aircraft system Flashcards

(48 cards)

1
Q

are designed to provide an uninterrupted flow of clean fuel to the engine

A

aircraft fuel system components

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2
Q

utilizes the force of gravity to transfer the fuel from the tanks to the engine

A

gravity-feed system

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3
Q

this places thee fuel tanks above the carburetor, and the fuel is gravity fed through the system and into the carburetor

A

gravity-feed system

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4
Q

if the design of the aircraft is such that gravity cannot be used to transfer, this is installed

A

fuel-pump system

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5
Q

aircraft with fuel-pump system have two fuel pumps

A

main pump system or engine driven pump and electrically driven auxiliary pump

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6
Q

pumps the fuel from the tank to the engine

A

main pump system or engine driven pump

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7
Q

provided for use in engine starting and in the event the engine pump fails

A

electrically driven auxiliary pump

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8
Q

other term for auxiliary pump

A

boost pump

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9
Q

provides reliability to the fuel system and is electrically driven by a switch in the cockpit

A

auxiliary pump

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10
Q

allows air into the tank as fuel is consumed

A

fuel vent

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11
Q

used to draw fuel from the tanks to vaporize fuel directly into the cylinders prior to starting the engine

A

fuel primer

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12
Q

during cold weather, when engines are difficult to start, this helps because there is not enough heat available to vaporize the fuel in the carburetor

A

fuel primer

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13
Q

allow air into the tank as fuel is consumed

A

fuel vents

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14
Q

normally located inside the wings of an airplane, have a filler on top of the wing through which they can be filled

A

fuel tanks

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15
Q

covers the opening of fuel tanks

A

filler cap

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16
Q

stores the fuel and protects from contaminants

A

fuel tanks

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17
Q

all fuel tanks are required to have what

A

sump and drain installed at their lowest point

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18
Q

provides a convenient location for water and sediment to settle, allowing it to be drained from the system

A

sump

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19
Q

indicate the amount of fuel measured by a sensing unit in each fuel tank and is displayed in gallons or pounds

A

fuel gauges / fuel quantity gauges

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20
Q

when do aircraft certification rules require accuracy in fuel gauges

A

when they read “empty”(but other reading than “empty” should be verified

21
Q

allows selection of fuel from various tanks

A

fuel selectors / selector valve

22
Q

four positions of a common type of selector

A

left, right, both, and off

23
Q

fuel flows through a small metal what from the tank to the engine

24
Q

fuel lines routed in an engine compartment present what

A

special maintenance consideration

25
often constructed from synthetic materials with the line's diameter being dependent upon the engine's fuel flow requirements
flexi fuel lines
26
also a kind of coarse filter used for separating solid particles of a different size.
strainer
27
usually used to remove large solid contaminant particles
strainer
28
used for fine filtration
filter
29
requires a main strainer or fuel filter to be installed in the fuel system to remove contaminants and to provide a method for draining the contaminants from the system
FAR Part 23
30
represents the lowest point in an aircraft's fuel system and should be checked periodically for contaminants that could restrict fuel flow to the engine
fuel strainer
31
explain the process that happens in the fuel strainers, sumps, and drains
after leaving the fuel tank and before the carburetor, fuel passes through a strainer that removes moisture and sediments that settle in a sump at the bottom of the strainer assembly
32
low point in a fuel system and/or fuel tank
sump
33
may contain a sump, fuel strainer, and fuel tank drains, which may be collocated
fuel system
34
why is water in the sump hazardous
in cold weather, the water can freeze and block fuel lines. in warm weather, it can flow into the carburetor and stop the engine
35
serves to remove water from the tank or to drain the fuel
drain valve
36
important of an aircraft drain valve
high quality seal
37
primary fuel pressure pumps in a pressure-feed fuel system
engine-driven fuel pumps
38
deliver a continuous supply of fuel at the proper pressure during engine operation
engine-driven fuel pumps
39
maintain a positive fuel pressure on the inlet side of the engine-driven fuel pump. this helps prevent pump cavitation and vapor lock by pressurizing the fuel in the lines
auxiliary fuel pumps / boost pump
40
may serve as a backup source for fuel pressure to the engine-driven fuel pump becomes clogged or fails
auxiliary fuel pumps / boost pump
41
if an engine has both engine-driven fuel pump and a boost pump, this must be incorporated into the fuel system
bypass valves or check valves
42
when pumps are in series this is used
bypass valves
43
when pumps are in par-all
check valves
44
purpose of of bypass and check valves
let fuel bypass the engine-driven pump during engine starting or in case the pump fails
45
purpose of this is the same as a reciprocating engine fuel system
turbine fuel system
46
must store, transfer, and meter fuel to a turbine engine in the proper amount and at the right pressure
turbine fuel system
47
what does a fuel system contain
tanks, lines, valves, pumps, filter devices, gauges, a fuel control unit, and fuel nozzles ++ fuel heater
48
required to eliminate fuel metering problems caused by ice crystals in the fuel