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DAB QUIZ 1 AMT 1303 (Sept22-Feb23)

Total questions: 41

Worksheet time: 21mins

Name
Class
Date
1.

Type your name

(a)  

2.

The word "________" refers to the theory, investigation, and classification of flight failures as well as the regulation, instruction, and training necessary to prevent such failures.

a)

Aviation safety

b)

Aviation security

c)

Aviation sector

3.

The overhaul, repair, inspection, or modification of an aircraft or aircraft component is known as _________

a)

Aircraft maintenance

b)

Aircraft management

c)

Aircraft manufacturer

4.

The majority of aeroplane failures are caused by ______ rather than maintenance problems.

a)

human emotion

b)

human ego

c)

Human error

5.

Why aircraft maintenance is very important?

a)

ensure the safety and comfort of passengers

b)

To achieve aircraft maintenance standardization among countries

c)

Effect on company image

6.

Who is National Authority in Malaysia?

a)

Department of Civil Aviation Malaysia (DCAM).

b)

Civil Aviation Authority of Malaysia (CAAM)

c)

Federal Aviation Authority of Malaysia (FAAM)

d)

Federal Aviation Administration

7.
Defect means...
a)
imperfection
b)
difficulty
c)
destroyed
d)
details
8.

The acronym LAME stands for

a)

Licensed Aircraft Maintenance Engineer

b)

Little Animals who Make Enchiladas

c)

Licensed Aviation Mechanical Engineer

d)

Licensed Aircraft Mechanical Engineer

9.

Which is NOT an airline maintenance inspection check?

a)

A checks

b)

C checks

c)

B checks

d)

AA checks

10.

Who is responsible for being certain an aircraft has has proper inspections?

a)

The owner/operator

b)

The pilot

c)

The mechanic

d)

The FAA

11.

_________________ that have to be done on all commercial aircraft after a certain amount of time and usage.

a)

Aircraft Maintenance Checks

b)

Aircraft Maintenance Customer

c)

Aircraft Manufacturing Checks

12.
A Fuselage Station is a
a)
lateral line on an aircraft wing.
b)
vertical line on aircraft fuselage.
c)
longitudinal line on the aircraft fuselage.
13.
Which of the following is primary structure for fuselage?
a)
Frame.
b)
Rib
c)
Stringer.
14.
One purpose of a rib is to
a)
support the bending loads on a fuselage.
b)
form the main lateral member in an aerofoil.
c)
maintain the correct contour of aerofoils covering.
15.
The two common configurations for landing gear arrangements are:
a)
Conventional and tricycle
b)
Traditional and bicycle
c)
Amphibian and belly gear
16.
Which statement below that can best relate to the advanced composite material?
a)
Low strength to weight ratio
b)
High strength to weight ratio
c)
High stiffness to strength ratio
17.
Main spar is classified as which structural category?
a)
Tertiary
b)
Secondary
c)
Primary
18.

What force is being exhibited here?

a)

Tensile

b)

Tension

c)

Torsion

d)

Compression

19.

The most common type of airframe construction is...

a)

semi-monocoque

b)

truss

c)

stressed frame

d)

monocoque

20.

In the picture, which letter is pointing to a Longeron?

a)

A

b)

B

c)

C

d)

D

21.

Monocoque fuselage are widely used in 1930s.

a)

TRUE

b)

FALSE

22.

The component of monocoque structure are;

a)

Bulkhead

b)

Skin

c)

Formers

d)

Stringers

23.

A fuselage structure that constructed of wood, steel, or aluminum tubing.

a)

Semimonocoque

b)

Monocoque

c)

Open Truss

24.

A fuselage structures that compose of Bulkhead. Formers and Stresses Skin.

a)

Open Truss

b)

Semimonocoque

c)

Monocoque

25.

The material which contains iron as the base metal ,is called

a)

Non ferrous

b)

Magnesium alloy

c)

Titanium alloy

d)

Ferrous metal

26.

Elasticity is

a)

The ability of the metal to retain its size and shape after the applied load

b)

The ability of a metal to change size and shape permanently

c)

The ability of the metal to return to its original size and shape

d)

The ability of the metal to have same physical and chemical properties

27.

The ability of the metal to be permanently drawn, bent, or twisted into various shapes

a)

Ductility

b)

Malleability

c)

Brittleness

d)

Hardness

28.

Which property of a metal allows to shape the metals to sheets

a)

Ductility

b)

Hardness

c)

Malleability

d)

Thermal expansion

29.

What is the maximum percentage of carbon added to iron ,to form carbon steel

a)

3%

b)

2%

c)

1.5%

d)

5%

30.

What material would be used where a high temperature application is required, e.g. a firewall?.                   

a)

Carbon / Graphite fibres

b)

Ceramic fibres

c)

Kevlar fibres

31.

Fabrics may be fitted to airframe structures by

a)

Always riveting

b)

Wood nails

c)

Tying on with string

32.
What is composite material?
a)
a mixture of two or more metal alloys that merge and dissolve together
b)
a mixture of iron and carbon
c)
a mixture of two or more different materials that do not merge or dissolve together
33.
Aircraft wood damage is mainly caused by:
a)
Moisture
b)
Salt
c)
mercury
34.
Galvanic corrosion is often identified as:
a)
reddish powder on the surface
b)
blisters on the surface
c)
pitting on the surface
35.
The corrosion that is caused by areas of potential difference within the metal grain is known as:
a)
surface corrosion
b)
Pitting corrosion
c)
Inter-granular corrosion
36.
Fretting corrosion is caused by:
a)
rubbing of two moving parts or surfaces
b)
potential differences between the metal grains
c)
Internal stress during manufacture of the part
37.
Corrosion found on ferrous metal is indicated by:
a)
whitish-grey powder on the surface
b)
reddish-brown powder on the surface
c)
blue-greenish salt on the surface
38.
What is the name of the pitch that has few threads per inch?
a)
Fine Pitch
b)
Coarse Pitch
c)
Medium Pitch
39.
The advantage of using a fine pitch screw thread is:
a)
greater resistance to slackening under vibration
b)
greater lead that gives more rapid action
c)
stronger threads (but weaker core diameter)
40.
The type of nut that can withstand severe vibration without loosening is:
a)
non-self locking nut
b)
self-locking nut
c)
castellated nut
41.
Microbiological corrosion in integral fuel tank with aviation kerosene is caused by:
a)
bacteria and fungus
b)
virus and stress action
c)
fungus and heat

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