Programming A Heading Intercept To The Final Approach Course - Honeywell GNS-XLS Operator's Manual

9. ENTER Key - DEPRESS.
An Intercept Message may
appear (NO COURSE
INTERCEPT, NO ARC
INTERCEPT, or INTER-
CEPT BEYOND
(Figure 3-103). If no mes-
sage appears the intercept
will occur on the TO side of
the selected TO waypoint.
The intercept messages are
based on the current aircraft
heading and track. Once the selected heading has been established,
the HEADING VECTOR Page may be viewed to determine the inter-
cept status. If NO COURSE INTERCEPT or NO ARC INTERCEPT
occurs, the message light will illuminate and these messages will be
displayed on the SYSTEM MESSAGES Page. To view one of these
messages on the HDG Page, use the Line Select Key to remove the
cursor from the page.
NOTE: BUSY - STANDBY may be displayed in yellow momentarily
while the intercept is calculated.
10. ENTER Key - DEPRESS to accept data and return to NAV page
1. The cursor is positioned over the Leg Change Mode if the
DTK has been entered manually on the Heading Page.
PROGRAMMING A HEADING INTERCEPT TO THE FINAL
APPROACH COURSE
This procedure non-precision approach may be accomplished using the
following steps:
1. HDG - DEPRESS to dis-
play the HEADING VEC-
TOR Page.
2. Type in the assigned
heading. (Figure 3-104)
3. ENTER Key - DEPRESS.
The cursor moves to the
heading mode field.
Rev. 6
Jul/98
HEADING VECTOR 1/1
HDG
<
INTERCEPT\
<
FIX
TO IAH
<
INTERCEPT BEYOND FIX
OK? ENTER
HEADING VECTOR 1/1
HDG
<
\
<
TO DRK
<
OK? ENTER
GNS-X Flight Management System
LS
System Operation
205
DTK
Figure 3-103
205
DTK 125
Figure 3-104
193
>
>
3-61