Operational Test of the Engine Interface Unit A320

1. Reason for the Job

    Self explanatory

    2. Job Set-up Information

    A. Referenced Information

    REFERENCEDESIGNATION
    Ref. 24-41-00-861-002-AEnergize the Aircraft Electrical Circuits from the External Power
    Ref. 24-41-00-861-002-A01Energize the Aircraft Electrical Circuits from the APU
    Ref. 24-41-00-861-002-A02Energize the Aircraft Electrical Circuits from Engine 1(2)
    Ref. 24-41-00-862-002-ADe-energize the Aircraft Electrical Circuits Supplied from the External Power
    Ref. 24-41-00-862-002-A01De-energize the Aircraft Electrical Circuits Supplied from the APU
    Ref. 24-41-00-862-002-A02De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
    Ref. 31-32-00-860-012-AProcedure to Get Access to the SYSTEM REPORT/TEST/ENG Page

    3. Job Set-up

    SUBTASK 73-25-34-861-050-A

    A.           Energize the aircraft electrical circuits Ref. AMM TASK 24-41-00-861-002

    SUBTASK 73-25-34-865-050-A

    B.            Make sure that this(these) circuit breaker(s) is(are) closed:

    PANELDESIGNATIONFINLOCATION
    49VUENGINE/1 AND 2/IGN/SYS A1JHA03
    FOR FIN 1000EM1(ENGINE-1)
    49VUENGINE/1/FADEC A/AND EIU 12KS1A04
    121VUENGINE/ENG1/OIL/PRESS2EN1N40
    121VUENGINE/ENG1/OIL/QTY1EN1N39
    121VUENGINE/IGN/ENG1/SYS B3JH1P41
    121VUENGINE/IGN/ENG1/SYS A BAT2JH1P39
    121VUENGINE/ENG1/FADEC B/AND EIU 14KS1R41
    FOR FIN 1000EM2(ENGINE-2)
    49VUENGINE/2/FADEC A/AND EIU 22KS2A05
    121VUENGINE/ENG2/OIL/PRESS2EN2N42
    121VUENGINE/ENG2/OIL/QTY1EN2N41
    121VUENGINE/IGN/ENG2/SYS B3JH2P42
    121VUENGINE/IGN/ENG2/SYS A BAT2JH2P40
    121VUENGINE/ENG2/FADEC B4KS2Q40

    SUBTASK 73-25-34-710-050-A

    C.            On the left or right MCDU, get SYSTEM REPORT/TEST, ENG Ref. AMM TASK 31-32-00-860-012.

    4.            Procedure

    SUBTASK 73-25-34-710-051-A

    A.           Do the test below:

    ACTIONRESULT
    1.Push the line key adjacent to the EIU1 (EIU2) indication.The EIU menu comes into view.
    2.Push the line key adjacent to the GROUND SCANNING indication.After a short time, the NO FAILURE message comes into view.
    3.On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.The CFDS menu comes into view.
    4.Stop the MCDU.

    5.            Close-up

    SUBTASK 73-25-34-862-050-A

    A.           De-energize the aircraft electrical circuits Ref. AMM TASK 24-41-00-862-002.

    Read me first

    All instructions and limitations given in those documents that relate to the resetting of systems both on the ground and in the air must be respected. No reset should be attempted without a thorough appreciation of the technical ramifications. No more than one computer should be reset at any one time. No reset should be attempted in flight unless specifically permitted by the QRH. Maintenance messages remaining after a reset require engineering investigation.

    If you encounter an ECAM warning or caution that is not available on our website, please take a photo and send it to our Telegram.

    Likewise, if you detect any discrepancies on the site, you can report them directly in our Telegram.

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