Powerplant IV Mod 2 Quiz

5.0(1)
studied byStudied by 10 people
5.0(1)
full-widthCall Kai
learnLearn
examPractice Test
spaced repetitionSpaced Repetition
heart puzzleMatch
flashcardsFlashcards
GameKnowt Play
Card Sorting

1/49

flashcard set

Earn XP

Description and Tags

Turbine Overhaul and Maintenance

Study Analytics
Name
Mastery
Learn
Test
Matching
Spaced

No study sessions yet.

50 Terms

1
New cards

What is the recommended method for repairing corrosion pitting on compressor stator vanes?

Blending

2
New cards

What are examples of blade damage in axial-flow and centrifugal-flow engines?

All of the above;

Damage to the outer half of the blade

Nicks and dents in the critical band

Cracks in the leading edges

3
New cards

Why is it important to follow the manufacturer's maintenance and overhaul manuals when performing repairs or inspections on turbine engines?

To ensure proper functioning of the engine

4
New cards

What is the recommended method for cleaning turbine blades during a hot section inspection?

Ultrasonic cleaning

5
New cards

What is the purpose of using a borescope inspection during a hot section inspection?

To check for cracks and warping

6
New cards

What is the importance of following the manufacturer's detailed assembly instructions during engine maintenance?

All of the above;

To extend the engine's service life

To prevent foreign material from entering the engine

To ensure efficient maintenance

7
New cards

Which marking material is recommended for parts directly exposed to the engine's gas path?

All answers are correct;

Felt tip marker and chalk

8
New cards

What method is recommended for inspecting combustion chambers for cracks?

Fluorescent penetrant inspection

9
New cards

Which type of crack is considered the most severe in combustion chambers?

Stress rupture cracks

10
New cards

What is the recommended method for reinstalling turbine blades after inspection?

Numbering the blades and reinstalling them in the same slots

11
New cards

What is the flat rating of a turbine engine?

The guaranteed thrust under specific operating conditions

12
New cards

Why is it important to monitor EGT during takeoff?

To prevent damage to the engine

13
New cards

What is the purpose of the N1 indicator in a turbine engine?

To indicate engine speed

14
New cards

Why is it impractical to measure turbine inlet temperature in most engines?

Because it is too hot

15
New cards

Why are tachometers usually calibrated in percent rpm?

To make it easier to compare different types of engines

16
New cards

What is the purpose of following manufacturer's operating instructions for starting and operating a turbine engine?

To avoid a hot or hung start

17
New cards

What is the appropriate action to take in case of an engine fire during start or ground operation?

Move the fuel lever to the off position and continue cranking or motoring the engine until the fire has been expelled from the engine.

18
New cards

How is the takeoff power for a turboprop engine calculated?

By determining the maximum allowable exhaust gas temperature and torquemeter pressure

19
New cards

What is the purpose of a continuity check in an aircraft EGT circuit?

To eliminate any error caused by one or more inoperative aircraft thermocouples

20
New cards

Why is regular testing and maintenance important for an EGT system?

All answers are correct;

To ensure the accuracy of the EGT indicator

To prevent potential errors in the system

To troubleshoot any issues that may arise

21
New cards

An APU is usually rotated during start by?

An electric starter

22
New cards

Fuel is normally supplied to an APU from

The airplanes main fuel supply

23
New cards

Frequently, an aircraft auxiliary power unit (APU) generator

Is identical to the engine-driven generators

24
New cards

Usually, the most load placed on an APU occurs when

The bleed air valve is opened

25
New cards

Fuel scheduling during APU start and under varying pneumatic bleed and electrical loads is maintained by

Automatically by the APU fuel control system

26
New cards

The function of an APU plenum is to

Stabilize the pressure before of the air before it enters the compressor

27
New cards

Standard sea level pressure is:

29.92 in. Hg

28
New cards

When in operation the speed of an APU

Remains at or near rated speed regardless of the load condition

29
New cards

An APU uses aircraft fuel, supplied under pressure by

Electric boost pump

30
New cards

An APU can provide redundancy to aircraft systems by

Providing a back up electrical and pneumatic source

31
New cards

Where is the highest temperature in a turbine engine with respect to the metal parts?

Turbine inlet nozzle vanes

32
New cards

What is the name given to the thermodynamic cycle of a APU gas turbine engine uses to produce electrical or pneumatic power?

Continuous combustion cycle

33
New cards

T or F:
Compressor inlet screens are used on Turboprops and APUs to prevent all FOD from entering the intake of the engine

False

34
New cards

T or F:
APUs are installed in the aircraft and are used to supply electrical power, air hydraulic pressure, and fuel to the aircraft engines when the main engines are not running.

False

35
New cards

T or F:
APU’s are small gas turbine engines or reciprocating-engine that power a generator, hydraulic pump, and air pump.

True

36
New cards

An APU can be operated:


Both A and B;
While the aircraft is in flight and While the aircraft is on the ground

37
New cards

T or F:
An APU is usually manually controlled

False

38
New cards

T or F:

An APU can only be operated while on the ground?

False

39
New cards

An APU is usually rotated during start by:

An electrical starter

40
New cards

Most APU’s have automatic controls for starting, stopping and maintaining operation within safe limits because:

They provide the correct sequencing of the start cycle

41
New cards

Where is the highest gas pressure in a turbojet engine?

At the outlet of the compressor section

42
New cards

The pressure of subsonic air as it flows through a convergent duct :

Decreases Pressure

43
New cards

Name the four basic types of Combustion Sections used in aircraft turbine engines?

Can type, Reverse-flow type, Annular type and Can-annular type

44
New cards

The exhaust section of a turbine engine is designed to

Impart a high exit velocity to the exhaust gases

45
New cards

Using Standard Day Conditions, What is the standard sea level temperature?

59 degrees F

46
New cards

Using Standard Day Conditions, What is the standard sea level pressure?

29.92 in. Hg

47
New cards

What are the two types of compressors used in turbine engines?

Axial and centrifugal flow

48
New cards

Where is the highest temperature in a turbine engine with respect to the metal parts?


Turbine inlet nozzle vanes


49
New cards

What are the three types of turbine blades?

Impulse, reaction and impulse-reaction

50
New cards

What is the name given to the thermodynamic cycle of a gas turbine engine to produce thrust?

Brayton cycle