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A-320 Chapter № 3. Autoflight
40問 • 1ヶ月前
  • Popovich
    • 通報

    問題一覧

  • 1

    3.1.* What information is supplied by the IR's and displayed on the PFD?

    A. Heading, attitude, and vertical speed

  • 2

    3.2.* A/THR in white color on the FMA means that A/THR is:

    C. Active

  • 3

    3.3.* What does the MCDU message “CHECK DATA BASE CYCLE” mean?

    A.The current date does not match the effective date of the active database

  • 4

    3.4.* Short term actions are actions through ______:

    B. FCU

  • 5

    3.5.* Long term actions are actions through ______:

    A. MCDU

  • 6

    3.6.* What does the MCDU “CHECK WEIGHT” message mean?

    B. FMC and FAC GW differs by more than 7t in flight

  • 7

    3.7.* The A/THR in CLB detent providing maximum available CLB thrust. Is it possible to obtain some additional thrust?

    B. Yes, by moving the thrust levers forward from the CL detent

  • 8

    3.8.* What is the minimum height for use of the Autopilot after liftoff?

    C. 100 ft

  • 9

    3.9.* Can the Autopilot be used for OEI Approach and Autoland?

    A. Yes

  • 10

    3.10.* During the takeoff phase the AP/FD SRS Mode:

    A. Provides guidance to maintain speed target of V2+10kt up to acceleration altitude

  • 11

    3.11.* What is the minimum height for use of A/P when CAT 2 or CAT 3 is not displayed on the FMA?

    B. 160 ft

  • 12

    3.12.* What is Alpha floor protection?

    A. The protection against aircraft stall and windshear. It has priority over all other protections

  • 13

    3.13.* When Alpha floor is activated, what power setting is automatically commanded and what FMA annunciation would appear in Column one?

    A. TOGA / A. FLOOR

  • 14

    3.14.* During NPA with FINAL APP mode in active and AP on, aircraft descends below MDA. What will happen to FMGC?

    A. At MDA -50 ft, if the AP is still engaged, DISCONNECT AP FOR LDG message pulses on the FMA to remind the flight crew that automatic landing is not available

  • 15

    3.15.* Holding the instinctive disconnect pushbutton on thrust levers for more than 15 seconds will:

    C. Disengage the A/THR (including Alpha Floor) for the remainder of the flight

  • 16

    3.16.* During the flight with active A/THR, the speed knob is pulled and turned to a selected speed which is lower than Alpha Prot. What speed will be maintained by the aircraft?

    A. VLS

  • 17

    3.17.* Default managed climb speed above 10,000 feet:

    B. Econ climb speed

  • 18

    3.19.* If two AP’s are engaged, what FMGC is master?

    A. FMGC1

  • 19

    3.20.* If no AP is engaged, and the FDs 1+2 are on, what FMGC is master?

    A. FMGC1

  • 20

    3.21.* If no AP/FD is engaged, which FMGC controls the Auto Thrust?

    A. FMGC1

  • 21

    3.22.* OPP FMGC IN PROCESS message is displayed on both MCDU scratchpads. FMGC operation is in:

    B. Single mode

  • 22

    3.23.* What is the Dual mode of FMGC operation?

    A. Both FMGCs are synchronized: each performs its own computations and exchanges data with the other through a crosstalk bus

  • 23

    3.24.* The INDEPENDENT OPERATION message is displayed on both MCDU scratchpads.

    A. Both FMGCs work independently and are linked only to peripherals on their own sides of the flight deck (“onside” peripherals)

  • 24

    3.25.* The “MAP NOT AVAIL” message displayed on ND indicates that:

    B. Either associated FMGC has failed or delivered an invalid aircraft position

  • 25

    3.26.* In what case the "NAV ACCUR UPGRAD" (or DOWNGRAD) message appears on the MCDU and the ND display?

    A. When one FMGC changes the NAV accuracy from LOW to HIGH (or HIGH to LOW)

  • 26

    3.27.* Radio navaids may be tuned in several ways:

    A. Three ways: Automatically by FMGC; Manually via the MCDU RAD NAV page; manually via the RMP

  • 27

    3.28.* Is it possible to manually tune radio navaids on the MCDU RAD NAV page and the RMP simultaneously?

