*[1] AIRPLANES WITH -420 EFIS SGs AND SUBSEQUENT *[2] AIRPLANES WITH -413 EFIS SGs AND SUBSEQUENT
 (e)  Push the LSK 6L (<INDEX) two times. 1) Make sure the CDU display shows the EFIS BITE TEST page.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-22-00
 ú ú 06A Page 521 ú Mar 15/96

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 F.  EFIS Discrete Status Tests
 NOTE: The EFIS DISCRETE STATUS pages on the CDU indicate the analog
____ discrete inputs to the EFIS. The status of each input is also shown on the DISCRETE STATUS pages.
 S 745-053
 (1)  Do the EFIS - Left Discrete Status Test as follows:
 (a)  
Push the LSK 1L (<EFIS LEFT BITE). 1) Make sure the CDU display shows the FAULT INDEX LEFT page.

 (b)  
Push the LSK 5L (<DISCRETE STATUS).

 1)  Make sure the CDU display shows the DISCRETE STATUS-L 1/2 page as follows:
 EFIS BITE TEST
 DISCRETE STATUS-L  1/2
 ADC SEL LEFT AIR/GROUND GROUND ANCDU SEL *[1] ----COMPARATOR ENABLED *[2] DME SEL LEFT FLT PATH MGMT ENABLED FMC SEL LEFT
 <INDEX

 *[1] AIRPLANES WITH -420 EFIS SGs AND SUBSEQUENT, The ANCDU SEL line will not show unless an ANCDU is installed.
 *[2] DISABLED for BEJ 101-112
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-22-00

 ú ú 16A Page 522 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (c)  Push the NEXT PAGE key on the CDU.
 1)  Make sure the CDU display shows the DISCRETE STATUS-L 2/2 page as follows:
 EFIS BITE TEST
 DISCRETE STATUS-L  2/2

 ILS SEL LEFT
 IRU SEL LEFT
 MAG/TRUE MAG
 MLS SEL ----SWC SEL LEFT
 VOR SEL LEFT

 <INDEX

 (d)  Push the LSK 6L (<INDEX) two times. 1) Make sure the CDU display shows the EFIS BITE TEST page.
 S 745-054
 (2)  Do the EFIS - Right Discrete Status Test as follows:
 (a)  
Push the LSK 2L (<EFIS RIGHT BITE). 1) Make sure the CDU display shows the FAULT INDEX RIGHT page.

 (b)  
Push the LSK 5L (<DISCRETE STATUS).

 1)  Make sure the CDU display shows the DISCRETE STATUS-R 1/2 page as follows:
 EFIS BITE TEST
 DISCRETE STATUS-R  1/2
 ADC SEL RIGHT AIR/GROUND GROUND ANCDU SEL *[1] ----COMPARATOR ENABLED *[2] DME SEL RIGHT FLT PATH MGMT ENABLED FMC SEL LEFT *[3]
 <INDEX

 *[1] AIRPLANES WITH -420 EFIS SGs AND SUBSEQUENT, The ANCDU SEL line will not show unless an ANCDU is installed.
 *[2] DISABLED for BEJ 101-112
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 34-22-00
 ú ú 43A Page 523 ú Nov 15/98

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 *[3] AIRPLANES WITH A DUAL FMC SYSTEM; the FMC SEL line will show RIGHT.
 (c)  Push the NEXT PAGE key on the CDU.
 1)  Make sure the CDU display shows the DISCRETE STATUS-R 2/2 page as follows:
 EFIS BITE TEST
 DISCRETE STATUS-R  2/2
 ILS SEL RIGHT IRU SEL RIGHT MAG/TRUE MAG MLS SEL ----SWC SEL RIGHT VOR SEL RIGHT
 <INDEX

 (d)  Push the LSK 6L (<INDEX) two times. 1) Make sure the CDU display shows the EFIS BITE TEST page.
 S 745-077
 (3) Push the INIT/REF key on the FMCS CDU to get out of the EFIS BITE.
 G.  IRS Transfer Switch and MCP Course Select Tests
 S 865-078
 (1)  
Make sure the attitude ball indicates within one degree of airplane pitch attitude and one degree of airplane roll attitude on the two EADIs.
　
中國航空網 m.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 導航 NAVIGATION 1(134)