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AMT 7A-05LC FINALS EXAM

Total questions: 100

Worksheet time: 50mins

Name
Class
Date
1.
  1. What is the width of material measured around the bends from edge to edge?

a)
  1. Total Developed Width

b)
  1. Setback

c)
  1. Flat

2.

What is the portion of a part that is not included in the bend?

a)
  1. Total Developed Width

b)
  1. Setback

c)
  1. Flat

3.

What is equal to the base measurement (MLD) minus the setback?

a)
  1. Total Developed Width

b)
  1. Setback

c)
  1. Flat

4.

What is the portion of a part that is not included in the bend?

a)
  1. Total Developed Width

b)
  1. Setback

c)
  1. Flat

5.

What is less than the sum of mold line dimensions since the metal is bent on a radius and not to a square corner as mold line dimensions indicate?

a)
  1. Total Developed Width

b)
  1. Setback

c)
  1. Flat

6.
  1. Who designates specifications for the materials to be used to ensure the finished part has the correct temper when it leaves the machines, planning every part?

a)
  1. Factory Engineers

b)
  1. Factory draftsmen

c)
  1. Engineers

7.
  1. Who prepares a layout for each part?

a)
  1. Factory Engineers

b)
  1. Factory draftsmen

c)
  1. Engineers

8.
  1. What is achieved by hammering or rolling metal under pressure? 

a)
  1. Stretching

b)
  1. Shrinking

c)
  1. Bumping

9.
  1. Does hammering a flat piece of metal cause the material in the hammered area to become thinner in that area?

a)
  1. Stretching

b)
  1. Shrinking

c)
  1. Bumping

10.
  1. What if the material in the horizontal flange will merely bend down at the center, and the length of that flange will remain the same?

a)
  1. Stretching

b)
  1. Shrinking

c)
  1. Bumping

11.
  1. Does metal get forced or compressed into a smaller area? 

a)
  1. Stretching

b)
  1. Shrinking

c)
  1. Bumping

12.
  1. What requires the combination of a hard surface, such as wood or steel?

a)
  1. Cold Shrinking

b)
  1. Shrinking

c)
  1. Hot Shrinking

13.
  1. What involves shaping or forming malleable metal by hammering or tapping?

a)
  1. Stretching

b)
  1. Shrinking

c)
  1. Bumping

14.
  1. What is critical to ensure the metal is not stretched too much, making it too thin, because sheet metal does not rebound easily?

a)
  1. Stretching

b)
  1. Shrinking

c)
  1. Bumping

15.
  1. Is the metal supported by a dolly, a sandbag, or a die?

a)
  1. Stretching

b)
  1. Shrinking

c)
  1. Bumping

16.
  1. What is folding, pleating, or corrugating a piece of sheet metal in a way that shortens it by turning down a flange on a seam?

a)
  1. Crimping

b)
  1. Folding

c)
  1. Bumping

17.
  1. What is it called to make a bend or crease in sheets, plates, or leaves?

a)
  1. Crimping

b)
  1. Folding

c)
  1. Bumping

18.
  1. What is often used to make one end of a piece of stove pipe slightly smaller so that one section may be slipped into another?

a)
  1. Crimping

b)
  1. Folding

c)
  1. Bumping

19.
  1. What is the shorter part of a formed angle?

a)
  1. Base Measurement

b)
  1. Leg

c)
  1. Flange

20.
  1. Can interfere with the operation of the aircraft's electrical and electronic systems by coupling electromagnetic energy to the system wiring and components

a)
  1. HFIR

b)
  1. HRIF

c)
  1. HIRF

21.
  1. What is increasingly dependent upon electrical/electronic systems, which can be susceptible to electromagnetic interference?

a)
  1. Operation of modern aircraft

b)
  1. Emitters

c)
  1. Modern Digital System

22.
  1. What are highly susceptible to HIRF?

a)
  1. Operation of modern aircraft

b)
  1. Emitters

c)
  1. Modern Digital System

23.
  1. What is increasing in number and in power. 

