34-42-02
ú ú 03 Page 503 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C.
D.
E.
A
737-300/400/500MAINTENANCE MANUAL
Access
(1) Location Zones 101/102 Flight Compartment 205 Electronic Compartment
Prepare for the Test
S 865-064
(1)
Supply electrical power (Ref 24-22-00/201).
S 715-037
(2)
Do the GPWS - Operational Test (Ref 34-42-02/501).System Interface Test
S 865-018
(1)
Open the RADIO ALTM-1 circuit breaker on the P18-1 panel.
(a)
BEJ 061-062, 101-112;
Make sure the INOP light comes on within 12 seconds.
(b)
BEJ 063-100, 113-999;
Make sure the INOP light remains off.
S 865-085
(2) BEJ 063-100, 113-999; Open the RADIO ALTM 2 circuit breaker on the P18-1 panel.
(a) Make sure the INOP light comes on within 12 seconds.
S 865-019
(3) Close the RADIO ALTM-1 circuit breaker on the P18-1 panel.
(a) Make sure the INOP light goes off.
S 865-084
(4) BEJ 063-100, 113-999; Close the RADIO ALTM 2 circuit breaker on the P18-1 panel.
(a) Make sure the INOP light remains off.
S 865-020
(5) Open the No. 1 AIR DATA CMPTR AC circuit breaker on the P18-2 panel.
(a) Make sure the INOP light comes on within 12 seconds.
S 865-021
(6) Close the No. 1 AIR DATA CMPTR AC circuit breaker on the P18-2 panel.
(a) Make sure the INOP light goes off.
S 865-022
(7) Open the VHF NAV VOR/ILS-1 circuit breaker on the P18-1 panel.
(a) Make sure the INOP light comes on within 18 seconds.
S 865-023
(8) Close the VHF NAV VOR/ILS-1 circuit breaker on the P18-1 panel.
(a) Make sure the INOP light goes off.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH -208 AND ON GPWC ú
34-42-02
ú ú 17 Page 504 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 865-024
(9) Set the VHF NAV switch to the BOTH ON 2 position.
(a) Make sure the INOP light does not come on.
S 865-025
(10)
Set the VHF NAV switch to the NORMAL position.
S 865-026
(11)
Open the GND PROX circuit breaker on the P18-1 panel.
(a) Make sure the INOP light comes on within 6 seconds.
S 865-027
(12) Close the GND PROX circuit breaker on the P18-1 panel.
(a) Make sure the INOP light goes off.
S 865-028
(13)
Open the SMC No. 1 AC and SMC No. 1 DC circuit breakers on the P18-2 panel.
S 865-029
(14)
Open the SMC No. 2 AC and SMC No. 2 DC circuit breakers on the P6-1 panel.
(a) Make sure the INOP light comes on within 12 seconds.
S 865-030
(15) Close the SMC No. 1 AC and SMC No. 1 DC circuit breakers on the P18-2 panel.
(a) Make sure the INOP light goes off.
S 865-031
(16) Close the SMC No. 2 AC and SMC No. 2 DC circuit breakers on the P6-1 panel.
F. Present Status Test
S 745-032
(1)
Set the switch on the GPWC front panel to the PRESENT STATUS position.
S 755-033
(2)
Make sure these messages show on the GPWC front panel:
(a)
IN TEST
(b)
AIRCRAFT TYPE 737-XXX
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH -208 AND ON GPWC ú
34-42-02
ú ú 13 Page 505 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(c)
BEJ 063-100, 113-999;
DUAL RADIO ALTIMETER SELECTED
(d)
ALT. LAMP FORMAT SELECTED
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(127)
