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Module 5 1
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  • 問題数 71 • 11/11/2024

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    問題一覧

  • 1

    The function of ring laser gyro is to measure

    angular rotation

  • 2

    Electromagnetic compatibility is achieved by

    Shielding, screening, earthling, bonding and interference filters

  • 3

    The colour that produced by DU which used during inflight engine starting and cross bleed message is

    Magenta

  • 4

    The color used for middle marker is

    amber

  • 5

    A typical fiber optic connector is

    coupling type with lens fitted

  • 6

    The ACARS is used to

    transmit or receive automatically or manually generated reports or messages to or from a ground station

  • 7

    The cabin crew can get access to the cabin applications via

    flight attendant panel or internal wireless data link

  • 8

    Suppose failure in level E software this will cause

    no effect

  • 9

    Which section will summarize the plan and test result:

    software Verification plan

  • 10

    Software can be modified by

    using the same rules as to modifications to hardware

  • 11

    If the magnetic field is parallel to the Y plate the direction of beam movement will be

    vertical axis

  • 12

    Rudder control

    yaw

  • 13

    When handling PCBs labeled ESDS the precaution are taken

    isolate electrical power before installing on aircraft

  • 14

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

    injures to occupants

  • 15

    Touching connector pins or other exposed conductors could cause

    damage to component may result

  • 16

    When incorporating an aerial cable it must be

    positioned separately from the loom

  • 17

    The angle between the reflected wave and the normal is called

    the angle of reflection

  • 18

    The refractive index of a core that is uniform and undergoes and abrupt change at the core- cladding boundary is what type of fiber

    Step index fiber

  • 19

    Before removing an assembly from an aircraft, with regards to HIRF, you must first ensure that

    there is minimum current flow between you and the assembly

  • 20

    Fibre Optic basic functions

    To convert an electrical input signal to an optical signal ,To send the optical signal over an optical fibre ,To convert the optical signal back to an electrical signal

  • 21

    The American Global Positioning System (GPS), also called NAVSTAR

    uses 24 satellites, with three or more spares, in orbit at any one time

  • 22

    All the information necessary for maintenance and trouble shooting is memorized in

    Non Volatile Memory

  • 23

    Fly-By-Wire system Flight control surfaces are all

    Electrically-controlled, Hydraulically-activatedElectrically-controlled, Hydraulically-activated

  • 24

    In fly by wire the maximum deflection of aileron is

    25degree

  • 25

    The devices Ability to dissipate the energy of discharge or withstand current levels involved is known as

    device ESD sensitivity. Or ESD susceptibility

  • 26

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

    90⁰

  • 27

    The refractive index of the core varies gradually as a function of radial distance from the fibre centre this is

    graded - index fibre

  • 28

    In fly by wire how many flight control computer are there

    seven computers

  • 29

    Fibre optic cable consists of

    a silica glass core with a cladding having a lower refractive index

  • 30

    The code for red colour in RGB colour production is

    100

  • 31

    Collection of data where the computer gets specific information is

    Databases

  • 32

    How many accelerometers are there in the INS system

    two accelerometers

  • 33

    The core size which is typically around 8 to 10 micrometers is related to

    Multimode Fibres

  • 34

    What is the Software Media

    Device that contains a copy of the software

  • 35

    In airbus core on board information system (OIS) a servicing tool used for the refueling operation is a part of

    avionics domain

  • 36

    The global positioning system (GPS) use the same principle as

    DME

  • 37

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

    make up the EFIS for commercial aircraft

  • 38

    What is the effect of a level 1 software failure

    Loss of aircraft and /or fatalities

  • 39

    Level A

    Catastrophic failure

  • 40

    The function of ring laser gyro is to measure

    angular rotation

  • 41

    F

    ailure conditions which prevent continued safe flight and landing

  • 42

    Ground loops are prevented by

    ground only one end of the

  • 43

    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

  • 44

    Rudder control

    yaw

  • 45

    Which Document provides guidance to aircraft constructors of software

    DO-178B/ED

  • 46

    All passenger seats are addressable means

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

  • 47

    In TCAS II the voice command – climb, crossing climb-means

    Climb at 1500 ft./min through the intruders altitude

  • 48

    The white colour production from the three primary colours represented by

    -111

  • 49

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

    Catastrophic

  • 50

    To reduce HIRF on radio equipment

    ensure all static wicks are in place

  • 51

    The Ribbon cables design has

    the highest fiber capacity, it can hold 204 fibers in a 0.5 inch cable

  • 52

    Before removing a card, electrical power sources should be

    isolated

  • 53

    Laser gyros, accelerometer and power supply output, computer and memory operation , and temperature parameters continually monitored by

    built-in test equipment (BITE)

  • 54

    Aircraft communication addressing and reporting systems is used to

    download aircraft status reports

  • 55

    Unlike the black and white CRT the colour CRT has

    three electron guns each dedicated to one of the primary colours, red, green, or blue

  • 56

    A single mode fibre operates best with what type of light source

    Laser

  • 57

    What are interrogator transmitter and receiver frequencies

    1030 MHz and 1090 MHz

  • 58

    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

  • 59

    According to GPS providing correct timing each satellite carries

    a very accurate atomic clock

  • 60

    What kind of light is used in fibre optic systems

    Infrared

  • 61

    The resistance of the wrist strap used as part of uni-static precaution should be

    250 kilohm- 1.5 megohms

  • 62

    In TCAS IF the monitoring system detects a problem

    it switching off the interrogator warns the crew and sends mode S message to ground interrogation

  • 63

    Testing of HIRF on aircraft system is done

    at and during production and testing (initial certification

  • 64

    A computer which is used as a primary source of information or data is called

    reference computer

  • 65

    Memory that retains data when power is removed is

    non-volatile memory

  • 66

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

    B

  • 67

    HIRF protection of LRUs is provided by

    built in filters and overvoltage circuits

  • 68

    When clamping cable looms containing co-axial cables

    avoid distortion to it, to maintain the dielectric constant.avoid distortion to it, to maintain the dielectric constant

  • 69

    The system which calculates a vertical profile that giver the shortest possible flying time at the lowest fuel consumption is

    FMS

  • 70

    The avionics bay in the larger aircraft are placed in

    below the floor

  • 71

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

    hardware modifications