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 EXTENSIO EXTENSION N FINAL APPR

LANDING & DECELERATION  A320- Versi Version on 03

PF

PNF 1. ELEC EMER CONFIG

DETECTION 

PF

CM1 FLIES THE AIRCRAFT NAVIGATES

LOSS OF AP, A/THR

LAND ASAP…Short ASAP…Short term decision

CONSIDER AUTOMATION USE 

ECAM ACTIO ACTIONS  NS  PF COMMUNICATES MAYDAY

ECAM PROCEDURE 

CFM :

IAE :

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

DECISION 

SUMMARY

WEATHER L D GD LDG DIST IST OPERATIONAL OP OPERATIONAL ERATIONAL AND AND COMMERCIAL COMMERCIAL CONSIDERATIONS CONSIDERATIONS

ATC DECISION DECISION NOTIFY

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……… STATUS………………………...REVIEW ………………...REVIEW SUMMARY…………..……………………….USE FMGS………………………………….PREPARE APPR BRIEFING ............………… ............ …………..PERFORM ..PERFORM FMGS PREPARATION : STANDARD

Done upon PF request 

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

1.00

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

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

PF

PNF 3. APPROACH

When landing gear down :

ECAM ACTIO ACTIONS  NS 

 Approach synthesis

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

PF ELEC

EMER CONFIGPNF

Electrical Electrical Emergency Emergency configurati configuration on = loss of all AC BUSES 

FL 240 

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 oppos opposite ite genera generator  tor  OR 



DECISION

the loss of all GEN OR 





the loss of all engines

simultaneo simultaneous us loss of all GEN 

suspect a short-circuit 

CONFIGURATION

Probability Probability of a successful successful APU GEN GEN coupling coupling is low LANDING GEAR EXTENSIO EXTENSION N FINAL APPR



Be aware that each APU start start attempt reduces reduces the battery battery time availability availability by approx. 3.5 mn. LANDING & DECELERATION  A320- Versi Version on 03

PF

PNF 1. ELEC EMER CONFIG

DETECTION 

CM1 FLIES THE AIRCRAFT NAVIGATES

PF LOSS OF AP, A/THR

LAND ASAP…Short ASAP…Short term decision

CONSIDER AUTOMATION USE  Single Chime ENG THRUST (every 5 sec) LOCKED PF Move the trust levers to theCOMMUNICATES actual thrust position MAYDAY

ECAM ACTIO ACTIONS  NS  ECAM PROCEDURE 

CFM :

IAE :

SYSTEM DISPLAY  STATUS  USE SUMMARY…………..….……..CRUISE part

RETURN TO NORMAL TASK SHARING  STATUS,or 

DECISION 

SUMMARY

WEATHER L D GD LDG DIST IST OPERATIONAL OP OPERATIONAL ERATIONAL AND AND COMMERCIAL COMMERCIAL CONSIDERATIONS CONSIDERATIONS

ATC DECISION DECISION NOTIFY

PURSER PURSER/PAX /PAX OPS … OPS …

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

PF

PNF 1. ELEC EMER CONFIG

DETECTION 

CM1

PF

The electrical electrical network is powered by batteries only during 3-5 sec while the RAT extends and FLIES THE AIRCRAFT LOSS the OF EMER AP, A/THR GEN comes in line NAVIGATES

LAND ASAP…Short ASAP…Short term decision

CONSIDER AUTOMATION USE  3-5 sec later 

ECAM ACTIO ACTIONS  NS  PF COMMUNICATES MAYDAY

ECAM PROCEDURE 

CFM :

IAE :

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

DECISION 

SUMMARY

WEATHER L D GD LDG DIST IST OPERATIONAL OP OPERATIONAL ERATIONAL AND AND COMMERCIAL COMMERCIAL CONSIDERATIONS CONSIDERATIONS

ATC DECISION DECISION NOTIFY

PURSER PURSER/PAX /PAX OPS … OPS …

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

PF

ECAM PROCEDURE

PNF

QRH

GRAVITY FUEL FEEDING 



2.00

ADIRS 2 & 3 remain supplied supplied by batteries batteries for 5 minutes minutes after the loss of both engine generators. generators.  ADIRS Therefore, Therefore, switching switching them off will save battery battery charge

