```  718-01 QUEIMADAS 11 AUGUST 1980                   FIRST TIME ON THIS FILE 15  1  0       THIS FILE I
S ALL OR PART OF TIME PERIOD 15  1  0 TO 16 50  0  DESCRIPTION OF RECORD --  54 PARAMETERS WERE SAVE
D AT THEIR RESPECTIVE RATES.  THIS REPRESENTS   54 SAMPLES/PROGRAM CYCLE WHERE A CYCLE IS 1.000 SEC
THE 27 CYCLES OF  54 SAMP/CYC = 1458 WERE THEN SCALED INTO 20 BIT INTEGERS AND PACKED 3 SAMPLES/WOR
D INTO 486 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     PILOT MICROPHONE SWITCH 1 (XMIT) (VDC)     XMIT1     VDC     = (N/ 1000.0) -  100.0
6)   1     PILOT MICROPHONE SWITCH 2 (XMIT) (VDC)     XMIT2     VDC     = (N/ 1000.0) -  100.0
7)   1     FIXED ZERO VOLTAGE (VDC)                   FZV       VDC     = (N/ 1000.0) -  100.0
8)   1     RAW INS LATITUDE (DEG)                     ALAT      DEG     = (N/ 1000.0) -  100.0
9)   1     RAW INS LONGITUDE (DEG)                    ALONG     DEG     = (N/ 1000.0) -  200.0
10)   1     AIRCRAFT TRUE HEADING (ARINC) (DEG)        THI       DEG     = (N/ 1000.0) -  100.0
11)   1     INS WANDER ANGLE (DEG)                     ALPHA     DEG     = (N/ 1000.0) -  100.0
12)   1     RAW INS GROUND SPD X COMPONENT (M/S)       XVI       M/S     = (N/ 1000.0) -  500.0
13)   1     RAW INS GROUND SPD Y COMPONENT (M/S)       YVI       M/S     = (N/ 1000.0) -  500.0
14)   1     RAW INS GROUND SPEED (M/S)                 GSF       M/S     = (N/ 1000.0) -  100.0
15)   1     AIRCRAFT PITCH ATTITUDE ANGLE (DEG)        PITCH     DEG     = (N/ 1000.0) -  100.0
16)   1     AIRCRAFT ROLL ATTITUDE ANGLE (DEG)         ROLL      DEG     = (N/ 1000.0) -  100.0
17)   1     AIRCRAFT TRUE HEADING (YAW) (DEG)          THF       DEG     = (N/ 1000.0) -  100.0
18)   1     RAW INS VERTICAL VELOCITY (M/S)            VZI       M/S     = (N/ 1000.0) -  500.0
19)   1     RAW DYNAMIC PRESSURE (FUSELAGE) (MB)       QCF       MB      = (N/ 1000.0) -  100.0
20)   1     CORRECTED DYNAMIC PRESR (FUSELAGE) (MB)    QCFC      MB      = (N/ 1000.0) -  100.0
21)   1     RAW STATIC PRESSURE (FUSELAGE) (MB)        PSF       MB      = (N/ 1000.0) -    0.0
22)   1     CORRECTED STATIC PRESR (FUSELAGE) (MB)     PSFC      MB      = (N/ 1000.0) -    0.0
23)   1     NACA PRESSURE ALTITUDE (M)                 HP        M       = (N/   10.0) -  500.0
24)   1     TOTAL TEMPERATURE (FUS. ROSEMOUNT) (C)     TTF       C       = (N/ 1000.0) -  100.0
25)   1     TOTAL TEMPERATURE (DEICED ROSEMNT) (C)     TTFH      C       = (N/ 1000.0) -  100.0
26)   1     AMBIENT TEMPERATURE (ROSEMOUNT) (C)        ATF       C       = (N/ 1000.0) -  100.0
27)   1     AMBIENT TEMP (DEICED ROSEMOUNT) (C)        ATFH      C       = (N/ 1000.0) -  100.0
28)   1     DEW/FROSTPOINT TEMP   (THERMOELEC) (C)     DP        C       = (N/ 1000.0) -  100.0
29)   1     DEWPOINT TEMPERATURE   (THERMOELEC) (C)    DPC       C       = (N/ 1000.0) -  100.0
30)   1     ABSOLUTE HUMIDITY   (THERMOELEC) (G/M3)    RHOTD     G/M3    = (N/ 1000.0) -  100.0
31)   1     TRUE AIRSPEED (FUSELAGE)  (M/S)            TASF      M/S     = (N/ 1000.0) -  100.0
32)   1     HORIZONTAL WIND DIRECTION (DEG)            WDRCTN    DEG     = (N/ 1000.0) -  100.0
33)   1     HORIZONTAL WIND SPEED (M/S)                WSPD      M/S     = (N/ 1000.0) -  100.0
34)   1     WIND VECTOR EAST COMPONENT (M/S)           UI1       M/S     = (N/ 1000.0) -  200.0
35)   1     WIND VECTOR NORTH COMPONENT (M/S)          VI1       M/S     = (N/ 1000.0) -  200.0
36)   1     WIND VECTOR LNGTDNL COMPONENT (M/S)        UX1       M/S     = (N/ 1000.0) -  200.0
37)   1     WIND VECTOR LATERAL COMPONENT (M/S)        VY1       M/S     = (N/ 1000.0) -  200.0
38)   1     RAW INS GROUND SPD EAST COMP (M/S)         VEW       M/S     = (N/ 1000.0) -  500.0
39)   1     RAW INS GROUND SPD NORTH COMP (M/S)        VNS       M/S     = (N/ 1000.0) -  500.0
40)   1     DISTANCE EAST OF START (KM)                DEI       KM      = (N/  100.0) - 1000.0
41)   1     DISTANCE NORTH OF START (KM)               DNI       KM      = (N/  100.0) - 1000.0
42)   1     AIRCRAFT C.G. ACCELERATION (M/S2)          CGAC      M/S2    = (N/ 1000.0) -  100.0
43)   1     DAMPED AIRCRAFT VERT VELOCITY (M/S)        WP3       M/S     = (N/ 1000.0) -  100.0
44)   1     PRESSURE-DAMPED INERTIAL ALTITUDE (M)      HI3       M       = (N/   10.0) -  500.0
45)   1     CABIN PRESSURE ,MB.                        PCAB      MB      = (N/ 1000.0) -    0.0
46)   1     DASIBI OZONE (VDC)                         DAO3      VDC     = (N/ 1000.0) -  100.0
47)   1     NBS (NCAR 14B) SIGNAL (VDC)                NBS       VDC     = (N/ 1000.0) -  100.0
48)   1     NBR (NCAR) RANGE (VDC)                     NBR       VDC     = (N/ 1000.0) -  100.0
49)   1     UMS (UNIMIC 14B) SIGNAL (VDC)              UMS       VDC     = (N/ 1000.0) -  100.0
50)   1     MAX PLANCK CO (MPCO) (VDC)                 MPCO      VDC     = (N/ 1000.0) -  100.0
51)   1     MAX PLWNCK H2 (MPH2) (VDC)                 MPH2      VDC     = (N/ 1000.0) -  100.0
52)   1     KURZ FLOW RATE (VDC)                       FRKURZ    VDC     = (N/ 1000.0) -  100.0
53)   1     SPARE 3 (VDC)                              SPARE3    VDC     = (N/ 1000.0) -  100.0
54)   1     SPARE 4 (VDC)                              SPARE4    VDC     = (N/ 1000.0) -  100.0

THERE ARE   1 PHYSICAL RECORDS IN THE HEADER FILE