2A651 Volume 3 Ure's

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1. What is the composition of jp-8 fuel?

Explanation

JP-8 fuel is a type of jet fuel used by the military. It is a mixture of gasoline and kerosene. This composition allows JP-8 to have a high energy density and a low freezing point, making it suitable for use in aircraft engines. The gasoline component provides high octane rating and better performance at high altitudes, while the kerosene component provides stability and prevents the fuel from freezing at low temperatures.

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About This Quiz
2A651 Volume 3 Ure

This quiz, titled '2a651 volume 3 ure's,' assesses knowledge on JP-8 fuel composition, its properties, and related aircraft fuel system components. It evaluates understanding of fuel system mechanics,... see morecritical for safe jet operation and maintenance. see less

2. The purpose of a fuel/oil cooler in a fuel system is to?

Explanation

The purpose of a fuel/oil cooler in a fuel system is to heat the fuel and cool the oil. This is important because fuel needs to be at the optimal temperature for combustion, and cooling the oil helps to prevent it from overheating and breaking down. By heating the fuel and cooling the oil, the cooler ensures that both components are functioning efficiently and effectively in the fuel system.

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3. The main fuel control allows the jet engine to safety accelerate, reducing the possibility of?

Explanation

The main fuel control in a jet engine is responsible for regulating the fuel flow to ensure a safe acceleration. By maintaining the correct fuel-air mixture, it prevents a flameout, which is the sudden extinguishing of the flame in the engine combustion chamber. This is crucial to avoid a loss of power and potential engine failure. Therefore, the main fuel control helps reduce the possibility of a flameout occurring during the engine's acceleration process.

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4. Use extreme care when working with labyrinth seals because of their?

Explanation

Labyrinth seals are constructed using soft metal, which makes them susceptible to damage. This is because soft metal is more prone to deformation and wear, especially when exposed to high pressures, temperatures, or friction. Therefore, extreme care must be taken when working with labyrinth seals to avoid any accidental damage that could compromise their effectiveness in sealing and protecting the components they are installed in.

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5. What are microscopic metallic particles in the oil system called?

Explanation

Microscopic metallic particles that are present in the oil system and are a result of wear and tear are called wear metals. These particles are generated from the friction between moving parts in the system and can indicate the condition of the machinery or engine. By analyzing the concentration and types of wear metals present in the oil, maintenance professionals can assess the level of wear and potential issues within the system.

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6. During a visual inspection, how can you tell when a fuel filter is clogged?

Explanation

A differential pressure indicator is actuated when a fuel filter is clogged. This means that there is a noticeable difference in pressure on either side of the filter, indicating a blockage. By observing the actuation of the differential pressure indicator, it can be determined that the fuel filter is clogged without the need for disassembling it.

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7. Which f100-pw-220 engine fuel system component controls pressurization of the core engine fuel system?

Explanation

The P&D valve controls the pressurization of the core engine fuel system. It regulates the flow of fuel to maintain the required pressure for efficient engine operation. The fuel nozzle, N2 sensor, and Tt 2.5 sensor are not directly responsible for controlling the pressurization of the fuel system.

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8. What is the basic function of an augmentor (afterburner) when it is not operating?

Explanation

The augmentor (afterburner) acts as the basic engine tailpipe when it is not operating. This means that it serves as the primary outlet for the engine exhaust gases.

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9. Calibration and/or adjustment screws that require setting during an engine trim procedure must be?

Explanation

During an engine trim procedure, calibration and/or adjustment screws need to be safety sealed and/or lockwired. This is done to ensure that the screws do not come loose or change position unintentionally, which could lead to incorrect engine performance. Safety sealing and lockwiring provide a physical barrier and secure the screws in place, preventing any unwanted adjustments or movements.

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10. On the t56 engine, how many and what type of fuel pumps are contained in the fuel pump and filter assembly?

Explanation

The correct answer is 2 gear; 1 boost. This means that in the fuel pump and filter assembly of the t56 engine, there are two gear pumps and one boost pump. The gear pumps are responsible for delivering fuel from the fuel tank to the engine, while the boost pump provides additional pressure to ensure proper fuel flow.

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11. Chip detectors have an electrical connection for making which type of check?

Explanation

Chip detectors have an electrical connection for making a continuity check. This means that they are designed to detect any breaks or interruptions in the electrical circuit. By ensuring that there is a continuous flow of electricity, chip detectors can effectively monitor the condition of the system and detect any potential issues or faults. This helps in maintaining the overall integrity and functionality of the system.

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12. What is the term for the process of producing voltage in a conductor when it passes through?

Explanation

Electromagnetic induction is the process of producing voltage in a conductor when it passes through a magnetic field. This phenomenon occurs when there is a change in the magnetic field strength or when the conductor moves relative to the magnetic field. As the conductor cuts through the magnetic lines of force, an electric current is induced in the conductor, resulting in the production of voltage. This principle is widely used in various electrical devices such as generators and transformers.

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13. What type of fuel control uses items such as thermocouples, relays, amplifiers, and solenoids to help control a jet engine?

Explanation

Electrohydromechanical fuel control uses items such as thermocouples, relays, amplifiers, and solenoids to help control a jet engine. This type of fuel control system combines both electrical and hydraulic components to regulate the flow of fuel to the engine. Thermocouples measure the temperature, relays and amplifiers control the electrical signals, and solenoids control the hydraulic valves. By integrating these different components, electrohydromechanical fuel control ensures precise and efficient fuel delivery, optimizing the performance of the jet engine.

