28 Fuel Flashcards

1
Q

what tasks need to be done by the fuel system?

A
  • fuel storage
  • fuel distribution
  • fuel dumping
  • indicating
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2
Q

what are the three most essential systems of the aircraft?

A

28 fuel, 32 landing gear, 27 flight controls

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3
Q

what regulates fuel certification requirements

A

subsection 951 - 1001 FAR Part 25

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4
Q

which fuel do reciprocating and jet engines each use?

A

recip -> high octane gasoline

jet -> kerosene

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5
Q

what is flashpoint

A

lowest temp at which a material will vaporize and can be ignited

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6
Q

how do flashpoint, density, and heating value of gasoline and jet a-1 compare

A

flashpoint -40, +40 (jet safer)
density: 720 vs 810 (jet slighty heavier)
heating value: 43.5 vs 42.5 (same)

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7
Q

why is a high flashpoint good

A

above the flashpoint, air bubbles form in the gas and this can lead to blockage of fuel distribution which is bad. (vapor lock)

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8
Q

what amount quantity is indicatied to pilots. How?

A
fuel mass -> more related to energy 
measure level (volume ) and density 
because density varies with temp
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9
Q

describe how and why water in feul is a problem and what is doen against it

A

how? air enters tanks when fuel leaves. air condenses (with decreasing temp).

why? less optimal engine performance
-can ice crystal and block fuel filters

sln:
water is denser so it goes to bottom, removed via water drain valves
-fuel heater before filter

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10
Q

describe the problem and sln of microorganisms in fuel tank

A

problem: they eat carbons and drink water and live in fuel tank. Problem to flow and indication. FOrm dark slime.

Sln: addatives + regularly empty tank

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11
Q

what is expansion space and give number

A

empty space (guarenteed) in fuel tank due to potential expansion of fuel from density change

2%

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12
Q

what is unusable fuel? what is done to reduce economic effects

A

fuel that is not guarenteed (under most adverve fuel feed cconditions) to be able to access.

scavenge pumps collect from from different tank areas (get in a321 down to 0.4%

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13
Q

what is a reason fuel can be moved around?

A

to change the CG and minimize trim drag

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14
Q

where is fuel taken from first? why?

A

center tank -> allow fuel weight to balance lift and reduce stress and bending moments on wing structures

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15
Q

what are three types of fuel tank construction

A
  • integral
  • bladder
  • rigid
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16
Q

what are three types of fuel tank construction

A
  • integral (part of structural members, with sealing material, baffles to prevent sloshing and checkvalves to keep fuel inboard where pumps are.
  • bladder (rubber flexible, in non-fuel-tight compartment) (for double layer or light craft)
  • rigid (removable, installed in a non-fuel-tight compartment for fuel tank)
17
Q

describe the tank vent system on larger aircraft

A

vent tanks are connected to main tanks via vent pipes. They can store overflow fuel and direct it back to main tanks via vent float valves.
vent tannk is open to air via a NACA inlet which increases pressure to slightly above ambient

18
Q

what is a symbiotic relationship between fuel (28) and 29 hydraulic and aircon

A

fuel is heat sink

19
Q

what are the two principles for engine feed

A
gravity feed (small high wing a/c
pressure feed (pumps. REQUIRED: one and a backup per engine)
20
Q

types of pupms

A

centrifugal pump, vane pump, ejector pump

21
Q

basis of centrifugal pump

A

inlet fuel through centrifugal impeller. (electrical connector)

22
Q

ley feature of ejector pump

A

-to scavenge fuel from other areas

23
Q

what features of tank are indicated

A

quantity, temp, pressure

24
Q

describe capacitance quantity indicator

A

stick with part in fuel and part in air. Fuel part will increase capacitance