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A-320 Chapter № 5. Electrical
26問 • 11ヶ月前
  • Popovich
    • 通報

    問題一覧

  • 1

    5.1.* Normal priority for supplying electrical power to AC busses is:

    C. Engine generators, external power then APU

  • 2

    5.2.* In normal configuration, the electrical power system provides ____ power.

    A. AC

  • 3

    5.3.* The electrical power system is constituted of:

    A. 2 engine generators and 1 APU generator

  • 4

    5.4.* Engine driven generators (GEN 1, GEN 2) supply _____ power.

    A. three phase 115/200V 400Hz

  • 5

    5.5.* The APU generator (APU GEN) supplies _____ power.

    A. three phase 115/200 V 400 Hz

  • 6

    5.6.* The ______ hydraulic system drives an emergency generator.

    A. BLUE

  • 7

    5.7.* The hydraulically driven emergency generator supplies ______ power.

    A. three phase 115/200V 400Hz

  • 8

    5.8.* Each engine-driven generator supplies its associated _____ directly:

    A. AC BUS

  • 9

    5.9.* In flight DC BUS in normally supplied ______ .

    A. via TR

  • 10

    5.10.* In case of a GEN1 or GEN2 failure it will be automatically replaced by:

    A. Other engine generator or APU GEN

  • 11

    5.11.* The RAT is connected directly (mechanically) to the Emergency Generator.

    B. False, The RAT powers the blue hydraulic system, which drives the Emergency generator by means of a hydraulic motor

  • 12

    5.12.* The emergency generator supplies power as long as:

    B. The RAT is deployed, and the aircraft speed is greater than 100kt

  • 13

    5.13.* The BAT FAULT light will illuminate when:

    B. The battery charge limiter is in fault

  • 14

    5.14.* You enter a dark cockpit, what action is necessary before checking the battery voltage?

    C. You have to verify that both batteries are off

  • 15

    5.15.* Having the APU started and EXT PWR pushbutton ON, how can you get the APU generator to power the electrical system?

    B. By pushing the EXT PWR pushbutton, thus disconnecting the external power

  • 16

    5.16.* The purpose of AUTO BUS TIE is to allow either engine-driven IDG to automatically power both main AC buses in the event of a generator loss until either ground power or the APU generator is activated.

    True

  • 17

    5.17.* Limitations associated with disconnecting an IDG:

    C. Never disconnect an IDG unless the engine is running, nor push the IDG disconnect pushbutton for more than 3 seconds

  • 18

    5.18.* What is the significance of the green circuit breakers?

    B. Green circuit breakers are monitored by the ECAM

  • 19

    5.19.* The RAT & EMER GEN red FAULT light illuminates on overhead panel, if:

    A. The EMER GEN is not supplying electrical power when AC BUS 1 and AC BUS 2 are not powered

  • 20

    5.20.* How many times can you reset a circuit breaker?

    B. Once, if authorized by the procedures

  • 21

    5.21.* To perform the computer reset, the related circuit breaker must be pulled, and the flight crew must:

    B. Wait 5 sec before pushing it back

  • 22

    5.22.* Can you reconnect an IDG in flight?

    C. No, it is not possible

  • 23

    5.23.* The battery charging cycle is required if during preliminary cockpit preparation the battery voltage is:

    A. at or below 25.5V

  • 24

    5.24.* Which communication and navigation radios are operational in the Emergency Electrical Configuration with the EMER GEN powering the system?

    A. ACP 1 and 2, VHF 1, HF1, RMP 1, VOR 1, and MMR 1

  • 25

    5.25.* If EXTERNAL power is available and within limits:

    B. The green AVAIL light will illuminate on the EXT PWR push button

  • 26

    5.26.* What source of power may be used for battery charging cycle?

    A. External power

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    問題一覧

  • 1

    5.1.* Normal priority for supplying electrical power to AC busses is:

    C. Engine generators, external power then APU

  • 2

    5.2.* In normal configuration, the electrical power system provides ____ power.

    A. AC

  • 3

    5.3.* The electrical power system is constituted of:

    A. 2 engine generators and 1 APU generator

  • 4

    5.4.* Engine driven generators (GEN 1, GEN 2) supply _____ power.

    A. three phase 115/200V 400Hz

  • 5

    5.5.* The APU generator (APU GEN) supplies _____ power.

    A. three phase 115/200 V 400 Hz

  • 6

    5.6.* The ______ hydraulic system drives an emergency generator.

    A. BLUE

  • 7

    5.7.* The hydraulically driven emergency generator supplies ______ power.

    A. three phase 115/200V 400Hz

  • 8

    5.8.* Each engine-driven generator supplies its associated _____ directly:

    A. AC BUS

  • 9

    5.9.* In flight DC BUS in normally supplied ______ .

    A. via TR

  • 10

    5.10.* In case of a GEN1 or GEN2 failure it will be automatically replaced by:

    A. Other engine generator or APU GEN

  • 11

    5.11.* The RAT is connected directly (mechanically) to the Emergency Generator.

    B. False, The RAT powers the blue hydraulic system, which drives the Emergency generator by means of a hydraulic motor

  • 12

    5.12.* The emergency generator supplies power as long as:

    B. The RAT is deployed, and the aircraft speed is greater than 100kt

  • 13

    5.13.* The BAT FAULT light will illuminate when:

    B. The battery charge limiter is in fault

  • 14

    5.14.* You enter a dark cockpit, what action is necessary before checking the battery voltage?

    C. You have to verify that both batteries are off

  • 15

    5.15.* Having the APU started and EXT PWR pushbutton ON, how can you get the APU generator to power the electrical system?

    B. By pushing the EXT PWR pushbutton, thus disconnecting the external power

  • 16

    5.16.* The purpose of AUTO BUS TIE is to allow either engine-driven IDG to automatically power both main AC buses in the event of a generator loss until either ground power or the APU generator is activated.

    True

  • 17

    5.17.* Limitations associated with disconnecting an IDG:

    C. Never disconnect an IDG unless the engine is running, nor push the IDG disconnect pushbutton for more than 3 seconds

  • 18

    5.18.* What is the significance of the green circuit breakers?

    B. Green circuit breakers are monitored by the ECAM

  • 19

    5.19.* The RAT & EMER GEN red FAULT light illuminates on overhead panel, if:

    A. The EMER GEN is not supplying electrical power when AC BUS 1 and AC BUS 2 are not powered

  • 20

    5.20.* How many times can you reset a circuit breaker?

    B. Once, if authorized by the procedures

  • 21

    5.21.* To perform the computer reset, the related circuit breaker must be pulled, and the flight crew must:

    B. Wait 5 sec before pushing it back

  • 22

    5.22.* Can you reconnect an IDG in flight?

    C. No, it is not possible

  • 23

    5.23.* The battery charging cycle is required if during preliminary cockpit preparation the battery voltage is:

    A. at or below 25.5V

  • 24

    5.24.* Which communication and navigation radios are operational in the Emergency Electrical Configuration with the EMER GEN powering the system?

    A. ACP 1 and 2, VHF 1, HF1, RMP 1, VOR 1, and MMR 1

  • 25

    5.25.* If EXTERNAL power is available and within limits:

    B. The green AVAIL light will illuminate on the EXT PWR push button

  • 26

    5.26.* What source of power may be used for battery charging cycle?

    A. External power