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In case of loss of both Fuel Control Monitoring Computers:

Correct! Wrong!

FAULT lights up on both CTR Tank pbs when:

Correct! Wrong!

In normal operation, engines are always fed from:

Correct! Wrong!

Maximum fuel temperature for JET A and JET A1 is:

Correct! Wrong!

The INNER tanks:

Correct! Wrong!

There are two fuel pumps in each collector cell. They normally are both selected ON and:

Correct! Wrong!

In case of Fuel Center Pumps fault:

Correct! Wrong!

The Airbus A330 fuel system:

Correct! Wrong!

Minimum fuel quantity for takeoff is:

Correct! Wrong!

The ECAM alerts that are related to fuel low level in the wing tanks (FUEL WING TK LO LVL, etc.) must not appear for takeoff.

In case of an "ALL ENGINES FLAME OUT" situation:

Correct! Wrong!

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The fuel system is fully automatic. The only actions required before flight are:

Correct! Wrong!

Automatic refueling ensures that:

Correct! Wrong!

Electrical power requirements for refueling are:

Correct! Wrong!

The L an R STBY PUMPS:

Correct! Wrong!

Fuel temperature is:

Correct! Wrong!

With tanks nearly empty, time for refueling all the tanks of the aircraft is approximately (depending on the nominal pressure) is:

Correct! Wrong!

Refueling can be accomplished:

Correct! Wrong!

To supply both engines with X - FEED Valve OPEN:

Correct! Wrong!

In normal conditions, the automatic control of CG begins:

Correct! Wrong!

When a tank fuel temperature is displayed amber:

Correct! Wrong!

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In ELEC EMER CONFIG:

Correct! Wrong!

A fuel imbalance should be corrected:

Correct! Wrong!

During manual fuel transfer from CTR to INNER Tank:

Correct! Wrong!

Refueling can be controlled from:

Correct! Wrong!

In normal operation, the automatic control of CG will stop:

Correct! Wrong!

Airbus A330 – Fuel