暗記メーカー

暗記メーカー

​
ログイン
A-320 Chapter № 15. Navigation and Surveillance
30問 • 1ヶ月前
  • Popovich
    • 通報

    問題一覧

  • 1

    15.1.* The ON BAT amber light comes on when:

    A. At least one ADIRU is supplied by Batteries or for a few seconds at the beginning of a complete IRS alignment.

  • 2

    15.2.* The ATT HDG and AIR DATA selectors on the Pedestal switching panel in NORM position indicate that:

    B. ADIRU1 is supplying data to PFD1 and ND1; ADIRU2 is supplying data to PFD2 and ND2

  • 3

    15.3.* What action is necessary to recover air data indications on PFD1 if ADR1 is lost?

    C. Switching the AIR DATA knob on the switching panel to CAPT 3

  • 4

    15.4.* When the Thrust Levers are moved to the takeoff position, the FMGS updates its position at takeoff using:

    C. The Navigation Database and the Takeoff Runway entered into the MCDU by the pilot

  • 5

    15.5.* Cost Index = 0 (zero) corresponds to:

    A. Minimum fuel consumption (max range)

  • 6

    15.6.* During a turnaround, you notice that there is a residual ground speed on both NDs. How do you correct this?

    C. It is possible to carry out a fast alignment by turning off and on all 3 ADIRs within 5 seconds

  • 7

    15.7.* If the FMGC detects low-navigation accuracy, then:

    B. The enhanced modes of EGPWS are automatically deactivated, while 5 GPWS basic modes remain active

  • 8

    15.8.* What sources could be used by the FMGC to compute its own radio position?

    C. DME/DME, VOR/DME, LOC, and their combinations

  • 9

    15.9.* At what height does the RA indication appear on PFD?

    C. 2500 feet

  • 10

    15.10.* Can the crew depress the RMP NAV pushbutton, and use the RMP for navigation simultaneously with FMGC autotuning?

    B. No, RMP backup tuning supersedes the autotuning function of both FMGCs

  • 11

    15.11.* Will the aircraft capture and navigate via the ILS signals, if the LS push button on the FCU is not pushed?

    Yes

  • 12

    15.12.* Selection of the correct takeoff runway on the FMGC prior to each flight is necessary because:

    C. Selection of the correct runway permits the FMGC to update its position at takeoff

  • 13

    15.13.* GPWS aural and visual warnings cannot be inhibited.

    False

  • 14

    15.14.* The speed scale must be replaced by Back-up Speed Scale in case of:

    C. Three ADRs failure

  • 15

    15.15.* All Navaids are normally autotuned by:

    B. FMGC

  • 16

    15.16.* ILS 1 information is displayed on ______ when operating in the rose ILS mode:

    C. PFD 1 & ND 2

  • 17

    15.17.* The intruders are classified as:

    A. 1- RA, 2 - TA, 3 - proximate, 4 – other

  • 18

    15.18.* When TCAS system will automatically select TA ONLY mode even if TCAS mode selector is in TA/RA position?

    B. Below 1000ft AGL

  • 19

    15.19.* What information will be provided on NDs if the flight crew set the TRAFFIC selector to THRT on ATC/TCAS panel?

    A. Intruders are displayed only if a TA or RA is present, and they are within 2700ft above and 2700ft below the aircraft

  • 20

    15.20.* During cockpit preparation you need to check the altitude indications on the PFDs. The maximum difference between both PFDs is:

    A. 20 feet

  • 21

    15.21.* For RVSM operation, check that the difference between each altitude indication displayed on PFDs (in the QNH reference) and the airport elevation is less than:

    C. 75 feet

  • 22

    15.22.* The ROPS is designed to alert the flight crew in the case of potential runway overrun situation for:

    A. dry and wet runway

  • 23

    15.23.* If during final approach the “IF WET: RWY TOO SHORT” amber message displayed on the PFD and the runway condition is wet or contaminated, the flight crew:

    C. must perform a go-around

  • 24

    15.24.* If during final approach, the IF WET: RWY TOO SHORT amber message is displayed on the PFD and the runway condition is dry, the flight crew:

    B. can disregard the message

  • 25

    15.25.* If during final approach, the RWY TOO SHORT red message is displayed on the PFD, the flight crew:

    B. must perform a go-around

  • 26

    15.26.* The ATSAW function does not modify the TCAS function.

    True

  • 27

    15.27.* The ATSAW function enables:

    C. to display enhanced information on the surrounding traffic

  • 28

    15.28.* The ATSAW detection capability is limited to aircraft flying within a maximum range of:

    C. 30 NM on either side

  • 29

    15.29.* The ATSAW detection capability is limited to aircraft flying within:

    B. 100 NM longitudinally

  • 30

    15.30.* The ATSAW detection capability is limited to aircraft flying within a maximum altitude range of:

    C. 9 900 ft (above and below the aircraft)

    • LIMITATION

    LIMITATION

    Popovich · 30問 · 2年前

    LIMITATION

    LIMITATION

    30問 • 2年前
    Popovich

    ВК РУз

    ВК РУз

    Popovich · 37問 · 1ヶ月前

    ВК РУз

    ВК РУз

    37問 • 1ヶ月前
    Popovich

    A-320 Chapter № 1. Aircraft general

    A-320 Chapter № 1. Aircraft general

    Popovich · 7問 · 1ヶ月前

    A-320 Chapter № 1. Aircraft general

    A-320 Chapter № 1. Aircraft general

    7問 • 1ヶ月前
    Popovich

    A-320 Chapter № 2. Air Conditioning / Pressurization / Ventilation

    A-320 Chapter № 2. Air Conditioning / Pressurization / Ventilation

    Popovich · 31問 · 1ヶ月前

    A-320 Chapter № 2. Air Conditioning / Pressurization / Ventilation

    A-320 Chapter № 2. Air Conditioning / Pressurization / Ventilation

    31問 • 1ヶ月前
    Popovich

    A-320 Chapter № 3. Autoflight

    A-320 Chapter № 3. Autoflight

    Popovich · 40問 · 1ヶ月前

    A-320 Chapter № 3. Autoflight

    A-320 Chapter № 3. Autoflight

    40問 • 1ヶ月前
    Popovich

    A-320 Chapter № 4. Communication

    A-320 Chapter № 4. Communication

    Popovich · 18問 · 1ヶ月前

    A-320 Chapter № 4. Communication

    A-320 Chapter № 4. Communication

    18問 • 1ヶ月前
    Popovich

    A-320 Chapter № 5. Electrical

    A-320 Chapter № 5. Electrical

    Popovich · 26問 · 1ヶ月前

    A-320 Chapter № 5. Electrical

    A-320 Chapter № 5. Electrical

    26問 • 1ヶ月前
    Popovich

    A-320 Chapter № 6. Equipment

    A-320 Chapter № 6. Equipment

    Popovich · 7問 · 1ヶ月前

    A-320 Chapter № 6. Equipment

    A-320 Chapter № 6. Equipment

    7問 • 1ヶ月前
    Popovich

    A-320 Chapter № 7. Fire protection

    A-320 Chapter № 7. Fire protection

    Popovich · 20問 · 1ヶ月前

    A-320 Chapter № 7. Fire protection

    A-320 Chapter № 7. Fire protection

    20問 • 1ヶ月前
    Popovich

    A-320 Chapter № 8. Flight Controls

    A-320 Chapter № 8. Flight Controls

    Popovich · 42問 · 1ヶ月前

    A-320 Chapter № 8. Flight Controls

    A-320 Chapter № 8. Flight Controls

    42問 • 1ヶ月前
    Popovich

    A-320 Chapter № 9. Fuel

    A-320 Chapter № 9. Fuel

    Popovich · 21問 · 1ヶ月前

    A-320 Chapter № 9. Fuel

    A-320 Chapter № 9. Fuel

    21問 • 1ヶ月前
    Popovich

    A-320 Chapter № 10. Hydraulic

    A-320 Chapter № 10. Hydraulic

    Popovich · 17問 · 1ヶ月前

    A-320 Chapter № 10. Hydraulic

    A-320 Chapter № 10. Hydraulic

    17問 • 1ヶ月前
    Popovich

    A-320 Chapter № 11. Ice and Rain

    A-320 Chapter № 11. Ice and Rain

    Popovich · 17問 · 1ヶ月前

    A-320 Chapter № 11. Ice and Rain

    A-320 Chapter № 11. Ice and Rain

    17問 • 1ヶ月前
    Popovich

    A-320 Chapter № 12. Indicating / Recording

    A-320 Chapter № 12. Indicating / Recording

    Popovich · 38問 · 1ヶ月前

    A-320 Chapter № 12. Indicating / Recording

    A-320 Chapter № 12. Indicating / Recording

    38問 • 1ヶ月前
    Popovich

    A-320 Chapter № 13. Landing gear

    A-320 Chapter № 13. Landing gear

    Popovich · 37問 · 1ヶ月前

    A-320 Chapter № 13. Landing gear

    A-320 Chapter № 13. Landing gear

    37問 • 1ヶ月前
    Popovich

    A-320 Chapter № 14. Lights

    A-320 Chapter № 14. Lights

    Popovich · 11問 · 1ヶ月前

    A-320 Chapter № 14. Lights

    A-320 Chapter № 14. Lights

    11問 • 1ヶ月前
    Popovich

    A-320 Chapter № 16. Oxygen

    A-320 Chapter № 16. Oxygen

    Popovich · 15問 · 1ヶ月前

    A-320 Chapter № 16. Oxygen

    A-320 Chapter № 16. Oxygen

    15問 • 1ヶ月前
    Popovich

    A-320 Chapter № 17. Pneumatic

    A-320 Chapter № 17. Pneumatic

    Popovich · 12問 · 1ヶ月前

    A-320 Chapter № 17. Pneumatic

    A-320 Chapter № 17. Pneumatic

    12問 • 1ヶ月前
    Popovich

    A-320 Chapter № 18. Water / Waste

    A-320 Chapter № 18. Water / Waste

    Popovich · 7問 · 1ヶ月前

    A-320 Chapter № 18. Water / Waste

    A-320 Chapter № 18. Water / Waste

    7問 • 1ヶ月前
    Popovich

    問題一覧

  • 1

    15.1.* The ON BAT amber light comes on when:

