Materials And Corrosion Chap 6 Flashcards

1
Q

Metals and alloys in aircraft should conform to …

A
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2
Q

How are metals and alloys identified

A

Colour codes

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3
Q

What do the British measure in

A

Standard wire gauge

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4
Q

What do french measure in

A

mm

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5
Q

What do Americans measure in

A

1000th of an inch

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6
Q

Def stan

A

Most frequently used in MOD

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7
Q

Conformity

A

A certificate to prove that the materials used are good quality

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8
Q

What is the colour coding

A

Used for rapid identification not to be used as sole means of identification

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9
Q

How are gauge sheets marked

A

Printed with ink on the surface

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10
Q

Ferrous metals

A

Contains mostly iron

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11
Q

Non-Ferrous metals

A

Contains no iron

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12
Q

Annealing

A

Changes the metal into a soft condition

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13
Q

Heat treatment

A

Metal is quenched and gives the metal specific properties

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14
Q

Refrigerated storage

A

Slows down the natural age process

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15
Q

Artificially age treatment

A

Precipitation (accelerated) treatment to get the maximum strength

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16
Q

Natural age process

A

Occurs at room temperature

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17
Q

Environmental damage

A

Includes corrosion, erosion and degradation of surface finish.

Prevention = coatings, tapes and corrosion prevention compounds

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18
Q

What does corrosion lead too

A

Reduce static strength, stress corrosion cracking, shortens fatigue life

19
Q

Composite structure gets affected by what ? (4)

A

Fuels oils lubricants and UV light

20
Q

Permanent coating

A

Includes paint

21
Q

Supplementary protective

A

Temporary
Eg PX24

22
Q

Iron and steel corrosion what do you see

A

Red rust deposits

23
Q

What do you see with Aluminium and magnesium alloys corrosion

A

White to grey powdery deposits (magnesium is fluffy)

24
Q

Most common
Surface corrosion

A

Sea air
Exhaust gases
Funnel smoke

25
Pitting corrosion
Local damage Contamination Surface protection is damaged Fault Thermal procedure changes
26
Intergranular corrosion
Very little to no external indication
27
Stress corrosion
Cause cracks
28
Fatigue corrosion
Cyclic stress from external load Cracks
29
Fretting corrosion
Two heavily loaded materials run together Removes natural protection
30
Crevice corrosion
High ratio of cathode to anode area Collects dust and moisture
31
Filiform corrosion
Starts at fasteners Under the paint Not very visible Damage is shallow and not very dangerous
32
Exfoliation or layer corrosion
Causes lifting of the metal surface Extensive damage can occur
33
Electrochemical corrosion
Most usual type Electrolytic effect Two materials which touch liquid Zinc copper
34
Husbandry procedures
Keep aircraft clean Keep aircraft dry Maintain protective coatings
35
Erosion
Loss of material from aircraft components by small particles such as grit, sand, stones, ice and water
36
How can you reduce erosion
Use of tape, anti-erosion paints suitable operation procedures
37
High temperature environments
Desert Arid salt Hot humid
38
Consequences of corrosion
Reduction in static strength Stress corrosion cracking Shortening of fatigue life
39
What are the two Corrosion removal processes
Mechanical Chemical
40
Pre treatment for corrosion
Clean the surface Paint again Don’t leave it to long cause clean surface could deteriorate again
41
Removal of acid
Solution of 10% by weight Sodium bicarbonate
42
PH level
Between 5-9
43
Removal of alkali
5% by weight Solution of chromic acid
44
Removal of micro organisms
Deposits removed with bristle brush Cleaned with hot water 50*C