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‐ In amber and an associated ECAM caution comes on in case of autobrake
system failure, or failure of both BSCU channels.
MAX, MED or LO indicates the selected rate (green). It is not displayed when the autobrake is
faulty.
(4) Wheel number identification
It is in white.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
BRAKES AND ANTISKID - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-32-30-20 P 5/8
FCOM 19 AUG 10
(5) III indications
It appears in green when :
In flight, the landing gear ‐ is extended, and the antiskid is valid, or
‐ On ground, when antiskid is activated and the brakes are released.
It is amber in case of :
‐ Residual pressure, or
‐ Brake release fault
The R (Release) indication is always in white.
(6) Brake temperature indications
‐ It is normally green (minimum indication 0 °C).
‐ The green arc appears on the hottest wheel, when one brake temperature exceeds 100 °C.
‐ The amber light, and associated ECAM caution, come on when the corresponding brake
temperature exceeds 300 °C.
In addition, on the hottest wheel, the arc becomes amber.
Note: Below 100 °C, the indicated brake temperature may be below the actual brake
temperature. This difference can reach 25 °C with an actual brake temperature of
30 °C, and it decreases when the temperature increases.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
BRAKES AND ANTISKID - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-32-30-20 P 6/8
FCOM 19 AUG 10
ECAM WHEEL PAGE
Applicable to: ,
(1) NORM BRK indication
Appears in amber in case of :
‐ normal braking is failed
‐ A/SKID & N/W STRG switch is at OFF (associated with ECAM caution)
‐ both BSCU channels are failed (associated with ECAM caution).
(2) ANTISKID indication
Appears amber associated with an ECAM caution in case of total BSCU failure or when the
A/SKID and N/W STRG switch is OFF or in case of anti-skid failure detected by the BSCU or in
flight with at least one engine running when green and blue systems are failed.
(3) AUTO BRK indication
Displayed : ‐ In green when the autobrake is armed ;
‐ In amber and an associated ECAM caution comes on in case of autobrake
system failure, or failure of both BSCU channels.
MAX, MED or LO indicates the selected rate (green). Not displayed when autobrake is faulty.
(4) Wheel number identification
It is in white.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
BRAKES AND ANTISKID - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-32-30-20 P 7/8
FCOM 19 AUG 10
(5) III indications
It appears in green when :
In flight, the landing gear ‐ is extended, and the antiskid is valid, or
‐ On ground, when antiskid is activated and the brakes are released.
It is amber in case of :
‐ Residual pressure, or
‐ Brake release fault
The R (Release) indication is always in white.
(6) Brake temperature indications
‐ It is normally green (minimum indication 0 °C).
‐ The green arc appears on the hottest wheel, when one brake temperature exceeds 100 °C.
‐ The amber light, and associated ECAM caution, come on when the corresponding brake
temperature exceeds 300 °C.
In addition, on the hottest wheel, the arc becomes amber.
Note: Below 100 °C, the indicated brake temperature may be below the actual brake
temperature. This difference can reach 25 °C with an actual brake temperature of
30 °C, and it decreases when the temperature increases.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
BRAKES AND ANTISKID - CONTROLS AND INDICATORS
Intentionally left blank
A330/A340 FLEET DSC-32-30-20 P 8/8
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
LANDING GEAR
BRAKES AND ANTISKID - WARNINGS AND CAUTIONS
A330/A340 FLEET DSC-32-30-30 P 1/4
FCOM 19 AUG 10
WARNINGS AND CAUTIONS
Applicable to:
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT
PHASE
INHIB
CONFIG PARK BRK ON
Parking brake is ON, when thrust levers are set to the
T.O or FLX T.O power position.
CRC MASTER
WARN
1, 2, 5
to 10
PARK BRK LO PR
NIL NIL
3 to 8
BRAKES HOT
The temperature of one brake is higher than 300 °C.
BRK FAN
HOT lt
4, 8,
9, 10
AUTO BRK FAULT
A tachometer is failed, or a servovalve is jammed
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 3(103)