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14. Which term describes a jet engine fuel metering device that is really two fuel controls in one component?

Explanation

A unified fuel metering device refers to a jet engine fuel control system that combines two separate fuel controls into a single component. This means that instead of having two separate controls for fuel metering, the unified system integrates both controls into one unit. This can provide greater efficiency and simplification in the fuel control system of a jet engine.

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15. In addition to the visual inspection, what other type of inspection does the t56 engine fuel nozzle require?

Explanation

The T56 engine fuel nozzle requires a spray pattern inspection in addition to the visual inspection. This means that besides visually inspecting the nozzle, it is also necessary to check the spray pattern produced by the nozzle. This is important as a proper spray pattern ensures efficient fuel combustion and optimal engine performance.

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16. What type of oil seal has soft metal as its basic composition and allows a small amount of airflow to prevent oil seepage?

Explanation

A labyrinth oil seal is made up of soft metal as its basic composition and allows a small amount of airflow to prevent oil seepage. This type of seal consists of multiple interlocking grooves or channels that create a tortuous path for the oil to flow through. This design helps to trap the oil within the seal and prevent it from leaking out. The soft metal composition allows for flexibility and durability, ensuring a reliable seal over time.

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17. In an engine oil tank, which device separates the air from the oil?

Explanation

A deaerator is a device used in an engine oil tank to separate air from the oil. It is designed to remove dissolved gases such as oxygen and carbon dioxide from the oil, which helps prevent oxidation and corrosion. This ensures that the oil remains clean and free from contaminants, improving the overall performance and longevity of the engine.

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18. Which item on the JFS provides pads for mounting the fuel atomizer assembly?

Explanation

The turbine plenum provides pads for mounting the fuel atomizer assembly.

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19. The hazardous property of modern jet engine oil the journeyman must be aware of its?

Explanation

The correct answer is corrosiveness. The question asks about the hazardous property of modern jet engine oil that a journeyman must be aware of. Corrosiveness refers to the ability of a substance to cause damage or destruction to materials it comes into contact with. In the context of jet engine oil, corrosiveness is important for a journeyman to be aware of because it can lead to damage and deterioration of engine components if not handled properly.

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20. Under what condition would you not receive an OAP laboratory sample report?

Explanation

If the results of the laboratory sample are normal, it means that there are no abnormalities or issues detected in the sample. Therefore, there would be no need to receive a report for the sample as there are no concerns or problems to address.

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21. What is the purpose of jet engine thrust reversers?

Explanation

The purpose of jet engine thrust reversers is to direct the engine thrust in the opposite direction. This is done to provide additional braking force during landing, allowing the aircraft to slow down more quickly. By redirecting the thrust forward instead of backward, the reversers help to counteract the forward motion of the aircraft and aid in deceleration. This is especially important for large commercial aircraft that require shorter landing distances and improved stopping capabilities.

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22. The SEM/EDX analysis process differs from conventional oil analysis in that the SEM/EDX?

Explanation

SEM/EDX analysis is a technique used to determine the elemental composition of a sample. In this process, particles must be oil-free for accurate analysis to take place. This is because the presence of oil can interfere with the analysis and lead to incorrect results. Therefore, it is important to ensure that the samples are free from oil before conducting SEM/EDX analysis. This is a key difference between SEM/EDX analysis and conventional oil analysis, where the focus is on analyzing the properties and condition of the oil itself.

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23. On an f100-pw-220 engine, what component permits oil to bypass the oil filter during cold weather starts?

Explanation

The correct answer is the filter assembly bypass valve. This component allows oil to bypass the oil filter during cold weather starts. This is necessary because cold temperatures can cause the oil to thicken, making it difficult for it to flow through the filter. By bypassing the filter, the oil can flow more easily and quickly reach the engine components, ensuring proper lubrication during startup.

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24. On an f110-ge-129 engine, compressor bleed air is used for anti-icing system prevents detrimental formation and accumulation of ice on front frame struts, forward centerbody, and?

Explanation

Compressor bleed air is used for the anti-icing system to prevent the formation and accumulation of ice on various parts of the engine. In this case, it is specifically used to prevent ice formation on the front frame struts, forward centerbody, and the fan inlet guide van flaps. The fan inlet guide van flaps are located at the entrance of the engine and are responsible for directing the airflow into the engine. By preventing ice formation on these flaps, the engine's performance and efficiency can be maintained.

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25. What law does the c-d supersonic inlet use to slow down the airflow?

Explanation

The correct answer is Bernoulli's law. The C-D supersonic inlet uses Bernoulli's law to slow down the airflow. Bernoulli's law states that as the speed of a fluid increases, its pressure decreases. In the case of the supersonic inlet, the high-speed airflow is slowed down by increasing the area of the inlet, which causes a decrease in velocity and an increase in pressure. This allows the supersonic airflow to be efficiently compressed and slowed down before entering the engine.

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26. Which stage of compressor air drives the augmenter fuel pump on an f100-pw-200 engine?

Explanation

The correct answer is 13th. In an F100-PW-200 engine, the 13th stage of the compressor is responsible for driving the augmenter fuel pump. The augmenter fuel pump is an important component that provides fuel to the afterburner for increased thrust.

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27. Which type of oil cooler operates on the same principle as a radiator in an automobile?

