aircraft material, hardware, and process Flashcards

1
Q

what is the alloy number of the most commonly used aluminum alloy for aircraft structural use

A

2024-T

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2
Q

what is the alloy number of a high strength aluminum ally that has zinc as an alloying compnent

A

7075

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3
Q

what type of composite material is used when stiffness is the prime requirement

A

graphite (carbon)

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4
Q

what type of composite material is used when toughness is the prime requirement

A

kevlar

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5
Q

why is a piece of steel tempered after it has been hardened

A

when steel is hardened it becomes brittle. tempering removes some of its brittleness

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6
Q

how is steel annealed

A

it is heated to just above its upper critical temp until it reached a uniform temp throughout, then it is cooled very slowly in the oven

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7
Q

how it steel hardened

A

it is heat to its critical temperature and then quenched in water, brine, or oil

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8
Q

what is meant by tempering steel

A

steel is first hardened; then some of the hardness is removed to relieve some of the internal stresses and brittleness

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9
Q

what is meant by case hardening

A

the surface of the metal is hardened by the infusion of carbon or aluminum nitride. the interior of the metal remains strong and tough

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10
Q

what are two methods of case hardening

A

carburizing and nitrating

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11
Q

how its steel nitrided

A

steel part is heated in a retort in which there is an atmosphere of ammonia (compound of nitrogen and hydrogen). Aluminum, an alloying element in the steel, combines with the nitrogen to form an extremely hard aluminum nitride on the surface of the steel

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12
Q

what is the method of solution heat treatment of an aluminum alloy

A

metal is hardened by heating it in a surface to specified temperature and immediately quenching it in water. It is soft when it is removed from the quench, but as it ages it hardeneds

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13
Q

what is the method of precipitation heat treating of an aluminum alloy

A

the metal is heated and quenched, then it is returned to the oven and heated to a lower temp. it is held at this temp for a specified time, then removed from the oven and allowed to cool in still air. this increases the strength and hardness of the metal. precipitation heat treating is also called artificial aging

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14
Q

what is another name for precipitation heat treatment

A

artificial aging

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15
Q

identify and explain the differences between heat-treated and non heat treated aluminum alloys

A

heat treated alloy designations are normally followed with a -T, followed by a number (1-10) that designates the type of heat treat. a common aircraft aluminum allot is 2024-T3. heat treated aluminum is stronger than non heat treated aluminum

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16
Q

why is it important that a piece of aluminum alloy be quenched immediately after it is removed from the heat treating oven

A

any delay in quenching aluminum alloy after It is removed from the oven will allow the grain structure to grow enough that intergranular corrosion is likely to form in the metal

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17
Q

describe and explain the forces placed on aircraft materials

A

tension-
compression-
torsion-
bending-
strain-
shear-

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18
Q

what type of loading should be avoided when using a self-locking nut on an aircraft bolt

A

a self-locking nut should not be used for any application where there are any rotational forces applied to the nut or to the bolt

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19
Q

what determines the correct grip length of a bolt used in an aircraft structure

A

the grip length of the bolt should be the same as the combined thickness of the materials being held by the bolt

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20
Q

how tight should the nut be installed on a clevis bolt that is used to attach a cable fitting to a control surface horn

A

the nut on a clevis bolt should not be tight enough to prevent the clevis bolt from turning in the cable fitting and the horn

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21
Q

what bolt is described by this number: AN6-14A

A

AN6= Hex bolt,6/16(3/8) inch diameter
14=length=1-4/8(1-1/2) inch long
A=the shank is not drilled for a cotter pin

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22
Q

what is indicated by a triangle on the head of a steel bolt

A

this is a close tolerance bolt

23
Q

what is a correct application for self-tapping sheet metal screw on an aircraft

A

they may be used to hold nonstructural component onto the aircraft

24
Q

how can you tell when a self-locking nut must be discarded

A

when you can screw the nut onto a bolt without having to use a wrench

25
Q

what is a channel nut

A

a series of nuts mounted loosely in a channel that is riveted to the aircraft structure. you can install screws in a channel nut without having to hold the nut with a wrench

