```    691-01   CCOPE    18 MAY 81  15/29/00           FIRST TIME ON THIS FILE 15 29  0       THIS FILE I
S ALL OR PART OF TIME PERIOD 15 29  0 TO 17 28  0  DESCRIPTION OF RECORD -- 101 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS  101 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 14 CYCLES OF 101 SAMP/CYC = 1414 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 472 60 BIT PACKED WORDS          --METHOD OF SCALING--  A BIAS AD(I) WAS ADDED TO EACH SAMPLE
OF EACH PARAMETER  TO ELIMINATE ANY NEGATIVE VALUES. THE BIASED SAMPLE WAS THEN MULTIPLIED BY P(I)
TO INSURE THE PROPER NUMBER OF DECIMAL PLACES WERE SAVED.  THE PACKED RECORD MAY BE UNPACKED BY RIGH
T JUSTIFYING 20 BITS AT A TIME AND REVERSING THE ABOVE SCALING PROCESS. AS EXAMPLE, S(I)=N/P(I)-AD(I
), WHERE N IS THE 20 BIT SCALED INTEGER, S(I) THE DESIRED UNSCALED PARAMETER, AD(I),P(I) THE CORRESP
ONDING SCALE FACTORS  THE ORDER, RATE, PLOT TITLE, PRINT LAB, UNITS, AD AND P SCALE FACTORS OF EACH
PARAMETER FOLLOW
1)   1     PROCESSOR TIME (SECONDS) AFTER MIDNIGHT    TIME      SEC     = (N/    1.0) -    0.0
2)   1     UNALTERED TAPE TIME (SEC) AFTER MIDNIGHT   TPTIME    SEC     = (N/    1.0) -    0.0
3)   1     LTN-51 ARINC TIME LAG (SEC)                TMLAG     SEC     = (N/ 1000.0) -  100.0
4)   1     EVENT MARKER WORD                          EVMRKS            = (N/    1.0) -    0.0
5)   1     FIXED ZERO VOLTAGE (VDC)                   FZV       VDC     = (N/ 1000.0) -  100.0
6)   1     RAW INS LATITUDE (DEG)                     ALAT      DEG     = (N/ 1000.0) -  100.0
7)   1     RAW INS LONGITUDE (DEG)                    ALONG     DEG     = (N/ 1000.0) -  200.0
8)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)        THI       DEG     = (N/ 1000.0) -  100.0
9)   1     INS WANDER ANGLE (DEG)                     ALPHA     DEG     = (N/ 1000.0) -  100.0
10)   1     RAW INS GROUND SPD X COMPONENT (M/S)       XVI       M/S     = (N/ 1000.0) -  500.0
11)   1     RAW INS GROUND SPD Y COMPONENT (M/S)       YVI       M/S     = (N/ 1000.0) -  500.0
12)   1     RAW INS GROUND SPEED (M/S)                 GSF       M/S     = (N/ 1000.0) -  100.0
13)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
14)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
15)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)          THF       DEG     = (N/ 1000.0) -  100.0
16)   1     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/ 1000.0) -  500.0
17)   1     RAW DYNAMIC PRESSURE (WING) (MB)           QCW       MB      = (N/ 1000.0) -  100.0
18)   1     RAW DYNAMIC PRESSURE (GUST)      (MB)      QCG       MB      = (N/ 1000.0) -  100.0
19)   1     CORRECTED DYNAMIC PRESR (WING)  (MB)       QCWC      MB      = (N/ 1000.0) -  100.0