    A. At least one ADIRU is supplied by Batteries or for a few seconds at the beginning of a complete IRS alignment.

  • 2

    15.2.* The ATT HDG and AIR DATA selectors on the Pedestal switching panel in NORM position indicate that:

    B. ADIRU1 is supplying data to PFD1 and ND1; ADIRU2 is supplying data to PFD2 and ND2

  • 3

    15.3.* What action is necessary to recover air data indications on PFD1 if ADR1 is lost?

    C. Switching the AIR DATA knob on the switching panel to CAPT 3

  • 4

    15.4.* When the Thrust Levers are moved to the takeoff position, the FMGS updates its position at takeoff using:

    C. The Navigation Database and the Takeoff Runway entered into the MCDU by the pilot

  • 5

    15.5.* Cost Index = 0 (zero) corresponds to:

    A. Minimum fuel consumption (max range)

  • 6

    15.6.* During a turnaround, you notice that there is a residual ground speed on both NDs. How do you correct this?

    C. It is possible to carry out a fast alignment by turning off and on all 3 ADIRs within 5 seconds

  • 7

    15.7.* If the FMGC detects low-navigation accuracy, then:

    B. The enhanced modes of EGPWS are automatically deactivated, while 5 GPWS basic modes remain active

  • 8

    15.8.* What sources could be used by the FMGC to compute its own radio position?

    C. DME/DME, VOR/DME, LOC, and their combinations

  • 9

    15.9.* At what height does the RA indication appear on PFD?

    C. 2500 feet

  • 10

    15.10.* Can the crew depress the RMP NAV pushbutton, and use the RMP for navigation simultaneously with FMGC autotuning?

    B. No, RMP backup tuning supersedes the autotuning function of both FMGCs

  • 11

    15.11.* Will the aircraft capture and navigate via the ILS signals, if the LS push button on the FCU is not pushed?

    Yes

  • 12

    15.12.* Selection of the correct takeoff runway on the FMGC prior to each flight is necessary because:

    C. Selection of the correct runway permits the FMGC to update its position at takeoff

  • 13

    15.13.* GPWS aural and visual warnings cannot be inhibited.

    False

  • 14

    15.14.* The speed scale must be replaced by Back-up Speed Scale in case of:

    C. Three ADRs failure

  • 15

    15.15.* All Navaids are normally autotuned by:

    B. FMGC

  • 16

    15.16.* ILS 1 information is displayed on ______ when operating in the rose ILS mode:

    C. PFD 1 & ND 2

  • 17

    15.17.* The intruders are classified as:

    A. 1- RA, 2 - TA, 3 - proximate, 4 – other

  • 18

    15.18.* When TCAS system will automatically select TA ONLY mode even if TCAS mode selector is in TA/RA position?

    B. Below 1000ft AGL

  • 19

    15.19.* What information will be provided on NDs if the flight crew set the TRAFFIC selector to THRT on ATC/TCAS panel?

    A. Intruders are displayed only if a TA or RA is present, and they are within 2700ft above and 2700ft below the aircraft

  • 20

    15.20.* During cockpit preparation you need to check the altitude indications on the PFDs. The maximum difference between both PFDs is:

    A. 20 feet

  • 21

    15.21.* For RVSM operation, check that the difference between each altitude indication displayed on PFDs (in the QNH reference) and the airport elevation is less than:

    C. 75 feet

  • 22

    15.22.* The ROPS is designed to alert the flight crew in the case of potential runway overrun situation for:

    A. dry and wet runway

  • 23

    15.23.* If during final approach the “IF WET: RWY TOO SHORT” amber message displayed on the PFD and the runway condition is wet or contaminated, the flight crew:

    C. must perform a go-around

  • 24

    15.24.* If during final approach, the IF WET: RWY TOO SHORT amber message is displayed on the PFD and the runway condition is dry, the flight crew:

    B. can disregard the message

  • 25

    15.25.* If during final approach, the RWY TOO SHORT red message is displayed on the PFD, the flight crew:

    B. must perform a go-around

  • 26

    15.26.* The ATSAW function does not modify the TCAS function.

    True

  • 27

    15.27.* The ATSAW function enables:

    C. to display enhanced information on the surrounding traffic

  • 28

    15.28.* The ATSAW detection capability is limited to aircraft flying within a maximum range of:

    C. 30 NM on either side

  • 29

    15.29.* The ATSAW detection capability is limited to aircraft flying within:

    B. 100 NM longitudinally

  • 30

    15.30.* The ATSAW detection capability is limited to aircraft flying within a maximum altitude range of:

    C. 9 900 ft (above and below the aircraft)