26
Q

of what two materials are cotter pins made

A

low-carbon steel and corrosion resistant steel

27
Q

what is the smallest size cable that is allowed to be used in the primary control system of an aircraft

A

1/8 inch diameter

28
Q

what type of control cable must be used when pulleys are used to change the direction of cable travel

A

extra-flexible cable (7x19)

29
Q

what is the purpose of safety wire

A

to prevent a nut, bolt, or other components from loosening

30
Q

after torquing a castellated nut, can the nut be loosened to align with the hole in a bolt for installing the cotter pin

A

no. never overtourque or loosen a torque nut to align safety wire or cotter pin holes. the nut should never be torqured to the minimum torque, and the tightened to align with the safety hole, without exceeding the maximum torque

31
Q

what kind of measuring is used to measure the runout of an aircraft engine crankshaft

A

a dial indicator

32
Q

what measuring instrument is used to measure the fit between a rocker arm shaft and its bushings

A

outside diameter of the shaft is measured with a micrometer caliper. the inside of the bushing is measured with a telescoping gauge and the same micrometer caliper

33
Q

in what increment can a veneer micrometer caliper be read

A

one ten thousand (0.0001) inch

34
Q

what is an advantage of vernier caliper over a micrometer caliper

A

the range of a vernier caliper if far greater than that of a micrometer caplier

35
Q

what precision tool is used to measure piston ring side clearance

A

thickness gauge

36
Q

what precision tools are used to measure the inside diameter of a cylinder

A

a telescoping gauge and micrometer caliper

37
Q

what precision tools are used to measure the inside diameter of a small hole

A

a small hole gauge and micrometer caliper

38
Q

what kind of solder is recommended for soldering electrical wires

A

60/40 resin-core solder

39
Q

what is the function of the flux used in soldering

A

flux covers the cleaned and heated metal to keep oxygen away from it so oxides cannot form. oxides keep the solder from adhering to the surface of the metal

40
Q

what are the three most common types of torque wrench

A

deflecting beam, dialing indicating, and micrometer setting types

41
Q

where would an aviation mechanic find the appropriate hardware specifications for use on a particular aircraft

A

in the aircraft manufacturers structural repair manual (SRM)

42
Q

where would an aviation mechanic find the material specifications for structural repairs on an aircraft

A

in the aircraft manufacturer illustrated parts catalog (IPC)

43
Q

why is it scratched that the surface of a piece of clad aluminum alloy not to be scratched

A

the pure aluminum used for the cladding is non corrosion, but the aluminum alloy below the cladding is susceptible to corrosion. if the cladding is scratched through, corrosion could form

44
Q

what is the preload value when torquing a nut

A

preload is the force or torque required to overcome the friction between the threads on the nut and the thread of the bolt prior to the nut containing the mating surface

45
Q

how is the preload value used when torquing a nut

A

the preload torque is added to the specific torque to obtain the required setting on the torque wrench

46
Q

how can the material of a bolt be identified

A

by manufacturer markings that are on the bolt head

47
Q

how is the welding flux removed from a piece of aluminum that has been gas-welded

A

it should be removed by scrubbing it with hot water and a bristle brush

48
Q

what are the visual characteristics of a good weld

A

a good weld is uniform in width; the ripples are even and well feathered into the base metal an show no burn due to overheating. the weld has good penetration and is free of gas pockets, porosity, or incursions

49
Q

what are the visual characteristics of a bad weld

A

a bad weld has irregular edges and considered variation in the depth of penetration. it often has the appearance of a cold weld

50
Q

what must be done to welded joint if it must be rewelded

A

all traces of the old weld must be removed so the new weld will penetrate the base metal

51
Q

what is meant by normalizing a piece of steel after it has been welded or machined

A

normalizing removes stresses that are locked into the material by welding or machining

52
Q

how I steel structure normalized after it has been welded

A

heat the steel structure to a temperature above its critical temperature and allow it to cool in still air

53
Q

what determines the size of tip that is to be used when gas-welding steel

A

the thickness of the material being welded. the size of the tip orifice determines the amount of flame produced and thus the amount of heat put into the metal