S 865-074
(6)
Make sure that all instrument switches are in the NORMAL position.
S 865-075
(7)
Make sure that the airplane is in the ground mode.
NOTE: The GROUND SENSING light is off to show the airplane is in
____ ground mode. You can find the GROUND SENSING light on the E11 shelf, forward of the nose wheel well.
S 865-076
(8)
Make sure that the autopilot is disengaged.
S 865-077
(9)
Make sure that the IRS ground speed is less than 20 knots or the FMC ground speed is less than 20 knots.
E. Current Status Quick Test (Group 10)
S 745-184
(1) Do the current status quick test:
(a)
Push the INIT/REF key on the Flight Management Computer System (FMCS) Control Display Unit (CDU) (Fig. 501) to show the POS INIT page or PERF INIT page.
(b)
Push the line-select key (LSK) adjacent to <INDEX to show the INIT REF INDEX 1/1 page.
(c)
Push the LSK adjacent to MAINT> to show the MAINT BITE INDEX 1/1 page.
NOTE: It is not possible to get access to the MAINT BITE INDEX
____ page (the prompt MAINT> is not shown on the CDU display) if the airplane is in the air mode.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
22-11-01
ú ú 05 Page 505 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
Flight Management Computer System Control Display Unit
Figure 501
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
22-11-01
ú ú 01 Page 506 ú Nov 15/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(d)
(e)
(f)
(g)
(h)
A
737-300/400/500MAINTENANCE MANUAL
Push the LSK adjacent to <DFCS to show the DFCS BITE TEST LINE MAINT 1/2 page.
NOTE:____If the CDU display shows DFCS BITE INOP CHECK FCC OR INTERFACE, make a check of the DFCS BITE preconditions for the causes. Push the INIT REF key to get out of the BITE.
Push the LSK adjacent to <CURRENT STATUS from the DFCS BITE
TEST LINE MAINT 1/2 page.
Do the preparation steps as shown on the CDU display.
Push the LSK adjacent to <CONTINUE to start the quick test.
Make sure that the quick test is completed with no failure.
NOTE: If a failure occurs, the test will stop and the TEST
____ FAILED indication will show on the CDU display.
QUICK TEST__________ GROUP NO./LIBRARY TEST NO.
DISCRETE INP 10.70 IRU 10.01 NAV RECEIVER 10.02 DADC 10.03 ATC 10.04 DME 10.05 ALPHA VANE 10.06 LRRA 10.07 ADI 10.08 MACH/AS 10.09 LNAV 10.11 AFDS FMA 10.13 MCP 10.16 N1 POT 10.17 FMC 10.18 M AUTO BITE 10.21 *[1] MCP DISPLAY 10.57
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
22-11-01
ú ú 01 Page 507 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
*[1] If library test 21 (Miscellaneous Test) fails, put code 100 into the CDU scratchpad then push LSK adjacent to RERUN>. If subtest 21.Q.112 on the FCC-B fails, the LRU fault should be PCWS XDUCER-CAPT instead of PCWS XDUCER-F/O. If subtest
21.Q.115 fails on the FCC-B side, the LRU fault should be PCWS XDUCER-F/O instead of PCWS XDUCER-CAPT.
(i) If a failure occurs, do these steps:
1) From the CDU display, make a note of the test name, the channel, and the LRU that caused the failure.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 1(117)
