One or more loud bangs can be heard; the parameters fluctuate but quic

normal. In most occurrences, the parameters are back to

idfied and corrected by the fl

e Flameout

. Fuel starvation  . Volcanic ash encounter
. Engine stall

. Control system malfunction

Flying at high speed a

The engine flameout will trigger a caution on thWhen no caution is available, an engine flameout is detected by: . A rapid decrease in EGT, N2 (N3 on RR engines), Fuel Flow, and N1 . The l
On most FADEC equipped engines, continuous ignition will b
when a flameout is detected. This ensures an automatic relight, if
e Vibrations
Engine vibrations may be caused by:
. Engine unbalance . Birdstrik
. Compressor blade loss . Icing conditions (ice may build up on the fan spinner and blades).
 

In case the vibration level exceeds a certain level, the ECAM advisory fu

(ie) will au

Wh such a level of vibratiingrity of the engine (blad

As a general rule

. Crosscheck the affected engi

. Reduce the thrust level of the affected engine below the advisory level if flight conditionsA sudden increase of the vibration level indicates a possible deter

Duing takeoff, the vibration indication should be stabilized once takeofIf the advisory threshold is reached, a low speed rejected takeoff may be

The vibrations should not vary significantly dur

the circumstances. Vibrations alone should not lead to an in-flight shutdown.

IV.6 Engine Parameter O

EGT Exceedance

Th EGT redline is the only redline that can be exceededmalfunction of the engine.

Due to the thermal inertia of the engine

the takeoff roll, close to rotation or just after lift-off. The dif

hours

Figure 8

Evolution of the EGT with OAT and Engine Wear

This means that, exceptionally, the engine may exceed the EGT redline withoufailure. In this case, the engine continues to deliver its thrust. Consequently, if the flight crew notices an EGT exceedance during the takeoff roll, the flight crew continues the takeoff and establishes the aircraft on the initial climb path, befor
applying the procedure. Note:
A limited number of small EGT exceedances may be allowed (as Maintenance Manual), but must be reported in the logbook

However, if the EGT suddenly increases when setting tN1, N2, N3 Exceedance N1, N2, N3 exceedances co
The associated procedure is usually to reduce thrust to return below the limits, and to shutdown the engine if it is not possible to return below the limits, or depending on the level of exceedance.
Oil Low Pressure / Oil Low Level In service experience shows
.
its fully sto
automatically reduced), and the aircraft speed (
the effect of a potential deployment. The affected engine must remain at idle for the rest of the flight (i.e. even in the absence of buffet) . The detection of buffet is the sign that the thrust reverser is at least partially deployed. If detected, the flight crew should reduce the aircraft speed, and shut down the affected eng
　
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