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ENG BLEED
FAULT lt
3, 4, 5, 7, 8
BLEED 1 (2) OFF
one engine bleed switched off with no fault
ENG BLEED
OFF lt
1, 3, 4, 5,
7, 8, 9, 10
APU BLEED FAULT
APU available and APU bleed valve position
disagrees with selected position.
NIL
APU BLEED LEAK
temperature > 124 °C detected by the loop
APU BLEED
FAULT lt
3, 4, 5, 7, 8
ENG 1 (2) BLEED ABNORM PR
regulated pressure is abnormal
SINGLE
CHIME
MASTER
CAUT BLEED
NIL 1, 3, 4, 5,
7, 8, 10
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
PNEUMATIC
WARNINGS AND CAUTIONS
A318/A319/A320/A321 FLEET DSC-36-30 P 2/4
FCOM 19 AUG 10
Continued from previous page
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT
PHASE
INHIB
ENG 1 (2) (1+2) BLEED LO TEMP
one (both) engine bleed below 150 °C in flight with
wing anti ice ON
3, 4, 5, 8
X BLEED FAULT
position disagree with selected position
SINGLE
CHIME
MASTER
CAUT
ENG 1 (2) HP VALVE FAULT
HP valve is abnormally closed
BLEED MONITORING FAULT
Both BMC faulty
L(R) WING LEAK DET FAULT
Both detection loops inop in one wing
NIL NIL
BLEED NIL
3, 4, 5, 7, 8
MEMO DISPLAY
APU BLEED appears in green if the APU is available and the APU BLEED pushbutton switch is
ON.
WARNINGS AND CAUTIONS
Applicable to:
,
,
MSN,
4719,,,
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
PNEUMATIC
WARNINGS AND CAUTIONS
A318/A319/A320/A321 FLEET DSC-36-30 P 3/4
FCOM 19 AUG 10
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT
PHASE
INHIB
ENG 1 (2) BLEED FAULT
engine 1 (2) running and bleed air pressure >
57 PSI (+ 3/- 0) or temperature :
> 257 °C for more than 55 s
or > 270 °C for more than 15 s
or > 290 °C for more than 5 s
1, 3, 4, 5,
7, 8, 10
L (R) WING LEAK
temperature > 124 °C detected by the loops
ENG 1 (2) BLEED LEAK
temperature > 204 °C detected by the loop and
engine 1 (2) running
ENG 1 (2) BLEED NOT CLSD
1. bleed valve not automatically closed during
engine start or with APU bleed selected or
2. bleed valve not closed with no pressure
upstream
ENG BLEED
FAULT lt
3, 4, 5, 7, 8
BLEED 1 (2) OFF
one engine bleed switched off with no fault
ENG BLEED
OFF lt
1, 3, 4, 5,
7, 8, 9, 10
APU BLEED FAULT
APU available and APU bleed valve position
disagrees with selected position.
NIL
APU BLEED LEAK
temperature > 124 °C detected by the loop
APU BLEED
FAULT lt
3, 4, 5, 7, 8
ENG 1 (2) BLEED ABNORM PR
regulated pressure is abnormal
SINGLE
CHIME
MASTER
CAUT BLEED
NIL 1, 3, 4, 5,
7, 8, 10
ENG 1 (2) (1+2) BLEED LO TEMP
one (both) engine bleed below 150 °C in flight with
wing anti ice ON
3, 4, 5, 8
X BLEED FAULT
position disagree with selected position
SINGLE
CHIME
MASTER
CAUT
ENG 1 (2) HP VALVE FAULT
HP valve is abnormally closed
BLEED MONITORING FAULT
Both BMC faulty
L(R) WING LEAK DET FAULT
Both detection loops inop in one wing
BLEED
3, 4, 5, 7, 8
BLEED MONIT SYS 1(2) FAULT
One BMC faulty
ENG 1(2) LEAK DET FAULT
Detection loop inop in pylon
NIL NIL
NIL
NIL
3, 4, 5,
6, 7, 8
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
PNEUMATIC
WARNINGS AND CAUTIONS
A318/A319/A320/A321 FLEET DSC-36-30 P 4/4
FCOM 19 AUG 10
MEMO DISPLAY
APU BLEED appears in green if the APU is available and the APU BLEED pushbutton switch is
ON.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
PNEUMATIC
ELECTRICAL SUPPLY
A318/A319/A320/A321 FLEET DSC-36-40 P 1/2
FCOM 19 AUG 10
BUS EQUIPMENT LIST
Applicable to: ALL
NORM EMER ELEC
AC DC AC
ESS
DC
ESS HOT
BMC 12 DC2 SHED
BLEED VALVES, ENG 1 SHED
HP VALVES AND
FAN AIR VALVES ENG 2 DC2
X-BLEED VALVE MAANUUTAOL CCOONNTTRROOLL DC2 SHED
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
　
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