a)
  1. Operation of modern aircraft

b)
  1. Emitters

c)
  1. Modern Digital System

24.
  1. Airframe Skin and Frame

a)
  1. Aircraft Structure

b)
  1. Electrical Wiring Installation Protection 

c)
  1. Equipment Protection 

25.
  1. LRU case, Electronics Input Output Protection

a)
  1. Aircraft Structure

b)
  1. Electrical Wiring Installation Protection 

c)
  1. Equipment Protection 

26.
  1. Solid or Braided Shielding Connectors. 

a)
  1. Aircraft Structure

b)
  1. Electrical Wiring Installation Protection 

c)
  1. Equipment Protection 

27.
  1. What is the first and generally most important step in HIRF maintenance?

a)
  1. Inspection

b)
  1. Special Inspection

c)
  1. Visual inspection

28.
  1. What is the most easily detected sign of an excessive load having been imposed during a landing? 

a)
  1. Wrinkled wing skin

b)
  1. Dents

c)
  1. Damaged skin

29.
  1. What should be performed after a flight through severe turbulence?

a)
  1. Inspection

b)
  1. Special Inspection

c)
  1. Visual inspection

30.
  1. What material may soften the fabric or loosen the fabric tapes of fabric covered aircraft?

a)
  1. paint

b)
  1. chemicals

c)
  1. metals

31.
  1. What can cause damage to the aircraft both visible and hidden?

a)
  1. Lightning Strike

b)
  1. Fire Damage

c)
  1. Heavy Landing

32.
  1. What may occur if the aircraft is not parallel to the runway when it lands or if the nose- or tail-wheel strikes the runway before the main wheels?

a)
  1. Fatigue

b)
  1. Stress

c)
  1. Overstressing

33.
  1. What may be expected following a heavy landing would normally be concentrated around the landing gear?

a)
  1. Primary Damage

b)
  1. Secondary Damage

c)
  1. Tertiary Damage

34.
  1. What may be found on the fuselage upper and lower skins and on the wing skin and structure?

a)
  1. Primary Damage

b)
  1. Secondary Damage

c)
  1. Tertiary Damage

35.
  1. What should be examined for creep, damage, and cuts?

a)
  1. Landing Gear

b)
  1. Fuselage

c)
  1. Mainplanes

36.
  1. What is given on the drawing or blueprint or may be obtained from the original part?

a)
  1. Base Measurement

b)
  1. Leg

c)
  1. Flange

37.
  1. What can be replaced with another brake radius bar with a different diameter?

a)
  1. Brake Radius Bars

b)
  1. Setback

c)
  1. Flat

38.
  1. Lay out the basic part using ________ layout procedures. 

a)
  1. Traditional

b)
  1. Bend

c)
  1. Trim out

39.
  1. Is often tangent to the radius and perpendicular to the edge

a)
  1. Traditional

b)
  1. Bend

c)
  1. Trim out

40.
  1. What are the present unique problems that require more calculations than 90° bends? 

a)
  1. open bends

b)
  1. open and close bends

c)
  1. close bends

41.
  1. If the flange is to be shrunk, place the flange across the ____.

a)
  1. V-block

b)
  1. D-block

c)
  1. B-block

42.
  1. Parts are usually hand formed with a concave flange, the inside edge, and a convex flange, the outside edge. 

a)
  1. Curved Flange

b)
  1. Plain Nose Rib

c)
  1. Concave Flange

43.
  1. It is formed by stretching, while the convex flange is formed by shrinking.

a)
  1. Curved Flange

b)
  1. Plain Nose Rib

c)
  1. Concave Flange

44.
  1. only one large convex flange is used

a)
  1. Curved Flange

b)
  1. Plain Nose Rib

c)
  1. Concave Flange

45.
  1. It is difficult to form, but the outside flange is broken up into smaller sections by relief holes.

a)
  1. Curved Flange

b)
  1. Plain Nose Rib

c)
  1. Concave Flange

46.
  1. These are placed at equally spaced intervals to absorb material and cause curving. 

a)
  1. Crimps

b)
  1. Holes

c)
  1. Nose Rib

47.
  1. What is formed by crimping, beading, putting in relief holes, and using a formed angle riveted on each end?

a)
  1. Crimps

b)
  1. Holes

c)
  1. Nose Rib

48.
  1. What is formed by shrinking the material over a form block?

