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mod 5 Safety - software - 5.14 - HIRF - HIRF EMI
26問 • 11ヶ月前
  • Yousef Alshammary
    • 通報

    問題一覧

  • 1

    Level A

    Catastrophic failure

  • 2

    Failure conditions which

    prevent continued safe flight and landing.

  • 3

    Failure may cause crash error or loss of critical function required to safety fly and land aircraft is

    Catastrophic

  • 4

    What is the effect of a level 1 software failure

    Loss of aircraft and /or fatalities

  • 5

    An aircraft system allocated a Criticality Category of Hazardous has software level of

    B

  • 6

    Suppose failure in level E software this will cause

    no effect

  • 7

    Modification to software will be subjected to the same approval procedures as are applied to

    hardware modifications

  • 8

    Collection of data where the computer gets specific information is

    Databases

  • 9

    What is the Software Media

    Device that contains a copy of the software

  • 10

    All passenger seats are addressable means

    by the computer which transmit data through the network directly to individual passenger seat

  • 11

    Failure system in the aircraft according to software error cause a significant reduction is safety margin which cause

    injures to occupants

  • 12

    Which Document provides guidance to aircraft constructors of software

    DO-178B/ED

  • 13

    Which section will summarize the plan and test result

    software Verification plan

  • 14

    Ground loops are prevented by

    ground only one end of the cable screen

  • 15

    When incorporating an aerial cable it must be

    positioned separately from the loom

  • 16

    The avionics bay in the larger aircraft are placed in

    below the floor

  • 17

    Electromagnetic compatibility is achieved by

    Shielding, screening, earthling, bonding and interference filters

  • 18

    In order to maintain HIRF protection, bonding checks between airframe and electrical components carrying voltages greater than 50 volts RMS or DC or main earth return should not exceed

    0.05 ohm

  • 19

    EMC gaskets shielding arrangement used to

    reduce the leakage of electromagnetic energy.

  • 20

    Primary flight display (PFD) and navigation display (ND) are two main display units that together

    make up the EFIS for commercial aircraft.

  • 21

    To reduce HIRF on radio equipment

    ensure all static wicks are in place

  • 22

    HIRF protection of LRUs is provided by

    built in filters and overvoltage circuits

  • 23

    The phase shift between the electric field oscillation and magnetic field oscillation is

