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 AIRCRAFT  LOSS OF AP, A/THR NAVIGATES  LAND 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 ACTIONS

•••

•••

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 1. ELEC EMER CONFIG

DETECTION The electrical network is powered by batteries PF CM1 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 term decision CONSIDER AUTOMATION USE 3-5 sec later

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

ECAM PROCEDURE

PNF

QRH

GRAVITY FUEL FEEDING

 2.00

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

Limit speeds & speed trend are recovered SPD LIM

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

A320 CFM

PF

ECAM PROCEDURE

PNF

QRH

GRAVITY FUEL FEEDING

 2.00

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

Limit speeds & speed trend are recovered SPD LIM

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

Setting N1 MODE to ON changes the thrust control from EPR mode to N1 rated mode. Overhead panel A320 IAE

PF

SYSTEM DISPLAY

PNF

Optional

Only EWD available :

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

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

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

PF

PNF

STATUS

To display the 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 the next STATUS page

QRH

1.00

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

Review FCOM 3.02 procedure (If time permits)

!

Important note regarding • fuel consumption • speed indication reliability

FCOM 3.02.24

PF

USE OF SUMMARY

PNF XX

1

3

DECISION

5

VAPP

2 4 8

A P

STATUS

7

P

PR E

P

IN

C R Z

E/WD PROC

AP

P

6 BRIEFING

PF

USE OF SUMMARY

PNF XX

1

3

DECISION

5

VAPP

2 4 8

A P

STATUS

7

P

PR E

P

IN

C R Z

E/WD PROC

AP

P

6 BRIEFING

PF

APPROACH SPEED COMPUTATION

Check that NEW DEST has been entered

PNF

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

VAPP = VREF + 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 LDG CONF VAPP

VLS

FULL

Add 10 kts (VREF) to VREF Add the wind correction Enter VAPP manually (Check minimum RAT speed)

LDG CONF

CONF 3 VAPP

VLS

FULL

LDG in CONF 3 :  Select CONF 3

PF

PNF

APPROACH SYNTHESIS

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

CONF 1 CONF 2

GO AROUND

FINAL APPR

 BACK TO ALTERNATE LAW

 NO AUTO CALLOUTS

CONF 3

LANDING GEAR EXTENSION

F/CTL DIRECT LAW  MANUAL PITCH TRIM USE

LANDING & DECELERATION BE AWARE OF :  NO REVERSER  NO NWS  NO ANTISKID (BRK PRESSURE MONITORED BY PNF)  PARTIAL LOSS OF GRND SPOILERS