• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-02 23:33来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

A
C 4
MASTER
C7
 AIR DATA VALIDPTT
DIM
TEST LOGIC LAMP D1153A
RAD ALT VALIDBITE DISPLAY GPWS INOP LIGHT
DRIVER
WINDSHEAR D12 LOC VALID
G/S VALIDINOP GPWC FAIL
IN AIR INHIBIT(SHT 3)
SEL CRS VALID
D  GPWC D1153B P3-7 GROUND PROX MODULEIRS VALIDBITE HI LEVEL
DEMOD 3B
AUDIO
PROCESSOR VALIDAUDIO INHIBIT&
NC POWER SUPPLY VALID
AUDIO OUT
LAMP
WINDSHEAR BITE DATA 3C
L SHT 3  AMP
AUDIO MESSAGE
G/S CANCEL LO LEVEL
CONFIG VALID
E
C13G/S GAIN REDUCE AUDIO OUT D2501A
DISCRETES VALIDD13
PROG PINS VALID K15 + SOFTWARE GPWS IN
G/S CANCEL  DISCRETEK14 -
D9
BUFFER HARDWARE
REMOTE ELECTRONICS UNITGROUND PROXIMITY WARNING COMPUTER (E2-4) (AUDIO SYSTEM) (E2-1)
Ground Proximity Warning System Schematic
Figure 3 (Sheet 2)


EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SUNDSTRAND MK V GPWC ú

 34-42-01
 ú ú 11 Page 7 ú Nov 12/01

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 11 Page 8 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

3000
2000
HEIGHT ABOVE TERRAIN (FT)
1000
0
*65 FT NOMINAL ON CLIMBING

SINK RATE (FPM)

Mode 1 - Excessive Descent Rate Figure 4
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SUNDSTRAND MK V GPWC ú

 34-42-01
 ú ú 03 Page 9 ú Nov 12/01

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
2500

2000
HEIGHTABOVE1500 TERRAIN(FT)
1000
500
0 0 1000 2000 3000 4000 5000 6000 7000 8000 9000

 

CLOSURE RATE (FPM)
MODE 2A - FLAPS NOT IN LANDING CONFIGURATION
600 HEIGHTABOVE400 TERRAIN800
(FT) 200
HEIGHT
ABOVE

500
TERRAIN
0

(FT)
0 400 800 1200
BAROMETRIC RATE (FPM)
MODE 2B - LOWER LIMIT
0
A0 1000 2000 3000 4000 CLOSURE RATE (FPM)

MODE 2B - FLAPS IN LANDING CONFIGURATIONMode 2 - Excessive Closure RateFigure 5


EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SUNDSTRAND MK V GPWC ú

 34-42-01

 ú ú 03 Page 10 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 6.  Ground Proximity Warning System Control Module (Fig. 1)
______________________________________________
 A.  The ground proximity warning control module is located on the first officer's instrument panel. It consists of an amber INOP indicator light, a SYS TEST switch, a guarded and lockwired FLAP INHIBIT switch and a guarded & lockwired GEAR INHIBIT switch. The INOP indicator light comes on when the monitor circuit in the computer senses a fault condition. The TEST switch provides a confidence check of the system, either in flight or on the ground. The FLAP INHIBIT switch enables the pilots to simulate a flap down condition and the GEAR INHIBIT switch enables the pilots to simulate a gear down condition when the switches are set to INHIBIT position. When placed in the INHIBIT position, the TOO LOW-FLAPS and TOO LOW-GEAR warnings are inhibited.
 7.  Warning Speaker
_______________
 A.  The aural warning signals from the GPWC are sent to the remote electronic unit (Shelf 1, equipment rack No. 2) to be processed. The aural warnings are then broadcast over the cockpit speakers (pilots overhead panel P5) and the flight interphone system.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 导航 NAVIGATION 3(115)