34-42-01
ú ú 11 Page 4 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SUNDSTRAND MK V GPWC ú
34-42-01
ú ú 09 Page 5 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
MAIN WHEEL WELL AREA
HARDWARE
WARN CARD (E1) PANEL (P7) GROUND PROXIMITY WARNING COMPUTER (E2-4)
Ground Proximity Warning System SchematicFigure 3 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SUNDSTRAND MK V GPWC ú
34-42-01
ú ú 11 Page 6 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
PULL UP STATUS
PRESENT
BITE GPWC
R
STATUS/
2
SPEECH PROM DISPLAY DISPLAY
HISTORY 0 0 0 0 0 0 0 0
TEST
3
PRIORITY MESSAGE - BASICCODE
AURAL
SWITCH
R
STATUS/HISTORY 4
MD&T
STATUS
M1 1
SIREN "WIND SHEAR WIND SHEAR" FLIGHT
PRESENT FLIGHTHISTORY
1
HISTORY
SHT "WHOOP WHOOP PULL UP"
2 2
CAPT PULL UP LT (P1)3
3 "TERRAIN"
3
PULL UP 4
"TOO LOW TERRAIN"
4
BITE MESSAGE FOR TEST
D1153BPULL UP LT
AURAL
THE GPWC SHALL DISPLAY PRESENT STATUS CONDITIONS
R
B7
2"PPRESENT STATUS" POSITION MOMENTARILY.
5 5
TOO LOW GEAR" WHEN THE STATUS/HISTORY SWITCH IS PLACED ON THE
WARNING
3
PRIORITY
A6
TOO LOW FLAP" _________________________________
EXAMPLE FOR A NO FAILURE MESSAGE: A.
6
R
N7
4
LOGIC
CHARACTER DISPLAYED
MD&T
1) @@@@@@@@
ALTITUDE CALLOUTS
7 1
2) IN TEST
C6
ALT AUDIO
3) AIRCRAFT TYPE 737-XXX BASIC
SHT
8 8
"SINK RATE" 4) FMC SELECTED
BASIC VOICESSELECT D6 F/O PULL UP LT (P3)
3
5) ALT LAMP FORMAT SELECTED
NC
6) SYSTEM OK
PROGRAM
9 9
"DON'T SINK" C7 MASTER
7) SOFTWARE VERSION IS XXX DD-MMM-YY
BELOW G/S P-INHIBIT
PINS
8) DATABASE VERSION IS XXX, XX-XXX-XX
D5
DIM PROGRAM
10 10
"GLIDE SLOPE" 9) END TEST
A
1
TEST COMMON A3
LOGIC
3
WARN INHIBIT LAMP
A
42 STEADY
DRIVER STEADY/FLASH
SOFTWARE HARDWARE ALT LAMP FORMAT
AURAL 2 PROGRAMB5 NC CAPT BELOW G/S LT (P1)
MASTER
PIN B15 BELOW G/S P-INHIBITSTEADY
DIM
STEADY/FLASH
AURALS BUFFERS A5 NC 2-6,8,9
A
BELOW G/S LT 1
D3 LAMP
CONFIDENCE TEST SEQUENCE
3
_____________LAMP OUTAURAL
A
DRIVER
4
AURAL 10
10 BELOW G/S, INOP TEST LOGIC
2
2 PULL UP, INOP
SELF TEST1 WINDSHEAR, INOP
DISCRETES A9F/O BELOW G/S LT (P3)
AURALS MOM AUDIO CANCELMOM AUDIO CANCEL
D8NC
G/S REPETITION
3-6,8-10 S653
GPWC INHIBIT D13
BUFFERS SELF TEST
D7SHT RATE AURAL MESSAGES 1-10
4
1
B BITE TEST FULL VOCAB TEST5 SECMASTER
IN AIR INHIBITSEQUENCE PROG PINA8INOP
DIM GAIN REDUCE AFTERBUFFERSA15
AURAL MESSAGES 1,2,10 11 1
4TH MESSAGE
TEST CONFIDENCE TEST
NC IN AIR INHIBIT LOGIC
A
72
ALT C/O GAIN REDUCEDISCRETE ALT C/O GAIN REDUCEA2123
BUFFER
GAIN REDUCEIN AIR INHIBIT BITE ENABLE GPWS INOP
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊 導(dǎo)航 NAVIGATION 3(114)
