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LOCAL
WARNING
FLT PHASE
INHIB
CONFIG PARK BRK ON
parking brake is on when thrust levers are set
at TO or FLX TO power position
CRC MASTER
WARN 1, 2, 5 to 10
PARK BRK ON
Parking brake is ON during flight.
NIL NIL
1 to 5,
8 to 10
BRAKES HOT
one brake temperature higher than 300 °C
HOT lt
on BRK
FAN pb sw
4, 8 to 10
AUTO BRK FAULT
failure of autobrake when armed 3 to 5
A/SKID NWS FAULT
• loss of normal brake system associated with
Y HYD sys lo press or
• failure of both BSCU channels
4, 5
ANTI SKID/NWS OFF
switch at OFF position
WHEEL
4, 5
HYD SEL FAULT
failure of brake normal selector valve or NWS
selector valve in open position
SINGLE
CHIME
MASTER
CAUT
SYS 1 (2) FAULT
failure of one BSCU channel NIL NIL
NIL
NIL
3 to 5, 7, 8
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
BRAKES AND ANTISKID - WARNINGS AND CAUTIONS
A318/A319/A320/A321 FLEET DSC-32-30-30 P 4/4
FCOM 19 AUG 10
Continued from previous page
E/WD : FAILURE TITLE
condition
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT PHASE
INHIB
RELEASED
Brake of one wheel is released. It is detected
when the landing gear is downlocked and,
at least one engine is running, and normal
braking is active.
4, 5
NORM BRK FAULT
Normal braking function is lost.
SINGLE
CHIME
MASTER
CAUT
3 to 5
ALTN BRK FAULT
Alternate braking function is lost. NIL NIL
WHEEL
3, 4, 5, 7, 8
ALTN L(R) RELEASED
Brakes of one gear is released. It is triggered
when the landing gear is downlocked, and
at least one engine is running, and alternate
braking is active.
NIL 3, 4, 5
NORM + ALTN FAULT
Normal and alternate functions are lost.
Parking brake available.
4, 5
BRK Y ACCU LO PR
The yellow accumulator is in low pressure.
SINGLE
CHIME
MASTER
CAUT
WHEEL
3, 4, 5, 7, 8
BRAKES-N/WS MINOR FAULT
Single system failure, loss of redundancy NIL NIL NIL 2 to 9
MEMO DISPLAY
If the parking brake is ON, the “PARK BRK” memo appears in green, ‐ during flight phases 1, 2,
9, and 10.
‐ If the autobrake is armed, AUTO BRK LO, AUTO BRK MED, or AUTO BRK MAX appears.
‐ If the autobrake is faulty," AUTO BRK OFF" appears.
‐ "BRK FAN" appears in green, if the BRK FAN pushbutton �� is ON .
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
BRAKES AND ANTISKID - ELECTRICAL SUPPLY
A318/A319/A320/A321 FLEET DSC-32-30-40 P 1/2
FCOM 19 AUG 10
BUS EQUIPMENT LIST
Applicable to:
NORM EMER ELEC
AC DC AC
ESS
DC
ESS HOT
BSCU CH 1 AC1 DC1
BSCU CH 2 AC2 DC2
PARK BRK CTL DC2 GRND/ FLT HOT1
PRESS INDICATOR X
BRK FAN CTL �� DC2
COOLING FANS ��
(Wheels 1, 2, 3, 4) AC2 DC2
BRAKES
COOLING FANS ��
(bogie : Wheels 5, 6, 7,
8)
AC1 DC1
BUS EQUIPMENT LIST
Applicable to:
,
,
MSN,,
4538,,
NORM EMER ELEC
AC DC AC
ESS
DC
ESS HOT
BSCU CH 1 AC1 DC1
BSCU CH 2 AC2 DC2
ABCU X X
PARK BRK CTL GRND/ FLT HOT1
PRESS INDICATOR X
BRK FAN CTL �� DC2
COOLING FANS ��
(Wheels 1, 2, 3, 4) AC2 DC2
BRAKES
COOLING FANS ��
(bogie : Wheels 5, 6, 7,
8)
AC1 DC1
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
BRAKES AND ANTISKID - ELECTRICAL SUPPLY
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-32-30-40 P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
TIRE PRESSURE INDICATING SYSTEM - DESCRIPTION
A318/A319/A320/A321 FLEET DSC-32-40-10 P 1/2
FCOM 19 AUG 10
DESCRIPTION
Applicable to:
, ,
MSN
The tire pressure indicating system includes :
a sensor that measures ‐ the pressure of each tire,
‐ a transmission unit that transmits the electrical pressure signal from the sensor to the computer,
‐ a tire pressure indicating unit computer that sends information to the ECAM for cautions and the
system page display.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
TIRE PRESSURE INDICATING SYSTEM - DESCRIPTION
　
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