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material hardware 100-150

Total questions: 51

Worksheet time: 26mins

Name
Class
Date
1.

101) Typically made to be used on clevis bolts that don’t have drilled shanks. This is refer to

a)

A. Shear self-locking nut

b)

B. Anchor nut

c)

C. Tinnerman nut

2.

102) Pitting corrosion is the result of ;

a)

A.Two dissimilar metal contact to each other

b)

B. Improper quenching two dissimilar metal contact to each other

c)

C. Uniform surface corrosion left untreated.

3.

103) Type of cable fastener that allows cable tension to be adjusted by using;

a)

A. Turnbuckle

b)

B. Swage terminal

c)

C. Tensiometer

4.

103) What is the quenching method for annealing heat treatment?

a)

A. Cool at room temperature

b)

B. Water.

c)

C. Hot air/Furnace cool.

5.

104) Hole repair can be accomplish by using;

a)

A. Helicoil.

b)

B. Go no go gauge

c)

C. Quarter turn fastener

6.

105) What is the hardness designation for H38

a)

A. Strain hardened and stabilized & Full-hard

b)

B. Strain hardened only & Three-quarter hard.

c)

C. Strain hardened and partially annealed & Half-hard.

7.

106) The white powder which forms on the surface of aluminum alloy when it corrodes is the indication of

a)

A. Surface corrosion

b)

B. Galvanic corrosion.

c)

C. Oxidation.

8.

107) Flexible hose used in aircraft system is classified in size according to the;

a)

A. Outside diameter

b)

B. Wall thickness

c)

C. Inside diameter

9.

108) In addition to prevent corrosion by its biodical action, an additive in fuel also serves as

a)

A. An anti-freeze to prevent water from freezing

b)

B. To prevent the formation of scum.

c)

C. Both A and B are correct.

10.

109) Which of the following aluminum alloys is most commonly used for aircraft structural parts requiring high strength?

a)

A.1100.

b)

B.2024.

c)

C.5052

11.

110) What is the main characteristic of magnesium alloys that makes them difficult to work at room temperature?

a)

A.Low tensile strength.

b)

B. High thermal conductivity.

c)

C.Low ductility

12.

111) Which process is used to improve the mechanical properties of aluminum after cold working?

a)

A. Annealing

b)

B. Heat aging.

c)

C. Normalizing.

13.

112) Which aluminum alloy is known for its high fatigue strength and is commonly used in aircraft applications?

a)

6061

b)

7075

c)

1100

14.

113) What is the key reason for using titanium in aerospace applications?

a)

A) High malleability.

b)

B) High strength-to-weight ratio.

c)

C) Low production cost.

15.

114) In which process are aluminum alloys heated and slowly cooled to achieve maximum softness and ductility?

a)

A. Solution heat treatment.

b)

B. Annealing.

c)

C. Quenching.

16.

115) Choose the correct answer below

a)

A. T10 – Solution heat-treated, strain hardened and then artificially aged.

b)

B. T5 - Annealed (cast product only).

c)

C. T3 – Solution heat-treated followed by strain hardening .

17.

116) Cadmium plating of surface treatment for steel is

a)

A. Sacrificial process.

b)

B. Electrolytic process

c)

C. Both a and b are correct

18.

117) What type of load generally applied to Roller bearing?

a)

A. Radial load.

b)

B. Thrust load.

c)

C. Radial and thrust.

19.

118) Below are the purpose of bearing EXCEPT?

a)

A. Reduce friction.

b)

B. Enhance speed and efficiency.

c)

C. Tension and compress movement.

20.

119) Of the listed materials listed the highest percentage of copper content is in:

a)

7075

b)

2024

c)

5056

21.

120) Which non-ferrous metal alloy is known for its high electrical conductivity and is often used for electrical wiring in aircraft?

a)

aluminums

b)

copper

c)

Magnesium

22.

121) What is the effect of natural aging in aluminum alloys after solution heat treatment?

a)

A. Increased corrosion resistance

b)

B. Increased strength over time.

c)

C. Reduced hardness

23.

122) Which aluminum alloy is primarily used for fuel tanks and pipelines in aircraft due to its excellent corrosion resistance?

a)

A.1100.

b)

B.7075

c)

C.5052

24.

123) What is the key feature of Monel metal, which makes it suitable for marine applications in aircraft?

a)

A.Low cost.

b)

B. High strength.

c)

C. Excellent corrosion resistance.

25.

124) Which material property of beryllium copper makes it suitable for use in precision bearings and spring washers?

a)

A. High thermal conductivity

b)

B. High tensile strength.

c)

B. High tensile strength.

26.

125) What is the main purpose of solution heat treatment in aluminum alloys?

a)

A.To increase hardness through rapid cooling.

b)

B.To soften the metal by slow cooling

c)

C.To decrease malleability

27.

126) What is the primary role of artificial aging in the heat treatment of aluminum alloys?

a)

A.To reduce internal stresses

b)

B.To improve machinability.

c)

C.To increase strength and hardness.

