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BLK 10 Final Exam Study Set 2

Total questions: 41

Worksheet time: 21mins

Name
Class
Date
1.

What type of inspection detects defects such as surface cracks or porosity?

a)

Magnetic particle

b)

Both are correct

c)

Liquid penetrant

2.

Which composite inspection method is also referred to as the ring or coin test?

a)

Tap test

b)

Ultrasonic inspection

3.

Control cables for the primary flight control surfaces tend to vibrate, the probable cause is:

a)

Excessive wear tension.

b)

Worn or defective control surfaces.

c)

Worn maintenance fittings.

4.

How does a rotorcraft compensate for blowback?

a)

By continuously moving the cyclic control aft as the velocity of the helicopter increases.

b)

By pulling aft on the collective control.

c)

By continuously moving the cyclic control forward as the velocity of the helicopter increases.

5.

Where can you find the scope and detail for annual and 100-hour inspections?

a)

FAR 43.13, Appendix A

b)

FAR 43.13, Appendix D

c)

FAR 43.13, Appendix C

6.

Which FAR deals with the acceptable rules of Airworthiness Directives?

a)

FAR 43.13, Appendix A

b)

FAR 43.13, Appendix D

c)

FAR 43.13, Appendix C

7.

When inspecting something at 100-hour inspection or an airplane equipped with a push-pull tube-type control system is true?

a)

The threaded rod ends should be adjusted in length for rigging purposes because the rod may have been properly positioned and staked during manufacture.

b)

The terminal rod ends and threads of the turnbuckles should be visible through the safety hole in the inspection hole provided.

c)

The threaded rod ends should be checked for the amount of thread engagement by means of the inspection hole provided.

8.

When installing electrical equipment, all necessary information should be obtained from:

a)

Illustrated parts manual for the aircraft

b)

The aircraft maintenance manual

c)

Maintenance instructions published by the aircraft and/or equipment manufacturer

9.

Aircraft directional stability is stability about which axis?

a)

Lateral

b)

Vertical

c)

Longitudinal

10.

Which statement is correct when an aircraft has not been approved for service after an annual inspection because of several items requiring minor repair?

a)

The person who performed the annual inspection may approve the aircraft for return to service.

b)

An appropriately rated mechanic may repair the defects, but an IA must approve the aircraft for return to service.

c)

An appropriately rated mechanic may repair and approve the aircraft for return to service.

11.

Information regarding approval for return to service of items below can be found in an aircraft TCDS?

a)

Minimum fuel grade.

b)

Maximum weight.

c)

Minimum flight crew.

12.

It has no difference whether an airplane is moving with respect to the air, or the air is moving with respect to the airplane.

a)

True

b)

False

13.

The cable-operated control system of an all-metal aircraft, the incorporating a temperature compensating device, has been rigged to the correct tension in a heated hangar. If the aircraft is operated in very cold weather, the cable tension will

a)

Decrease when the aircraft structure and cables become cold.

b)

Increase when the aircraft structure and cables become cold.

c)

Not be affected by temperature change.

14.

Aircraft control lock systems must be designed and installed so that the

a)

Pilot can operate the elevator control in the normal manner, but takeoff is prevented.

b)

Pilot can operate the elevator control in the normal manner, but the control system is disconnected.

c)

Pilot can operate the elevator control in the normal manner, but the control system is locked.

15.

After repairing a fabric-covered aircraft, the surface should be rebalanced to

a)

Its manufacturer's specifications.

b)

Its symmetry axis.

c)

Its normal flight position.

16.

Operating control from the left will always move in the same direction.

a)

True

b)

False

17.

Pilot can see the relative position of the trim tab from the cockpit.

a)

True

b)

False

18.

The elevator control position of the trim tab becomes inappropriate if the primary flight control system fails.

a)

True

b)

False

19.

Which FAR requires the requirements for certification of airmen other than flight crewmembers?

a)

Part 65

b)

Part 91

c)

Part 43

20.

