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Approach speed must be increased, due to the loss of flaps.
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
ALTN LAW: PROT LOST
INOP SYS
G+Y HYD
F/CTL PROT
STABILIZER
REVERSER 1+2
SPLR 1+2+4+5
FLAPS
YAW DAMPER
AP 1+2
ANTI SKID
N.W. STEER
NORM BRK
AUTO BRK
L/G RETRACT
CARGO DOOR (If Y RSVR LO
LVL)
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 115/156
FCOM 19 AUG 10
HYD G+Y SYS LO PR (Cont'd)
WHEN L/G DN: DIRECT LAW
See (1)
BRK Y ACCU PR ONLY
See (2)
SLATS SLOW
See (3)
(1) AL2t landing gear extension, control reverts to direct law in pitch, as well as in roll. (Refer to
00011770 **Not found**).
(2) 7 full brake applications are available.
(3) Note: Following a yellow hydraulic system failure, the parking brake may be inoperative due to
yellow accumulator low pressure.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
HYDRAULIC
A318/A319/A320/A321 FLEET PRO-ABN-29 P 116/156
FCOM 19 AUG 10
HYD G+Y SYS LO PR
Applicable to: MSN
LAND ASAP
PTU..............................................................................................................................................OFF
AFFECTED PUMPS......................................................................................................................OFF
�� If yellow sys lost by ENG 2 PUMP LO PR:
YELLOW ELEC PUMP.............................................................................................................ON
MANEUVER WITH CARE
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
L2 Flight control normal laws and associated protections are lost. Only load factor limitation, high and
low speed stability are provided (alternate law with reduced protection).
L1MAX SPEED..........................................................................................................................320/0.77
L2 Speed is limited due to loss of high speed protection.
L1�� If yellow sys recovered:
L2 Refer to 99 Duref Cible FCOM
L1�� If yellow sys not recovered:
L2 Refer to PRO-ABN-10 Landing with Slats or Flaps Jammed.
L1
SECONDARY FAILURES
*F/CTL
*WHEEL
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
HYDRAULIC
A318/A319/A320/A321 FLEET PRO-ABN-29 P 117/156
FCOM 19 AUG 10
HYD B+Y SYS LO PR
Applicable to:
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 118/156
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
　
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