20)   1     CORRECTED DYNAMIC PRESR (GUST)      (MB)   QCGC      MB      = (N/ 1000.0) -  100.0
21)   1     RAW STATIC PRESSURE (FUSELAGE) (MB)        PSF       MB      = (N/ 1000.0) -    0.0
22)   1     RAW STATIC PRESSURE (BOOM) (MB)            PSB       MB      = (N/ 1000.0) -    0.0
23)   1     CORRECTED STATIC PRESR (FUSELAGE) (MB)     PSFC      MB      = (N/ 1000.0) -    0.0
24)   1     CORRECTED STATIC PRESSURE (BOOM) (MB)      PSBC      MB      = (N/ 1000.0) -    0.0
25)   1     NACA PRESSURE ALTITUDE (M)                 HP        M       = (N/   10.0) -  500.0
26)   1     GEOMETRIC (RADIO) ALTITUDE (M)             HGM       M       = (N/ 1000.0) -  100.0
27)   1     TOTAL TEMPERATURE (BOOM ROSEMOUNT) (C)     TTB       C       = (N/ 1000.0) -  100.0
28)   1     TOTAL TEMPERATURE(REVERSE FLOW) (C)        TTRF      C       = (N/ 1000.0) -  100.0
29)   1     TOTAL TEMPERATURE (FAST RESPONSE) (C)      TTKP      C       = (N/ 1000.0) -  100.0
30)   1     AMBIENT TEMP.(BOOM ROSEMOUNT)(C)           ATB       C       = (N/ 1000.0) -  100.0
31)   1     AMBIENT TEMPERATURE (REVERSE-FLOW) (C)     ATRF      C       = (N/ 1000.0) -  100.0
32)   1     AMBIENT TEMP (FAST RESPONSE)  (C)          ATKP      C       = (N/ 1000.0) -  100.0
33)   1     RADIOMETRIC SURFACE TEMP (PRT-5)  (C)      PRT5      C       = (N/ 1000.0) -  100.0
34)   1     DEW/FROST POINT TEMP ( E-G+G)(RT-BOT)(C)   DPRB      C       = (N/ 1000.0) -  100.0
35)   1     DEW/FROST POINT TEMP(GN EAST)(RT-TOP)(C)   DPRT      C       = (N/ 1000.0) -  100.0
36)   1     DEWPOINT TEMPERATURE ( E-G+G)(RT-BOT)(C)   DPRBC     C       = (N/ 1000.0) -  100.0
37)   1     DEWPOINT TEMPERATURE(GN EAST)(RT-TOP)(C)   DPRTC     C       = (N/ 1000.0) -  100.0
38)   1     ABSOLUTE HUMIDITY ( E-G+G)(RT-BOT)(G/M3)   RHOTDB    G/M3    = (N/ 1000.0) -  100.0
39)   1     ABSOLUTE HUMIDITY(GN EAST)(RT-TOP)(G/M3)   RHOTDT    G/M3    = (N/ 1000.0) -  100.0
40)   1     RAW LYMAN ALPHA HYGROMETER OUTPUT (VDC)    VLA       VDC     = (N/ 1000.0) -  100.0
41)   1     AIRCRAFT TRUE AIRSPEED (WING) (M/S)        TASW      M/S     = (N/ 1000.0) -  100.0
42)   1     AIRCRAFT TRUE AIRSPEED (GUST) (M/S)        TASG      M/S     = (N/ 1000.0) -  100.0
43)   1     RAW J-W LIQUID WATER CONTENT (G/M3)        LWC       G/M3    = (N/ 1000.0) -  100.0
44)   1     CORRCTD J-W LIQUID WATER CONTENT (G/M3)    LWCC      G/M3    = (N/ 1000.0) -  100.0
45)   1     ATTACK ANGLE ( LEFT FIXED VANE) (DEG)      AFIXL     DEG     = (N/ 1000.0) -  100.0
46)   1     ATTACK ANGLE (RIGHT FIXED VANE) (DEG)      AFIXR     DEG     = (N/ 1000.0) -  100.0
47)   1     SIDESLIP ANGLE (TOP FIXED VANE)  (DEG)     BFIXT     DEG     = (N/ 1000.0) -  100.0
48)   1     SIDESLIP ANGLE (BOTTOM FIXED VANE) (DEG)   BFIXB     DEG     = (N/ 1000.0) -  100.0
