The function of a feed box in the fuel tank is to

In a compensated capacitance type quantity indicating system, the contents gauge of a half-full fuel tank indicates a fuel mass of 8000 lb. If a temperature rise increased the volume of fuel by 5 %, the indicated fuel weight would :

Fire precautions to be observed before refuelling are :

The fuel supply system on a jet engine includes a fuel heating device, upstream of the main fuel filter so as to:

On most transport jet aircraft, the low pressure pumps of the fuel system are supplied with electric power of the following type:

The fuel crossfeed system:

The purpose of the baffles in an aircraft"s integral fuel tank is to:

On a transport type aircraft the fuel tank system is vented through:

The types of fuel tanks used on most modern transport aircraft are:

Fuel dump systems are required:

The pressurization of tanks is maintained by the fuel:

On a jet aircraft fuel heaters are :

The automatic fuelling shut off valve:

During fuelling the automatic fuelling shut off valves will switch off the fuel supply system when:

(For this question use annex 021-980A) The diagram shown in annex represents a jet fuel system. The fuel- flow measurement is carried out :

The maximum quantity of fuel that can be dumped with the jettisoning system is:

The purpose of baffle check valves fitted in aircraft fuel tanks is to :

The cross-feed fuel system enables:

The vapor lock is :

The refueling in a transport jet aircraft is made ...

The fuel system boost pumps are used to :

The cross-feed fuel system is used to :

The fuel system boost pumps are submerged in the fuel ..

The capacitance type fuel gauging system indicates the fuel quantity by measuring the:

Fuel pumps submerged in the fuel tanks of a multi-engine aircraft are: