Sensor Messages - Honeywell GNS-XLS Operator's Manual

Page Display Definitions
ADVISORY: (continued)
*WPT ALERT
WPT MEM FULL
VNAV WPT ALERT
VSPD FAIL

SENSOR MESSAGES

The following are sensor messages that may appear on the SEN-
SOR MESSAGES Page. All messages will cause the MSG annunci-
ator to flash unless other wise noted with an asterisk*.
Sensor Message
ACCURACY WARN
ALIGN
ATTITUDE
BATTERY WARN
CHECK QUAL
*DESELECTED
2-78
The aircraft is within 30 seconds ETE of the
next leg lateral change. Message annuncia-
tor will not illuminate.
All 999 waypoint locations have been used
in flight plans or as FROM or TO waypoints.
Aircraft is within 1 minute ETE of #TOD or
path intercept point. Message annunciator
will not illuminate. However the discrete
WPT annunciator will flash for 10 seconds
then go steady
The system vertical speed input has failed.
Explanation
The integrity monitoring system that moni-
tors the satellite constellation (RAIM) has
detected a GPS horizontal position error that
is outside the alarm threshold for the phase
of flight in progress. (.3NM Approach; 1NM
Terminal; 2NM Enroute)
The IRS is in the alignment mode and is not
yet NAV RDY.
The IRS is in the Attitude mode.
The sensor is operating on its own internal
battery.
The VPU quality factor has exceeded the
pilot entered advisory quality factor.
The sensor has been manually deselected
and will no longer contribute to the computa-
tion of composite (blended) position.
Message annunciator will not illuminate.
GNS-X Flight Management System
LS
Rev. 3
Sep/96