28.

127) What is the main advantage of composite materials in aircraft structures?

a)

A.Lower cost.

b)

B. Higher density

c)

C. Higher strength-to-weight ratio.

29.

128) Which statement of rigid fluid line below is correct?

a)

A. Used extensively on aircraft to connect stationery parts to moving parts.

b)

B. Known as hose.

c)

C. Used in stationary applications where long, relatively straight runs are possible.

30.

129) What type of seal that is one way seal?

a)

A. Gasket.

b)

B. O-Ring packing

c)

C. V-Ring packing

31.

130) The application of dipping steel in the molten zinc is known as

a)

A. Metal spraying.

b)

B. Cadmium plating

c)

C. Galvanizing.

32.

131) What is Backlash?

a)

A. Inserted between two or more other gear wheels.

b)

B. Typically used in conveyor systems.

c)

C. Clearance between mating components

33.

132) What is the function of leaf spring?

a)

A. It provides dampness and springing function for heavy vehicles .

b)

B. Also known as spiral torsion, clock springs or brush springs

c)

C. It is also a form of helical spring.

34.

133) What is the purpose of using rivets made of 2024 or 7075 aluminum alloys in aircraft?

a)

A.To reduce the weight of the structure.

b)

B.To provide high strength for structural fastening

c)

C.To improve corrosion resistance

35.

134) What is the key characteristic of 6061 aluminum alloy that makes it versatile for use in various aircraft components?

a)

A) High malleability

b)

B) Excellent corrosion resistance.

c)

C) High electrical conductivity

36.

135) Which non-ferrous metal is widely used in aircraft for parts requiring good wear resistance and toughness, such as bushings and bearings?

a)

A. Copper.

b)

B. Brass.

c)

C. Beryllium copper

37.

136) What is the primary reason for using titanium in aircraft parts exposed to high temperatures?

a)

A. High strength-to-weight ratio

b)

B. Excellent electrical conductivity

c)

C.Low cost

38.

137) Which of the following aluminum alloys is typically used for aircraft fuselage skin due to its high strength?

a)

1100.

b)

2024

c)

7079

39.

138) What is the primary advantage of using composite materials in aircraft construction?

a)

A.Lower cost.

b)

B. Higher density

c)

C. Higher strength-to-weight ratio.

40.

139) Which alloy is commonly used for aircraft structural rivets due to its high strength?

a)

1101

b)

2024

c)

5052

41.

140) Which material is often used for parts in aircraft engines that must withstand both high temperatures and corrosion?

a)

A. Aluminum alloy

b)

B. Copper alloy.

c)

C.Titanium alloy

42.

141) What is the primary purpose of quenching in the heat treatment of aluminum alloys?

a)

A. Increase ductility.

b)

B. Increase hardness and strength.

c)

C. Reduce thermal expansion.

43.

142) What is the primary advantage of using foam-based cleaners on vertical surfaces?

a)

A.They provide longer dwell time and prevent dripping.

b)

B.They improve surface gloss.

c)

C.They are more cost-effective than liquid cleaners.

44.

143) What is the recommended procedure for cleaning de-icing boots?

a)

A. Wash with mild soap and water, then apply a protective conditioner.

b)

B. Rinse with high-pressure water.

c)

C. Immerse in solvent-based cleaners.

45.

144) Why should the interior of engine cowls be cleaned regularly?

a)

A.To enhance the engine’s aesthetic appearance.

b)

B.To remove grease and debris that could affect engine cooling

c)

C.To improve access during maintenance

46.

145) After cleaning an aircraft’s exhaust area, what should be inspected?

a)

A.The presence of streaks or residues.

b)

B.The condition of heat-resistant coatings and fasteners.

c)

C.The type of cleaning agent used

47.

146) Why is it important to inspect control cables after cleaning?

a)

A.To verify cleanliness and check for signs of wear or corrosion.

b)

B.To confirm proper alignment of the cables

c)

C.To enhance the gloss of the surrounding area.

48.

147) What is the purpose of using chemical-resistant footwear during cleaning?

a)

A.To enhance mobility in slippery conditions.

b)

B.To prevent cleaning agents from soaking through and causing skin irritation

c)

C.To meet uniform safety standards

49.

148) Why should personnel avoid overfilling spray bottles with cleaning agents?

a)

A.To reduce waste in case of spills

b)

B.To ensure consistent spray pressure.

c)

C.To prevent accidental leakage or overflow during use

50.

149) How should cleaning sponges used for acrylic windows be maintained?

a)

A. Rinse thoroughly and store in a sealed container

b)

B. Dry completely to avoid mold growth.

c)

C. Wash with kerosene to remove contaminants

51.

150) Why is it important to regularly replace worn cleaning tools?

a)

A.To improve cleaning efficiency and avoid damaging surfaces

b)

B.To enhance tool durability

c)

C.To ensure compatibility with cleaning agents.