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8/18/2019 A330 ECAM Philosophy
1/14
PFPF PNFPNFCommon LR
ECAM PHILOSOPHY
LR - Version 02b
SITUATION ASSESSMENT / DECISION
DETECTION
ECAM ACTIONS
ECAM PROCEDURE
SYSTEM DISPLAY ( if required )
STATUS
LDG DISTLD G D I
ST
WEATHER
WEATHER
OPERATIONAL AND
COMMERCIALCONSIDERATIONS
O
PERATIONAL AND
COMMERCIALCONSIDERATIONS
NOTIFYNO
TIFY
DECISIONDECISION
OPS …OPS …
PURSER /PAXPURSER /P
AX
ATC
ATC
STATUS,or
SUMMARY
8/18/2019 A330 ECAM Philosophy
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PFPF PNFPNFCommon LR
First pilot who notices:
MASTER CAUTION/MASTER WARNING……………RESET
ANNOUNCE………………………...…..”TITLE OF FAILURE”
FLIES THE AIRCRAFT
NAVIGATES
1. DETECTION
If failure at takeoff:
400ft AGLNO ACTION until , with safe flight path established.
CONSIDER AUTOMATION USE : A/THR, AP
LRL R
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PFPF PNFPNFCommon LR
2. ECAM PROCEDURE
ORDER…………….………………”ECAM ACTIONS”
ECAM ACTIONS COMPLETE……….CHECK
CONFIRM……….… CLEAR “name of SYS”?
ECAM ………………..………..CONFIRM (using SD
and overhead panel)
ECAM ACTIONS……………….PERFORM
REQUEST………CLEAR “name of SYS”?
ECAM………………………………..CLEAR
Both pilots should confirmirreversible/guarded actions
This is to be repeated for each failure displayed on theECAM.
Example :
LAND ASAP
*Task sharing:As soon as he announced “ECAMACTIONS”, the PF is in charge of
communications, until all the ECAMactions have been completed.
PF
A330 A340
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PFPF PNFPNFCommon LR
3. SYSTEM DISPLAY Analysis
CONFIRM………… CLEAR “name of SYS”?
SYSTEM PAGE DISPLAYED……….ANALYSE
REQUEST…………...CLEAR “name of SYS”?
SYSTEM DISPLAY…………………..CLEAR
This is to be repeated until all the displayed system pageshave been reviewed, and the STATUS page is displayed.
If a SYSTEM page is displayed on the lower ECAM screen:
8/18/2019 A330 ECAM Philosophy
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PFPF PNFPNFCommon LR
4. STATUS
CONFIRM………………..…………READ STATUS
CONFIRM……………………………CLEAR STATUS
REQUEST….………………………………..STATUS?
STATUS …………………………………...……..READ
LIMITATIONS……………………...….….CHECK
PROC………………...……………..…CONSIDER
LANDING DIST&SPEED INCREMENT..CHECKINOP SYS……………………………...….CHECK
REQUEST…………………………CLEAR STATUS ?
STATUS…………………………………………CLEARANNOUNCE………ECAM ACTIONS COMPLETED
Landing distance and approach speed
computation:
•For complex procedures (dual hydraulic
failure or electrical emergency
configuration): Use SUMMARY
•For other cases:
Review FCOM procedure:
3
Applying ECAM procedure ensures
flight safety.
However, referring to FCOM 3.02, if
time permits, may provide useful
additional information.
0 2 – A B N -
E M E R
RETURN TO NORMAL TASK SHARING
QRH
1.00
8/18/2019 A330 ECAM Philosophy
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PFPF PNFPNFCommon LR
5. SITUATION ASSESSMENT/DECISION
LDG DIST
LDG DIST
WEATHER
WEATHER
OPERATIONAL AND
COMMERCIALCONSIDERATIONS
OPERATIONAL AND
COMMERCIALCONSIDERATIONS
NOTIFY
NOTIFY
DECISION
DECISION
OPS …
OPS …
PURSER / PAX
PURSER / PAX
ATC
ATC
STATUS, or
SUMMARY
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PFPF PNFPNFCommon LR
6. SYNTHESIS
FLY / NAV
ECAM ACTIONS(until STATUS page)
Consider:Normal C/L
OEB
Computer resets
CONTINUE ECAM
(STATUS page)
APPROACH C/L
ECAM APPROACHPROC (if any)
APPROACHPREPARATION
Briefing
DECISION
COM
T
E A
M
W
O
R
K
8/18/2019 A330 ECAM Philosophy
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PFPF PNFPNFCommon LR
IRREVERSIBLE / GUARDED ACTIONS
CONFIRMATION
Confirmation from both pilots is required, when the action concerns:
How to proceed for confirmation ?
Master switch or ADIRS control
PNFPNFHand on related control:
REQUEST……………….………..CONFIRM ?
ACTION…………………………….PERFORM
PFPF
ACTION…………………………..….CHECK
ANSWER………………..………..CONFIRM
PNFPNFPFPF
ACTION…………………………..….CHECK
ANSWER………………..………..CONFIRM
Hand on related control:
REQUEST……………….………..CONFIRM ?
ACTION…………………………….PERFORM
How to proceed for confirmation ?
