Aircraft fuel systems Flashcards

1
Q

What is the purpose of a fuel jettisoning (dump) system?

A

It is an emergency system provided so that the flight crew can quickly bring the weight of the airplane down to the maximum landing weight.

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2
Q

When would a fuel jettison system be required for small aircraft?

A

It is required when the maximum takeoff weight is more than the maximum landing weight.

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3
Q

What are a few types of fuel tanks (cells)?

A

Bladder-type fuel tank, integral fuel tanks, and welded or riveted fuel tanks.

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4
Q

what supports the weight of fuel in bladder-type fuel cell?

A

The structure of the cavity that the cell fit into.

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5
Q

What is “wet-wing” type construction?

A

integral fuel cells.

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6
Q

What markings must be placed near the fuel filler opening on reciprocating engine aircraft?

A

The word “Avgas” and the minimum fuel grade.

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7
Q

What are the advantages of a single point pressure fueling system?

A

Pressure fueling, sometimes referred to as single-point or underwing fueling, greatly reduces the time required to service large aircraft. It also eliminates aircraft skin damage from hoses and hose nozzles, and reduces the chance of fuel contamination.

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8
Q

why should you wait a period of time after fueling before checking fuel sumps?

A

To allow time for water and contamination to settle to the drain point.

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9
Q

Why should the fuel sumps of aircraft be drained before the first flight of the day?

A

To remove any water that has condensed in the fuel and collected in the sump.

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10
Q

What does water look like when in fuel that has been drained from the sumps?

A

It looks like clear balls of jelly.

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11
Q

What is the purpose of a fuel temperature indicator on a turbine engine?

A

It is a means for checking the temperature of the fuel in the tanks at the engine to determine when there may be a danger of ice crystals forming in the fuel. (to monitor the temp of fuel to determine when there might be donner).

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12
Q

What is the purpose of warning lights in connection with fuel system?

A

Warning lights may be used to indicate when the fuel pressure is too low, or to indicate when the fuel quantity in a tank is below a certain amount.

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13
Q

Where are electrical operated valve-in-transit indicator lights used?

A

On large multiengine aircraft, each of the fuel crossfeed and line valves may be provided with valve in-transit indicator lights. The light is on only during the time the valve is in motion and is off when movement is complete.

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14
Q

Why do fuel selectors have detents?

A

So the pilot can feel when the switch is in a specific position.

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15
Q

What are four general types of fuel quantity gauges?

A

sight glass, mechanical, electrical, and electronic.

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16
Q

Which type of fuel quantity gauge is considered to be more accurate than the other types?

A

The electronic-capacitance type, because it measures by weight.

17
Q

Describe the sensor used in an electronic type fuel quantity indicating system?

A

It is a tubular capacitor that extends across the tank from top to bottom.

18
Q

What is a drip gauge?

A

An under-wing bayonet type fuel gauge that consists of a calibrated hollow drip tube that is drawn out from the lower wing surface. When the top of the tube reaches the level of the fuel, the tube will begin to drip indicating fuel level.

19
Q

What is a cross-feed system?

A

An interconnected fuel system designed so that fuel can be fed from any tank to any engine.

20
Q

What is the purpose of the baffles in a fuel tank?

A

To prevent the fuel from surging as a result of changes in attitude of the aircraft.

21
Q

What is an electrical operated fuel tank shutoff valve in-transit light?

A

A light that indicates when the valve is in motion.

22
Q

What indictors could be used to determine when there may be danger of ice crystals forming in the fuel of a turbine-powered aircraft?

A

Fuel temperature or a differential pressure type indicators.

23
Q

What is a pressure fueling system sometimes referred to?

A

Single point fueling system.

24
Q

What method may be used to check a fuel tank for leaks after a weld has been performed?

A

The tank is pressurized with ½ to 3.5 PSI air pressure and a soapy solution is added to detect any leaks.

25
Q

What should be done with old gaskets and seals when replacing fuel system components?

A

when replacing fuel system components?
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