Explanation

An air oil cooler operates on the same principle as a radiator in an automobile. Both the air oil cooler and the radiator work by transferring heat from the fluid (oil or coolant) to the surrounding air. In an air oil cooler, the fluid flows through a series of fins that are exposed to the air. As the air passes over the fins, it absorbs the heat from the fluid, cooling it down. This cooled fluid is then circulated back into the system. This principle of heat transfer is similar to how a radiator in an automobile cools down the engine coolant by transferring heat to the air.

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28. Discharge air used for aircraft engine anti-icing to heat-critical areas is taken from which engine area?

Explanation

The discharge air used for aircraft engine anti-icing is taken from the compressor area. The compressor is responsible for compressing the incoming air before it enters the combustion chamber. This compressed air is then used for various purposes, including anti-icing to prevent ice formation on critical areas of the engine. By utilizing the discharge air from the compressor, heat can be provided to these areas, ensuring that they remain ice-free during flight.

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29. Who is responsible for ensuring that the OAP operate properly?

Explanation

The project monitor is responsible for ensuring that the OAP (Operational Analysis Plan) operates properly. They oversee the project and monitor its progress, making sure that all aspects of the plan are being executed correctly. They are responsible for identifying any issues or challenges that may arise and finding solutions to address them. The project monitor ensures that the OAP is implemented according to the set guidelines and objectives, and they provide guidance and support to the team members involved in the project.

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30. Before taking an oil sample form a drain, drain enough fluid into a container in order to?

Explanation

Before taking an oil sample from a drain, it is necessary to drain enough fluid into a container in order to remove any water and sludge that may have accumulated in the oil. This is important because water and sludge can contaminate the oil and affect its performance and lubricating properties. By draining off the water and sludge, the oil sample obtained will be more representative of the oil's condition and will provide more accurate information for analysis.

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31. The f100 engine augmentor's primary nozzle actuator is driven by cables from the?

Explanation

The primary nozzle actuator of the F100 engine augmentor is driven by the convergent exhaust nozzle control. This control system is responsible for adjusting the position of the exhaust nozzle, which helps regulate the flow of exhaust gases and optimize engine performance. By manipulating the convergent exhaust nozzle control, the engine can effectively control thrust and improve efficiency.

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32. At room temperature, how many times longer willit take water to settle out of jp-8 that out of gasoline?

Explanation

Water will take 4 times longer to settle out of JP-8 compared to gasoline at room temperature.

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33. Jet aircraft operating at moderately high altitudes increase the fuel system's susceptibility to an icing condition, further aggravated by the?

Explanation

Jet aircraft operating at moderately high altitudes increase the fuel system's susceptibility to an icing condition. This is further aggravated by the higher viscosity of jet fuels. Higher viscosity means that the fuel is thicker and flows less easily. In cold temperatures, this can lead to the formation of ice crystals or ice particles in the fuel, which can clog the fuel system and cause engine failure. Therefore, the higher viscosity of jet fuels increases the likelihood of icing in the fuel system at high altitudes.

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34. When in primary mode, what controls the operation of the f100-pw-220 engine?

Explanation

The DEEC (Digital Electronic Engine Control) controls the operation of the F100-PW-220 engine when in primary mode. DEEC is responsible for monitoring and adjusting various engine parameters such as fuel flow, temperature, and pressure to ensure optimal performance and efficiency. It receives inputs from sensors and uses algorithms to make real-time adjustments, ensuring smooth and reliable engine operation.

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35. On an f100-pw-220 engine, the deec is cooled by?

Explanation

The DEEC (Digital Electronic Engine Control) on an F100-PW-220 engine is cooled by fuel. The DEEC is responsible for monitoring and controlling various engine parameters, such as fuel flow, temperature, and pressure. Since fuel is already present in the engine, it can be used as a cooling medium for the DEEC. This helps in dissipating the heat generated by the control unit, ensuring its proper functioning and longevity.

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36. Which type of oil pump consists of a gear and rotor within a housing?

Explanation

A gerotor oil pump consists of a gear and rotor within a housing. This type of pump uses the meshing of the gear and rotor to create a pumping action, drawing oil into the pump and then forcing it out under pressure. The gear and rotor design allows for efficient and reliable oil flow, making gerotor pumps commonly used in various applications, including automotive engines.

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37. The primary benefit of identifying an impending failure through the OAP is?

Explanation

The primary benefit of identifying an impending failure through the OAP is improved safety. By detecting potential failures in advance, necessary measures can be taken to prevent accidents or injuries. This ensures a safer working environment for both employees and equipment operators.

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38. Core engine fuel flow sequence on an f100-pw-220 engine starts at the main fuel pump and then goes through the?

Explanation

The correct answer is mfc, fuel/oil cooler, p&d, and fuel nozzles. The core engine fuel flow sequence on an F100-PW-220 engine starts at the main fuel control (mfc), which regulates the flow of fuel. From there, the fuel flows through the fuel/oil cooler, where it is cooled before entering the engine. Next, the fuel passes through the p&d (pressure and drain) system, which further regulates and drains any excess fuel. Finally, the fuel is delivered to the engine combustion chamber through the fuel nozzles.

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39. Once the cooling airflow has done the its job of cooling the turbine section, where does it go?

Explanation

After the cooling airflow has completed its task of cooling the turbine section, it is directed into the gas stream to exit the engine. This means that the cooled airflow is mixed with the hot gases produced by the engine and is expelled out of the engine. This ensures that the cooling airflow does not go to waste and is effectively utilized in the overall functioning of the engine.

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40. On an f100 engine, the breather pressurizing valve is interanlly mounted in the?

