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B777 - Part 3
50問 • 3年前
  • Angelo Ortiz
  • 通報

    問題一覧

  • 1

    What does the EICAS message "NO LAND 3" mean when FLARE and ROLLOUT armed are displayed on the FMA?

    The autoland system does not have redundancy for triple channel autoland.

  • 2

    Which MCP actions are accomplished during preflight?

    Arm left and right autothrottle, turn left and right FD switches ON, check Bank Limit Switch in AUTO.

  • 3

    What position should the A/P DISENGAGE bar be in during the MCP preflight?

    UP in the A/P engaged position

  • 4

    What is the sequence of steps to use FLCH to climb to FL250 at 280 kts?

    Set FL250 in the ALTITUDE window, push FLCH switch, then set 280 kts in the IAS/MACH window.

  • 5

    What is the sequence of steps to use FLCH to descend to 5000 feet at 240 kts?

    Set 5000 feet in the ALTITUDE window, push FLCH switch, then set 240 kts in the IAS/MACH window.

  • 6

    What is the sequence of steps to change airspeed with VNAV engaged, using speed intervention?

    Push the IAS/MACH selector, then change the IAS/MACH window to the new airspeed

  • 7

    What is the sequence of steps to reduce airspeed with VNAV engaged, using speed intervention?

    Push the IAS/MACH selector, then change the IAS/MACH window to the lower airspeed

  • 8

    With TRK SEL engaged, what is the CORRECT sequence of steps to turn right to heading 150 degrees using the HDG SEL mode?

    Push the HDG/TRK reference switch, verify HDG SEL on the FMA, then rotate the HDG/TRK selector to the right to set 150 in the HDG/TRK window.

  • 9

    With HDG SEL engaged, what is the CORRECT sequence of steps to turn right to track 150 degrees using the TRK SEL mode?

    Push the HDG/TRK reference switch, verify TRK SEL on the FMA, then rotate the HDG/TRK selector to the right to set 150 in the HDG/TRK window.

  • 10

    Which switch engages the autothrottle with the A/T ARM switches in ARM above 400 feet?

    A/T engage switch

  • 11

    When V/S shows in the V/S-FPA window, what are the correct steps to make a 2. 6 degree FPA descent?

    Set new altitude, push VS/FPA reference switch, push VS/FPA switch and set 2. 6 degree flight path angle.

  • 12

    What action resets the autopilot system and warning system, and cancels the AUTOPILOT DISC message?

    Pushing the autopilot disconnect switch a second time.

  • 13

    What switch resets the autothrottle system and also cancels the AUTOTHROTTLE DISC message?

    Autothrottle disconnect switch

  • 14

    Which A/T ARM switch configuration causes the AUTOTHROTTLE R message to display?

    Left switch ON, right switch OFF

  • 15

    What will a second push of the TO/GA switch do during the takeoff above 80 knots, with LNAV and VNAV armed?

    Disarms LNAV and VNAV

  • 16

    What will the autopilot do if you override the control column?

    Disengage

  • 17

    What happens to bank angle protection if the A/P DISENGAGE bar is selected down?

    Bank angle protection is disabled.

  • 18

    Above what altitude can you discontinue a Localizer approach mode by pushing the LOC switch a second time?

    1500 feet RA

  • 19

    Pushing the TOGA switch after takeoff with LNAV and VNAV engaged and the flaps not up causes which of the following conditions?

    LNAV and VNAV remain engaged, the autothrottle engages in THR REF and the takeoff thrust derates are removed.

  • 20

    Pushing the TOGA switch a second time with the glideslope captured below 1500 feet RA causes which of the following conditions?

    Engages the autothrottle in THR REF mode.

  • 21

    Which ATC REQUESTED REPORT CANNOT be armed for automatic downlink to ATC?

    MAINTAINING FL330

  • 22

    What must the aircrew do in order to converse with the mechanic servicing the engine at the engine nacelle?

