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SplitPDFFile 38

The document contains a series of questions related to the refueling and hydraulic systems of the A320/321 aircraft. It covers topics such as fuel tank sensors, refuel processes, and the operation of hydraulic systems in various scenarios. Specific questions address the functionality of components and responses to system failures during flight.

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kindaichi39
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11 views1 page

SplitPDFFile 38

The document contains a series of questions related to the refueling and hydraulic systems of the A320/321 aircraft. It covers topics such as fuel tank sensors, refuel processes, and the operation of hydraulic systems in various scenarios. Specific questions address the functionality of components and responses to system failures during flight.

Uploaded by

kindaichi39
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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Page: 38

A320/321 Issue : 00 6-2016

QUESTIONS BANK Revision : 01 6-2016

B. All fuel tanks are full, refuel process stopped automatically.


C. Any high level sensor detected fuel.

262.When performing the refuel, defuel, Ground transfer, the R/D electrical circuit is
enable by? (A,B1,B2)
A. Power from the aircraft electrical net work only.
B. Carrying out HI LVL test.
C. Contact R/D panel door switch.

263.What happens when low level is detected in the inner cell? (B1,B2)
A. Inner cell transfer valves open.
B. Inner cell transfer valves close to isolate the inner cells
C. Pumps restart to suck fuel from outer cells.

264.In which cell are the full level sensors fitted? (B1,B2)
A. Inner cells only.
B. Outer cells only.
C. Inner and outer cells.

265.To which tank does the re-circulated fuel returns? (B1,B2)


A. Inner cells.
B. Outer cells.
C. Center tanks.

ATA-29 HYDRAULIC:

266.In flight, if the blue electric pump fails the blue system: (A,B1,B2)
A. Is lost.
B. Can be recovered by the RAT.
C. Can be recovered by the PTU.
D. Both B and C.
267.Which component(s) send a Warning and Fault signals on the blue hydraulic
system? (B1,B2)
A. Only the low air pressure switch
B. Only the low level detector
C. The high level detector
D. Overheat sensor, low air pressure switch and low level detector
268.In flight, the blue hydraulic system can be supplied by: (B1,B2)
A. The RAT and the electrical pump.
B. The engine driven pump.
C. The PTU (Power Transfer Unit).

38

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