A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 36
2. 00A
SEQ 001
MISCELLANEOUS
OVERWEIGHT LANDING 2.25
WINDSHIELD/WINDOW CRACKED/ARCING 2.26
VOLCANIC ASH ENCOUNTER 2.26
BOMB ON BOARD 2.27
VAPP DETERMINATION 2.31
APPR SPD-LDG DIST CORRECTIONS FOR FAILURES 2.32
R TRIPPED C/B RE-ENGAGEMENT 2.34
COMPUTER RESET 2.34
ECAM ADVISORY CONDITIONS 2 40
A319/A320/A321
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ABNORMAL PROCEDURES
REV 32
2.01
SEQ 110
Apply the following procedure (not displayed on ECAM) in case of total loss of the cabin pressure control leading to overpressure.
* PACK 1 or 2 OFF
* BLOWER + EXTRACT OVRD
Cabin air is extracted overboard.
* AP FREQUENTLY MONITOR
• If AP > 9 PSI
PACK 1 + 2 OFF
LAND ASAP
Before 10 minutes from landing :
PACK 1 + 2 OFF
BLOWER + EXTRACT AUTO
CAUTION
A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 36
2.02
SEQ 001
Do not apply this procedure if ENG BLEED 1 was lost due to : . LEAK on side 1
. ENG 1 FIRE
. Start Air Valve 1 failed open.
MAX FL 200
Descend rapidly to FL 200 to recover the bleed supply from the APU.
- APU START
Start the APU during the descent.
* AT OR BELOW FL 200 :
* If ENG 2 BLEED loss due to :
LEAK on side 2 or
ENG 2 FIRE or
Start Air Valve 2 failed open
- X BLEED SHUT
* PACK2 (if above FL 150) OFF
Only if PACK 1 is available.
* WING A.ICE OFF
APU BLEED must not be used for wing anti-ice.
* APU BLEED ON
AVOID ICING CONDITIONS
A319/A320/A321
o,®_
ABNORMAL PROCEDURES
REV 32
2.03
SEQ 110
The "SPEED SPEED SPEED" synthetic voice is triggered every 5 seconds whenever the aircraft energy goes below a threshold under which thrust shall be increased to recover a positive flight path angle.
* THR LEVERS PUSH
Increase the thrust until the warning disappears.
Flight time on batteries only may be increased to at least 30 minutes as follows :
* ENG MODE SEL NORM
* ANTI ICE PITOT 1 C/B (D02) PULL
* 26 V ADIRU 1 C/B (F07) PULL
CM 1 altitude, speed, and vertical speed indication on PFD are lost. Use standby instruments.
* 7 minutes before landing :
- ANTI ICE PITOT 1 C/B (D02) RESET
* After 1 minute :
CAUTION
This time delay is necessary to ensure reliable speed information even in icing conditions when the ADIRU is reset to ON.
- 26 V ADIRU 1 C/B (F07) RESETA319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 36
2.04
SEQ 002
- LANDING CONF CONF 3
* Repeat the following until landing configuration is reached :
* SPEED SEL VFE NEXT - 5 KT
Decelerate towards VFE NEXT — 5 KT, but not below VLS. If turbulence, the pilot may decide to decelerate to a lower speed (not below VLS) to avoid VFE exceedance.
NOTE : . Autopilot may be used down to 500 feet AGL. As it is not tuned for abnormal
configurations, its behavior can be less than optimum and must be monitored.
Approach with selected speed is recommended.
A/THR is recommended, except in the case of a G+B SYS LO PR warning. OVERSPEED warning and VLS, displayed on the PFD, are computed according to the actual flaps/slats position.
VFE and VFE NEXT are displayed on the PFD according to the FLAPS' lever position. If not displayed, use the placard speeds.
If VLS is greater than VFE NEXT (overweight landing), FLAPS lever can be set to the next required position while speed is reduced to follow VLS reduction, as
surfaces extend. The VFE warning threshold should not be triggered.
In this case, disconnect the A/THR. A/THR can be re-engaged when landing configuration is established.
As speed reduces through VFE NEXT :
* FLAPS LEVER ONE STEP DOWN
* When landing configuration is established :
* DECELERATE TO CALCULATED APPROACH SPEED IN FINAL APPROACH
FOR GO AROUND
The table on page 2.05 provides the MAX SPEEDS for abnormal configurations.
* IF SLATS FAULT
* FOR CIRCUIT
* MAINTAIN SLAT/FLAP CONFIGURATION
* Recommended speed : MAX SPEED - 10 KT
* FOR DIVERSION
* SELECT CLEAN CONFIGURATION
Recommended speed for flaps retraction is between MAX SPEED - 10 KT and MAX SPEED.
* Recommended speed : MAX SPEED - 10 KT
* IF FLAPS FAULT
* FOR CIRCUIT
* MAINTAIN SLAT/FLAP CONFIGURATION
* Recommended speed : MAX SPEED - 10 KT
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