Explanation

The breather pressurizing valve on an F100 engine is internally mounted in the gearbox. This means that it is located within the gearbox itself, rather than in the oil tank, oil filter, or oil pump. The purpose of the breather pressurizing valve is to regulate the pressure within the gearbox, ensuring that it remains at the appropriate level for optimal performance and lubrication.

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41. If the red button on an f100-pw-220 engine oil filter pops out and remains extended, the ?

Explanation

When the red button on an f100-pw-220 engine oil filter pops out and remains extended, it indicates that the design pressure differential has been exceeded. This means that the pressure difference between the inlet and outlet of the oil filter has reached or surpassed the maximum limit set by the design specifications. This could be due to various reasons such as a clogged filter or a malfunctioning component, causing an abnormal pressure buildup in the system.

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42. On an f100-pw-220 engine, how many modes is the mfc capable of operating in?

Explanation

The MFC (Main Fuel Control) on an F100-PW-220 engine is capable of operating in two modes.

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43. On an f100-pw-220 engine, the air/oil coolers are mounted on the fan duct and use?

Explanation

The air/oil coolers on an f100-pw-220 engine are mounted on the fan duct and use secondary fan airflow as a coolant. This means that the coolers are designed to take advantage of the airflow generated by the secondary fan, which helps to cool the engine oil. By using this airflow as a coolant, the engine is able to maintain optimal operating temperatures and prevent overheating.

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44. The ACAWS message low oil level advisory for the ae2100d3 engine occurs when the engine oil level drops below?

Explanation

The ACAWS message low oil level advisory for the ae2100d3 engine occurs when the engine oil level drops below 4 US gallons. This means that the engine is designed to provide a warning when the oil level falls below this threshold. It is important to maintain an adequate oil level to ensure proper lubrication and prevent damage to the engine.

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45. What are the two main types of augmentor (afterburner) ignition systems?

Explanation

The two main types of augmentor (afterburner) ignition systems are torch igniter and pilot burner ring. A torch igniter is a device that provides a high-energy spark to ignite the fuel-air mixture in the augmentor, while a pilot burner ring is a continuous flame that is used to stabilize the combustion process in the augmentor. These two components work together to ensure proper ignition and sustained combustion in the afterburner system.

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46. On a simple ac generator, which item takes the current from the slip rings to operate the electrical device?

Explanation

In a simple AC generator, the brushes are responsible for taking the current from the slip rings to operate the electrical device. The brushes make physical contact with the slip rings, which are connected to the rotating loop or armature of the generator. As the armature rotates, the brushes maintain contact with the slip rings, allowing the current to flow from the generator to the electrical device. The brushes act as conductive contacts, transferring the electrical energy to the device for operation.

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47. How many sparks per second can the ae2100d3 ignition excitiers produce?

Explanation

The ae2100d3 ignition exciters can produce a range of 4 to 7 sparks per second.

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48. In what position must the td valve switches be placed in order to make the t56 engine fuel trimming system inoperative?

Explanation

The correct answer is "null". In order to make the T56 engine fuel trimming system inoperative, the TD valve switches must be placed in the "null" position. This means that the switches should not be in any specific position or mode, but rather in a neutral or inactive state. Placing the switches in the "null" position would effectively disable the fuel trimming system and prevent any adjustments or modifications to the fuel flow.

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49. When an engine is not operating, static preload for a carbon oil seal is provided by?

Explanation

When an engine is not operating, the static preload for a carbon oil seal is provided by spring pressure. This means that the carbon oil seal is compressed by a spring, creating a constant force that maintains the seal's contact with the mating surface. This helps to prevent leakage of oil or other fluids when the engine is not in use. Air pressure, oil pressure, and hydraulic pressure are not suitable options for providing static preload in this scenario.

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50. Which type of combustion chamber does the JFS use?

Explanation

The JFS (Jet Fuel Starter) uses an annular combustion chamber. An annular combustion chamber is a type of combustion chamber in which the fuel and air mixture is ignited in a ring-shaped chamber. This design allows for efficient and uniform combustion, resulting in better fuel efficiency and lower emissions. The annular combustion chamber is commonly used in gas turbine engines, including the JFS, due to its compact design and ability to handle high-pressure conditions.

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51. Which unit of an ac ignition system develop 20,000 volts?

Explanation

A transformer is a device that can increase or decrease the voltage of an electrical current. In an AC ignition system, a transformer is used to step up the voltage from the battery to a much higher level, typically around 20,000 volts. This high voltage is necessary to create a spark in the spark plugs, which ignites the fuel-air mixture in the engine. Therefore, the transformer is the unit of an AC ignition system that develops 20,000 volts.

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52. On early ignition systems, what is the purpose of compositors in an ignition system?

Explanation

The purpose of capacitors in an early ignition system is to step up the voltage high enough to break down the air gap of the igniter plug. Capacitors store electrical energy and release it quickly when needed, allowing for a higher voltage to be generated and ensuring a strong spark to ignite the fuel mixture in the engine. This helps to improve the efficiency and reliability of the ignition system.

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53. What engine section houses the JFS combustion section?

Explanation

The turbine plenum is the engine section that houses the JFS (Jet Fuel Starter) combustion section. The JFS is a small turbine engine used to start the main engine of an aircraft. It provides the necessary airflow and ignition for the main engine to start and operate. The turbine plenum is responsible for housing and protecting the JFS combustion section during operation.

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54. Which part of a generator acts as an automatic switching device, changing alternating current to direct current?

