— MAN START OFF
— ENG MASTER (affected) OFF
— AIR BLEED PRESS ESTABLISH
— ENG MODE SEL CRANK
— MAN START ON
* When burning has stopped :
— MAN START OFF
— ENG MODE SEL NORM
— A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 35
2.24
SEQ 025
The ECAM's VIB advisory (N1 ...- 6 units, N2 ...- 4.3 units) is mainly a guideline to induce the crew to monitor engine parameters more closely.
VIB detection alone does not require engine shutdown.
NOTE : 1. High engine vibrations may be accompanied by cockpit and cabin smoke, and/or
the smell of burning. This may be due only to compressor blade tip contact with associated abradable seals.
2. High N1 vibrations are generally accompanied by perceivable airframe
vibrations.
High N2 vibrations can occur without perceivable airframe vibrations.
If no icing conditions :
- ENG PARAMETERS CHECK
Check engine parameters and especially EGT ; crosscheck with the other engine. Report in the maintenance log.
• If rapid increase above the advisory :
- THRUST LEVER (affected engine) RETARD
Flight conditions permitting, reduce N1 to maintain the vibration level below the advisory threshold.
Note : If the VIB indication does not decrease following thrust reduction, this may
indicate other engine problems. Apply the adequate procedure.
If icing conditions :
An increase in N1 vibrations in icing conditions, with or without engine anti-ice, may be due to fan blades and/or spinner icing.
- A/THR OFF
- ENGINE ANTI-ICE CHECK
If ENG ANTI-ICE is off, switch it ON at idle fan speed, one engine after the other at an approximate 30-second interval.
- THRUST LEVER (one engine at a time) .. INCREASE THRUST
Increase thrust to a setting compatible with the flight phase. The VIB level will return to normal after ice is shed, despite a slight increase during acceleration.
Resume normal operation.
NOTE : When vibrations above the advisory level have been experienced during the flight, and
if possible, shut down the engine after landing, for taxiing.
A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 35
2.25
SEQ 025
LDG CONF DETERMINE
When an overweight landing has to be performed after an operational turnback, refer to the corresponding RTOW chart, or to FCOM to find the approach and landing configuration given as a function of the approach climb limiting weight.
NOTE: For weights greater than 70000 kg (or 154 000 lb), S speed is greater than VFE CONF 2 (200 knots). Consequently, on the FCU, the crew must select a speed below 200 knots before setting FLAPS 2. When in FLAPS 2, the crew can use managed speed again.
LDG DIST CHECK
PACK 1 and 2 OFF or supplied by APU
Selecting packs OFF (or supplied from APU) will increase the maximum thrust available from the engines in the event of a go-around.
* In the final approach stages
* TARGET SPEED VLS
Reduce the selected speed on the FCU to reach VLS at runway threshold.
Touch down as smoothly as possible (Maximum V/S at touchdown 360 ft/min).
* At main landing gear touchdown
* REVERSE THRUST USE MAX AVAILABLE
* After nosewheel touchdown
* BRAKES APPLY AS NECESSARY
Maximum braking may be used after nosewheel touchdown. But if landing distance permits, delay or reduce braking to fully benefit from the available runway length.
* Landing complete
* BRAKE FANS (‹ ON
Be prepared for tire deflation, if temperatures exceed 800° C.
A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 36
2.26
SEQ 001
— MAX FL 230
— CAB PRESS MODE SEL MAN
— MAN V/S CTL AS RQRD
Set the cabin altitude, according to the table below.
AP
FL
100
150
200
230
5 PSI
CABIN ALTITUDE
0
3000
6000
8000
• When starting the final descent :
— CAB PRESS MODE SEL AUTO
— Affected WINDOW/WINDSHIELD ANTI ICE C/B PULL
In case of electrical arcing, pull the circuit breaker of the affected window/windshield heating system
. ANTI ICE L WSHLD C/B AF10 . ANTI ICE/WINDOWS L C/B X14
. ANTI ICE R WSHLD C/B AF03 . ANTI ICE/WINDOWS R C/B W14
Accomplish the following, while making a 180° turn.
— ATC NOTIFY
— A/THR OFF
— THRUST (conditions permitting) DECREASE
— CREW OXYGEN MASKS ON/100%
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