Honeywell International Inc. KX165A Manuale Utente
BENDIX/KING
KX 155A/165A
KX 155A/165A
COMM/NAV SYSTEM
10542I02.ZIPRCD
Page 3-17
Rev 2, Apr/2000
bolic aircraft indicates the relative position of the selected course. For backcourse operation, set
the course pointer to the inbound localizer front course. The deviation bar position relative to the
symbolic aircraft then represents the position of the backcourse with respect to the aircraft. Figure
3-16 displays the control functions for the KI 525.
the course pointer to the inbound localizer front course. The deviation bar position relative to the
symbolic aircraft then represents the position of the backcourse with respect to the aircraft. Figure
3-16 displays the control functions for the KI 525.
FIGURE 3-16 KI 525A INDICATOR AND CONTROLS
3.4
KI 229 RMI OPERATION
The KNI 229 Radio Magnetic Indicator provides bearing information to both ADF and VOR sta-
tions by means of two pointers, each of which is read against the compass card. The servo drive
compass card displays heading information derived from ARINC type X, Y, Z, compass headings.
The double pointer is dedicated solely to a ADF DC SIN/COS source. The single pointer is as-
signed to VOR information.
tions by means of two pointers, each of which is read against the compass card. The servo drive
compass card displays heading information derived from ARINC type X, Y, Z, compass headings.
The double pointer is dedicated solely to a ADF DC SIN/COS source. The single pointer is as-
signed to VOR information.
NOTE
The single pointer can be switched between VOR
and ADF by means of an external switch as ex-
plained in the installation manual of the KNI 229.
3.5
OTHER INDICATORS
Refer to respective installation manuals for operation instructions of other indicators.
PRELIMINARY - SUBJECT TO CHANGE WITHOUT NOTICE