a)
  1. Convex Surfaces

b)
  1. Concave Surfaces

c)
  1. Surfaces

49.
  1. What can be done on a form block or female die, or on a sandbag?

a)

Shrinking

b)

Bumping

c)

Stretching

50.
  1. Designed for form block bumping must have the same dimensions and contour as the outside of the blister

a)

Wooden Die

b)

Wooden Block

c)

Sandbag Bumping

51.
  1. What is one of the most difficult methods of hand forming sheet metal because there is no exact forming block to guide the operation?

a)

Wooden Die

b)

Wooden Block

c)

Sandbag Bumping

52.
  1. What can cause visible damage, like small circular holes on the aircraft external skin?

a)

Lighting

b)

Lightning

c)

Lights

53.
  1. What is designed to withstand repeated landings within an aircraft weight limit and within a vertical descent speed limit?

a)

Landing Gear

b)

Fuselage

c)

Engines

54.
  1. It is only performed after abnormal events, which could possibly have caused damage to the aircraft or impaired the airworthiness.

a)

Unscheduled Checks

b)

Scheduled Checks

c)

Planned Checks

55.
  1. After an extremely hard landing or other unusual loads on the landing gear.

a)

Damaged Landing

b)

Unusual Landing

c)

Hard Landing

56.
  1. For damage evaluation consult the manufacturer, before the aircraft is put back into service.

a)

Engine

b)

Engine Fire

c)

Engine Flood

57.
  1. When performing any abnormal event inspection, always follow the detailed procedures in the aircraft maintenance manual.

a)

Special Inspections

b)

Scheduled Inspections

c)

Unscheduled Inspections

58.
  1. During the service life of an aircraft, occasions may arise when something out of the ordinary care and use of the aircraft might happen that could possibly affect its airworthiness. 

a)

Special Inspections

b)

Scheduled Inspections

c)

Unscheduled Inspections

59.
  1. Visual inspection is the first and most important step that is often sufficient to find the deterioration of the protective features.

a)

HFIR

b)

HRIF

c)

HIRF

60.
  1. Are extremely rare to aircraft.

a)

Lighting Strikes

b)

Lightning Strikes

c)

Lights Strikes

61.
What can cause visible damage, like small circular holes on the aircraft external skin?
a)
Lighting
b)
Lightning
c)
Lights
62.
What is designed to withstand repeated landings within an aircraft weight limit and within a vertical descent speed limit?
a)
Landing Gear
b)
Fuselage
c)
Engines
63.
It can only performed after abnormal events, which could possibly have caused damage to the aircraft or impaired the airworthiness
a)
Unscheduled Checks
b)
Scheduled Checks
c)
Planned Checks
64.
After an extremely hard landing or other unusual loads on the landing gear.
a)
Damaged Landing
b)
Unusual Landing
c)
Hard Landing
65.
For damage evaluation consult the manufacturer, before the aircraft is put back into service.
a)
Engine
b)
Engine Fire
c)
Engine Flood
66.
When performing any abnormal event inspection, always follow the detailed procedures in the aircraft maintenance manual.
a)
Special Inspections
b)
Scheduled Inspections
c)
Unscheduled Inspections
67.
During the service life of an aircraft, occasions may arise when something out of the ordinary care and use of the aircraft might happen that could possibly affect its airworthiness.
a)
Special Inspections
b)
Scheduled Inspections
c)
Unscheduled Inspections
68.
Visual inspection is the first and most important step that is often sufficient to find the deterioration of the protective features.
a)
HFIR
b)
HRIF
c)
HIRF
69.
What are extremely rare to aircraft?
a)
Lighting Strikes
b)
Lightning Strikes
c)
Lights Strikes
70.
What can interfere with the operation of the aircraft's electrical and electronic systems by coupling electromagnetic energy to the system wiring and components?
a)
HFIR
b)
HRIF
c)
HIRF
71.
What is increasingly dependent upon electrical/electronic systems, which can be susceptible to electromagnetic interference?
a)
Operation of modern aircraft
b)
Emitters
c)
Modern Digital System
72.
What are highly susceptible to HIRF?
a)
Operation of modern aircraft
b)
Emitters
c)
Modern Digital System
73.
What are increasing in number and in power?
a)
Operation of modern aircraft
b)
Emitters
c)
Modern Digital System
74.
Airframe Skin and Frame
a)
Aircraft Structure
b)
Electrical Wiring Installation Protection
c)
Equipment Protection
75.
LRU case, Electronics Input Output Protection
a)
Aircraft Structure
b)
Electrical Wiring Installation Protection
c)
Equipment Protection
76.
Solid or Braided Shielding Connectors.
a)
Aircraft Structure
b)
Electrical Wiring Installation Protection
c)
Equipment Protection
77.
What is the first and generally most important step in HIRF maintenance?
a)
Inspection
b)
Special Inspection
c)
Visual inspection
78.
What is the most easily detected sign of an excessive load having been imposed during a landing.
a)
Wrinkled wing skin
b)
Dents
c)
Damaged skin
79.
What should be performed after a flight through severe turbulence?
a)
Inspection
b)
Special Inspection
c)
Visual inspection
80.
What material may soften the fabric or loosen the fabric tapes of fabric covered aircraft?
a)
paint
b)
chemicals
c)
metals
81.

