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59 Cards in this Set

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  • Back
The ____ provides a uniform, turbulence-free supply of air to the compressor throughout all operating conditions.
Inlet Section
Page 1-3
The primary function of the ____ section is to increase the pressure of the mass of air entering the engine inlet and to discharge it into the combustion section at the correct velocity, temperature, and pressure.
Compressor Section
Page 1-4
The secondary function of the _____ section is to supply engine bleed air to cool the internal parts in the hot section, supply heated air for engine anti-icing, and supply air to the aircraft for use in the airframe systems.
Compressor
Page 1-4
What 2 types of compressors used in turbine engines?
Centrifugal, Axial
Page 1-4
On centrifugal compressors The ___ allows the air to spread out, slow down, and increase pressure.
Diffuser
Page 1-5
The ____ compressor design uses rows of rotating blades (rotors) and stationary blades (stators).
Axial
Page 1-5
What are 2 types of Stator vanes?
Fixed, Variable
Page 1-5
The purpose of the ____ section is to add heat energy to the gases flowing from the compressor.
Combustion Secton
Page 1-6
Primary air is approximately ___ percent of the air from the compressor and is used to support combustion of the fuel.
25%
Page 1-6
Secondary air is the remaining ___ percent and is used to provide a cooling blanket between the flame and the liner to prevent excessive heat damage.
75%
Page 1-6
The function of the ___ section is to extract heat energy from the expanding gases to drive various components.
Turbine
Page 1-8
The ____ section directs the flow of hot gas from the turbine rearward in a manner to prevent turbulence and to increase the exit velocity of the gas.
Exhaust
Page 1-8
The ____ section provides a place to mount and drive accessories needed for operation and control of the engine and aircraft systems
Accessory
Page 1-8
The _____ engine is a gas turbine engine that delivers power through a shaft to drive a propeller.
TurboProp
Page 1-11
A _____ engine is a gas turbine engine that delivers power through a shaft to turn a rotor or set of rotors.
Turboshaft
Page 1-10
A _____ is a turbine engine that utilizes a ducted multibladed propeller to provide thrust.
Turbofan
Maintain ____ feet from front of the engine intake
25ft
Maintain ____ feet from the side or rear of the engine intake
5 ft
Hazard area may extend ____ feet or beyond from the exhaust section, depending on throttle setting
200 ft
How wide is the propeller plane of rotation mark?
3 inches
Noise levels at or greater than ___ db require single hearing protection.
85 db
Page 1-12
Noise levels greater than ____ db require internal and external hearing protection.
105 db
Page 1-12
The two methods for servicing a turbine engine lubrication system are ____ and _____.
Gravity and Pressure
Page 1-13
When using the ____ method, the technician fills the oil system from a pressurized servicing cart reservoir.
Pressure
Page 1-13
____ servicing is the method by which the oil is poured into the servicing port.
Gravity
Page 1-13
What manual can you find the proper PPE for ground runs?
CGTO 85-00-110
Page 1-13
____ is the intergranular or transgranular cracking of a metal caused by the combined effects of constant tensile stress (internal or applied) and corrosion.
Stress Corrosion
2-3
____ is discoloration and a likely loss of hardness resulting from high temperatures.
Burning
2-3
_____ is a series of deep scratches caused by foreign particles between moving parts or careless assembly or disassembly techniques.
Scoring
2-3
_____ is severe chafing or fretting in which metal is transferred from one part to another.
Galling
2-3
_____ is a condition of surface erosion caused by minute movement between two parts usually clamped together with considerable unit pressure.
Fretting
Page 2-3
What are two types of filters used in gearbox assemblies?
Replaceable, Reuseable
Page 2-3
What are 2 types of oil samples?
Routine and special
Page 2-3
What does an APU supply to an aircraft?
Electric and pneumatic
Page 3-2
Auxiliary Power Units normally operate at about ___ percent RPM under varying condition loads.
100%
Page 4-2
The two types of starters used on Coast Guard aircraft are?
Starter Generator and Pneumatic Starters
Page 4-2
Air turbine starters are capable of developing ____ as much torque as the electric starter.
Twice
Page 4-3
A _____ is a schedule that allows a device to operate for a given period of time with a cooling down period required before the device can be operated again.
Duty Cycle
Page 4-4
What is the most common oil system used in CG aircraft.
Dry Sump
Page 5-2
Why do oil tanks have expansion space?
Allows oil expansion from heat and foaming
What are 2 types of oil coolers?
Air and Fuel cooled
Page 5-4
What does the identification tape look like for oil lubrication?
yellow with squares
page 4-6
What is the most commonly used type of oil pump used on Coast Guard aircraft?
Gear type
Quiz
A ____ is a heat sensitive unit that completes an electrical circuit at a certain temperature.
Thermal Switch
Page 6-3
The ____ system provides a warning only during a rapid rise in temperature.
Thermocouple
Page 6-3
The ____ system measures the total resistance of the full sensing loop by averaging the total temperature as well as any single hot spot.
Kidde
Page 6-5
The ____ system is non-averaging but will indicate when any portion of its sensing element reaches the alarm temperature.
Fenwall
Page 6-5
The ____ fire detection system is a type of continuous loop consisting of a stainless steel tube containing a discrete element.
Lindberg
Page 6-5
What does the Fire protection identity tag look like?
Brown with diamonds
Page 6-9
______ are performed to check the relative alignment and adjustment of an aircraft’s main structural components, flight control surfaces, and flight control system.
Rigging Checks
Page 7-2
_____ are performed to check the relative alignment of the flight controls to the aircraft structural stops.
Clearance checks
Page 7-2
The ______ is used to measure the tension of aircraft control cables.
Cable Tensiometer
Page 7-4
The ______ is used to check angles during performance of rig/range checks for the HH-65.
Vernier Scale
Page 7-4
You must perform _____ when re-rigging the helicopter.
Blade Tracking
Page 7-9
____ is high-temperature corrosion that starts with excessive levels of sodium and sulfur in the air and fuel mixture entering the engine.
Sulfidation
Page 8-9
Stator vane bowing is a vane that is curved, and it is usually caused by _____.
High Heat
Page 8-10
What manual is the AFTO 2J-1-13?
Cleaning of Gas Turbine Aircraft Engines and Parts Manual
Page 8-13
___ is a simple, inexpensive, and reliable method used for detecting defects, which are open to the surface of the part to be inspected.
Dye Penetrate
8-22
___ is an NDI method used for detecting discontinuities on or near the surface in materials that can be magnetized
Magnetic Particle
8-23