Final Materials/Processing 8245-77 & 8289-8307 Flashcards
1- 8246. Which of the following describe the effects of annealing steel and aluminum alloys?
A ) Decreasing internal stresses and softening of the metal.
B ) Softening of the metals and improved corrosion
resistance.
C ) Improved corrosion resistance.
A ) Decreasing internal stresses and softening of the
metal.
2- 8257. What is generally used in the construction of aircraft exhaust collectors, stacks, and manifolds?
A ) Stainless steel.
B ) Titanium
C ) Aluminum
A—Stainless steel.
3- 8257-1. What metal has special short-time heat properties and is used in the construction of aircraft firewalls?
A ) Stainless steel.
B ) Chrome molybdenum alloy steel.
C ) Titanium alloy.
C—Titanium alloy.
4- 8259. Alclad is a metal consisting of
A ) aluminum alloy surface layers and a pure aluminum
core.
B ) pure aluminum surface layers on an aluminum alloy core.
C ) a homogeneous mixture of pure aluminum and aluminum alloy.
B ) pure aluminum surface layers on an aluminum alloy core.
5) 8273. The core material of Alclad 2024-4 is
A ) heat-treated aluminum alloy, and the surface material is commercially pure aluminum.
B ) commercially pure aluminum, and the surface material is heat-treated aluminum alloy.
C ) strain-hardened aluminum alloy, and the surface material is commercially pure aluminum.
A ) heat-treated aluminum alloy, and the surface material is commercially pure aluminum.
6) 8274. The aluminum code number 1100 identifies what type of aluminum?
A ) Aluminum alloy containing 11 percent copper.
B ) Aluminum alloy containing zinc.
C ) 99 percent commercially pure aluminum.
C —99 percent commercially pure aluminum.
7) 8245.
What type of corrosion may attack the grain boundaries of aluminum alloys when the heat treatment process has been improperly accomplished?
has been improperly accomplished?
A ) Concentration cell.
B ) Intergranular.
C ) Fretting.
B ) Intergranular.
8) 8247
Which heat-treating process of metal produces a hard, wear-resistant surface over a strong, tough core?
.
A ) Case hardening.
B ) Annealing.
C ) Tempering.
A ) Case hardening.
9) 8248.
Which heat-treating operation would be performed when the surface of the metal is changed chemically by introducing a high carbide or nitride content?
A ) Tempering.
B ) Normalizing.
C ) Case Hardening.
.
C — Case hardening.
10) 8249. Normalizing is a process of heat treating?
A ) aluminum alloys only.
B ) Iron-base metals only
C ) both
B-iron-base metals only.
11) 8251
The reheating of a heat treated metal, such as with a welding torch.
A ) has little or no effect on a metal’s heat treated
characteristics.
B ) has a cumulative enhancement effect on the
original heat treatment.
C ) can significantly alter a metal’s properties in the
reheated area.
C ) can significantly alter a metal’s properties in the reheated
12) 8253
What aluminum alloy designations indicate that the metal has received no hardening or tempering treatment?
A ) 3003-F
B ) 5052-H36.
C ) 6061-O
A ) 3003-F
13) 8254
Which material cannot be heat treated repeatediy without harmful effects?
A ) Unclad aluminum alloy in sheet form.
B ) 6061-9 stainless steel.
C ) Clad aluminum alloy.
C ) Clad aluminum alloy.
14) 8255
What is descriptive of the annealing process af steel during and after it has been annealed?
A ) Rapid cooling; high strength.
B ) Slow cooling; low strength.
C ) Slow cooling; increased resistance to wear.
B — Slow cooling: low strength.
15) 8250. Which of the following occurs when a mechanical force such as rolling, hammering, or bending is repeatedly applied to most metals at room temperature?
C.–The metals become strain or work hardened or cold
worked.
16) 8252
Why is steel tempered after being hardened?
.
C — To relieve its internal stresses and reduce its brittleness.
17) 8258
Unless otherwise specified or required, aircraft bolts should be installed so that the bolthead is
C — downward, or in a forward direction.
18) 8260
A fiber-type, self-locking nut must never be used on an aircraft if the bolt is
.
C — subject to rotation.
19) 8260-1. Self-locking nuts may be used on aircraft provided that
C—the bolt or nut is not subject to rotation.
20) 8267
(Refer to Figure 43.) Identify the clevis bolt illustrated.
B — 3.
21) 8271
Where is an AN clevis bolt used in an airplane?
C — Only for shear load applications.
22) 8275
Aircraft bolts are usually manufactured with a
C — class 3 fit for the threads
23) 8261-1
Which is an acceptable safety device for a castle nut when installed on secondary structures?
.
C — Cotter pin.