Cleaning and Corrosion control Flashcards

1
Q

what is used to clean transparent plastic windshields and windows of an aorcraft

A

mild soap and lots of Clean water

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2
Q

that is used to neutralize the electrolyte from a lead-acid battery that has been spilled on an aircraft structure

A

solution of bicarbonate of soda and water

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3
Q

what is used to neutralize the electrolyte from a nickel-cadmium batter that has been spilled on an aircraft structure

A

solution of boric acid and water, or vinegar

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4
Q

what solvent is recommended for removing grease from aircraft fabric prior to doping it

A

Methyl-ethyl-ketone (MEK) or lacquer thinner

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5
Q

what is the proper way to clean plastics

A

flush the plastic with clean water. Remove dirt by hand. plastics are easily scratched and usage or rags is not recommended

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6
Q

what causes corrosion

A
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7
Q

where is filiform corrosion most likely to occur on an aircraft

A

under a dense coating of topcoat enamel such as polyurethane. Filiform corrosion is caused by improperly cured primer

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8
Q

where is fretting corrosion most likely to occur on an aircarft

A

in a location where there is slight amount of relative movement between two components and no way for the corrosive residue to be removed as it forms

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9
Q

where is intergranular corrosion most likely to occur on an aircraft

A

along the grain boundaries of aluminum alloys that have been improperly heat-treated. Extruded aluminum alloy is susceptible to inter granular corrosion

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10
Q

where is stress corrosion most likely to occur on an aircraft

A

in an metal component that is continually under a tensile stress. The metal around holes on casting fitted with pressed in bushings is susceptible to stress corrosion

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11
Q

what areas of an aircraft are more most prone to corrosion

A

battery compartment, exhaust system and exhaust trails, wheel wells, lower areas of the belly (bilge), piano hinges, areas of dissimilar metal contact, welded areas inside of fuel tanks (especially integral tanks), metal fittings under high stress, lavatories, and food services areas

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12
Q

what is used to keep corrosion from forming on structural aluminum alloys

A

an oxide coating or aluminum cladding

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13
Q

how should an A&P minimize corrosion at piano hinges

A

piano hinges should be kept as clean and dry as practicable and lubricated with a low-viscosity moisture dispersing agent

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14
Q

how is the inside of structural steel tubing protected from corrosion

A

the tubing is filled with hot linseed oil and then drained

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15
Q

how does filiform corrosion usually appear on an aircraft structure

A

threadlike line of puffiness under a film of polyurethane or other dense finish system topcoats

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16
Q

what must be done to a piece of aluminum alloy to remove surface corrosion and to treat the metal to prevent further corrosion

A

remove the corrosion residue with a bristle brush or a nylon scrubber. Neutralize the surface with chromic acid or with some type of conversion coating. Protect the surface from further corrosion with a coat of paint

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17
Q

how may rust be removed from a highly stressed metal part

A

by glass blasting, by careful polishing with mild abrasive paper, or by using fine buffing compound on a cloth buffing wheel

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18
Q

what tools are proper for removing corrosion from aluminum alloy

A

Aluminum wool or aluminum wire brushes. severe corrosion can be removed with a rotary file

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19
Q

what type of device is used to remove surface corrosion from a piece of magnesium alloy

A

a stiff hog-bristle brush

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20
Q

what must be done to piece of aluminum alloy to remove surface corrosion and to treat the metal to prevent further corrosion

A

remove the corrosion residue with a bristle brush or a nylon scrubber. Neutralize the surface with chromic acid or type of conversion coating. Protect the surface from further corrosion with a coat of paint

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21
Q

how is rust removed from a highly stressed metal part

A

by glass bead blasting, by careful polishing with mild abrasive paper, or by using fine buffing compound on a cloth buffing wheel

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22
Q

what is corrosion preventive compound (CPC)

A

a waxy sealant or thin film dielectric that can be sprayed into aircraft structures to coat the surface and work its way between skins to prevent corrosion

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23
Q

what type of environment would CPC normally be used in

A

CPC are used in corrosive environments such as aerial agricultural spray operations and saltwater environment

24
Q

how are CPC applied to aircraft structure

A

CPC are normally applied with high pressure spray equipment that creates a fog of the CPC material inside the aircraft structure. Long spray wands are used to reach difficult to access areas

25
Q

what is used to clean to composite material prior to repair

A

acetone or methyl-ethyl-ketone(MEK) is commonly used. It is important to verify that the solvent residue is compatible with the resin system