    90⁰

  • 24

    When carrying out a bonding check on a surface protected by anodic film

    The anodic film should be removed locally to ensure a good contact

  • 25

    When clamping cable looms containing co-axial cables

    avoid distortion to it, to maintain the dielectric constant

  • 26

    Testing of HIRF on aircraft system is done

    at and during production and testing (initial certification

    • mod 3 3.1 - 3.2 - 3.3

    mod 3 3.1 - 3.2 - 3.3

    Yousef Alshammary · 24問 · 12ヶ月前

    mod 3 3.1 - 3.2 - 3.3

    mod 3 3.1 - 3.2 - 3.3

    24問 • 12ヶ月前
    Yousef Alshammary

    mod 3 3.4 - 3.5 - 3.6

    mod 3 3.4 - 3.5 - 3.6

    Yousef Alshammary · 39問 · 12ヶ月前

    mod 3 3.4 - 3.5 - 3.6

    mod 3 3.4 - 3.5 - 3.6

    39問 • 12ヶ月前
    Yousef Alshammary

    mod 3 3.7 - 3.8 - 3.9

    mod 3 3.7 - 3.8 - 3.9

    Yousef Alshammary · 38問 · 11ヶ月前

    mod 3 3.7 - 3.8 - 3.9

    mod 3 3.7 - 3.8 - 3.9

    38問 • 11ヶ月前
    Yousef Alshammary

    mod 3 3.10 - 3.11 - 3.12

    mod 3 3.10 - 3.11 - 3.12

    Yousef Alshammary · 41問 · 11ヶ月前

    mod 3 3.10 - 3.11 - 3.12

    mod 3 3.10 - 3.11 - 3.12

    41問 • 11ヶ月前
    Yousef Alshammary

    mod 3 3.13 - 3.14 - 3.15

    mod 3 3.13 - 3.14 - 3.15

    Yousef Alshammary · 39問 · 11ヶ月前

    mod 3 3.13 - 3.14 - 3.15

    mod 3 3.13 - 3.14 - 3.15

    39問 • 11ヶ月前
    Yousef Alshammary

    mod 3 3.16 - 3.17 - 3.18

    mod 3 3.16 - 3.17 - 3.18

    Yousef Alshammary · 27問 · 11ヶ月前

    mod 3 3.16 - 3.17 - 3.18

    mod 3 3.16 - 3.17 - 3.18

    27問 • 11ヶ月前
    Yousef Alshammary

    mod 5 5.1 - EFIS - DAC - A429 - A629 - AND - NAND

    mod 5 5.1 - EFIS - DAC - A429 - A629 - AND - NAND

    Yousef Alshammary · 34問 · 11ヶ月前

    mod 5 5.1 - EFIS - DAC - A429 - A629 - AND - NAND

    mod 5 5.1 - EFIS - DAC - A429 - A629 - AND - NAND

    34問 • 11ヶ月前
    Yousef Alshammary

    mod 5 OR - Buses - Buf Reg - 5.10 - RL - Basic

    mod 5 OR - Buses - Buf Reg - 5.10 - RL - Basic

    Yousef Alshammary · 29問 · 11ヶ月前

    mod 5 OR - Buses - Buf Reg - 5.10 - RL - Basic

    mod 5 OR - Buses - Buf Reg - 5.10 - RL - Basic

    29問 • 11ヶ月前
    Yousef Alshammary

    mod 5 Single - multimund - optical - 5.11 - LCD - 5.12 - PCB - 5.13

    mod 5 Single - multimund - optical - 5.11 - LCD - 5.12 - PCB - 5.13

    Yousef Alshammary · 38問 · 11ヶ月前

    mod 5 Single - multimund - optical - 5.11 - LCD - 5.12 - PCB - 5.13

    mod 5 Single - multimund - optical - 5.11 - LCD - 5.12 - PCB - 5.13

    38問 • 11ヶ月前
    Yousef Alshammary

    mod 5 5.15

    mod 5 5.15

    Yousef Alshammary · 25問 · 11ヶ月前

    mod 5 5.15

    mod 5 5.15

    25問 • 11ヶ月前
    Yousef Alshammary

    mod 5 Numbering System

    mod 5 Numbering System

    Yousef Alshammary · 16問 · 11ヶ月前

    mod 5 Numbering System

    mod 5 Numbering System

    16問 • 11ヶ月前
    Yousef Alshammary

    7.1

    7.1

    Yousef Alshammary · 18問 · 11ヶ月前

    7.1

    7.1

    18問 • 11ヶ月前
    Yousef Alshammary

    7.2

    7.2

    Yousef Alshammary · 11問 · 11ヶ月前

    7.2

    7.2

    11問 • 11ヶ月前
    Yousef Alshammary

    7.3 - 7.4

    7.3 - 7.4

    Yousef Alshammary · 32問 · 11ヶ月前

    7.3 - 7.4

    7.3 - 7.4

    32問 • 11ヶ月前
    Yousef Alshammary

    7.5

    7.5

    Yousef Alshammary · 9問 · 11ヶ月前

    7.5

    7.5

    9問 • 11ヶ月前
    Yousef Alshammary

    7.6 - 7.8

    7.6 - 7.8

    Yousef Alshammary · 8問 · 11ヶ月前

    7.6 - 7.8

    7.6 - 7.8

    8問 • 11ヶ月前
    Yousef Alshammary

    7.9

    7.9

    Yousef Alshammary · 10問 · 11ヶ月前

    7.9

    7.9

    10問 • 11ヶ月前
    Yousef Alshammary

    7.10

    7.10

    Yousef Alshammary · 12問 · 11ヶ月前

    7.10

    7.10

    12問 • 11ヶ月前
    Yousef Alshammary

    7.11

    7.11

    Yousef Alshammary · 7問 · 11ヶ月前

    7.11

    7.11

    7問 • 11ヶ月前
    Yousef Alshammary

    6.3

    6.3

    Yousef Alshammary · 46問 · 11ヶ月前

    6.3

    6.3

    46問 • 11ヶ月前
    Yousef Alshammary

    問題一覧

  • 1

    Level A

    Catastrophic failure

  • 2

    Failure conditions which

    prevent continued safe flight and landing.

  • 3

    Failure may cause crash error or loss of critical function required to safety fly and land aircraft is

    Catastrophic

  • 4

    What is the effect of a level 1 software failure

    Loss of aircraft and /or fatalities

  • 5

    An aircraft system allocated a Criticality Category of Hazardous has software level of

    B

  • 6

    Suppose failure in level E software this will cause

    no effect

  • 7

    Modification to software will be subjected to the same approval procedures as are applied to

    hardware modifications

  • 8

    Collection of data where the computer gets specific information is

    Databases

  • 9

    What is the Software Media

    Device that contains a copy of the software

  • 10

    All passenger seats are addressable means

    by the computer which transmit data through the network directly to individual passenger seat

  • 11

    Failure system in the aircraft according to software error cause a significant reduction is safety margin which cause

    injures to occupants

  • 12

    Which Document provides guidance to aircraft constructors of software

    DO-178B/ED

  • 13

    Which section will summarize the plan and test result

    software Verification plan

  • 14

    Ground loops are prevented by

    ground only one end of the cable screen

  • 15

    When incorporating an aerial cable it must be

    positioned separately from the loom

  • 16

    The avionics bay in the larger aircraft are placed in

    below the floor

  • 17

    Electromagnetic compatibility is achieved by

    Shielding, screening, earthling, bonding and interference filters

  • 18

    In order to maintain HIRF protection, bonding checks between airframe and electrical components carrying voltages greater than 50 volts RMS or DC or main earth return should not exceed

    0.05 ohm

  • 19

    EMC gaskets shielding arrangement used to

    reduce the leakage of electromagnetic energy.

  • 20

    Primary flight display (PFD) and navigation display (ND) are two main display units that together

    make up the EFIS for commercial aircraft.

  • 21

    To reduce HIRF on radio equipment

    ensure all static wicks are in place

  • 22

    HIRF protection of LRUs is provided by

    built in filters and overvoltage circuits

  • 23

    The phase shift between the electric field oscillation and magnetic field oscillation is

    90⁰

  • 24

    When carrying out a bonding check on a surface protected by anodic film

    The anodic film should be removed locally to ensure a good contact

  • 25

    When clamping cable looms containing co-axial cables

    avoid distortion to it, to maintain the dielectric constant

  • 26

    Testing of HIRF on aircraft system is done

    at and during production and testing (initial certification