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Turbine Overhaul and Maintenance
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What is the recommended method for repairing corrosion pitting on compressor stator vanes?
Blending
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
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
What is the recommended method for cleaning turbine blades during a hot section inspection?
Ultrasonic cleaning
What is the purpose of using a borescope inspection during a hot section inspection?
To check for cracks and warping
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
Which marking material is recommended for parts directly exposed to the engine's gas path?
All answers are correct;
Felt tip marker and chalk
What method is recommended for inspecting combustion chambers for cracks?
Fluorescent penetrant inspection
Which type of crack is considered the most severe in combustion chambers?
Stress rupture cracks
What is the recommended method for reinstalling turbine blades after inspection?
Numbering the blades and reinstalling them in the same slots
What is the flat rating of a turbine engine?
The guaranteed thrust under specific operating conditions
Why is it important to monitor EGT during takeoff?
To prevent damage to the engine
What is the purpose of the N1 indicator in a turbine engine?
To indicate engine speed
Why is it impractical to measure turbine inlet temperature in most engines?
Because it is too hot
Why are tachometers usually calibrated in percent rpm?
To make it easier to compare different types of engines
What is the purpose of following manufacturer's operating instructions for starting and operating a turbine engine?
To avoid a hot or hung start
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.
How is the takeoff power for a turboprop engine calculated?
By determining the maximum allowable exhaust gas temperature and torquemeter pressure
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
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
An APU is usually rotated during start by?
An electric starter
Fuel is normally supplied to an APU from
The airplanes main fuel supply
Frequently, an aircraft auxiliary power unit (APU) generator
Is identical to the engine-driven generators
Usually, the most load placed on an APU occurs when
The bleed air valve is opened
Fuel scheduling during APU start and under varying pneumatic bleed and electrical loads is maintained by
Automatically by the APU fuel control system
The function of an APU plenum is to
Stabilize the pressure before of the air before it enters the compressor
Standard sea level pressure is:
29.92 in. Hg
When in operation the speed of an APU
Remains at or near rated speed regardless of the load condition
An APU uses aircraft fuel, supplied under pressure by
Electric boost pump
An APU can provide redundancy to aircraft systems by
Providing a back up electrical and pneumatic source
Where is the highest temperature in a turbine engine with respect to the metal parts?
Turbine inlet nozzle vanes
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
T or F:
Compressor inlet screens are used on Turboprops and APUs to prevent all FOD from entering the intake of the engine
False
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
T or F:
APU’s are small gas turbine engines or reciprocating-engine that power a generator, hydraulic pump, and air pump.
True
An APU can be operated:
Both A and B;
While the aircraft is in flight and While the aircraft is on the ground
T or F:
An APU is usually manually controlled
False
T or F:
An APU can only be operated while on the ground?
False
An APU is usually rotated during start by:
An electrical starter
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
Where is the highest gas pressure in a turbojet engine?
At the outlet of the compressor section
The pressure of subsonic air as it flows through a convergent duct :
Decreases Pressure
Name the four basic types of Combustion Sections used in aircraft turbine engines?
Can type, Reverse-flow type, Annular type and Can-annular type
The exhaust section of a turbine engine is designed to
Impart a high exit velocity to the exhaust gases
Using Standard Day Conditions, What is the standard sea level temperature?
59 degrees F
Using Standard Day Conditions, What is the standard sea level pressure?
29.92 in. Hg
What are the two types of compressors used in turbine engines?
Axial and centrifugal flow
Where is the highest temperature in a turbine engine with respect to the metal parts?
Turbine inlet nozzle vanes
What are the three types of turbine blades?
Impulse, reaction and impulse-reaction
What is the name given to the thermodynamic cycle of a gas turbine engine to produce thrust?
Brayton cycle