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时间:2011-09-19 15:54来源:蓝天飞行翻译 作者:航空
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The following table shows how the position of the LRU equals the status of the discrete inputs: (VHF COMM IS THE EXAMPLE USED IN THE TABLE BELOW)
TRANSCEIVER POSITION  SDI 1, PIN A9  SDI 0, PIN B9 
1 or 2 or 3  OPEN  OPEN 
1  OPEN  COMM 
2  COMM  OPEN 
3  COMM  COMM 


Central Maintenance Computer Status (NOT INSTALLED)
This page shows the status of the central maintenance computer (CMC) input to the VHF transceiver. The VHF transceivers receive no input from a central maintenance computer; so the status is INACTIVE.
Failures Recorded for Previous Flight Legs
If the LRU has failure data stored for previous flight legs, the LRU shows the FAILURES HAVE BEEN RECORDED page. From this page, you can select YES to see the failure data. Or, you can select MORE to see the other status pages. Sixty five flight legs are recorded. There is no timeout in this mode when the aircraft is on the ground.
If the LRU does not have any failure data stored for previous flights, the LRU does not show this page.
Flight Faults Legs Page One
-"DATE" (not active)
-"DEPT" departure city (not active)
-"DEST" destination city (not active)
-"F#" flight number (not active)
-"A/C" aircraft tail number (not active) Dashes are displayed for all these non-active fields
Flight Faults Legs Page Two Thru Four
-"FC" is fault code
-"UTC" is the time the fault occured (not active)
-"R" is repetition or number of occurances in the flight leg
-"P" is flight phase (not active)
-"O" is origin of the fault, (External of the LRU = E. Internal to the
LRU = I) Zeros across a row is an indication that no faults occurred.
January 2005
23-12

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SOUTHWEST AIRLINES PROPRIETARY(c) All rights reserved
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL

A23-12-00-021.fm

P#M P -1C EYD A T A : O PEN P#M P -7D ATAVC E / : O PEN P#M P -7C RE T U R N M O R DIS C RE T E S 1 TTP U SH : O PE N E K D 


P#M P -14 DSSQ LC : O PEN P#M P -13 OFFFR EQ : O PEN P#M P -8C RE T U R N M O R DIS C RE T E S 2 RNAI R / : O P E N E G D B C H 

P# M P -2A STFC T : OPE N P# M P -4A EN B DLDR : O P E N P# M P -8B RE T U R N MOR DI S C RE T E S 3 OFT X C : O PEN E T F TE 

INACM C1 : CT I V E 6A / -P# M P 6 B INACM C2 : CT I V E 6C / -P# M P 6 D RE T U R N M O R C MC # 1 SE L EC T E D E 

 

FLIGHT  LEG: 01 
FC UTC  RPO 
EH _ _ _ _  4_E 
00 0000  000 
000000  000 
000000  000 
000000  000 
RETURN  MORE 


January 2005
23-12
SOUTHWEST AIRLINES PROPRIETARY(c) All rights reserved

A23-12-00-018a.fm
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL

VOR/MB/MMR/DME/RA/VHF COMM - FAULT CODE TABLES
Fault Code Tables
The fault codes on the following tables provide a description for external faults for the VOR/MB, MMR, DME, RA, and VHF COMM. The external fault codes can be accessed via the LRU BITE.
After the initial BITE is complete and external faults are noted. Press the MAINT key to view fault codes.
The fault codes are also displayed on the Flight Leg Recorded Fault Screen under FC. See prior pages for BITE menu navigation.
NOTE:  LCD fault codes listed in the following tables are for external LRU faults. Internal faults to the LRU’s are not listed.
January 2005
23-12

- 272 -
SOUTHWEST AIRLINES PROPRIETARY(c) All rights reserved
SOUTHWEST AIRLINES.
737-700 MAINTENANCE TRAINING MANUAL

VOR/MB/MMR/DME/RA/VHF COMM - FAULT CODE TABLES VOR/MARKER BEACON RECEIVER RVA-36B
 
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