Honeywell GNS-XL GPS Receiver User Manual


 
DIS:
The direct distance in nauti-
cal miles and tenths from the
aircraft present position to
the holding fix. (Figure 2-21)
ETE:
The estimated time enroute
to the next time over holding
fix based on the path around
the Hold “racetrack”. (Figure
2-21)
INBOUND CRS (course):
The inbound holding course in whole degrees. (Figure 2-21)
GS:
The current groundspeed. (Figure 2-21)
WIND:
The current wind direction referenced to True North and speed in
knots. (Figure 2-21)
NOTE: The leg change mode (AUTO or MAN normally displayed on
the last line of NAVIGATION Page 1) is not displayed while holding.
NAVIGATION 2/4 (Page 2 of 4)
Pressing the NAV Key again will display the second NAVIGATION
Page and the following can be observed.
FR/DIRECT/HOLD/PROCEDURE TURN/DME ARC:
Same as discussed for NAVIGATION 1/4.
TO/AT/AR/HP/PT:
Same as discussed for NAVIGATION 1/4.
NX/Holding Status:
Same as discussed for NAVIGATION 1/4.
Page Display Definitions
2-17
GNS-XL Flight Management System
Rev. 0
Oct/96
HOLD RIGHT AUTO
AT MEI 20:41
EXIT HOLD 00:07.9
DIS 4.8
ETE 00:07.9
INBOUND CRS 101
GS 154
WIND 286/ 12
NAVIGATION 1/4
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Figure 2-21