Explanation

The commutator is the part of a generator that acts as an automatic switching device, changing alternating current to direct current. It consists of a series of metal segments that are connected to the rotating armature of the generator. As the armature rotates, the commutator reverses the direction of the current flowing through the armature coils, ensuring that the output of the generator is in the form of direct current. This allows for the efficient conversion of the alternating current produced by the generator into the direct current needed for many electrical devices.

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55. What provides the PTO shaft that is used to drive the csd?

Explanation

The PTO shaft used to drive the csd is provided by the engine adapter. This component connects the engine to the csd and allows the transfer of power from the engine to the shaft. Engine fittings, aircraft fittings, and aircraft adapter are not directly involved in providing the PTO shaft for driving the csd.

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56. The temperature datum system static check must be made whenever which component has been replaced?

Explanation

The temperature datum system static check must be made whenever the power section has been replaced. This is because the power section is a critical component that can affect the temperature readings in the system. By conducting a static check, any discrepancies or errors in the temperature datum system can be identified and corrected, ensuring accurate temperature measurements and proper functioning of the system.

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57. Which type of oil system stores the oil in a tank fitted to the side of the engine?

Explanation

A dry sump oil system stores the oil in a separate tank that is mounted externally to the engine, typically on the side. This design allows for a larger oil capacity and better oil control compared to a wet sump system, where the oil is stored in a pan at the bottom of the engine. The dry sump system is commonly used in high-performance and racing engines to prevent oil starvation during extreme maneuvers and to improve overall lubrication efficiency.

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58. On the F-15 secondary power system CGB, how are the isolation decouplers extended?

Explanation

The isolation decouplers on the F-15 secondary power system CGB are extended hydraulically.

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59. What is used to open and close flap-type and iris-type variable-exhaust nozzle systems?

Explanation

The correct answer is "air pressure for both types." Flap-type and iris-type variable-exhaust nozzle systems are operated using air pressure. This means that air pressure is used to open and close both types of nozzle systems.

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60. What component heats augmentor fuel to provide better vaporization and combustion?

Explanation

The fuel/oil cooler heats the augmentor fuel to provide better vaporization and combustion.

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61. Which t56 engine component receives 120 percent of the engine fuel requirement?

Explanation

The TD valve receives 120 percent of the engine fuel requirement.

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62. When the null orifice on the t56 engine td valve is set at zero, how much fuel will the valve bypass?

Explanation

When the null orifice on the T56 engine TD valve is set at zero, it means that there is no bypass for fuel. Therefore, the valve will not bypass any fuel, resulting in a 0% bypass.

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63. When classified as to structure, which of the following is not a type of an oil pump?

Explanation

The correct answer is rotogear because it is not a type of oil pump. Gear, gerotor, and sliding vane are all types of oil pumps commonly used in various applications. However, rotogear is not recognized as a specific type of oil pump in the industry.

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64. The ae2100d3 oil tank pendulum is designed to supply pressurized oil for approximately how long during negative G conditions?

Explanation

The ae2100d3 oil tank pendulum is designed to supply pressurized oil for a minimum of 10 seconds during negative G conditions. This means that even in situations where there is a loss of gravity, the oil tank pendulum will continue to provide pressurized oil for at least 10 seconds.

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65. Approximately how many gpm does the ae2100d3 PUAD  lube and scavenge pump provide at engine PTO?

Explanation

The AE2100D3 PUAD (Power Unit Accessory Drive) lube and scavenge pump provides approximately 5 gallons per minute (gpm) at engine PTO (Power Take Off).

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66. The f117-pw-100 fan thrust reverser door upper right and left sensors send a signal to which channel or channels of the EEC?

Explanation

The correct answer is "a channel." The f117-pw-100 fan thrust reverser door upper right and left sensors send a signal to only one channel of the EEC.

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67. Which item intitially rotates the JFS?

Explanation

The hydraulic motor is the item that initially rotates the JFS. This is because a hydraulic motor is designed to convert hydraulic energy into mechanical energy, which allows it to power the rotation of the JFS. The other options, such as the ESS PTO, electric motor mounted on the aircraft, and engine PTO, are not typically involved in the initial rotation of the JFS.

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68. The slide-type resistor in the EGT circuit is used to?

Explanation

The slide-type resistor in the EGT circuit is used to calibrate the EGT indicator in the flight station. This means that it is used to adjust the EGT readings on the indicator to ensure accuracy. By adjusting the slide-type resistor, the EGT readings can be calibrated to match the actual temperature measurements. This is important for accurate monitoring of engine performance and ensuring that the engine is operating within safe limits.

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69. What is the primary input power to the main ignition system?

Explanation

The primary input power to the main ignition system is 28 vdc. This means that the main ignition system requires a direct current power supply with a voltage of 28 volts. It does not require an alternating current power supply or a higher voltage such as 120 volts. The 28 vdc power source is specifically designed to meet the requirements of the main ignition system and ensure its proper functioning.

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70. On the t56 engine, the manifold pressure switch opens to de-energize the fuel enrichment relay when fuel pressure, in psi, in the manifold reaches?

Explanation

The manifold pressure switch on the T56 engine opens to de-energize the fuel enrichment relay when the fuel pressure in the manifold reaches 50 psi. This means that once the fuel pressure reaches this level, the switch will cut off the power supply to the fuel enrichment relay, which is responsible for providing additional fuel to the engine during certain conditions. This helps to regulate the fuel flow and maintain optimal performance of the engine.

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71. What component monitors the ae2100d3 ignition excitiers spark rate?

