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categories:
* FAULTS
* KEY TEST
* COLOR TEST
* DISPLAY TEST
* CONFIG
* SOFTWARE OPTIONS
* POWER SUPPLY (P/S)
* TEMPERATURE
* LIGHT
* LAMP TEST
* CALIBRATION.
NOTE: Power supply, temperature, light, lamp test, and
calibration are used primarily for bench test of the
CDU.
The EXIT prompt (LSK 6L) selects the FMCS BITE INDEX page.
FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - LCD CDU
EFFECTIVITY
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FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - LCD CDU
FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - LCD CDU
EFFECTIVITY
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GENERAL
A second FMCS BITE maintenance page is for selection of the
hardware configuration (H/W CONFIG) page.
The H/W CONFIG page shows this data for the FMC:
* Hardware part number
* Serial number
* Elapsed Time Indiacator (ETI)
* Processor speed.
The INDEX prompt (LSK 6L) selects the FMCS BITE page 2/2.
FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - H/W CONFIG
EFFECTIVITY
SHZ 001-003 (POST SB 737-34-1650 AND PRE SB 737-34A1801) OR PRE SB
737-34-1918; SHZ 009-999 PRE SB 737-34-1918 OR (POST SB 737-34-1650
AND PRE SB 737-34A1801)
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FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - H/W CONFIG
FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - H/W CONFIG
EFFECTIVITY
SHZ 001-003 (POST SB 737-34-1650 AND PRE SB 737-34A1801) OR PRE SB
737-34-1918; SHZ 009-999 PRE SB 737-34-1918 OR (POST SB 737-34-1650
AND PRE SB 737-34A1801)
34-61-00
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THIS PAGE IS INTENTIONALLY LEFT BLANK
FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - H/W CONFIG
34-61-00
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
General
To see the CDU faults page, first select FAULTS on line select
key (LSK) 1L from the CDU MAINT BITE INDEX page. This
selects the CDU BITE DISPLY INDEX page.
CDU BITE DISPLAY INDEX Page
This page shows the fault history for the last ten full power-up
cycles. When no faults are recorded during a cycle, the data
field is blank.
To see the fault data for a specific cycle, select that line select
key. This selects the CDU BITE DISPLAY page for that power up
cycle.
Line select key 6L shows the INDEX prompt. This selects the
CDU MAINT BITE INDEX page.
CDU BITE DISPLAY Page
This page shows the fault data for a specific cycle. Up to a
maximum of five faults are recorded per cycle. The header
shows the cycle number.
This data shows for each fault:
* Failed unit
* Failure description
* Fault state
* Failure frequency
* Failure time
* Extended fault code.
The failed unit can show FMC, CDU, or USER 1-5 where USER is
an airplane sub-system.
These are the failure descriptions that can show:
* PROCESSOR
* WATCHDOG TIMER
* 429 FAULT
* ANNUN FAULT
* LCD
* KEYBOARD
* MEMORY
* R/C TIMER (resistor/capacitor)
* POWER SUPPLY
* LIGHT SENSOR
* ADC (analog to digital converter)
* TEMP SENSOR
* FMC FAULT
* SUB-SYSTEM FAULT
* EDC (error detection and correction logic)
* SOFTWARE FAULT
* FONTROM (read only memory).
The fault state shows if the fault is steady (S) or intermittent (I).
All faults are initially recorded as a steady fault. If the fault later
goes away, the indication changes to intermittent.
FMCS - TRAINING INFORMATION POINT - CDU BITE PAGES - FAULTS
EFFECTIVITY
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The failure frequency shows the number of times the fault
　
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