What can cause damage to the aircraft both

visible and hidden?

a)
  1. Lighting

b)

Lightning

c)

Lights

82.

What is designed to withstand repeated landings within an aircraft weight limit and within a vertical descent speed limit?

a)

Landing Gear

b)
  1. Fuselage

c)
  1. Engines

83.

It can only performed after abnormal events,

which could possibly have caused damage to

the aircraft or impaired the airworthiness

a)

Unscheduled Checks

b)

Scheduled Checks

c)

Planned Checks

84.

After an extremely hard landing or other unusual loads on the landing gear.

a)

Damaged Landing

b)

Unusual Landing

c)

Hard Landing

85.

For damage evaluation consult the manufacturer, before the aircraft is put back

into service.

a)

Engine

b)

Engine Fire

c)

Engine Flood

86.

When performing any abnormal event inspection, always follow the detailed procedures in the aircraft maintenance manual.

a)

Special Inspections

b)

Scheduled Inspections

c)

Unscheduled Inspections

87.

During the service life of an aircraft, occasions may arise when something out of the ordinary care and use of the aircraft might happen that could possibly affect its airworthiness.

a)

Special Inspections

b)

Scheduled Inspections

c)

Unscheduled Inspections

88.

Visual inspection is the first and most important step that is often sufficient to find the deterioration of the protective features.

a)

HFIR

b)

HRIF

c)

HIRF

89.

What are extremely rare to aircraft?

a)

Lighting Strikes

b)

Lighting Strikes

c)

Lighting Strikes

90.

What can interfere with the operation of the aircraft's electrical and electronic systems by coupling electromagnetic energy to the system wiring and components?

a)

HRIF

b)

HFIR

c)

HIRF

91.

What is increasingly dependent upon electrical/ electronic systems, which can be susceptible to electromagnetic interference?

a)

Operation of modern aircraft

b)

Emitters

c)

Modern Digital System

92.

What are highly susceptible to HIRF?

a)

Operation of modern aircraft

b)

Emitters

c)

Modern Digital System

93.

What are increasing in number and in power?

a)

Operation of modern aircraft

b)

Emitters

c)

Modern Digital System

94.
  1. Airframe Skin and Frame

a)

 Aircraft Structure

b)

Electrical Wiring Installation Protection

c)

Equipment Protection

95.

Solid or Braided Shielding Connectors.

a)

Aircraft Structure

b)

Electrical Wiring Installation Protection

c)

Equipment Protection

96.

What is the first and generally most important

step in HIRF maintenance?

a)

Inspection

b)

Special Inspection

c)

Visual inspection

97.

What is the most easily detected sign of an excessive load having been imposed during a landing.

a)

Wrinkled wing skin

b)

Dents

c)

Damaged skin

98.

What should be performed after a flight through severe turbulence?

a)

Inspection

b)

Special Inspection

c)

Visual inspection

99.

What material may soften the fabric or loosen the fabric tapes of fabric covered aircraft?

a)

paint

b)

chemicals

c)

metals

100.

LRU case, Electronics Input Output Protection

a)

Aircraft Structure

b)

Electrical Wiring Installation Protection

c)

Equipment Protection