corrosion Flashcards

1
Q

inevitable result when metals are exposed to water, air, etc.

A

corrosion

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2
Q

what aircraft needs since they contain some metal

A

constant inspection and cleaning to minimize the destructive effects of corrosion

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3
Q

what can corrosion result to

A

significant decrease in the thickness of original load bearing material that can lead to loss of structural integrity and catastrophic failure

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4
Q

what leads to the early detection of corrosion

A

routine in-service inspections and consequent rectification

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5
Q

deterioration of the metal by chemical or electrochemical attack

A

metal corrosion

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6
Q

effects of deterioration

A

change the smooth surface, weaken the interior, or damage or loosen adjacent parts

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7
Q

main source of corrosion in an aircraft

A

water or water vapor containing salt with oxygen in the atmosphere

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8
Q

two types of corrosion

A

direct chemical attack and electrochemical attack

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9
Q

corrosion process always involves what

A

metal that is attacked or oxidized suffers (anodic change) and corrosive agent is reduced (undergoing cathodic change)

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10
Q

attack resulting from a direct exposure of a bare surface to caustic liquid or gaseous agents

A

direct chemical attack

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11
Q

common agents causing direct chemical attack on aircrafts

A
  • spilled battery acid or fumes from batteries
  • welding residual
  • caustic cleaning solutions
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12
Q

types of fluxes used in these are corrosive which attack the metals or alloys

A

brazing, soldering, and welding

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13
Q

what are hygroscopic in nature and absorb moisture which causes severe pitting

A

flux residues

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14
Q

should be kept tightly capped and as far from aircraft as possible

A

caustic cleaning solution

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15
Q

may be likened chemically to the electrolytic reaction that takes place in electroplating, anodizing, or in a dry cell battery

A

electrochemical attack

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16
Q

reaction in electrochemical attack requires what

A

medium, usually water

17
Q

capable of conducting a tiny current of electricity

A

water

18
Q

what happens during electrochemical attack

A

quantity of corrosive agent is reduced and is not renewed or removed, may completely react with metal, becoming neutralized

19
Q

basis for effective corrosion control

A

regular cleaning, surface refinishing, medium is removed and minute electrical circuit is eliminated

20
Q

responsible for most forms of corrosion on aircraft structure and component parts

A

electrochemical attack

21
Q

types of corrosion

A

intergranular corrosion, galvanic, exfoliation, oxidation, fretting, uniform surface, filiform surface, pitting or general surface, stress, concentration cell corrosion

22
Q

occurs any time two dissimilar metals make electric contact in the presence of an electrolyte

A

galvanic corrosion

23
Q

When metals of the same galvanic grouping are joined together, what happens?

A

show little tendency for galvanic corrosion

24
Q

an advanced form of intergranular corrosion and shows itself by lifting up the surface grains of a metal by the force of expanding corrosion products occurring at the grain boundaries just below the surface.

A

exfoliation corrosion

25
Q

what is the visible evidence of intergranular corrosion

A

most often seen on extruded sections where grain thickness is usually less than in rolled forms.

26
Q

difficult to detect in its initial stage

A

exfoliation corrosion

27
Q

One of the simpler forms of corrosion is “dry” corrosion

A

oxidation corrosion

28
Q

When a metal such as aluminum is exposed to a gas containing oxygen, a chemical reaction takes place on the surface between the metal and the gas.

A

oxidation corrosion

29
Q

best way to protect iron from dry corrosion

A

keep oxygen from coming into contact with its surface and temporarily by covering the surface with oil or grease, or permanently with a coat of paint.

30
Q

deterioration of material that occurs at the interface of two contacting surfaces due to small oscillatory movements arising between them in the presence of a corrosive medium.

A

fretting corrosion

31
Q

former involves the creation of localized pits / small holes in the material surface which can be deep and significant to structural integrity whilst the latter corrosion form starts with a more widely dispersed uniform surface etching that dulls the surface and can progress to generate a rougher or frosted surface appearance.

A

pitting or general surface

32
Q

This occur when the metal is subjection to tensile stress in the presence of a corrosive environment.

A

stress corrosion

33
Q

can occur only in the presence of tensile stresses

A

stress corrosion

34
Q

common place for stress corrosion

A

between rivets in a stressed skin, around pressed in bushing or tapered pipe fittings.

35
Q

is corrosion of metals in a metal-to-metal joint, corrosion at the edge of a joint even though the metals are identical, or corrosion of a spot on a metal’s surface covered by a foreign material.

A

concentration cell corrosion

36
Q

type of corrosion is an attack along the grain boundaries of an alloy and commonly results from a lack of uniformity in the alloy structure.

A

intergranular corrosion

37
Q

particularly susceptible to intergranular corrosion

A

aluminum alloys and stainless steels

38
Q

Where an area of unprotected metal is exposed to an atmosphere containing battery fumes, exhaust gases, or industrial contaminants, a uniform attack over the entire surface occurs.

A

uniform surface corrosion

39
Q

the corrosion presents as random threadlike filaments under the paint often with the paint bulging in blisters raised by the corrosion products.

A

filiform surface corrosion