    Position the SERV INTPH switch to ON

  • 23

    What does illumination of the offside tuning light mean?

    One of the other radio tuning panels is tuning a radio normally tuned by this panel.

  • 24

    What is indicated by an illuminated PAPER light on the flight deck printer?

    The flight deck printer is out of paper or the paper is jammed.

  • 25

    What does the •SELCAL communication EICAS alert message indicate?

    A VHF or HF selective call has been received and is waiting to be answered.

  • 26

    A high-low chime sounds and a •COMM communications alert message appears on EICAS. What action should you take?

    Push the COMM switch on the display select panel and view the uplinked message on the MFD.

  • 27

    Which statement about the VHF radios is true?

    VHF L is configured for voice communication only.

  • 28

    What can the First Officer do to regain audio control if his audio control panel fails?

    Position the OBS AUDIO selector to F/O, then use the Observer's audio control panel.

  • 29

    What is true about ATC data link operation?

    The crew must manually log on to a participating ATC facility

  • 30

    Which of the following data values does NOT provide crew feedback, by turning green, when you comply with an ATC uplink message?

    VOR frequency

  • 31

    What does the •COMM communication EICAS alert message indicate when accompanied by a high-low chime?

    A or B

  • 32

    What does the EICAS message "RADIO TRANSMIT" indicate?

    A VHF or HF radio transmitter is keyed for 30 seconds or more.

  • 33

    Which method of providing a CABIN READY signal to the flight deck is not a normal use of the cabin interphone system?

    By a CABIN ALERT EICAS communications message.

  • 34

    What is indicated by an illuminated FAIL light on the flight deck printer?

    The flight deck printer has failed.

  • 35

    On the ground with both engines shut down, any VHF radio that transmits for more than ___ seconds is automatically disable and dashes appear in the tuning panel frequency window for that radio.

    35

  • 36

    When an HF transmitter is keyed after a frequency change the antenna tunes. While the antenna is being tuned, a tone can be heard through the audio system. How much time must be allowed for the antenna to tune?

    Tuning takes a maximum of 15 seconds.

  • 37

    Which statement about the Radio Tuning Panel is not correct?

    The center radio tuning panel is normally associated with VHF C and HF C.

  • 38

    How many seconds of VHF radio transmission results in an automatic disabling of the transmitter and dashes appearing in the tuning panel frequency window for that radio when on the ground with both engines shut down?

    35 seconds

  • 39

    When an HF transmitter is keyed after a frequency change, the antenna tunes and a tone can be heard through the audio system. How long does the HF radio take to accomplish the tuning?

    Tuning takes a maximum of 15 seconds.

  • 40

    Which statement about the Offside Tuning Light is not correct?

    The center Radio Tuning panel is normally associated with VHF C and HF C.

  • 41

    What does a series of dashes in both windows of a Radio Tuning Panel indicate?

    Dashes appear in both windows when the selected radio is failed or has been disconnected.

  • 42

    What automatic switching will occur if you start the APU with primary and secondary external power on the BUS TIE system?

    The APU connects to the BUS TIE and replaces secondary external power on the left main bus.

  • 43

    What will occur if a single IDG is powering both buses, and the PRIMARY EXTERNAL POWER switch is selected ON?

    Primary external power connects to both busses and the IDG power source is removed.

  • 44

    How can you power the ground handling bus before shutdown if primary external power is not available?

    Start the APU.

  • 45

    Which bus operates only on the ground?

    The ground handling bus

  • 46

    What is the primary source of DC power during normal flight?

    Transformer rectifier units

  • 47

    What provides DC power on this airplane?

    Transformer rectifier units

  • 48

    When does the right transfer bus isolate from the right main bus?

    When system configures to autoland

  • 49

    What is the electrical configuration during autoland?

    The right transfer bus isolates from the right main AC bus.

  • 50

    What is the primary electrical power source for flight control system?

