperature in temperautre table."
      crankHot         = "Cranking pulse width at maximum temperature in temperautre table."
      asePctCold       = "After start warmup percent enrichment add-on value at minimum temperature in temperature table."
      asePctHot        = "After start warmup percent enrichment add-on value at maximum temperature in temperature table."
      aseCountCold     = "After start enrichment number of cycles at minimum temperature in temperature table."
      aseCountHot      = "After start enrichment number of cycles at maximum temperature in temperature table."
      taeColdA         = "Cold (-40F) accel added time."
      taeColdM         = "Cold (-40F) accel multiply factor (%)."
      tpsThresh        = "TPSdot threshhold for acc/decel enrichment."
      mapThresh        = "MAPdot threshhold for acc/decel enrichment."
      taeTime          = "Duration for accel enrichment(s)."
      tdePct           = "Deceleration fuel cut amount in percent. 100% is no cut, 0% is complete cut of fuel."
      floodClear       = "TPS value for flood clear. No fuel injected if TPS is above this value while cranking."
      TPSOXLimit       = "Maximum TPS value for O2 closed loop active."
      tpsProportion    = "Weight (0-100) to be given to TPSdot over MAPdot for accel enrichment."
      baroCorr         = "Baro Correction options: None or Initial MAP Reading or Two Independent Sensors"
      egoType          = "EGO options: Disabled or Narrow Band or Dual Narrow Band or Single Wide Band or Dual Wide Band"
      egoCount         = "Number of tach pulse counts between EGO corrections to fuel."
      egoDelta         = "Percent step change in fuel for EGO corrections."
      egoLimit         = "Maximum percentage EGO correction can add or subtract from fuel."
#if   NARROW_BAND_EGO
	  egoTarget        = "NBO2 voltage for switch point between rich and lean."
#else
      AFRTarget        = "Stoichiometric AFR between rich and lean."
#endif
      tempUnits        = "Celcius or Fahrenheit for temperasture units."
      MAFOption        = "Mass Air Flow sensor options: no-MAF, MAF-only, MAF/MAP blending, MAF for fuel + MAP for table load."
      MAFpin           = "MAF signal connection options: MAF on MAP pin or MAF on Baro Pin or MAF on Knock Pin"
      DualSpkOptn      = "Dual spark options (Microsquirt): No Dual Spark or Dual Tach Inputs or Falling Cam Sync with Tach or Wheel or Rising Cam Sync with Tach or Wheel or Single Crank Wheel Input or Single Cam Wheel Input or Dual Inputs, Timing from 1 cam tooth or M-0 Wheel w/ Falling Crank Sync or M-0 Wheel w/ Rising Crank Sync"
      fastIdleT        = "Fast idle OFF temperature (idle control = ON/OFF only)."
      egoTemp          = "Minimum coolant temperature before EGO feedback is active."
      egoRPM           = "Minimum RPM before O2 closed loop is active."
      reqFuel          = "Fuel pulsewidth at 100 kPa before any other adjustments."
      divider          = "Divide factor for input tach pulses. Converts number of tach opulse to crank revolutions."
      alternate        = "Option to alternate injector banks: Simultaneous or Alternating"
      injOpen          = "Injector open-close time. I.e. the time when the injector is supposed to be on but is not injecting fuel."
      injPwmT          = "Time after Injector pulse starts to start PWM. Used to limit current flow in low impedance injectors."
      injPwmPd         = "Injector PWM period - keep between 10-25 KHz. Used to limit current flow in low impedance injectors."
      injPwmP          = "Injector PWM duty cycle (in %). Used to limit current flow in low impedance injectors."
      battFac          = "Battery voltage correction factor for fuel pulse width."
      twoStroke        = "Enigne type: Four-stroke or Two-stroke"
      injType          = "Port Injection (one injector for each cylinder) or Throttle Body (injectors shared by cylinders)"
      nInjectors       = "Total number of injectors."
      OddAng           = "Spark advance offset between cylinders/banks for dual spark outputs."
      rpmLF            = "Lag filter coefficient for RPM."
      mapLF            = "Lag filter coefficient for MAP."
      tpsLF            = "Lag filter coefficient for TPS."
      egoLF            = "Lag filter coefficient for EGO."
      adcLF            = "Lag filter coefficient for CLT/MAT/Battery voltage."
      knkLF            = "Lag filter coefficient for knock input."
      AMCOption        = "Automatic Mixture Control Options: Disabled or RAM Update or FLASH Update"
      dualTable        = "Dual table use: Single Table or Dual Table"
      algorithm        = "Alpha-N Fuel Calc Algorithm: None, Use MAP/TPS bend, MAP/TPS blend but don't use MAP as a multiplier."
      alphDir          = "Choose whether alphaN used below low rpm or above high rpm."
      alpha_baro_spkadv= "Alpha-N spark retard versus baro factor above 100 kPa."
      AfrAlpha         = "Option to use map,tps(alphaN) blend algorithm for WBO2 AFR."
      AFRStoich        = "Stoichiometric air/fuel ratio for fuel used."
	  AFRStoichNB      = "Stoichiometric voltage for fuel used."
