FWS
1. ALL WARN PRODUCED IN FWC EXCEPT EGPWS WARN
2. ALL CRT CAN I/W EACH OTHER
3. SDAC(SYS DATA ANALOGE CONVERTOR) PRODUCES THE SYS PAGES
4. FWC#1 POWERED FROM (401XP) EMR AND NORM AC BUS, FWC#2 JUST FROM NORM BUS
5. WARN LEVELS:
3: EMR RED +CRC
2: ABNORMAL AMBER +SC
1: NO CHIME
0: INFORMS THE SITUATION
6. LEVEL 3 GENEREATED IN BOTH FWC BUT OTHER WARN DIVIDED TO HALF FOR EACH ECAM:
L/H: WARN AND STATUS AND MEMO
R/H: IS SYS PAGES
7. CLR P/B WILL BE ON WHEN WARN PAGE OR STATUS PAGE DISPLAYED
8. SYS PAGE ARE 14 BUT 12 CAN BE SEL+ CRUISE PAGE AND ENG START PAGE AUTO
10. AUTO CALL OUT PRODUCED IN FWC FROM 400FT TO 3FT
11. LAND CONFIG FAIL AND FIRE NOT INHIBITED IN ANY PHASE OF FLT
12. FWC PRODUCES 12 FLT PHASE TO INHIBT MANY WARN
13. CHIMES IN FWC:
SC (SINGLE CHIME): AMBER
CRC (CONTINUOUS REPEATITIVE CHIME): RED
CLICK: LAND CAPIBILITY CHANG
CAVALRY CHARGE: A/P DISCONNECT
C CHORD: ALT ALERT
BUZZER: SELCAL AND CABIN
KETTLE: DECISION HEIGHT
CRICKET: STALL WARN
14. SDAC PRODUCES ALL AMBER AND WHITE AND MEMO
15. IF SDAC FAIL ECAM SHOWS ONLY FUEL QTY (NO MEMO)
16. ONE FWC FAIL: HALF OF AMBER LIT LOST
17. FWC CIRCUIT:
ACQUIRE: ACQ#1 SENDS TO PROC#2, IF ACQ FAIL HALF AMBER FAULT LOST
PROCESS: IF FAIL OTHER ONE DONE, FWC FAULT ON MTP
18. BOTH FWC FAIL: CRUISE PAGE DISPLAYED(ENG PARAMETER AND AIR COND IF ENG P/B PRESS)
19. ONE CRT FAIL SHOWS BLACK WITH WHITE LINE IT MUST BE OFF (SGU CAN SHOW ALL SYS PAGE AND WARN IN ONE CRT
20.SGU (SYMBOL GEN UNIT) INPUTS: FWS, SDAC, FQIC, ADC
21. RCL P/B MUST HELD FOR 3SEC TO RECALL FAULTS
22. EMR CANCEL P/B CAN CANCEL THE EGPWS AUDIO
23. ECAM TEST POSSIBLE IN GND ONLY
24. IN NORMAL CONFIG L/H DU FEED BY SGU#1 AND FWC’S AND R/H DU BY SGU#2 AND SDAC
25. CB MONITOR NOT AVAIL WHEN ENG RUN (OIL PRESS SW GIVE THIS SIG)
26. CRUISE AVAIL IF BOTH DU HEALTHY
27. AMBER LIT CLEARED DON’T COMING BACK BUT RED’S DO IF FAULT STILL EXIST
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