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Landing gear is extended by gravity to preserve green
system integrity Refer to PRO-ABN-32 L/G GRAVITY
EXTENSION.
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
INOP SYS
B+Y HYD
R ELEV
SPLR 2+3+4
SPD BRK
AP 1+2
N/W STRG
ALTN BRK
CARGO DOOR (If Y RSVR LO
LVL)
REVERSER 2
B ELEC PUMP
EMER GEN (If B RSVR LO LVL)
YAW DAMPER 2
CAT 2
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
HYDRAULIC
A318/A319/A320/A321 FLEET PRO-ABN-29 P 132/156
FCOM 19 AUG 10
HYD B+Y SYS LO PR (Cont'd)
SLATS/FLAPS SLOW
See (1)
(1)
L12
Note: Following a yellow hydraulic system failure, the parking brake may be inoperative due to
yellow accumulator low pressure.
HYD B+Y SYS LO PR
Applicable to: ,
MSN,,,,
L2Note: If the yellow system has been lost by low level or overheat, “HYD PTU FAULT” should
appear to demand the PTU pb-sw at OFF.
L1 LAND ASAP
�� If yellow sys lost by ENG 2 PUMP LO PR:
YELLOW ELEC PUMP.............................................................................................................ON
�� If blue sys lost by ELEC PUMP LO PR:
RAT................................................................................................................................MAN ON
MIN RAT SPD....................................................................................................................140 KT
AFFECTED PUMPS......................................................................................................................OFF
MAX SPEED..........................................................................................................................320/0.77
L2Note: Flight controls remain in normal law.
L1MANEUVER WITH CARE
�� If blue or yellow sys recovered:
L2 See procedure for single failure.
L1�� If neither system recovered:
SECONDARY FAILURES
*F/CTL
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
HYDRAULIC
A318/A319/A320/A321 FLEET PRO-ABN-29 P 133/156
FCOM 19 AUG 10
HYD B+Y SYS LO PR (Cont'd)
L12
STATUS
MIN RAT SPD..........................................................140 KT
(If B PUMP LO PR)
MAX SPEED.......................................................... 320/0.77
MANEUVER WITH CARE
APPR PROC
DUAL HYD LO PR
(Line not displayed for dual LO LVL).
�� If sys lost by RSVR LO AIR PR:
In approach, system lost by RSVR LO AIR PR may be
recovered at low altitude.
RELATED PUMP................................................................ON
�� If sys lost by RSVR OVHT:
In approach, system lost by RSVR OVHT may be recovered
if OVHT indication disappears.
�� IF BLUE OVHT OUT:
BLUE ELEC PUMP................................................. AUTO
�� IF YELLOW OVHT OUT:
YELLOW ENG 2 PUMP...............................................ON
�� IF HYD NOT RECOVERED (line not displayed for dual LO
LVL):
L/G.................................................................... GRVTY EXTN
Landing gear is extended by gravity to preserve green
system integrity Refer to PRO-ABN-32 L/G GRAVITY
EXTENSION.
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
INOP SYS
B+Y HYD
R ELEV
SPLR 2+3+4
SPD BRK
AP 1+2
N/W STRG
ALTN BRK
CARGO DOOR (If Y RSVR LO
LVL)
REVERSER 2
B ELEC PUMP
EMER GEN (If B RSVR LO LVL)
YAW DAMPER 2
CAT 2
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
HYDRAULIC
A318/A319/A320/A321 FLEET PRO-ABN-29 P 134/156
FCOM 19 AUG 10
HYD B+Y SYS LO PR (Cont'd)
SLATS/FLAPS SLOW
See (1)
(1)
L12
Note: Following a yellow hydraulic system failure, the parking brake may be inoperative due to
yellow accumulator low pressure.
HYD Y ELEC PUMP LO PR OR OVHT
Applicable to:
L2 If the ELEC PUMP overheats, or if the Y ELEC PUMP fails, while the Y ENG PUMP and the PTU
are inoperative:
L1 YELLOW ELEC PUMP................................................................................................................. OFF
ASSOCIATED PROCEDURES
　
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