26
Q

where is dissimilar metal corrosion most likely to occur on an aircraft

A

anywhere different types of metal come in contact with each other, especially where moisture is present

27
Q

what can be used to repair the anodized surface of an aluminum alloy

A

a chemical conversion coating such as alodine

28
Q

what are three types of primer that may be used when painting an aircraft

A

zinc chromate primer, wash primer, and epoxy

29
Q

what type of thinner is used with zinc chromate primer

A

Toluol or toluene

30
Q

what type of primer is used when the maximum protection of the metal is required

A

epoxy primer

31
Q

what are some different types of primer materials

A

wash primer, red iron oxide, gray enamel undercoat, urethane, epoxy, zinc chromate

32
Q

how thick should a coat of wash primer be that is used on an aluminum alloy aircraft structure

A

it should be thing enough that it does not hide the surface of the metal

33
Q

what are some different types of topcoat materials

A

dope, synthetic enamel, lacquers, polyurethane, urethane, acrylic urethanes

34
Q

what is the primary structure purpose of a finish on a composite material

A

to protect the composite structure from ultraviolet degradation

35
Q

what are the methods used to remove finishes from a composite material

A

by light sanding or abrasive blast with plastic materials

36
Q

when mixing epoxy paint, should the converter be added to the resin or the resin to the converter

A

converter should always be added to the resin, never the resin to the converter

37
Q

what should be done to a corroded aluminum alloy surface after the corrosion has been removed by mechanical methods

A

surface should be treated with a chemical conversion coating before the topcoats are applied

38
Q

what may be done to the surface to prevent filiform corrosion beneath the topcoat

A

be sure that the primer is properly and completely cured

39
Q

how it the finish removed form a fiberglass aircraft component that is being repaired

A

the finish must be sanded off. paint remover can soften the resin of which the component is made

40
Q

how can a vinyl film decal be removed from an aluminum alloy surface

A

place a cloth saturated with cyclohexanone or MEK over the decal until it is softened, and scrape it off of the surface with a plastic scraper

41
Q

why is retarder used in dope when the dope is being sprayed in humid conditions

A

the retarder slows the drying of the dope and keeps it from blushing

42
Q

what is meant by dope blushing, and what causes it

A

Blushing is a a condition in a dope finished component in which moisture from the atmosphere condenses on the surface and causes some of the cellulose to precipitate from the finish. Blushing leaves a porous, dull, and weak finish
Blushing may be caused by the temperature being too low, the humidity being too high, or by drafts or sudden changes in the temp

43
Q

what causes blushing in a dope finish

A

too high humidity

44
Q

what causes fisheyes in the finish

A

localized surface contamination

45
Q

where are the registration marks required marks required to be placed on a fixed-wing aircraft

A

on the vertical tail surface or on the side of the fuselage

46
Q

what is the generally required dimensions of the registration numbers on the side of a fixed-wing aircraft

A

12 inched tall and 2/3 as wide as they are high. the letters M and W may be as wide as they are high. The humeral 1 and 1/6 wide as it is high

47
Q

what is the regulation regarding the color of the registration marks

A

the color must contrast with he background and be legible

48
Q

what is a cause of poor adhesion between the topcoat and the fill coats on a fabric surface

A

too much aluminum powder in the aluminum pigmented dope

49
Q

what is a cause of rough finish on a freshly sprayed surface

A

too high automizing air pressure on the spray gun

50
Q

what causes sags and runs on a surface that has just been sprayed

A

too much finishing material being applied on one coat

51
Q

what causes orange peel, or spray mottle, in a finish

A

incorrect paint viscosity or improper setting of the spray gun

52
Q

what cause pinholes in a finish

A

excessive atomizing air on the spray gun

53
Q

what safety precaution must be observed when sweeping a paint room that has dried dope or lacquer overspray on the floor

A

the floor must be wet down with water before it is swept. static electricity from dry sweeping can cause a fire

54
Q

what personal protection equipment (PPE) should be used while painting

A

respirator, eye protection, and skin protection

55
Q

why are some portions of the structure of an aircraft dope proofed before they are covered with fabric

A

dope proofing keeps the fabric from sticking to the structure when the first coat of dope is applied. the fabric normally sags enough to touch the structure before it begins to pull that

56
Q

what are some key application techniques for a quality paint job

A

correct spray pressure and spray gun setting, proper spray gun handling (even, overlapping spray patterns, spray gun distance) and good lighting

57
Q

why should control surfaces be balanced after painting

A

weight and distribution of the paint may have changed, and the control surface may be out of tolerance