Which FAA form should be used to record a major repair or alteration on an aircraft?

a)

Form 43

b)

Form 91

c)

Form 337

21.

The purpose of the vertical fin is to provide:

a)

Lateral stability.

b)

Directional stability.

c)

Longitudinal stability.

22.

The purpose of issuing Airworthiness Directives (ADs) is to:

a)

Correct an unsafe condition.

b)

Notify owners of new regulations.

c)

Instruct maintenance personnel.

23.

Which of the following are advantages of magnetic particle inspections?

a)

Imitate results.

b)

Parts do not need to be demagnetized after testing.

c)

Correct or unsafe condition.

24.

Where would you find precise information to perform a symmetry alignment check for a particular aircraft?

a)

Aircraft Specification or Type Certificate Data Sheet.

b)

Aircraft Service or Maintenance Manual.

c)

Manufacturer's service bulletins.

25.

The purpose of spring tabs or servo tabs is to:

a)

Contribute to the balance of the control surface.

b)

Increase the force needed by the pilot to change the flight control position.

c)

Assist the pilot in moving the control surfaces.

26.

Where would an AME mechanic find descriptions of aircraft systems, lubrication instructions, methods of:

a)

Overhaul manual.

b)

Maintenance manual.

c)

Leveling acc.

27.

Which manual contains complete instructions for maintenance of all systems and components installed in the aircraft?

a)

Overhaul manual.

b)

IPC.

c)

TCDS.

28.

Which inspection program allows an annual inspection to be conducted in phases?

a)

Progressive.

b)

Calendar.

c)

100-hour.

29.

If the control stick or an aircraft with properly rigged flight controls is moved forward and to the right, the left aileron will move:

a)

Up and the elevator will move down.

b)

Down and the elevator will move down.

c)

Down and the elevator will move up.

30.

Which FAR deals with General Operating and Flight Rules?

a)

FAR Part 21

b)

FAR Part 91

c)

FAR Part 43

31.

Which type of flight control has aerodynamically positioned a control surface that requires too much force to move manually?

a)

Balance tabs

b)

Servo tabs

c)

Spring tabs

32.

Where would you find the operating conditions that make a 100-hour inspection mandatory?

a)

14 CFR Part 21

b)

14 CFR Part 91

c)

14 CFR Part 43

33.

If the level of an airplane's control is correct but the airplane is heavy in the controls, what is the most probable cause?

a)

The control cables are rigged to the proper tension.

b)

The control cables tension is too loose.

c)

The control cables tension is too tight.

34.

Which of the following describes the type design of an aircraft and sets forth the limitations prescribed by the Administrator?

a)

Supplemental Type Certificate

b)

Airworthiness Certificate

c)

Type Certificate Data Sheet

35.

What must be issued before a modification may be made to a type certificated aircraft?

a)

Advisory Circular

b)

Maintenance Service Bulletin

c)

Supplemental Type Certificate

36.

If the manufacturer's checklist for the annual or 100-hour inspection is not available, what checklist reference would you use?

a)

FAR 91

b)

FAR 43 Appendix A

c)

FAR 43 Appendix D

37.

Where can you find a formal description of the aircraft engine, or propeller?

a)

AMM

b)

TCDS

c)

AC 43.13 1B

38.

Which fuselage construction relies largely on the strength of the skin to overcome or carry the primary loads?

a)

Monocoque type

b)

Truss type

c)

Semimonocoque type

39.

What physical factors are involved in the aspect ratio of airplane wings?

a)

Thickness and chord

b)

Dihedral and angle of attack

c)

Span and chord

40.

Airplane firewalls are not typically made from:

a)

Titanium

b)

Stainless steel

c)

Aluminum

41.

Airworthiness Directives (ADs) are designed to notify:

a)

Certain owners and operators of records, techniques, and acceptable practices for inspection and alteration of aircraft

b)

Condition under which the aircraft may continue to be operated

c)

Specific in the aircraft maintenance manual.