PF ECAM PHILOSOPHYPNF - SmartCockpit · pf ecam philosophypnf a320 - version 04b situation...

12
PF PF PNF PNF ECAM PHILOSOPHY A320 - Version 04b SITUATION ASSESSMENT / DECISION DETECTION ECAM ACTIONS ECAM PROCEDURE SYSTEM DISPLAY ( if required ) STATUS LDG DIST LDG DIST WEATHER WEATHER OPERATIONAL AND COMMERCIAL CONSIDERATIONS OPERATIONAL AND COMMERCIAL CONSIDERATIONS NOTIFY NOTIFY DECISION DECISION OPS … OPS … PURSER / PAX PURSER / PAX ATC ATC STATUS, or SUMMARY

Transcript of PF ECAM PHILOSOPHYPNF - SmartCockpit · pf ecam philosophypnf a320 - version 04b situation...

  • PFPF PNFPNFECAM PHILOSOPHY

    A320 - Version 04b

    SITUATION ASSESSMENT / DECISION

    DETECTION

    ECAM ACTIONS

    ECAM PROCEDURE

    SYSTEM DISPLAY ( if required )

    STATUS

    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

  • PFPF PNFPNF

    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

  • PFPF PNFPNF2. ECAM ACTIONS

    ORDER…………….………………”ECAM ACTIONS”

    ECAM ACTIONS COMPLETE……….CHECK

    CONFIRM……….… CLEAR “name of SYS”?

    ECAM ………………..………..CONFIRM (using SDand 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 ofcommunications, until all the ECAMactions have been completed.PF

  • PFPF PNFPNF3. SYSTEM DISPLAYS

    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:

  • PFPF PNFPNF4. STATUS

    CONFIRM………………..…………READ STATUS

    CONFIRM……………………………CLEAR STATUS

    REQUEST….………………………………..STATUS?

    STATUS …………………………………...……..READ

    LIMITATIONS……………………...….….CHECKPROC………………...……………..…CONSIDERLANDING DIST&SPEED INCREMENT..CHECKINOP SYS……………………………...….CHECK

    REQUEST…………………………CLEAR STATUS ?STATUS…………………………………………CLEARANNOUNCE………ECAM ACTIONS COMPLETED

    Landing distance and approach speedcomputation:

    •For complex procedures (dual hydraulicfailure or electrical emergencyconfiguration): Use SUMMARY

    •For other cases:

    Review FCOM procedure:

    3

    Applying ECAM procedure ensuresflight safety.However, referring to FCOM 3.02, iftime permits, may provide usefuladditional information.

    02–

    AB

    N-

    EM

    ER

    RETURN TO NORMAL TASK SHARING

    QRH

    1.00

  • PFPF PNFPNF5. SITUATION ASSESSMENT/DECISION

    LDG DISTLDG DIST

    WEATHERWEATHER

    OPERATIONAL ANDCOMMERCIAL

    CONSIDERATIONS

    OPERATIONAL ANDCOMMERCIAL

    CONSIDERATIONS

    NOTIFYNOTIFY

    DECISIONDECISION

    OPS …OPS …

    PURSER / PAXPURSER / PAX

    ATCATC

    STATUS, or

    SUMMARY

  • PFPF PNFPNF6. SYNTHESIS

    FLY / NAV

    ECAM ACTIONS(until STATUS page)

    Consider:Normal C/L

    OEBComputer resets

    CONTINUE ECAM(STATUS page)

    APPROACH C/L

    ECAM APPROACHPROC (if any)

    APPROACHPREPARATION

    Briefing

    DECISION

    COM

    TEAM

    WORK

  • PFPF PNFPNFIRREVERSIBLE / GUARDED ACTIONSCONFIRMATION

    Confirmation from both pilots is required, when the action concerns:

    How to proceed for confirmation ?

    PNFPNFHand on related control:

    REQUEST……………….………..CONFIRM ?

    ACTION…………………………….PERFORM

    PFPF

    ACTION…………………………..….CHECK

    ANSWER………………..………..CONFIRM

    Master switch orADIRS control

    Any guarded switch Thrust lever is a PF actiongiven that it may influence flight path

    !

    How to proceed for confirmation ?

    PNFPNFPFPF

    ACTION…………………………..….CHECK

    ANSWER………………..………..CONFIRM

    Hand on related control:

    REQUEST……………….………..CONFIRM ?

    ACTION…………………………….PERFORM

  • PFPF PNFPNF2. ECAM ACTIONS

    ORDER…………….………………”ECAM ACTIONS”

    ECAM ACTIONS COMPLETE……….CHECK

    CONFIRM……………………………….CLEAR

    ECAM ………………..………..CONFIRM (using SDand 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 ofcommunications, 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

  • PFPF PNFPNFLANDING DISTANCE COMPUTATION

    SYS FAILURE AFAILURE B 3

    NORM (1)

    1.21.1

    10

    _

    (1) If NORM is indicated for landing configuration, and if CONF3 is used, apply an additional 1.1 coefficient to the landingdistance.

    Determine the landingdistance coefficient.

    Determine the landingdistance in CONF FULLCONF FULLwithout failure

    Apply the coefficientdetermined above to thisdistance.

    APPR SPD-LDG DIST CORRECTIONSFOR FAILURES

    LANDING DISTANCE WITHOUTAUTOBRAKE – CONF FULL

    QRH

    2.00

    QRH

    4.00

  • PFPF PNFPNFAPPROACH SPEED COMPUTATION

    Select CONF FULLRead VREF = VLS CONF FULL

    AddVREF to VREF

    Add wind correction, if applicable

    Enter VAPP manually

    If LDG in CONF 3 :

    Select CONF 3

    MCDU PERF APPRpage

    LDG CONFCONF 3

    LDG CONF

    FULL

    VLSVAPP

    If the ECAM shows :“APPR SPEED……….VREF+VREF”:

    VAPP = VREF + VREF + WIND CORRECTION (if applicable)

    Note: This computation must bedone according to the appropriateweight at destination, so, withF-PLN properly updated.

    VREF is given:

    On the ECAM, and

    On the QRH

    Wind correction onlyapplies when VREF islower than 20 kts.

  • PFPF PNFPNF4. STATUS

    CONFIRM………………..…………READ STATUS

    CONFIRM……………………………CLEAR STATUS

    REQUEST….………………………………..STATUS?

    STATUS …………………………………...……..READ

    LIMITATIONS……………………...….….CHECKPROC………………...……………..…CONSIDERLANDING DIST&SPEED INCREMENT..CHECKINOP SYS……………………………...….CHECK

    REQUEST…………………………CLEAR STATUS ?STATUS…………………………………………CLEARANNOUNCE………ECAM ACTIONS COMPLETED

    Landing distance and approach speedcomputation:

    •For complex procedures (dual hydraulicfailure or electrical emergencyconfiguration): Use SUMMARY

    •For other cases:

    Review FCOM procedure:

    3

    Applying ECAM procedure ensuresflight safety.However, referring to FCOM 3.02, iftime permits, may provide usefuladditional information.

    02–

    AB

    N-

    EM

    ER

    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

    2.00

    QRH

    6.00