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F/CTL ALTN LAW
(PROT LOST)
L2 The flight control normal laws and associated protections are lost. Only load factor limitation is
furnished (alternate law without protection).
L1MAX SPEED..........................................................................................................................320/0.77
L2 Speed is limited due to loss of high speed protection.
L1 SPD BRK.......................................................................................................................DO NOT USE
�� If blue sys recovered:
L2 Refer to 99 Duref Cible FCOM
L1�� If blue sys not recovered:
L2 (Refer to PRO-ABN-10 Landing with Slats or Flaps Jammed).
L1
SECONDARY FAILURES
*WHEEL
*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 75/156
FCOM 19 AUG 10
HYD G+B SYS LO PR (Cont'd)
L12
STATUS
MIN RAT SPD (IF RAT OUT)...................................140 KT
(If B PUMP LO PR)
MAX SPEED.......................................................... 320/0.77
MANEUVER WITH CARE
SPD BRK.......................................................DO NOT USE
APPR PROC
DUAL HYD LO PR
(Line not displayed for a double LO LVL):
�� If sys lost by RSVR LO AIR PR:
RELATED PUMPS............................................................. ON
�� If sys lost by RSVR OVHT:
�� IF BLUE OVHT OUT:
BLUE ELEC PUMP................................................. AUTO
�� IF GREEN OVHT OUT:
GREEN ENG 1 PUMP.................................................ON
�� IF HYD NOT RECOVERED (line not displayed for a
double LO LVL):
A/THR................................................................................OFF
Select the target speed on the FCU. Due to the loss of
slats and some flight control surfaces, the A/THR may not
satisfactorily maintain speed.
FOR LDG............................................................ USE FLAP 3
GPWS LDG FLAP 3...........................................................ON
�� WHEN SPD 200 KT (displayed when slats are
retracted):
L/G..............................................................GRVTY EXTN
Refer to PRO-ABN-32 L/G GRAVITY EXTENSION
Extend the landing gear at 200 kt to revert sooner in
direct law. This provides, below 200 kt , a better pitch
INOP SYS
G+B HYD
F/CTL PROT
L ELEV
L+R AIL
SPLR 1+3+5
SLATS
AP 1+2
N/W STRG
AUTO BRK
NORM BRK
L/G RETRACT
REVERSER 1
EMER GEN (If B RSVR LO LVL)
B ELEC PUMP
YAW DAMPER 1
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 76/156
FCOM 19 AUG 10
HYD G+B SYS LO PR (Cont'd)
control than in alternate law with one elevator lost and all
slats lost.
APPR SPD...............................................................VREF +25 KT
Approach speed must be increased, due to the loss of ailerons
and slats.
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
ALTN LAW: PROT LOST
WHEN L/G DN: DIRECT LAW
See (1)
FLAPS SLOW
(1) AL2t landing gear extension, control reverts to direct law in pitch, as well as in roll. (Refer to
00011770 **Not found**)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
HYDRAULIC
A318/A319/A320/A321 FLEET PRO-ABN-29 P 77/156
FCOM 19 AUG 10
HYD G+B SYS LO PR
Applicable to:
,
L2Note: If green system has been lost because of fluid low level or overheat, “HYD PTU FAULT”
should appear demanding that the flight crew switches the PTU OFF.
L1 LAND ASAP
�� If blue sys lost by ELEC PUMP LO PR:
RAT................................................................................................................................MAN ON
MIN RAT SPD....................................................................................................................140 KT
AFFECTED PUMPS......................................................................................................................OFF
MANEUVER WITH CARE
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
L2 The flight control normal laws and associated protections are lost. Only load factor limitation is
furnished (alternate law without protection).
　
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