      AFRStoichWB      = "Stoichiometric air/fuel ratio for fuel used."
      alpha_lorpm      = "Low RPM for alpha-N blending."
      alpha_hirpm      = "High RPM for alpha-N blending."
      alphaMAPtable    = "Table of fabricated MAP values (from [tps,rpm] pairs) to use with VE table to detemrine fuel pulse width."
      amap_tps         = "TPS values for alpha-N to MAP table."
      amap_rpm         = "RPM values for alpha-N to MAP table."
      baud             = "Serial port communications rate (115200 for MS-II/Sequencer)."
      MAPOXLimit       = "Maximum MAP value (kPa) for O2 closed loop."
      board_type       = "This board's type: 1 = MS-II, 4 = MShift/GPIO."
      mycan_id         = "CAN ID for this board. Normally 0 for engine controller."
      fet_delay        = "Delay from time ignition FET line goes active to spark."
      vr_delay         = "Delay of VR sensor from tooth present to 0 crossing."
      ECUType          = "1 for MS-II, 2 for MicroSquirt"
      MapThreshXTD2    = "MAPdot threshhold for the start of the switch from X-Tau Accel to Decel parameters."
      pwImpulse        = "Additional time to be added to normal pulse width at Time between Added Fuel intervals."
      impulseSec       = "Time between squirts to be added to the normal fuel pulsewidth."
      nImpulse         = "Number of injections to be made at Time between Added Fuel intervals."
      mapdotSample     = "Minimum time between MAP samples to compute MAPdot."
      tpsdotSample     = "Minimum time between TPS samples to compute TPSdot."
      ASEHot           = "ASE on hot restart options: Disable ASE on Hot Start or Enable ASE on Hot Start"
      InjStart         = "Specifies when after tach pulse to start fuel injection. Value in percent of crank angle between tach pulses."
      MapThreshXTD     = "MAPdot threshhold for the start of the switch from X-Tau Accel to Decel parameters."
      MapThreshXTA     = "MAPdot threshhold for the start of MAP Trending for faster AE/XTau enrichment."
      trendmapLimit    = "Maximum amount of change in MAP at any given sample."
      psEnabled        = "Enable/disable spare port use."
      psCondition      = "Spare port condition."
      psConnector      = "Spare port logic WRT other condition."
      psInitValue      = "Spare port initial value (at controller startup)."
      psPortValue      = "Spare port value when conditions are met."
      psOutSize        = "Sapre port hysteresis value (minimum change before spare port status will change)."
      psOutOffset      = "."
      psThreshold      = "."
      psHysteresis     = "."
      aeTaperTime      = "Acceleration enrichment tail-off duration."
      AFRMult          = "Choose whether to use Combined VE/AFR table or Separate VE & AFR table. Combined inclues (AFR Stoich./AFR table) in fuel equation."
      aeEndPW          = "End pulse width of accel enrichment after taper time."
      egoAlgorithm     = "Simple or Transport Delay or PID/Smith Predictor"
      egoKP            = "EGO PID proprotional gain."
      egoKI            = "EGO PID intergral factor."
      egoKD            = "EGO PID derivative factor."
      egoKdelay1       = "Coefficient 1 used to calculate EGO transport: delay = Delay1 + Delay2*120000/(MAP*RPM)."
      egoKdelay2       = "Coefficient 2 used to calculate EGO transport: delay = Delay1 + Delay2*120000/(MAP*RPM)."
      flexFuel         = "Disabled or Enabled"
      prime_delay      = "After controller start up, wait this long for fuel pump before commanding prime pulse."
      fuelFreq         = "Table of fuel sensor freq(Hz) vs %fuel corr."
         fuelFreq0     = "Table of fuel sensor freq(Hz) vs %fuel corr."
         fuelFreq1     = "Table of fuel sensor freq(Hz) vs %fuel corr."
      fuelCorr         = "Table of fuel sensor freq(Hz) vs %fuel corr."
         fuelCorr0     = "Table of fuel sensor freq(Hz) vs %fuel corr."
         fuelCorr1     = "Table of fuel sensor freq(Hz) vs %fuel corr."
      AMCstep          = "Percentage of AMC correction to be applied when RAM VE table updated."
      AMCdve           = "Minimum AMC correction before it will be applied in burn."
      AMCve_rpm        = "Current RPM must be within this tolerance of a VE table bin before AMC correction is applied."
      AMCve_map        = "Current MAP must be within this tolerance of a VE table bin before AMC correction is applied."
      AMCramve_dt      = "Time the engine must operate with AMC vertex tolerances before AMC correction is applied to that vertex."
      AMCT_thresh      = "Minimum time between flash burns of AMC updated RAM VE table ."
      AMCupdate_thresh = "Minimum number of AMC RAM VE table vertex updates before VE table is burned to flash (made permanent)."