Explanation

The NIU (Network Interface Unit) component is responsible for monitoring the ae2100d3 ignition exciters spark rate. It serves as the interface between the engine's digital electronic control system and the ignition system. The NIU receives information from various sensors and sends commands to control the ignition system, including monitoring the spark rate. This ensures proper ignition timing and efficient engine performance.

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72. The two air source requirements for a pneumatic starter to operate properly are sufficient?

Explanation

A pneumatic starter requires both sufficient volume and pressure of air to operate properly. Volume refers to the amount of air available, while pressure refers to the force with which the air is delivered. Without enough volume, there may not be enough air to power the starter, and without sufficient pressure, the air may not be delivered with enough force to initiate the starter. Therefore, both volume and pressure are necessary for a pneumatic starter to function effectively.

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73. On the t56 engine, at what percent of engine rpm is the ignition system turned off?

Explanation

The correct answer is 65%. The ignition system on the t56 engine is turned off at 65% of engine rpm. This means that once the engine reaches this speed, the ignition system is no longer needed to keep the engine running smoothly.

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74. Which type of oil system design places the oil cooler in the pressure subsystem?

Explanation

A hot tank oil system design places the oil cooler in the pressure subsystem. In this design, the oil cooler is located within the hot tank, where the oil is pressurized. This allows the oil to be cooled down as it flows through the cooler, ensuring that the oil temperature remains within the desired operating range. Placing the oil cooler in the pressure subsystem helps to maintain the efficiency and effectiveness of the cooling process, as the oil is cooled while under pressure.

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75. What is the output VAC of the AE2100d3 alternator stator?

Explanation

The output VAC of the AE2100d3 alternator stator is in the range of 20 to 40 vac.

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76. The OSG on the cartridge-pneumatic starter consists of a body containing?

Explanation

The OSG (Over Speed Governor) on the cartridge-pneumatic starter consists of two pinned flyweights and a piston. The flyweights are connected to the shaft and rotate with it. When the starter exceeds a certain speed, the centrifugal force causes the flyweights to move outward, which in turn pushes the piston. This movement triggers the ignition and starts the engine. Therefore, the presence of two pinned flyweights and a piston in the OSG is essential for the proper functioning of the cartridge-pneumatic starter.

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77. The f100 engine augmentor's exhaust nozzle is variable to control engine?

Explanation

The F100 engine's augmentor's exhaust nozzle is variable in order to control both the engine's thrust and the fan stall margin. By adjusting the exhaust nozzle, the engine can regulate the amount of thrust it produces, as well as maintain a safe margin to prevent fan stall. This allows for better performance and control of the engine during operation.

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78. From where does the ae2100d3 ignition system receive its electrical power?

Explanation

The ae2100d3 ignition system receives its electrical power from the engine-mounted alternator stator. The alternator stator is a component of the engine that generates electrical power and supplies it to various systems in the aircraft. It is responsible for charging the aircraft's battery and providing power to the ignition system, among other electrical components.

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79. On an f108-cf-100 engine anti-ice system, what is the purpose of the air injector on the air regulator?

Explanation

The air injector on the air regulator in an F108-CF-100 engine anti-ice system is used to control air temperature and pressure. It helps to regulate the flow of air, ensuring that the temperature and pressure are maintained within the desired range. This is important for the proper functioning of the engine and to prevent any damage or inefficiencies that could occur due to extreme temperatures or pressure levels.

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80. On early ignition systems, the high-energy capacitor-type ignition system does not include a?

Explanation

The high-energy capacitor-type ignition system does not include a centrifugal switch. A centrifugal switch is commonly found in older ignition systems and is used to control the timing of the spark by opening and closing the circuit at specific engine speeds. However, the high-energy capacitor-type ignition system uses a different mechanism to control the timing, such as an electronic control unit or a distributor with an optical sensor. Therefore, a centrifugal switch is not necessary in this type of ignition system.

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81. The compressor bledd system reduce the probability of compressor stall in a dual-rotor engine by?

Explanation

The compressor bleed system reduces the probability of compressor stall in a dual-rotor engine by reducing the amount of air available to the N2 compressor. When air is bled from the compressor, it reduces the overall pressure and mass flow through the compressor. This helps to prevent the compressor from stalling, which can occur when the airflow is disrupted or becomes unstable. By reducing the amount of air available to the N2 compressor, the compressor bleed system helps to maintain stable and efficient engine operation.

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82. The f100-pw-100 engine oil pressure varies with rear compressor rotor speeds (n2), engine inlet oil temperature, and ?

Explanation

The f100-pw-100 engine oil pressure varies with rear compressor rotor speeds (n2), engine inlet oil temperature, and oil nozzle condition. The condition of the oil nozzle, which is responsible for delivering oil to various parts of the engine, can affect the oil pressure. If the oil nozzle is damaged or clogged, it may not deliver oil properly, leading to a decrease in oil pressure. Therefore, the oil nozzle condition is an important factor that can impact the oil pressure in the engine.

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83. The t56 engine speed-sensitive control, measured in rpm, lets electrical current flow to the fuel and ignition system at?

Explanation

The correct answer is 16% rpm. The t56 engine speed-sensitive control allows electrical current to flow to the fuel and ignition system at a rate of 16% of the engine's revolutions per minute. This control system adjusts the fuel and ignition timing based on the engine speed, ensuring optimal performance and efficiency.

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84. An f110-ge-129 engine contains how many stages fo VSV?

