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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-31-00-017
ILS - ADI DISPLAYS
ILS - ADI DISPLAYS
EFFECTIVITY
SHZ ALL 34-31-00
Page 35
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-31-00-017
General
To show ILS displays on the CDS, set the EFIS control panel
mode selector to the APP position. You must also tune a valid
ILS frequency on the NAV control panel.
Normal Display
The glideslope deviation pointer and scale show at the right of
the NAV display. The glideslope deviation pointer is magenta
and the scale is white.
The glideslope scale is the standard four dot scale where each
dot equals 0.35 degrees of deviation. The glideslope deviation
pointer gives fly-to signals to intercept the glideslope beam.
The course pointer points to the number that you set on the
DFCS MCP.
The localizer deviation indicator and scale shows at the bottom
of the NAV display. The localizer scale is white and the localizer
deviation indicator is magenta.
The deviation scale is the standard four dot scale. One dot is
equal to 1 degree of deviation. The localizer deviation indicator
shows the deviation to the left or right of the runway centerline.
The NAV data source shows in white at the upper right corner of
the display. It shows the source of the data for the ILS displays.
To the right of the NAV data source is the active ILS frequency
display.
The ILS frequency display shows the active ILS frequency and
the selected course. If the ILS ground station transmits a morse
coded station identifier, the letter identifier replaces the numeric
frequency when the receiver captures the ground station signal.
Fail Display
For invalid ILS data, the CDS replaces the localizer deviation
scale and indicator with the amber LOC flag when the localizer
receiver fails. The amber G/S flag replaces the glideslope
deviation scale and pointer when the glideslope receiver fails.
ILS - EXPANDED ILS DISPLAY
EFFECTIVITY
SHZ ALL 34-31-00
Page 36
D633A101-SHZ1 Jun 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-31-00-018
ILS - EXPANDED ILS DISPLAY
ILS - EXPANDED ILS DISPLAY
EFFECTIVITY
SHZ ALL 34-31-00
Page 37
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-31-00-018
General
To show the centered ILS NAV display, push the CTR switch on
the EFIS control panel mode selector switch.
Normal Displays
The glideslope deviation pointer and scale show to the right of
the HSI display. The glideslope pointer is magenta and the
scale is white.
The glideslope scale is the standard four dot scale. Each dot
equals 0.35 degrees of deviation. The pointer gives fly-to
commands to intercept the glideslope beam.
The course pointer points to the number that you set on the
DFCS MCP.
The localizer deviation indicator and scale show in the center of
the HSI compass card. The localizer deviation indicator is
magenta and the scale is white.
The localizer scale is the standard four dot scale. Each dot is
equal to 1 degree of deviation. The deviation indicator shows
the deviation to the left or the right of the runway centerline.
The NAV data source shows in white in the upper right corner of
the display. It shows the source of data for the ILS display. The
active ILS frequency shows to the right of the NAV data source.
The ILS frequency display shows the active ILS frequency and
the selected course. If the ILS ground station transmits a morse
coded station identifier, then the letter identifier replaces the
numeric frequency when the receiver captures the ground
station signal.
Fail Display
For invalid ILS data, the CDS replaces the localizer scale and
deviation indicator with the amber LOC flag when the localizer
receiver fails. The amber G/S flag replaces the glideslope scale
and pointer when the glideslope receiver fails.
ILS - CENTERED ILS DISPLAY
EFFECTIVITY
SHZ ALL 34-31-00
Page 38
D633A101-SHZ1 Jun 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-31-00-019
ILS - CENTERED ILS DISPLAY
ILS - CENTERED ILS DISPLAY
EFFECTIVITY
SHZ ALL 34-31-00
Page 39
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
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