a320-elec emer config
TRANSCRIPT
PFPF PNFPNFELEC EMER CONFIG
CONFIGURATION
FINAL APPR
LANDING GEAR EXTENSION
LANDING & DECELERATION
ELEC EMER
LAND ASAP
ECAM ACTIONS
DECISION
FL 240
AC BUSES 1 & 2FAULT
A320 - Version 03
PFPF PNFPNF
DETECTION
DECISION
RETURN TO NORMAL TASK SHARING
LDG DISTLDG DIST
WEATHERWEATHER
OPERATIONAL ANDCOMMERCIAL
CONSIDERATIONS
OPERATIONAL ANDCOMME RCIAL
CONSIDERATIONS
NOT IFYNOT IFY
DECISIONDECISION
OPS …OPS …
PURSER / PAXPURSER / PAX
ATCATC
STAT US, or
SUMMARY
CM1CM1 PFPFFLIES THE AIRCRAFT LOSS OF AP, A/THR
NAVIGATES LAND ASAP…Short term decision
CONSIDER AUTOMATION USE
1. ELEC EMER CONFIG
ECAM ACTIONSECAM PROCEDURE
SYSTEM DISPLAY
STATUSUSE SUMMARY…………..….……..CRUISE part
PF
COMMUNICATESMAYDAY
CFM : IAE :
FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD
PFPF PNFPNF2. APPROACH PREPARATION
ECAM STATUS………………………...REVIEW
SUMMARY…………..……………………….USE
FMGS………………………………….PREPARE
APPR BRIEFING ............…………..PERFORM
FMGS PREPARATION :
STANDARD
+
MANUAL INSERTION OF VAPPVAPP
APP BRIEFING :
STANDARD
+
STATUS
+
ELEC EMER CONFIG summary :APP, LDG & G/A parts
QRH
1.00
Done upon PF request
FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD
PFPF PNFPNF3. APPROACH
When landing gear down :
Approach synthesis
ECAM ACTIONS
FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD
PFPF PNFPNFELEC EMER CONFIG
CONFIGURATION
FINAL APPR
LANDING GEAR EXTENSION
LANDING & DECELERATION
ELEC EMER
LAND ASAP
ECAM ACTIONS
DECISION
FL 240
AC BUSES 1 & 2FAULT
A320 - Version 03
Electrical Emergency configuration = loss of all AC BUSES
It may be caused by :
the loss of one engine and the failure of the opposite generator
OR
the loss of all GEN
OR
the loss of all engines
Be aware that each APU start attempt reduces the battery time availability by approx. 3.5 mn.
Probability of a successfulAPU GEN coupling is low
simultaneous loss of all GEN suspect a short-circuit
PFPF PNFPNF
DETECTION
DECISION
RETURN TO NORMAL TASK SHARING
LDG DISTLDG DIST
WEATHERWEATHER
OPERATIONAL ANDCOMMERCIAL
CONSIDERATIONS
OPERATIONAL ANDCOMME RCIAL
CONSIDERATIONS
NOT IFYNOT IFY
DECISIONDECISION
OPS …OPS …
PURSER / PAXPURSER / PAX
ATCATC
STAT US, or
SUMMARY
CM1CM1 PFPFFLIES THE AIRCRAFT LOSS OF AP, A/THR
NAVIGATES LAND ASAP…Short term decision
CONSIDER AUTOMATION USE
1. ELEC EMER CONFIG
ECAM ACTIONSECAM PROCEDURE
SYSTEM DISPLAY
STATUSUSE SUMMARY…………..….……..CRUISE part
PF
COMMUNICATESMAYDAY
CFM : IAE :
FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD
Move the trust levers tothe actual thrust position
Single Chime(every 5 sec)
ENG THRUSTLOCKED
••• •••
PFPF PNFPNF
DETECTION
DECISION
RETURN TO NORMAL TASK SHARING
LDG DISTLDG DIST
WEATHERWEATHER
OPERATIONAL ANDCOMMERCIAL
CONSIDERATIONS
OPERATIONAL ANDCOMME RCIAL
CONSIDERATIONS
NOT IFYNOT IFY
DECISIONDECISION
OPS …OPS …
PURSER / PAXPURSER / PAX
