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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
(d) Line 6
1
Line 6 displays the headers, TSPO, beginning in column 2 and, POC,
beginning in column 15. The LRU time since power-on is displayed
right-justified from column 12.
2
The UTC is displayed as hh:mm, where hh represents the UTC hours from
00 to 23 and mm represents the UTC minutes from 00 to 59. The UTC is the
time the failure was stored in the failure memory log on this flight leg.
Dashes are displayed if no valid UTC data is available.
3
Line 6 displays the power-on count value from 0 to 65535 right-justified from
column 23.
(e) Line 7
1
Line 7 displays the headers, TEMP, beginning in column 2, and GSPD,
beginning in column 15. The LRU-failed SRU (or PSU) temperature is
displayed right-justified from column 12. Dashes are displayed if no valid
temperature data is available. The groundspeed is displayed right-justified
from column 23.
(f) Line 8
1
Line 8 displays the headers, PHASE, beginning in column 2, and DC,
beginning in column 15. The flight phase is displayed right-justified from
column 12. If a numbered flight phase is not available, then an a or g is
shown in column 12, as appropriate. The DC state is displayed as DC0,
DC0', DC1, DC1', or DC2 right-justified from column 23.
Honeywell International Inc. Do not copy without express permission of Honeywell.
23- -20- -35
Page 6--89
15 Jul 2006
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