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aircraft material, hardware, and processes (part 1)
  • William Poore

  • 問題数 25 • 6/5/2024

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    問題一覧

  • 1

    Magnetic particle inspection is used primarily to detect

    flaws on or near the surface

  • 2

    Liquid penetrant inspection method may be used on which of the following?

    ferrous and nonferrous metals and nonporous plastic

  • 3

    Which if the following factors are considered essential knowledge for X-ray exposure?

    material thickness and density and the type of defect to be detected

  • 4

    One way a part may be demagnetized after magnetic particle inspection is by

    slowly moving the part out of an AC magnet field of sufficient strength

  • 5

    Which type crack can be detected by magnetic particle inspection using either circular or longitudinal Magnetization?

    45 degrees

  • 6

    The pattern for an inclusion is a magnetic particle buildup forming

    Parallel lines

  • 7

    What defects will be detected by magnetizing a part using continuous longitudinal magnetization with a cable?

    Defects perpendicular to the long axis of the part

  • 8

    Circular magnetization of a part can be used to detect which defects?

    Defects, parallel to the long axis of the part

  • 9

    Which of the following describe the effects of annealing Steel and aluminum alloys?

    Decreasing internal stresses and softening of the metal

  • 10

    What is generally used in the construction of aircraft, exhaust collectors, stacks, and manifolds?

    Stainless steel

  • 11

    What metal has special short term heat properties and is used in the construction of aircraft firewall?

    titanium alloy

  • 12

    Alclad Is a metal consisting of

    pure aluminum surface layers on an aluminum alloy core

  • 13

    The core material of Alclad 2024-T4 is

    heat treated aluminum alloy, and the surface material is commercially pure aluminum

  • 14

    The aluminum code number 1100 identifies what type of aluminum?

    99% commercially, pure aluminum

  • 15

    An aircraft part may be demagnetized by subjecting it to a magnetizing force from Alternating current that is gradually reduced in strength. an aircraft part may be demagnetized by subjecting it to a magnetizing force from direct current that is alternately Reversed in direction and gradually reduced in strength Regarding the above statement

    both one and two are true .

  • 16

    What type of corrosion may attack the grain bound-Aries Of aluminum alloys when the heat treatment process has been improperly accomplished?

    intergranular

  • 17

    Which heat treating Process of metal produces a hardware resistant surface over a strong, tough core?

    case hardening

  • 18

    Which heat treating operation would be performed when the surface of the metal is changed, chemically by introducing a high carbide or nitride Contant?

    case hardening

  • 19

    Normalizing is a process of heat treating

    Iron based metals only

  • 20

    The reheating of a heat treated metal such as with a welding torch

    Can significantly alter a metals properties in the reheated area

  • 21

    What aluminum alloy designations indicate that the metal has received no hardening or tempering treatment?

    3003-F

  • 22

    Which material cannot be heat treated repeatedly without harmful effects?

    clad aluminum alloy

  • 23

    What is descriptive of the annealing process of steel during and after it has been annealed

    slow cooling, low strength .

  • 24

    Which of the following occurs when a mechanical force, such as rolling hammering, or bending, is repeatedly applied to most metals at room temperature

    The metals become strain or work hardened, or cold worked

  • 25

    Why is steel tempered after being hardened?

    To reveal its internal stresses, and reduce its brittleness