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-The LOC and G/S flags show momentarily
-For the first 3 seconds, one dot left of localizer deviation and one
dot up of glideslope deviation.
-For the next 3 seconds, one dot right of localizer deviation and
one dot down of glideslope deviation

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SOUTHWEST AIRLINES PROPRIETARY(c) All rights reserved
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL
COURSE
ACTIVE STANDBY
TFR
MAP
PLN
VOR
148
TEST
COURSE
APP
SWITCH
N
VOR 1
VOR 2 SELECTOR
CTR
A
OFF
OFF
TEST
V
INOP
INOP
MODE SELECTOR

NAV CONTROL PANEL  EFIS CONTROL PANEL  DFCS MODE CONTROL PANEL 
DME112 HDG 148 M TAS --- GS0  DME112 GS0 HDG 148 M TAS --- 112DME GS0 HDG 148 M TAS ---
20  20  20 
G / S 
ILS 1 ---/---LOC  108.10  ILS 1 108.10 ---/--- ILS 1 108.10 ---/---
FAIL ILS DATA  FIRST 3 SECONDS OF TEST  NEXT 3 SECONDS OF TEST 
LOCALIZER = ONE DOT LEFT DISPLAY GLIDESLOPE = ONE DOT UP DISPLAY  LOCALIZER = ONE DOT RIGHT DISPLAY GLIDESLOPE = ONE DOT DOWN DISPLAY 
ILS - SELF-TEST 
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A34-31-00-021.fm
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A34-31-00-023.fm
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL

ILS - SELF-TEST Test Continued from previous page.
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SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL

A34-31-00-023.fm
ILS
ILS
ILS
ILS
LOC
FAIL ILS DATA

FIRST 3 SECONDS OF TEST NEXT 3 SECONDS OF TEST
LOCALIZER = ONE DOT LEFT DISPLAY LOCALIZER = ONE DOT RIGHT DISPLAY GLIDESLOPE = ONE DOT UP DISPLAY (ADI) GLIDESLOPE = ONE DOT DOWN DISPLAY (ADI)
ILS - SELF-TEST
G /S
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A34-24-00-006.fm
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL

ILS - SELF-TEST Test Continued from the previous page.
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SOUTHWEST AIRLINES PROPRIETARY(c) All rights reserved
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL

OFF APP 
B/CRS 
OFF APP 
B/CRS 
INVALID DATA DISPLAY 
UP/LEFT DISPLAY  OFF APP  B/CRS 
DOWN/RIGHT DISPLAY 
START TEST  END TEST 

A34-24-00-006.fm
ILS - SELF-TEST
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SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL

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DME SELF TEST
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A34-55-00-015.fm
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL

DME SYSTEM - TEST DISPLAY
General
To start the test tune an inactive VOR or ILS frequency on the respective NAV control panel and press the test button on the panel. The test can also be started from the bite panel on the DME receiver located in the E&E compartment.
During a ground test or a self test, the display units show these indications:
- The DME fail condition for two seconds 
- The DME NCD condition for the next two seconds 
- The DME normal condition to end the test. 

The DME normal condition is the distance that shows before the test starts.
　
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