aircraft fuel systems Flashcards

1
Q

why are fuel tanks divided into compartments or have baffles installed in them

A

the compartments or baffles keep the fuel from surging back and forth as the aircraft changes its attitude in flight

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2
Q

how is a fuel leak indicated on a reciprocating engine powered aircraft

A

the dye in the gasoline stains the area around the leak

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3
Q

what is the function of the sump in a fuel tank

A

the sump, or lowest point, in a fuel tank is located below the fuel outlet. the sump collects water and contaminants and will have a drain to remove them

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4
Q

what are the three different types of fuel tanks

A

built up tanks, integral tanks, bladder tanks

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5
Q

what a problem can occur in a bladder tank with blocked vent

A

as internal tank pressure decreases, the pressure differential between the atmosphere and the tank can cause the tank restraint to fail and the tank can collapse and block the fuel outlet

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6
Q

how do you prepare an aluminum fuel tank for welding

A

remove all fuel and thoroughly wash the tank, inside and out, with hot water and detergent. the tank should be purged with live steam for at least 30 minutes to remove all residual fuel and vapors

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7
Q

after welding an aluminum fuel tank, to what pressure should the tank be tested

A

3.5 PSI

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8
Q

why is a fuel jettisoning or dump system required for some aircraft

A

a fuel dump system is installed on most large aircraft and allows the flight crew to jettison, or dump, fuel to lower the gross weight of the aircraft to its allowable landing weight

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9
Q

what color is grade 100 LL fuel

A

blue

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10
Q

how can you detect jet fuel in the sample taken from the tank sump drains

A

jet fuel is basically clear and it has an odor similar to kerosine

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11
Q

what must be done after fuel system strainer has been cleaned or replaced

A

the system must be tested for leaks by pressurizing the system with the boost pump, if one is used

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12
Q

what must be done if the sump drains sample shows traces of jet fuel

A

the fuel system must be drained and flushed out with the proper grade aviation gasoline

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13
Q

what is used as the sensor in the fuel tank for an electronic type fuel quantity indication system

A

tubular capacitors that extend across the fuel tank from top to bottom

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14
Q

what is the principle upon which the electronic type fuel quantity indicating system operates

A

tubular capacitors extending across the fuel tanks change their capacitance as the fuel level changes. the dielectric constant (k) of the fuel is approximately twice that of air

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15
Q

what is used as a sensor in the fuel tank for the older resistance type fuel quantity indicating system

A

a variable resistor with an arm that is moved by float riding on top of the fuel in the tank

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16
Q

what is the purpose of a drip gauge in the fuel tank of a large aircraft

A

the drip gauge allows a mechanic to check the fuel level in a tank from the bottom of the tank

17
Q

When must the quantity indicating system indicate zero?

A

During level flight when the fuel in the tank is equal to the unusable fuel supply