    Permanent magnet generators

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    問題一覧

  • 1

    What does the EICAS message "NO LAND 3" mean when FLARE and ROLLOUT armed are displayed on the FMA?

    The autoland system does not have redundancy for triple channel autoland.

  • 2

    Which MCP actions are accomplished during preflight?

    Arm left and right autothrottle, turn left and right FD switches ON, check Bank Limit Switch in AUTO.

  • 3

    What position should the A/P DISENGAGE bar be in during the MCP preflight?

    UP in the A/P engaged position

  • 4

    What is the sequence of steps to use FLCH to climb to FL250 at 280 kts?

    Set FL250 in the ALTITUDE window, push FLCH switch, then set 280 kts in the IAS/MACH window.

  • 5

    What is the sequence of steps to use FLCH to descend to 5000 feet at 240 kts?

    Set 5000 feet in the ALTITUDE window, push FLCH switch, then set 240 kts in the IAS/MACH window.

  • 6

    What is the sequence of steps to change airspeed with VNAV engaged, using speed intervention?

    Push the IAS/MACH selector, then change the IAS/MACH window to the new airspeed

  • 7

    What is the sequence of steps to reduce airspeed with VNAV engaged, using speed intervention?

    Push the IAS/MACH selector, then change the IAS/MACH window to the lower airspeed

  • 8

    With TRK SEL engaged, what is the CORRECT sequence of steps to turn right to heading 150 degrees using the HDG SEL mode?

    Push the HDG/TRK reference switch, verify HDG SEL on the FMA, then rotate the HDG/TRK selector to the right to set 150 in the HDG/TRK window.

  • 9

    With HDG SEL engaged, what is the CORRECT sequence of steps to turn right to track 150 degrees using the TRK SEL mode?

    Push the HDG/TRK reference switch, verify TRK SEL on the FMA, then rotate the HDG/TRK selector to the right to set 150 in the HDG/TRK window.

  • 10

    Which switch engages the autothrottle with the A/T ARM switches in ARM above 400 feet?

    A/T engage switch

  • 11

    When V/S shows in the V/S-FPA window, what are the correct steps to make a 2. 6 degree FPA descent?

    Set new altitude, push VS/FPA reference switch, push VS/FPA switch and set 2. 6 degree flight path angle.

  • 12

    What action resets the autopilot system and warning system, and cancels the AUTOPILOT DISC message?

    Pushing the autopilot disconnect switch a second time.

  • 13

    What switch resets the autothrottle system and also cancels the AUTOTHROTTLE DISC message?

    Autothrottle disconnect switch

  • 14

    Which A/T ARM switch configuration causes the AUTOTHROTTLE R message to display?

    Left switch ON, right switch OFF

  • 15

    What will a second push of the TO/GA switch do during the takeoff above 80 knots, with LNAV and VNAV armed?

    Disarms LNAV and VNAV

  • 16

    What will the autopilot do if you override the control column?

    Disengage

  • 17

    What happens to bank angle protection if the A/P DISENGAGE bar is selected down?

    Bank angle protection is disabled.

  • 18

    Above what altitude can you discontinue a Localizer approach mode by pushing the LOC switch a second time?

    1500 feet RA

  • 19

    Pushing the TOGA switch after takeoff with LNAV and VNAV engaged and the flaps not up causes which of the following conditions?

    LNAV and VNAV remain engaged, the autothrottle engages in THR REF and the takeoff thrust derates are removed.

  • 20

    Pushing the TOGA switch a second time with the glideslope captured below 1500 feet RA causes which of the following conditions?

    Engages the autothrottle in THR REF mode.

  • 21

    Which ATC REQUESTED REPORT CANNOT be armed for automatic downlink to ATC?

    MAINTAINING FL330

  • 22

    What must the aircrew do in order to converse with the mechanic servicing the engine at the engine nacelle?

    Position the SERV INTPH switch to ON

  • 23

    What does illumination of the offside tuning light mean?

    One of the other radio tuning panels is tuning a radio normally tuned by this panel.

  • 24

    What is indicated by an illuminated PAPER light on the flight deck printer?

    The flight deck printer is out of paper or the paper is jammed.

  • 25

    What does the •SELCAL communication EICAS alert message indicate?

    A VHF or HF selective call has been received and is waiting to be answered.

  • 26

    A high-low chime sounds and a •COMM communications alert message appears on EICAS. What action should you take?

    Push the COMM switch on the display select panel and view the uplinked message on the MFD.

  • 27

    Which statement about the VHF radios is true?

    VHF L is configured for voice communication only.

  • 28

    What can the First Officer do to regain audio control if his audio control panel fails?

    Position the OBS AUDIO selector to F/O, then use the Observer's audio control panel.

  • 29

    What is true about ATC data link operation?

    The crew must manually log on to a participating ATC facility

  • 30

    Which of the following data values does NOT provide crew feedback, by turning green, when you comply with an ATC uplink message?

    VOR frequency

  • 31

    What does the •COMM communication EICAS alert message indicate when accompanied by a high-low chime?

    A or B

  • 32

    What does the EICAS message "RADIO TRANSMIT" indicate?

    A VHF or HF radio transmitter is keyed for 30 seconds or more.

  • 33

    Which method of providing a CABIN READY signal to the flight deck is not a normal use of the cabin interphone system?

    By a CABIN ALERT EICAS communications message.

  • 34

    What is indicated by an illuminated FAIL light on the flight deck printer?

    The flight deck printer has failed.

  • 35

    On the ground with both engines shut down, any VHF radio that transmits for more than ___ seconds is automatically disable and dashes appear in the tuning panel frequency window for that radio.

    35

  • 36

    When an HF transmitter is keyed after a frequency change the antenna tunes. While the antenna is being tuned, a tone can be heard through the audio system. How much time must be allowed for the antenna to tune?

    Tuning takes a maximum of 15 seconds.

  • 37

    Which statement about the Radio Tuning Panel is not correct?

    The center radio tuning panel is normally associated with VHF C and HF C.

  • 38

    How many seconds of VHF radio transmission results in an automatic disabling of the transmitter and dashes appearing in the tuning panel frequency window for that radio when on the ground with both engines shut down?

    35 seconds

  • 39

    When an HF transmitter is keyed after a frequency change, the antenna tunes and a tone can be heard through the audio system. How long does the HF radio take to accomplish the tuning?

    Tuning takes a maximum of 15 seconds.

  • 40

    Which statement about the Offside Tuning Light is not correct?

    The center Radio Tuning panel is normally associated with VHF C and HF C.

  • 41

    What does a series of dashes in both windows of a Radio Tuning Panel indicate?

    Dashes appear in both windows when the selected radio is failed or has been disconnected.

  • 42

    What automatic switching will occur if you start the APU with primary and secondary external power on the BUS TIE system?

    The APU connects to the BUS TIE and replaces secondary external power on the left main bus.

  • 43

    What will occur if a single IDG is powering both buses, and the PRIMARY EXTERNAL POWER switch is selected ON?

    Primary external power connects to both busses and the IDG power source is removed.

  • 44

    How can you power the ground handling bus before shutdown if primary external power is not available?

    Start the APU.

  • 45

    Which bus operates only on the ground?

    The ground handling bus

  • 46

    What is the primary source of DC power during normal flight?

    Transformer rectifier units

  • 47

    What provides DC power on this airplane?

    Transformer rectifier units

  • 48

    When does the right transfer bus isolate from the right main bus?

    When system configures to autoland

  • 49

    What is the electrical configuration during autoland?

    The right transfer bus isolates from the right main AC bus.

  • 50

    What is the primary electrical power source for flight control system?

    Permanent magnet generators