49)   1     WIND VECTOR EAST GUST COMPONENT (M/S)      UI1       M/S     = (N/ 1000.0) -  200.0
50)   1     WIND VECTOR NORTH GUST COMPONENT (M/S)     VI1       M/S     = (N/ 1000.0) -  200.0
51)   1     WIND VECTOR VERTICAL GUST COMP (M/S)       WI1       M/S     = (N/ 1000.0) -  100.0
52)   1     WIND VECTOR LNGTDNL GUST COMP. (M/S)       UX1       M/S     = (N/ 1000.0) -  200.0
53)   1     WIND VECTOR LATERAL GUST COMP. (M/S)       VY1       M/S     = (N/ 1000.0) -  200.0
54)   1     HORIZONTAL WIND DIRECTION (DEG)            WDRCTN    DEG     = (N/ 1000.0) -  100.0
55)   1     HORIZONTAL WIND SPEED (M/S)                WSPD      M/S     = (N/ 1000.0) -  100.0
56)   1     RAW INS GROUND SPD EAST COMP (M/S)         VEW       M/S     = (N/ 1000.0) -  500.0
57)   1     RAW INS GROUND SPD NORTH COMP (M/S)        VNS       M/S     = (N/ 1000.0) -  500.0
58)   1     DISTANCE EAST OF SUNDAY CREEK (KM)         DEI       KM      = (N/  100.0) - 1000.0
59)   1     DISTANCE NORTH OF SUNDAY CREEK (KM)        DNI       KM      = (N/  100.0) - 1000.0
60)   1     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
61)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP3       M/S     = (N/ 1000.0) -  100.0
62)   1     PRESSURE-DAMPED INERTIAL ALTITUDE (M)      HI3       M       = (N/   10.0) -  500.0
63)   1     RELATIVE HUMIDITY (PER CENT)               RHUM     PER CENT = (N/ 1000.0) -  100.0
64)   1     TEMPETATURE AT LCL(C)                      TLCL      C       = (N/ 1000.0) -  100.0
65)   1     PRESSURE AT LCL   (MB)                     PLCL      MB      = (N/ 1000.0) -  100.0
66)   1     MIXING RATIO      (G/KG)                   RM     G/KG       = (N/ 1000.0) -  100.0
67)   1     EQUIVALENT POTENTIAL TEMPERATURE (K)       ETHETA    K       = (N/ 1000.0) -  100.0
68)   1     POTENTIAL TEMPERATURE (K)                  THETA     K       = (N/ 1000.0) -  100.0
69)   1     SPECIFIC HUMIDITY (G/KG)                   SPHUM    G/KG     = (N/ 1000.0) -  100.0
70)   1     VIRTUAL POTENTIAL TEMPERATURE (K)          VTHETA    K       = (N/ 1000.0) -  100.0
71)   1     PMS PROBE 200Y                             200Y     IDWD     = (N/ 1000.0) -  100.0
72)   1     PROBE 1/CELL 1 ACCMULATION(COUNTS)         SUM1/ 1   COUNTS  = (N/ 1000.0) -  100.0
73)   1     PROBE 1/CELL 2 ACCMULATION(COUNTS)         SUM1/ 2   COUNTS  = (N/ 1000.0) -  100.0
74)   1     PROBE 1/CELL 3 ACCMULATION(COUNTS)         SUM1/ 3   COUNTS  = (N/ 1000.0) -  100.0
75)   1     PROBE 1/CELL 4 ACCMULATION(COUNTS)         SUM1/ 4   COUNTS  = (N/ 1000.0) -  100.0
76)   1     PROBE 1/CELL 5 ACCMULATION(COUNTS)         SUM1/ 5   COUNTS  = (N/ 1000.0) -  100.0
77)   1     PROBE 1/CELL 6 ACCMULATION(COUNTS)         SUM1/ 6   COUNTS  = (N/ 1000.0) -  100.0