Explanation

The correct answer is 3 because an f110-ge-129 engine contains three stages of VSV (Variable Stator Vanes). These vanes are adjustable components located in the compressor section of the engine. They help to control the airflow and optimize engine performance at different operating conditions.

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85. Oil is supplied to the f-15 JFS through the?

Explanation

The correct answer is the CGB oil system. The CGB (Combustion Gas Bearing) oil system supplies oil to the f-15 JFS (Jet Fuel Starter) for lubrication and cooling purposes. The CGB oil system ensures that the JFS operates smoothly and efficiently by providing the necessary lubrication to its components.

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86. Which t56 engine component sends the fuel to the fuel manifold?

Explanation

The correct answer is the td valve. The td valve is responsible for sending the fuel to the fuel manifold in the t56 engine. It controls the flow of fuel and ensures that it is distributed properly to the fuel manifold.

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87. How many linear hydraulic actuators are used to deploy and stow the fan thrust on the f117-pw-100 engine?

Explanation

The correct answer is 4. This suggests that there are four linear hydraulic actuators used to deploy and stow the fan thrust on the F117-PW-100 engine.

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88. On an f110-ge-129 engine, compressor bleed air is used for anti-icing, customer bleed, and ?

Explanation

Compressor bleed air is used for various purposes in an engine. In the case of an f110-ge-129 engine, it is used for anti-icing to prevent ice formation on critical components. It is also used for customer bleed, which refers to providing air to other systems or equipment on the aircraft. Additionally, compressor bleed air is used for low-pressure turbine cooling functions. This means that it helps in cooling down the low-pressure turbine, which is important for its efficient operation. However, it is not used for VSV actuator control or IGV actuator control. It is also not directly involved in the operation of the main engine fuel pump.

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89. On a dual-spool, axial-flow engine, what controls thrust production of the engine?

Explanation

Controlling the turbine inlet temperature is the correct answer because it directly affects the thrust production of the engine. By regulating the temperature of the air entering the turbine, the engine can optimize the combustion process and ensure efficient power generation. Higher turbine inlet temperatures result in increased thrust production, while lower temperatures can reduce thrust. Therefore, controlling the turbine inlet temperature is crucial for maintaining optimal engine performance and maximizing thrust output.

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90. On the t56 engine, what compares the desired throttle setting from the coordinator with the actual TIT signal from the thermocouples?

Explanation

The TD amplifiers on the T56 engine compare the desired throttle setting from the coordinator with the actual TIT (Turbine Inlet Temperature) signal from the thermocouples. These amplifiers help to regulate and control the engine's throttle based on the temperature readings, ensuring that the engine operates within safe limits and optimally.

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91. On a t56 engine, what controls the rotary movement of the fuel control metering valve?

Explanation

The compressor inlet pressure controls the rotary movement of the fuel control metering valve on a T56 engine. This is because the compressor inlet pressure directly affects the amount of air entering the engine, which in turn determines the fuel-air mixture ratio. By adjusting the position of the fuel control metering valve based on the compressor inlet pressure, the engine can maintain the optimal fuel-air mixture for efficient combustion and performance.

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92. What ae2100d3 component drives the PGB lube and scavenge pump?

Explanation

The GMAD (Gearbox Mounted Accessory Drive) is the component that drives the PGB (Propeller Gearbox) lube and scavenge pump.

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93. On an f108 engine, whcih manifold is anti-ice air ducted from?

Explanation

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94. On an f110-ge-129 engine, which component supplies fuel pressure to operate the IGV actuator?

Explanation

The main engine control is responsible for supplying fuel pressure to operate the IGV (Inlet Guide Vane) actuator on an f110-ge-129 engine. This component regulates the fuel flow and controls various engine functions, including the operation of the IGV actuator. The IGV actuator adjusts the position of the inlet guide vanes to optimize airflow into the engine, ensuring efficient combustion and overall engine performance.

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95. During jet engine deceleration, a hydromechanical fuel control schedules fuel flow as a function of?

Explanation

During jet engine deceleration, a hydromechanical fuel control schedules fuel flow as a function of burner pressure. Burner pressure is an important parameter that affects the combustion process in the engine. By adjusting the fuel flow based on the burner pressure, the fuel control system can maintain the desired level of combustion efficiency and power output during deceleration. This helps to ensure smooth and controlled deceleration of the jet engine.

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96. The core reverser lock proximity sensors are mounted on the?

Explanation

The correct answer is actuator. The core reverser lock proximity sensors are mounted on the actuator. This implies that the sensors are placed on the actuator mechanism, which is responsible for controlling and operating the core reverser lock.

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97. How many independent circuits are within an f100-pw-100 engine ignition system?

Explanation

The correct answer is 3 because an f100-pw-100 engine ignition system typically consists of three independent circuits. Each circuit is responsible for providing ignition to a different set of fuel nozzles, ensuring redundancy and reliability in the engine's ignition process. Having multiple independent circuits allows the engine to continue operating even if one or two circuits fail, enhancing safety and performance.

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98. On the f117-pw-100 engine, what component controls hydraulic power for actuating both the fan and core thrust reversers?

Explanation

The control valve is the component that controls hydraulic power for actuating both the fan and core thrust reversers on the F117-PW-100 engine. It regulates the flow of hydraulic fluid to the reversers, allowing them to be activated and controlled as needed. The electronic engine control, hydraulic pump, and fuel control are not directly responsible for controlling hydraulic power for the reversers.

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99. On an f108-cf-100 engine, the variable bleed valve bleed air from the?

