A320 ELEC EMER CONFIG

PF ELEC

EMER CONFIGPNF

FL 240
ELEC EMER

AC BUSES 1 & 2
FAULT

LAND ASAP
ECAM ACTIONS
DECISION

CONFIGURATION

LANDING GEAR EXTENSION
FINAL APPR

LANDING & DECELERATION

A320 - Version 03

PF

PNF
1. ELEC EMER CONFIG

DETECTION

CM1  PF
FLIES THE AIRCRAFT  LOSS OF AP, A/THR
NAVIGATES  LAND ASAP…Short term decision
CONSIDER AUTOMATION USE

ECAM ACTIONS
PF
COMMUNICATES
MAYDAY

ECAM PROCEDURE

CFM :

IAE :

SYSTEM DISPLAY
STATUS
USE SUMMARY…………..….……..CRUISE part
RETURN TO NORMAL TASK SHARING

DECISION

ST AT US, or
SUMM ARY

WE ATHER
WEATHER
LDG DIS
DIST
T
OPERATIONAL
OPERATIONALAND
AND
COMME
COMMERCIAL
RCIAL
CONS IDERATIONS
CONSIDERATIONS

ATC
DECISION
DECISIO N
NOT IFY

PURSER
PURSER/ PAX
/ PAX
OPS …
OPS …

FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD

PF

PNF
2. APPROACH PREPARATION
ECAM STATUS………………………...REVIEW
SUMMARY…………..……………………….USE
FMGS………………………………….PREPARE
APPR BRIEFING ............…………..PERFORM
FMGS PREPARATION :

Done upon PF request

STANDARD
+
MANUAL INSERTION OF VAPP
APP BRIEFING :
STANDARD
+
STATUS
+
QRH

ELEC EMER CONFIG summary :
APP, LDG & G/A parts
1.00

FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD

PF

PNF
3. APPROACH

When landing gear down :

ECAM ACTIONS

Approach synthesis

FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD

PF ELEC
FL 240

EMER CONFIGPNF

Electrical Emergency configuration = loss of all AC BUSES
ELEC EMER

AC BUSES 1 & 2
FAULT

LAND ASAP
It may be caused by :

the loss ECAM of oneACTIONS engine and the failure of the opposite generator
OR

DECISION

the loss of all GEN
OR
the loss of all engines

 simultaneous loss of all GEN

suspect a short-circuit

CONFIGURATION

Probability of a successful
APU GEN coupling is low

LANDING GEAR EXTENSION

FINAL APPR

Be aware that each APU start attempt reduces the battery time availability by approx. 3.5 mn.
LANDING & DECELERATION

A320 - Version 03

PF

PNF
1. ELEC EMER CONFIG

DETECTION

CM1  PF
FLIES THE