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L2 This will also switch off the associated ADR.
L1 ELAC 2..................................................................................................................OFF THEN ON
ELAC 1..................................................................................................................OFF THEN ON
L2Note: When the ELAC 1 computer is reset on ground, the pitch trim returns to the ground
setting position (0 °).
After corrective action (faulty IR switched off and ELACs reset), pitch alternate law
with reduced protections is recovered.
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
MAX SPEED...................................................................................................................... 320 KT
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 83/164
FCOM 19 AUG 10
NAV IR DISAGREE (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 be displayed, when CONF 3 is selected.
APPR SPD................................................................... VREF + 10
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)
INOP SYS
F/CTL PROT
(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
NAVIGATION
A318/A319/A320/A321 FLEET PRO-ABN-34 P 84/164
FCOM 19 AUG 10
NAV IR DISAGREE
Applicable to:
L2 Disagreement between two IRs, the third one having failed or been rejected by the ELACs. Pitch
direct, roll direct, and yaw mechanical laws become active. All protections (pitch and roll) are lost.
L1 ATT.....................................................................................................................................X CHECK
L2 Use the standby horizon to determine the faulty IR.
L1�� IF DISAGREE CONFIRMED:
FAULTY IR.............................................................................................................................OFF
L2 This will also switch off the associated ADR.
L1 ELAC 2..................................................................................................................OFF THEN ON
ELAC 1..................................................................................................................OFF THEN ON
L2Note: When the ELAC 1 computer is reset on ground, the pitch trim returns to the ground
setting position (0 °).
After corrective action (faulty IR switched off and ELACs reset), pitch alternate law
with reduced protections is recovered.
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
MAX SPEED...................................................................................................................... 320 KT
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 85/164
FCOM 19 AUG 10
NAV IR DISAGREE (Cont'd)
L2 Disagreement between two IRs, the third one having failed or been rejected by the ELACs. Pitch
direct, roll direct, and yaw mechanical laws become active. All protections (pitch and roll) are lost.
L1 ATT.....................................................................................................................................X CHECK
L2 Use the standby horizon to determine the faulty IR.
L1�� IF DISAGREE CONFIRMED:
FAULTY IR P/B..................................................................................................................... OFF
L2 This will also switch off the associated ADR.
L1 ELAC 2..................................................................................................................OFF THEN ON
ELAC 1..................................................................................................................OFF THEN ON
L2Note: When the ELAC 1 computer is reset on ground, the pitch trim returns to the ground
setting position (0 °).
　
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