78)   1     PROBE 1/CELL 7 ACCMULATION(COUNTS)         SUM1/ 7   COUNTS  = (N/ 1000.0) -  100.0
79)   1     PROBE 1/CELL 8 ACCMULATION(COUNTS)         SUM1/ 8   COUNTS  = (N/ 1000.0) -  100.0
80)   1     PROBE 1/CELL 9 ACCMULATION(COUNTS)         SUM1/ 9   COUNTS  = (N/ 1000.0) -  100.0
81)   1     PROBE 1/CELL10 ACCMULATION(COUNTS)         SUM1/10   COUNTS  = (N/ 1000.0) -  100.0
82)   1     PROBE 1/CELL11 ACCMULATION(COUNTS)         SUM1/11   COUNTS  = (N/ 1000.0) -  100.0
83)   1     PROBE 1/CELL12 ACCMULATION(COUNTS)         SUM1/12   COUNTS  = (N/ 1000.0) -  100.0
84)   1     PROBE 1/CELL13 ACCMULATION(COUNTS)         SUM1/13   COUNTS  = (N/ 1000.0) -  100.0
85)   1     PROBE 1/CELL14 ACCMULATION(COUNTS)         SUM1/14   COUNTS  = (N/ 1000.0) -  100.0
86)   1     PROBE 1/CELL15 ACCMULATION(COUNTS)         SUM1/15   COUNTS  = (N/ 1000.0) -  100.0
87)   1     PROBE 2/CELL 1 CONCENTRATION (CTS/LITER)   YCN/01    N/LTR   = (N/ 1000.0) -  100.0
88)   1     PROBE 2/CELL 2 CONCENTRATION (CTS/LITER)   YCN/02    N/LTR   = (N/ 1000.0) -  100.0
89)   1     PROBE 2/CELL 3 CONCENTRATION (CTS/LITER)   YCN/03    N/LTR   = (N/ 1000.0) -  100.0
90)   1     PROBE 2/CELL 4 CONCENTRATION (CTS/LITER)   YCN/04    N/LTR   = (N/ 1000.0) -  100.0
91)   1     PROBE 2/CELL 5 CONCENTRATION (CTS/LITER)   YCN/05    N/LTR   = (N/ 1000.0) -  100.0
92)   1     PROBE 2/CELL 6 CONCENTRATION (CTS/LITER)   YCN/06    N/LTR   = (N/ 1000.0) -  100.0
93)   1     PROBE 2/CELL 7 CONCENTRATION (CTS/LITER)   YCN/07    N/LTR   = (N/ 1000.0) -  100.0
94)   1     PROBE 2/CELL 8 CONCENTRATION (CTS/LITER)   YCN/08    N/LTR   = (N/ 1000.0) -  100.0
95)   1     PROBE 2/CELL 9 CONCENTRATION (CTS/LITER)   YCN/09    N/LTR   = (N/ 1000.0) -  100.0
96)   1     PROBE 2/CELL10 CONCENTRATION (CTS/LITER)   YCN/10    N/LTR   = (N/ 1000.0) -  100.0
97)   1     PROBE 2/CELL11 CONCENTRATION (CTS/LITER)   YCN/11    N/LTR   = (N/ 1000.0) -  100.0
98)   1     PROBE 2/CELL12 CONCENTRATION (CTS/LITER)   YCN/12    N/LTR   = (N/ 1000.0) -  100.0
99)   1     PROBE 2/CELL13 CONCENTRATION (CTS/LITER)   YCN/13    N/LTR   = (N/ 1000.0) -  100.0
100)   1     PROBE 2/CELL14 CONCENTRATION (CTS/LITER)   YCN/14    N/LTR   = (N/ 1000.0) -  100.0
101)   1     PROBE 2/CELL15 CONCENTRATION (CTS/LITER)   YCN/15    N/LTR   = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE
691-01   CCOPE    18 MAY 81  15/29/00
THIS FILE IS ALL OR PART OF THE TIME PERIOD 15        29         0         TO   17        28         0
DESCRIPTION OF TAPE:
HEADER FILE --   832 BITS (104 ASCII CHARACTERS) PER LOGICAL RECORD
112 LOGICAL HEADER RECORDS PER PHYSICAL RECORD
93184 BITS PER PHYSICAL HEADER RECORD
DATA FILE --  2020 BITS PER LOGICAL DATA RECORD
14 LOGICAL DATA RECORDS PER PHYSICAL RECORD
28280 BITS PER PHYSICAL DATA RECORD```