A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 35
2.22
SEQ 060
A319/A320/A321
o,®_
ABNORMAL PROCEDURES
REV 36
2.21
SEQ 100
If IR alignment is lost, the navigation mode is inoperative (red ATT flag on the PFD and red HDG flag on the ND).
Aircraft attitude and heading may be recovered by applying the following procedure. The aircraft must stay level, with constant speed for 30 seconds.
— MODE SELECTOR ATT
ALIGN light on for 30 seconds. ATT MODE displayed on the CDU.
— LEVEL A/C ATTITUDE HOLD
— CONSTANT NC SPEED MAINTAIN
— DISPLAY SYS switch AFFECTED SYS
— DISPLAY DATA switch HDG
* MCDU INITIALIZATION :
— DATA (MCDU KEY) PRESS
The DATA INDEX page is displayed.
— IRS MONITOR (2L KEY) PRESS
The IRS MONITOR page is displayed.
— NC HEADING ENTER
The heading must be entered in the SET HDG field (5R KEY).
* CDU INITIALIZATION :
Depending on the CDU keyboard installed, an "H" may be written on the "5" key :
* If "H" is written on the "5" key :
— H KEY PRESS
Degree marker, 0 decimal point, ENT and CLR lights come on.
— A/C HEADING ENTER
* If "H" is not written on the "5" key :
— NC HEADING ENTER
Enter the aircraft's magnetic heading on the CDU keyboard. Then, press the ENT key to enter data.
Example : To enter a heading of 320°, dial 3, 2, 0, 0 then press ENT.
Heading will be displayed on the associated ND.
"HDG---ATT MODE" will be displayed on the CDU.
Due to IR drift, the magnetic heading has to be periodically
crosschecked and updated with standby compass, if required.A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 35
2.22
SEQ 060
A319/A320/A321
oniatTri
ABNORMAL PROCEDURES
REV 36
2.23
SEQ 025
ENG 1(2) STALL
* N2 between 50 % and IDLE :
— ENG MASTER (affected engine) OFF
ENG 1 (2) SHUT DOWN
* N2 above IDLE (title and procedure not displayed on ECAM) :
* On ground :
— ENG MASTER (affected engine) OFF
* In flight :
— THR LEVER (affected engine) IDLE
— ENG PARAMETERS (affected engine) CHECK
* Abnormal
— ENG MASTER (affected engine) OFF
ENG 1 (2) SHUT DOWN
—
* Normal :
— ENG A.ICE (affected engine) ON
— WING A.ICE ON
— THR LEVER (affected engine) SLOWLY ADVANCE
* If a stall recurs : — THR LEVER (affected engine) REDUCE
* If a stall does not recur : Continue engine operation.
*
For performance reasons, do not extend flap full until established on a final descent to landing.
If a level off is expected during final approach, perform the approach and landing in CONF 3.
CAUTION
External fire agents can cause severe corrosive damage and should, therefore, only be considered after having applied following procedure :