Explanation

The correct answer is the N1 compressor. In a F108-CF-100 engine, the variable bleed valve is responsible for bleeding air from the N1 compressor. The N1 compressor is the low-pressure compressor stage of the engine, and bleeding air from this stage helps regulate the flow and pressure of air within the engine.

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100. On an f108-cf-100 engine, the direction of the variable bleed valve rotation is controlled by the?

Explanation

The direction of the variable bleed valve rotation on an F108-CF-100 engine is controlled by the fuel gear motor.

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In an engine oil tank, which device separates the air from the oil?
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The hazardous property of modern jet engine oil the journeyman must be...
Under what condition would you not receive an OAP laboratory sample...
What is the purpose of jet engine thrust reversers?
The SEM/EDX analysis process differs from conventional oil analysis in...
On an f100-pw-220 engine, what component permits oil to bypass the oil...
On an f110-ge-129 engine, compressor bleed air is used for anti-icing...
What law does the c-d supersonic inlet use to slow down the airflow?
Which stage of compressor air drives the augmenter fuel pump on an...
Which type of oil cooler operates on the same principle as a radiator...
Discharge air used for aircraft engine anti-icing to heat-critical...
Who is responsible for ensuring that the OAP operate properly?
Before taking an oil sample form a drain, drain enough fluid into a...
The f100 engine augmentor's primary nozzle actuator is driven by...
At room temperature, how many times longer willit take water to settle...
Jet aircraft operating at moderately high altitudes increase the fuel...
When in primary mode, what controls the operation of the f100-pw-220...
On an f100-pw-220 engine, the deec is cooled by?
Which type of oil pump consists of a gear and rotor within a housing?
The primary benefit of identifying an impending failure through the...
Core engine fuel flow sequence on an f100-pw-220 engine starts at the...
Once the cooling airflow has done the its job of cooling the turbine...
On an f100 engine, the breather pressurizing valve is interanlly...
If the red button on an f100-pw-220 engine oil filter pops out and...
On an f100-pw-220 engine, how many modes is the mfc capable of...
On an f100-pw-220 engine, the air/oil coolers are mounted on the fan...
The ACAWS message low oil level advisory for the ae2100d3 engine...
What are the two main types of augmentor (afterburner) ignition...
On a simple ac generator, which item takes the current from the slip...
How many sparks per second can the ae2100d3 ignition excitiers...
In what position must the td valve switches be placed in order to make...
When an engine is not operating, static preload for a carbon oil seal...
Which type of combustion chamber does the JFS use?
Which unit of an ac ignition system develop 20,000 volts?
On early ignition systems, what is the purpose of compositors in an...
What engine section houses the JFS combustion section?
Which part of a generator acts as an automatic switching device,...
What provides the PTO shaft that is used to drive the csd?
The temperature datum system static check must be made whenever which...
Which type of oil system stores the oil in a tank fitted to the side...
On the F-15 secondary power system CGB, how are the isolation...
What is used to open and close flap-type and iris-type...
What component heats augmentor fuel to provide better vaporization and...
Which t56 engine component receives 120 percent of the engine fuel...
When the null orifice on the t56 engine td valve is set at zero, how...
When classified as to structure, which of the following is not a type...
The ae2100d3 oil tank pendulum is designed to supply pressurized oil...
Approximately how many gpm does the ae2100d3 PUAD  lube and...
The f117-pw-100 fan thrust reverser door upper right and left sensors...
Which item intitially rotates the JFS?
The slide-type resistor in the EGT circuit is used to?
What is the primary input power to the main ignition system?
On the t56 engine, the manifold pressure switch opens to de-energize...
What component monitors the ae2100d3 ignition excitiers spark rate?
The two air source requirements for a pneumatic starter to operate...
On the t56 engine, at what percent of engine rpm is the ignition...
Which type of oil system design places the oil cooler in the pressure...
What is the output VAC of the AE2100d3 alternator stator?
The OSG on the cartridge-pneumatic starter consists of a body...
The f100 engine augmentor's exhaust nozzle is variable to control...
From where does the ae2100d3 ignition system receive its electrical...
On an f108-cf-100 engine anti-ice system, what is the purpose of the...
On early ignition systems, the high-energy capacitor-type ignition...
The compressor bledd system reduce the probability of compressor stall...
The f100-pw-100 engine oil pressure varies with rear compressor rotor...
The t56 engine speed-sensitive control, measured in rpm, lets...
An f110-ge-129 engine contains how many stages fo VSV?
Oil is supplied to the f-15 JFS through the?
Which t56 engine component sends the fuel to the fuel manifold?
How many linear hydraulic actuators are used to deploy and stow the...
On an f110-ge-129 engine, compressor bleed air is used for anti-icing,...
On a dual-spool, axial-flow engine, what controls thrust production of...
On the t56 engine, what compares the desired throttle setting from the...
On a t56 engine, what controls the rotary movement of the fuel control...
What ae2100d3 component drives the PGB lube and scavenge pump?
On an f108 engine, whcih manifold is anti-ice air ducted from?
On an f110-ge-129 engine, which component supplies fuel pressure to...
During jet engine deceleration, a hydromechanical fuel control...
The core reverser lock proximity sensors are mounted on the?
How many independent circuits are within an f100-pw-100 engine...
On the f117-pw-100 engine, what component controls hydraulic power for...
On an f108-cf-100 engine, the variable bleed valve bleed air from the?
On an f108-cf-100 engine, the direction of the variable bleed valve...
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