    No

  • 28

    3.29.* MCDU scratchpad message: “SPECIF VOR-D UNAVAIL” appears when:

    A. The VOR or VOR/DME to be autotuned has previously been deselected by the flight crew

  • 29

    3.30.* MCDU scratchpad message: “RWY/LS MISMATCH” appears when

    C. The LS frequency entered on the RAD NAV page does not match the LS associated with the destination runway

  • 30

    3.31.* With FPV on, FD’s off, will the FD bars be automatically restored on the PFD?

    A. In SRS | GA TRK modes during go-around

  • 31

    3.32.* When the aircraft overflies a flight plan discontinuity with the NAV mode:

    A. The NAV mode automatically reverts to the HDG (TRK) mode

  • 32

    3.33.* Choose the correct FMA during descent:

    C. THR.IDLE | DES | NAV

  • 33

    3.34.* The yaw bar is displayed in green on the PFD:

    A. In RWY mode on takeoff, in FLARE and ROLL OUT modes at landing, below 30 ft RA and if a localizer signal is available

  • 34

    3.35.* The energy circle symbol on the ND is:

    A. Only displayed if the lateral guidance mode is HDG or TRACK

  • 35

    3.36.* Choose the correct FMA during climb:

    C. THR.CLB | CLB | NAV

  • 36

    3.37.* Energy circle symbol on the ND represents:

    A. The required distance to land

  • 37

    3.38.* In case of engine failure after V1 bank angle is limited to_____ up to maneuvering speed minus_____:

    А. 15deg/10kts

  • 38

    3.39.* The AP/FD TCAS mode:

    A. Guides the A/C through autopilot in case of a TCAS RA

  • 39

    3.40.* How does the AP/FD TCAS mode become active?

    B. It automatically engages when a Resolution Advisory (RA) is triggered

  • 40

    3.41.* How does a flight crew knows that the AP/FD TCAS mode will be available in case of Resolution Advisory?

    C. By checking the FMA to have TCAS mode armed in blue in case of TA

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    問題一覧

  • 1

    3.1.* What information is supplied by the IR's and displayed on the PFD?

    A. Heading, attitude, and vertical speed

  • 2

    3.2.* A/THR in white color on the FMA means that A/THR is:

    C. Active

  • 3

    3.3.* What does the MCDU message “CHECK DATA BASE CYCLE” mean?

    A.The current date does not match the effective date of the active database

  • 4

    3.4.* Short term actions are actions through ______:

    B. FCU

  • 5

    3.5.* Long term actions are actions through ______:

    A. MCDU

  • 6

    3.6.* What does the MCDU “CHECK WEIGHT” message mean?

    B. FMC and FAC GW differs by more than 7t in flight

  • 7

    3.7.* The A/THR in CLB detent providing maximum available CLB thrust. Is it possible to obtain some additional thrust?

    B. Yes, by moving the thrust levers forward from the CL detent

  • 8

    3.8.* What is the minimum height for use of the Autopilot after liftoff?

    C. 100 ft

  • 9

    3.9.* Can the Autopilot be used for OEI Approach and Autoland?

    A. Yes

  • 10

    3.10.* During the takeoff phase the AP/FD SRS Mode:

    A. Provides guidance to maintain speed target of V2+10kt up to acceleration altitude

  • 11

    3.11.* What is the minimum height for use of A/P when CAT 2 or CAT 3 is not displayed on the FMA?

    B. 160 ft

  • 12

    3.12.* What is Alpha floor protection?

    A. The protection against aircraft stall and windshear. It has priority over all other protections

  • 13

    3.13.* When Alpha floor is activated, what power setting is automatically commanded and what FMA annunciation would appear in Column one?

    A. TOGA / A. FLOOR

  • 14

    3.14.* During NPA with FINAL APP mode in active and AP on, aircraft descends below MDA. What will happen to FMGC?

