amcr Flashcards

1
Q

three classification of damage

A

negligible, repairable, non-repairable

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2
Q

is damaged that may be corrected by a simple procedure with no restrictions on flight operations

A

negligible

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3
Q

is damaged to the skin, bond, or core that places restrictions on the aircraft or part

A

repairable

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4
Q

is damaged beyond established repair limits

A

non-repairable

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5
Q

defect on the outer surface that does not involve damage to the structural reinforcing fibers

A

cosmetic defects

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6
Q

often caused by chipping or scratching during handling

A

cosmetic defects

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7
Q

occurs when foreign object strike the part

A

impact damage

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8
Q

is a defect on the outer surface that does not involve damage to the structural reinforcing fibers

A

impact damage

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9
Q

most common cause of impact damage

A

careless handling during transportation or storage, or standing parts on their edge without adequate protection

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10
Q

is a separation of fabric layers of a material in a laminate

A

delamination

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11
Q

delamination occurs as a result of several causes like?

A

impact, moisture in the fabric, lightning strikes

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12
Q

another type of delamination

A

unbond or disbond

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13
Q

occurs when the skin of the sandwich structure becomes separated from the core

A

disbond / unbond

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14
Q

can occur in advanced composite structures just as in metallic ones

A

cracks

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15
Q

may occur from impact damage, over-torquing fasteners, or as a result of fastener pull-through. holes filled in the wrong location, wrong size, wrong number of holes can also be classified as this.

A

hole damage

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16
Q

are not easily detected however, they could lead to extensive damage

A

tiny holes

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17
Q

types of damage

A

cosmetic defects, impact damage, delamination, cracks, hole damage

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18
Q

used to detect cracks, surface irregularities, and surface defects such as delamination and blistering

A

visual inspections

19
Q

one of the most important tools used to detect internal flaws or delamination

A

coin tap test

20
Q

uses a high frequency sound wave as a means of detecting flaws in a part by beaming a high frequency wave response, delamination, flaws, or other condition are detected

A

ultrasonic inspections

21
Q

is time versus amplitude display read from left to right

22
Q

takes a cross-sectional view of the material being tested and used as an oscilloscope screen to compare the sample

23
Q

imaging shows the shape, size, and location of the damage, but does not show the depth

24
Q

locates flaws by temperature variations at the surface of a damaged part. heat is applied to the part then the temperature gradients are measured using an infrared camera or film

A

thermography

25
Q

it calls for the suspected part to be heated and then photographed using a laser light source and a special infrared camera film system

A

laser holography

26
Q

used to detect disbands or water in honeycomb and impact damage

A

laser holography

27
Q

used to detect cracks that cannot be visually detected, both internally and externally

A

radiography

28
Q

useful in detecting the extent of the damage that cannot be visually detected

A

radiography

29
Q

used to determine whether the resins have reached their proper strength such as the barcol tester

A

hardness testing

30
Q

used successfully for detecting cracks in metallic surfaces, however, it should not be used with advance composite because if it is allowed to sit on the surface, the wicking action of the fibers may take the dye penetrant and would no longer bond the new material

A

dye-penetrant

31
Q

types of inspections

A

visual inspection, coin tap test, ultrasonic inspection, thermography, laser holography, radiography, hardness testing, dye-penetrant

32
Q

a superficial, non-structural filler is used to restore a surface to keep fluids out until a more permanent repair is made

A

cosmetic repair

33
Q

this type of repair will not regain any strength and is used only where strength is unimportant.

A

cosmetic repair

34
Q

this type of repair can be effective in limited instances, where the delamination is restricted to one ply.

A

resin injection

35
Q

quick and cheap repair

A

resin injection

36
Q

this type of repair can hope to slow the spread of delamination and is generally considered a temporary measure

A

resin injection

37
Q

this type of repair can gain some strength

A

semi-structural plug/patch

38
Q

mechanically-fastened plug and patch repair can be especially effective where thick solid laminated are used, since they take the bolt loads well

A

semi-structural plug/patch

39
Q

Full structural repairs using bolted doublers can be used in heavily loaded solid laminates. This is often the only practical means of repairing such structures.

A

structural mechanically-fastened doubler

40
Q

often used to perform repairs to lightly loaded thin laminate structures

A

structural bonded external doubler

41
Q

this type of repair is especially common using wet lay-up materials

A

structural bonded external doubler

42
Q

This repair restores full structural properties by forming a joint between the prepared repair area and the repair patch

A

structural flush repair

43
Q

made by replacing each ply of the composite laminate that has been removed from the damage area

A

structural flush repair

44
Q

types of repair

A

cosmetic repair, resin injection, semi-structural plug/patch, structural mechanically-fastened doubler, structural bonded external doubler, structural flush repair