Limit speeds & speed trend are recovered SPD LIM

FAC 1 reset The rudder trim is recovered recovered although although no indication indication is available available

 A320 CFM 

PF

ECAM PROCEDURE

PNF

QRH

GRAVITY FUEL FEEDING 



2.00

 ADIRS ADIRS 2 & 3 remain supplied supplied by batteries batteries for 5 minutes minutes after the loss of both engine generators. generators. Therefore, Therefore, switching switching them off will save battery battery charge

Limit speeds & speed trend are recovered SPD LIM

FAC 1 reset The rudder trim is recovered recovered although although no indication indication is available available

Setting N1 MODE to ON changes changes the thrust control control from EPR mode to N1 rated mode. mode.

Overhead   panel   A320 IAE 

PF

SYSTEM DISPLAY

PNF

Optional

Only EWD EWD available available :

If needed, analyse analyse SYSTEM SYSTEM page displayed displayed on the upper ECAM screen: screen: OTHER SYSTEM PAGES ELEC

ELEC key on ECP…………PRESS and HOLD ELEC PAGE DISPLAYED.………....ANALYSE REQUEST…………………..”CLEAR REQUEST……………… …..”CLEAR ELEC ?” ?”

CONFIRM………………… CONFIRM …………………….”CLEAR ….”CLEAR PRESS” PRESS key on ECP..…….…………...RELEASE

PF

PNF

STATUS

To display display the status status : ANNOUNCE………………………………”STATUS ?” CONFIRM………………………”READ STATUS”

QRH

1.00



STATUS key on ECP…………….PRESS and HOLD

ELEC EMER CONFIG – SYS REMAINING 

Status overflow :

STATUS PAGE

… release the STATUS key on ECP and push it again within 2 sec to display display the next STATUS STATUS page page

QRH

1.00

Compute the LDG DIST with the SUMMARY, according to the estimated weight weight at DEST

Review FCOM 3.02 procedure (If time permits)

!

Important note regarding • fuel consumptio consumption n • speed indication reliability

FCOM 3.02.24

PF

USE OF SUMMARY

PNF XX

E/WD PROC

1

3

DECISION

5    N    I

STATUS

2 4 8

   P    P A

VAPP

   Z    R C

   P    E    R P

7

  P  A  P

6 BRIEFING

PF

USE OF SUMMARY

PNF XX

E/WD PROC

1

3

DECISION

5    N    I

STATUS

2 4 8

   P    P A

VAPP

   Z    R C

   P    E    R P

7

  P  A  P

6 BRIEFING

PF

APPROACH SPEED COMPUTATION

Check that NEW DEST has been entered

VAPP = VREF +

PNF

Ensure that VLS & VAPP are based on the proper weight weight at destination destination

VREF (10 kt) + wind correction VREF is given: MCDU PERF APPR page



On the ECAM, and



On the QRH



Select CONF FULL



Read VREF = VLS CONF FULL



Add 10 kts ( VREF) to VREF



Add the wind correction



Enter VAPP manually

LDG CONF VAPP

VLS

FULL

(Check minimum RAT speed ) LDG CONF

CONF 3 VAPP

VLS

FULL

LDG in CONF 3 : 

Select CONF 3

PF

Approach flown manually with with raw data data : no AP  ALTN LAW  FD A/THR

CONF 1

CONF 2

GO AROUND 

PNF

APPROACH SYNTHESIS

FINAL APPR

BACK TO ALTERNATE ALTERNATE LAW



CONF 3

LANDING GEAR EXTENSION

NO AUTO CALLOUTS

F/CTL DIRECT LAW 

LANDING & DECELERATION BE AWARE OF : 

NO REVERSER



NO NWS



NO ANTISKID

(BRK PRESSURE MONITORED BY PNF) 

PARTIAL LOSS OF GRND SPOILERS

MANUAL PITCH TRIM USE