Any guarded switch Thrust lever is a PF actiongiven that it may influence flight path
!
8/18/2019 A330 ECAM Philosophy
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PFPF PNFPNFCommon LR
IRREVERSIBLE / GUARDED ACTIONS
CONFIRMATION
Confirmation from both pilots is required, when the action concerns:
Master switch or ADIRS control
How to proceed for confirmation ?
PNFPNFHand on related control:
REQUEST……………….………..CONFIRM ?
ACTION…………………………….PERFORM
PFPF
ACTION…………………………..….CHECK
ANSWER………………..………..CONFIRM
PNFPNFPFPF
ACTION…………………………..….CHECK
ANSWER………………..………..CONFIRM
Hand on related control:
REQUEST……………….………..CONFIRM ?
ACTION…………………………….PERFORM
How to proceed for confirmation ?
Any guarded switch Thrust lever is a PF actiongiven that it may influence flight path
!
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PFPF PNFPNFCommon LR 2. ECAM PROCEDURE
ORDER…………….………………”ECAM ACTIONS”
ECAM ACTIONS COMPLETE……….CHECK
CONFIRM……………………………….CLEAR
ECAM ………………..………..CONFIRM (using SD
and overhead panel)
ECAM ACTIONS……………….PERFORM
REQUEST………CLEAR “name of SYS”?
ECAM………………………………..CLEAR
Both pilots should confirmirreversible/guarded actions
This is to be repeated for each failure displayed on theECAM.
Example :
LAND ASAP
*Task sharing:As soon as he announced “ECAMACTIONS”, the PF is in charge of communications, until all the ECAMactions have been completed.
PF
Depending on the failure, , or , may be displayed, in
the right column of the ECAM procedure.
RED : Land at the next suitable airport.
AMBER : Assess the seriousness of the situation and consider the
selection of a suitable airport.
LAND ASAP LAND ASAP
LAND ASAP
LAND ASAP
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PFPF PNFPNFCommon LR
LANDING DISTANCE COMPUTATION
SYS FAILURE A NORM (1) - 1.1
FAILURE A 3 10 1.2
(1) If NORM is indicated for landing configuration, and if CONF3 is used, apply an additional 1.1 coefficient to the landingdistance.
Determine the landing
distance coefficient.
Determine the landingdistance in CONF FULLCONF FULL
without failure
Apply the coefficientdetermined above to thisdistance.
APPR SPD-LDG DIST CORRECTIONS FOR FAILURES
LANDING DISTANCE WITHOUT AUTOBRAKE – CONF FULL
QRH
2.00
QRH
4.00
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APPROACH SPEED COMPUTATION
Select CONF FULL
Read VREF = VLS CONF FULL
Add VREF to VREF
Add wind correction, if applicable
Enter VAPP manually
If LDG in CONF 3 :
Select CONF 3
MCDU PERF APPRpage
LDG CONF
CONF 3
LDG CONF
FULL
VLSVAPP
VAPP = VREF + VREF + WIND CORRECTION (if applicable)
Note: This computation must be done according to the appropriate weight at destination, so, with
F-PLN properly updated.
When applicable, VREF is
given on the QRH.
In this case:
Wind correction only
applies when VREF is
lower than 20 kts.
If the ECAM shows a VLS :
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PFPF PNFPNFCommon LR
APPROACH SPEED COMPUTATION
The ECAM shows a VLS, while the QRH shows a VREF .
VLS increase due to
the actualconfiguration VREF =
VLS CONF FULL
VLS OF THE
LANDING CONF
Speed increase for
handling qualities
Shown on PFD,
when landing
conf is
selected
VLS
shownon
ECAM
VREF
shown
onQRH
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PFPF PNFPNFCommon LR 4. STATUS
CONFIRM………………..…………READ STATUS
CONFIRM……………………………CLEAR STATUS
REQUEST….………………………………..STATUS?
STATUS …………………………………...……..READ
LIMITATIONS……………………...….….CHECK
PROC………………...……………..…CONSIDER
LANDING DIST&SPEED INCREMENT..CHECKINOP SYS……………………………...….CHECK
REQUEST…………………………CLEAR STATUS ?
STATUS…………………………………………CLEARANNOUNCE………ECAM ACTIONS COMPLETED
Landing distance and approach speed
computation:
•For complex procedures (dual hydraulic
failure or electrical emergency
configuration): Use SUMMARY
•For other cases:
Review FCOM procedure:
3
Applying ECAM procedure ensures
flight safety.
However, referring to FCOM 3.02, if
time permits, may provide useful
additional information.
0 2 – A B N -
E M E R
RETURN TO NORMAL TASK SHARING
QRH
1.00
The PNF should not start reading the STATUS before confirmation from the PF.
For any priority reason Status analysis can be postponed by PFe.g. C/L, ATC communication…
In some cases, some other checks or actions may have to be performed, before reading the STATUS:
In case of failure at takeoff, the NORMAL TAKEOFF C/LNORMAL TAKEOFF C/L has to be performed
OEBOEB (if applicable) is to be applied at that time (Refer to QRH 6.00),
Computer resetsComputer resets may be considered (Refer to QRH 2.00)
QRH
6.00QRH
2.00