- 289 -
SOUTHWEST AIRLINES PROPRIETARY(c) All rights reserved
A34-46-00-038.fm
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL
GPWS - SELF-TEST - LEVEL 6
General Description
The GPWC has a level six discrete input test.
The level six self-test can be done from the GPWC or the GPW module. Use a 600 ohm headphone to listen to the test information when you do the test from the GPWC. Plug the headphone into the jack on the front panel of the GPWC.
Use the self-test button on the front panel of the GPWC or the GPW module to get access to level six. The self-test buttons have these two modes:
-Short cancel - push the button for less than two seconds
-Long cancel - push the button for more than two seconds.
Use the self-test buttons for these functions:
-Start self-test level one
-Go to the next item or flight leg within a test
-Go to the next self-test level
-End the self-test.
When test levels 2 through 5 end, the aural message PRESS TO CONTINUE shows. Push the self-test button to go to the next test level. When the level one test ends, there is no aural message. If you do not push the self-test button within three seconds, the self-test ends.
Level Six Self-test - Discrete Input Test
A level six test finds changes in discrete inputs.
The test starts with the aural message DISCRETE TEST. If the condition of a discrete input changes, you hear the new state of the discrete.
NOTE: The landing gear handle must be in the Off position to test the gear inhibit switch on the GPW module.
NOTE: Before moving the landing gear handle install landing gear locking pins.
You hear the aural message DISCRETE INPUT TEST - PRESS TO CANCEL every 60 seconds. Push a short or long cancel to end the self-test.
January 2005
34-46
- 290 -
SOUTHWEST AIRLINES PROPRIETARY(c) All rights reserved
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL
DISCRETE INPUT INPUT SOURCE ANNUNCIATIONS
GEAR INHIBIT SWITCH GPW MODULE LANDING GEAR DOWN LANDING GEAR UP
FLAP INHIBIT SWITCH GPW MODULE LANDING FLAPS NOT LANDING FLAPS
GLIDESLOPE INHIBIT SWITCH P1-3 AND P3-1 GLIDESLOPE CANCELLED GLIDESLOPE ENABLED
TERRAIN INHIBIT SWITCH GPW MODULE TERRAIN OFF TERRAIN ON
TERRAIN RELAY 1 LEFT EFIS TERR SWITCH TERRAIN RELAY 1 ON TERRAIN RELAY 1 OFF
TERRAIN RELAY 2 RIGHT EFIS TERR SWITCH TERRAIN RELAY 2 ON TERRAIN RELAY 2 OFF
LEVEL 6 DISCRETE INPUT TEST
A34-46-00-038.fm
GPWS - SELF-TEST - LEVEL 6
January 2005
34-46
- 291 -
SOUTHWEST AIRLINES PROPRIETARY(c) All rights reserved
A34-46-00-039.fm
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL
GPWS - STATUS LEDS
Purpose
There are three status LEDs on the front panel of the ground proximity warning computer (GPWC). The LED indicators show the status of the GPWC when power is supplied. The LEDs turn on for these conditions:
-External fault - yellow
-Computer OK - green
-Computer fail - red.
The yellow external fault LED shows that the GPWC has detected an external interface fault. The green computer OK LED shows that the GPWC is operating with no internal faults. The red computer fail LED shows that the GPWC has an internal fault.
NOTE: VISIT THE HONEYWELL EGPWS WEBSITE www.egpws.com FOR ACCESS TO ADDTIONAL INFORMATION AND FREE PDF DOCUMENTS
January 2005
34-46
- 292 -
SOUTHWEST AIRLINES PROPRIETARY(c) All rights reserved
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL
FAULT EXTERNAL OK COMPUTER FAIL COMPUTER ACTIONS
OFF GREEN OFF NORMAL OPERATION
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-700 AVIONCS BITE HANDBOOK 航电自测设备手册 2(28)