ATCATC
STAT US, or
SUMMARY
CM1CM1 PFPFFLIES THE AIRCRAFT LOSS OF AP, A/THR
NAVIGATES LAND ASAP…Short term decision
CONSIDER AUTOMATION USE
1. ELEC EMER CONFIG
ECAM ACTIONSECAM PROCEDURE
SYSTEM DISPLAY
STATUSUSE SUMMARY…………..….……..CRUISE part
PF
COMMUNICATESMAYDAY
CFM : IAE :
FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD
The electrical network is powered by batteriesonly during 3-5 sec while the RAT extends and
the EMER GEN comes in line
3-5 sec later
PFPF PNFPNFECAM PROCEDURE
GRAVITY FUEL FEEDINGQRH
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
The rudder trim is recovered although noindication is available
FAC 1 reset
SPDLIM
A320 CFM
PFPF PNFPNFECAM PROCEDURE
GRAVITY FUEL FEEDINGQRH
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
The rudder trim is recovered although noindication is available
FAC 1 reset
SPDLIM
A320 IAE
Setting N1 MODE to ON changes the thrust control fromEPR mode to N1 rated mode.
Overheadpanel
PFPF PNFPNFSYSTEM DISPLAY
If needed, analyse SYSTEM page displayed on the upper ECAM screen:
Optional
Only EWD available :
OTHER SYSTEM PAGES
CONFIRM…………………….”CLEAR PRESS”
ELEC key on ECP…………PRESS and HOLDELEC PAGE DISPLAYED.………....ANALYSEREQUEST…………………..”CLEAR ELEC ?”
PRESS key on ECP..…….…………...RELEASE
ELEC
PFPF PNFPNFSTATUS
Status overflow :STATUS
PAGE
Review FCOM 3.02 procedure (If time permits)
!Important note regarding• fuel consumption• speed indication reliability
FCOM
3.02.24
ELEC EMER CONFIG –SYS REMAINING
Compute the LDG DIST with the SUMMARY,according to the estimated weight at DEST
ANNOUNCE………………………………”STATUS ?”
STATUS key on ECP…………….PRESS and HOLDCONFIRM………………………”READ STATUS”
… release the STATUS key on ECP and push it
again within 2 sec to display the next STATUS page
To display the status :
QRH
1.00
QRH
1.00
PFPF PNFPNFUSE OF SUMMARY
STATUS
E/WDPROC 1
INCRZ
DECISION
2 APPPREP
VAPP
BRIEFING
4
5
6
APP
7
8
3
XX
PFPF PNFPNFUSE OF SUMMARY
STATUS
E/WDPROC 1
INCRZ
DECISION
2 APPPREP
VAPP
BRIEFING
4
5
6
APP
7
8
3
XX
PFPF PNFPNFAPPROACH SPEED COMPUTATION
Select CONF FULL
Read VREF = VLS CONF FULL
Add 10 kts (VREF) to VREF
Add the wind correction
Enter VAPP manually
(Check minimum RAT speed)
LDG in CONF 3 :
Select CONF 3
MCDU PERF APPRpage
LDG CONFCONF 3
LDG CONF
FULLVLSVAPP
FULLVLSVAPP
VAPP = VREF + VREF (10 kt) + wind correction
Check that NEW DESThas been entered
Ensure that VLS & VAPP are basedon the proper weight at destination
VREF is given:
On the ECAM, andOn the QRH
PFPF PNFPNFAPPROACH SYNTHESIS
LANDING & DECELERATIONBE AWARE OF :
NO REVERSER
NO NWS
NO ANTISKID(BRK PRESSURE MONITORED BY PNF)
PARTIAL LOSS OF GRND SPOILERS
GO AROUND
BACK TO ALTERNATE LAW
CONF 1
CONF 2
CONF 3
Approach flown manuallywith raw data : no AP
FDA/THR
ALTN LAW
F/CTL DIRECT LAW
MANUAL PITCH TRIM USE
FINAL APPR
NO AUTO CALLOUTS
LANDING GEAREXTENSION