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L2 Attitude information is lost on one side (Captain or first officer).
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST
L2 Flight control normal laws are lost .Pitch alternate law with static stability becomes active.
All protections, except maneuver protections, are lost.
L1MAX SPEED...................................................................................................................... 320 KT
L2 Speed is limited, due to the loss of high speed protection.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A318/A319/A320/A321 FLEET PRO-ABN-34 P 70/164
FCOM 19 AUG 10
NAV IR 1+2(1+3)(2+3) FAULT (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320 KT
APPR PROC
FOR LDG...................................................................USE FLAP 3
Do not select CONF FULL, so as not to degrade handling
qualities.
GPWS LDG FLAP 3................................................................. ON
Will appear, when CONF 3 is selected.
APPR SPD : VREF + 10 KT
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
At landing gear extension, control reverts to direct law, in pitch,
as well as in roll (Refer to STLO-ABN-27-J F/CTL DIRECT LAW).
IR (AFFECTED) MAY BE AVAIL IN ATT
Refer to PRO-ABN-34 IR ALIGNMENT IN ATT MODE
INOP SYS
F/CTL PROT
IR 1 (2)(3)
IR 1+2 or 1 + 3 or 2+3
AP 1+2
A/THR
YAW DAMPER 1 (1)
YAW DAMPER 2 (2)
GPWS TERR (if IR 1 fault)
TCAS
See (3)
CAT 2
Note: In case of an
IR 1 fault, the
TCAS may be
inoperative
(depending
on the TCAS
manufacturer).
If the IR 1 is
available in ATT
mode, the TCAS
can be recovered
by entering the
aircraft magnetic
heading into the
CDU, as per IR
ALIGNMENT
IN ATT MODE
procedure.
(1) (in case of an IR 1 + 3 fault)
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A318/A319/A320/A321 FLEET PRO-ABN-34 P 71/164
FCOM 19 AUG 10
NAV IR 1+2(1+3)(2+3) FAULT (Cont'd)
(2) (in case of an IR 2 + 3 fault)
(3) In case of an IR 1 fault, the TCAS may be inoperative (depending on the TCAS manufacturer). If
the IR 1 is available in ATT mode, the TCAS can be recovered by entering the aircraft magnetic
heading into the CDU, as per IR ALIGNMENT IN ATT MODE procedure.
NAV IR 1+2(1+3)(2+3) FAULT
Applicable to:
�� If IR 1 + 2 FAULT :
ATT HDG SWTG.............................................................................................................. CAPT 3
L2 Set IR 3 (If available) to the Captain's side.
Attitude information is lost on first officer's PFD.
L1�� If IR 1 + 3 (or 2 + 3) FAULT :
ATT HDG SWTG................................................................................................................ NORM
L2 Attitude information is lost on one side (Captain or first officer).
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST
L2 Flight control normal laws are lost .Pitch alternate law with static stability becomes active.
All protections, except maneuver protections, are lost.
L1MAX SPEED...................................................................................................................... 320 KT
L2 Speed is limited, due to the loss of high speed protection.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
NAVIGATION
A318/A319/A320/A321 FLEET PRO-ABN-34 P 72/164
FCOM 19 AUG 10
NAV IR 1+2(1+3)(2+3) FAULT (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320 KT
APPR PROC
FOR LDG...................................................................USE FLAP 3
Do not select CONF FULL, so as not to degrade handling
qualities.
GPWS LDG FLAP 3................................................................. ON
Will appear, when CONF 3 is selected.
APPR SPD : VREF + 10 KT
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
At landing gear extension, control reverts to direct law, in pitch,
　
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