    A. At MDA -50 ft, if the AP is still engaged, DISCONNECT AP FOR LDG message pulses on the FMA to remind the flight crew that automatic landing is not available

  • 15

    3.15.* Holding the instinctive disconnect pushbutton on thrust levers for more than 15 seconds will:

    C. Disengage the A/THR (including Alpha Floor) for the remainder of the flight

  • 16

    3.16.* During the flight with active A/THR, the speed knob is pulled and turned to a selected speed which is lower than Alpha Prot. What speed will be maintained by the aircraft?

    A. VLS

  • 17

    3.17.* Default managed climb speed above 10,000 feet:

    B. Econ climb speed

  • 18

    3.19.* If two AP’s are engaged, what FMGC is master?

    A. FMGC1

  • 19

    3.20.* If no AP is engaged, and the FDs 1+2 are on, what FMGC is master?

    A. FMGC1

  • 20

    3.21.* If no AP/FD is engaged, which FMGC controls the Auto Thrust?

    A. FMGC1

  • 21

    3.22.* OPP FMGC IN PROCESS message is displayed on both MCDU scratchpads. FMGC operation is in:

    B. Single mode

  • 22

    3.23.* What is the Dual mode of FMGC operation?

    A. Both FMGCs are synchronized: each performs its own computations and exchanges data with the other through a crosstalk bus

  • 23

    3.24.* The INDEPENDENT OPERATION message is displayed on both MCDU scratchpads.

    A. Both FMGCs work independently and are linked only to peripherals on their own sides of the flight deck (“onside” peripherals)

  • 24

    3.25.* The “MAP NOT AVAIL” message displayed on ND indicates that:

    B. Either associated FMGC has failed or delivered an invalid aircraft position

  • 25

    3.26.* In what case the "NAV ACCUR UPGRAD" (or DOWNGRAD) message appears on the MCDU and the ND display?

    A. When one FMGC changes the NAV accuracy from LOW to HIGH (or HIGH to LOW)

  • 26

    3.27.* Radio navaids may be tuned in several ways:

    A. Three ways: Automatically by FMGC; Manually via the MCDU RAD NAV page; manually via the RMP

  • 27

    3.28.* Is it possible to manually tune radio navaids on the MCDU RAD NAV page and the RMP simultaneously?

    No

  • 28

    3.29.* MCDU scratchpad message: “SPECIF VOR-D UNAVAIL” appears when:

    A. The VOR or VOR/DME to be autotuned has previously been deselected by the flight crew

  • 29

    3.30.* MCDU scratchpad message: “RWY/LS MISMATCH” appears when

    C. The LS frequency entered on the RAD NAV page does not match the LS associated with the destination runway

  • 30

    3.31.* With FPV on, FD’s off, will the FD bars be automatically restored on the PFD?

    A. In SRS | GA TRK modes during go-around

  • 31

    3.32.* When the aircraft overflies a flight plan discontinuity with the NAV mode:

    A. The NAV mode automatically reverts to the HDG (TRK) mode

  • 32

    3.33.* Choose the correct FMA during descent:

    C. THR.IDLE | DES | NAV

  • 33

    3.34.* The yaw bar is displayed in green on the PFD:

    A. In RWY mode on takeoff, in FLARE and ROLL OUT modes at landing, below 30 ft RA and if a localizer signal is available

  • 34

    3.35.* The energy circle symbol on the ND is:

    A. Only displayed if the lateral guidance mode is HDG or TRACK

  • 35

    3.36.* Choose the correct FMA during climb:

    C. THR.CLB | CLB | NAV

  • 36

    3.37.* Energy circle symbol on the ND represents:

    A. The required distance to land

  • 37

    3.38.* In case of engine failure after V1 bank angle is limited to_____ up to maneuvering speed minus_____:

    А. 15deg/10kts

  • 38

    3.39.* The AP/FD TCAS mode:

    A. Guides the A/C through autopilot in case of a TCAS RA

  • 39

    3.40.* How does the AP/FD TCAS mode become active?

    B. It automatically engages when a Resolution Advisory (RA) is triggered

  • 40

    3.41.* How does a flight crew knows that the AP/FD TCAS mode will be available in case of Resolution Advisory?

    C. By checking the FMA to have TCAS mode armed in blue in case of TA