      CWOption         = "Cold warm-up option: Two-Point or Table" 
      knkOption        = "Knock option: Disabled or Safe Mode or Aggressive Mode"
      knkDirection     = "Below threshold or Above threshold"
      knk_maxrtd       = "Maximum total retard when knock occurs."
      knk_step1        = "Ignition retard/advance steps when knock first happens."
      knk_step2        = "Ignition retard/advance steps when knock has stopped."
      knk_trtd         = "Time between knock retard corrections."
      knk_tadv         = "Time between knock advance corrections."
      knk_dtble_adv    = "Change in table advance required to restart advance until knocking or reach table value."
      knk_ndet         = "Number knock signals required for valid detection."
      knk_maxmap       = "No knock retard above this MAP."
      knk_lorpm        = "No knock retard below this RPM."
      knk_hirpm        = "No knock retard above this RPM."
      knk_rpm          = "Table of RPM vs knock threshhold."
      knk_thresh       = "Table of RPM vs knock threshhold."
      triggerTeeth     = "Nominal (include missing) teeth for wheel decoding. (Set to 0 for no wheel decoding)."
      No_Miss_Teeth    = "Number of consecutive missing teeth."
      No_Skip_Teeth    = "Number of teeth (between tach pulses) to be skipped."
      Delay_Teeth      = "Number of teeth to delay after 1st tooth after the missing tooth(s) before 1st tach synch declared."
      ICISR_tmask      = "Time after tach input capture during which further interrupts are inhibited to mask coil ring or VR noise."
      ICISR_pmask      = "Percentage of time between signals after tach input capture during which further interrupts are inhibited to mask coil ring or VR noise."
      injTestMode      = "Can put controller in injector test mode: chosse from Normal Mode or Test Mode or Repeat Test"
      ae_lorpm         = "RPM at which normal accel enrichment just starts to scale down."
      ae_hirpm         = "RPM at which normal accel enrichment is reduced to 0."
      fuelSpkDel       = "Table of flex fuel sensor frequency vs spark advance correction."
         fuelSpkDel0   = "Table of flex fuel sensor frequency vs spark advance correction."
         fuelSpkDel1   = "Table of flex fuel sensor frequency vs spark advance correction."
      injTestSqrts     = "Number of squirts in test/clean mode."
      injTestPW        = "Pulse width for testing/ cleaning injectors."
      injTestOffTime   = "Time between injector test squirts."
      CID              = "Engine displacement in cubic inches. (61 cubic inches is aprox. 1L = 1000cc)."
      alpha            = "Coefficient for ignition time prediction."
      beta             = "Coefficient for ignition time prediction."
      gamma            = "Coefficient for ignition time prediction."
      acc_synchk       = "Check for tach timing synch options: Check Only at Steady Speed or Check Accel and Steady Speed or Check Decel and Steady Speed or Check Always"       
      veTable1         = "Volumetric efficiency table."
      veTable2         = "Volumetric efficiency table."
      advanceTable     = "Ignition spark advance table."
      AMCNBurns        = "Cumulative number of AMC flash burns. Grabbed from controller when MSQ settings downloaded,."
      primePWTable     = "Prime pulse width table (if not using 2pt.)."
      crankPWTable     = "Cranking pulse width table (if not using 2pt.)."
      asePctTable      = "After Start Enrichment percent table (if not using 2pt.)."
      aseCntTable      = "After Start Enrichment pulse width table (if not using 2pt.)."
      matTemps         = "MAT temperatures for spark retard."
      matRetard        = "Spark retard versus manifold air temperature."
      xTauOption       = "X-Tau accel enrichment options: Off or Accel/Decel Only or Warm-up + Accel/Decel"
      spkN2O           = "Spark retard subtracted from normal advance while N2O is active."
      XAccTable        = "X factor for percent of injected fuel that clings to port wall as function of rpm (during accel)."
      TauAccTable      = "Time constant for fuel puddle dissipation versus RPM (accel)."
      XDecTable        = "X factor for percent of injected fuel that clings to port wall as function of rpm (during decel)."
      TauDecTable      = "Time constant for fuel puddle dissipation versus RPM (decel)."
      XTrpms           = "RPM bin values for X-Tau."
      XClt             = "Coolant temperature bin values for X."
      TauClt           = "Coolant temperature bin values for Tau."
      fRate            = "Steady state fuel flow rate of one injector."
      baroCorrVals     = "Barometric pressures for baro correction table."
      matCorrTemps     = "Air temperatures for air density correction table."
      baroCorrDelta    = "Barometric corrections added to base value to correct for varying exhaust size."
      matCorrDelta     = "Air density orrections added to base value to correct for varying MAT sensor location."
      MAFFlow          = "MAF flow bins values for MAF table corrections."
      MAFCor           = "Corrections to MAF factor table for real time tuning/intake mods. 100% = no correction."
      MAFRPM1          = "For blended MAF: Use MAP only below this RPM, unless 'inverted' below."
      MAFRPM2          = "For blended MAF: Use MAF only above this RPM, unless 'inverted' below."
      MAFDir           = "Choose when to use MAF/MAP/blend: Use Above or Invert Above"
      VEIXOptn         = "Choose whether to use (kpa*1000)/baro instead of kpa as the index to VE, AFR, spark advance tables."
      MatRtdRPMHi      = "Full MAT spark retard is applied above this RPM."
      MatRtdRPMLo      = "No MAT spark retard is applied below the this RPM."
