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时间:2011-04-01 08:39来源:蓝天飞行翻译 作者:航空
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____ page (the prompt MAINT> is not shown on the CDU display) if the airplane is in the air mode.
 (d)  
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.

 (e)  
Push the LSK adjacent to <CURRENT STATUS from the DFCS BITE TEST LINE MAINT 1/2 page.

 (f)  
Do the preparation steps as shown on the CDU display.

 (g)  
Push the LSK adjacent to <CONTINUE to start the quick test.

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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

PAGE NUMBER
TITLE BLOCK
Flight Management Computer System Control Display Unit
Figure 501

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 QUICK TEST__________  GROUP NO./LIBRARY TEST NO._________________________
 DISCRETE INP  10.70
 IRU  10.01
 VOR/ILS  10.02
 DADC  10.03
 ATC  10.04
 DME  10.05
 ALPHA VANE  10.06
 LRRA  10.07
 ADI  10.08
 MASI  10.09
 LNAV  10.11
 AFDS FMA  10.13
 MCP  10.16
 N1 POT  10.17
 FMC  10.18
 FMA AUTO BITE  10.20
 M AUTO BITE  10.21 *[1]
 MCP DISPLAY  10.57

 *[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-F/O.
 (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.
 NOTE: Before you replace a defective component, do the
____ BITE on the system (if it is applicable) and on the FMS interface subsystems with the defective component.
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 ú ú 05 Page 507 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 2)  If it is necessary to do the quick test again, push the LSK adjacent to RERUN>.
 3)  To get the test result data, use the CDU keyboard to put the engineering code 100 into the scratchpad. Push the LSK 6R.
 4) To get out of the test result data, push the E key on the CDU keyboard. Push the LSK 6R. 5) Push the LSK adjacent to <CONTINUE to continue the quick test.
 (j)  If no failure occurs, the CDU display shows *QUICK TEST PASSED* and the Additional Tests Selection page.
 NOTE: This permits the selection of the Interactive/Surface
____ tests for the five systems shown on the CDU display.
 ~............................ | DFCS BITE TEST | | SUMMARY -A/-B 10. | | *QUICK TESTS PASSED* | | SELECT ADDITIONAL TESTS | | | | <AUTOPILOT | | | | <FLIGHT DIRECTOR | | | | <MACH TRIM SYSTEM | | | | <SPEED TRIM SYSTEM | | | | <ALTITUDE ALERT EXIT> | 2............................1
 F.  Autopilot Test (Group 11)
 
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