Electrical And Environmental 2A656 Volume 4

During an operational check of the bleed air distribution system, leaks can be best detected by both listening and feeling. Listening can help identify any abnormal hissing or whistling sounds that may indicate a leak, while feeling for any air movement or temperature changes can also indicate the presence of a leak. Using both senses together provides a more comprehensive approach to detecting leaks in the system.

The correct answer is "primary heat exchanger." The pre-cooler in an aircraft's bleed air cooling air system is responsible for cooling the high-pressure air from the engine before it enters the air cycle machine. The primary heat exchanger is designed to efficiently transfer heat from the hot bleed air to the cooler ambient air, ensuring that the air entering the air cycle machine is at the correct temperature for cooling the aircraft's systems.

A rawhide mallet is used when installing air-conditioning ducting to ensure alignment and sealing. This type of mallet is made from rawhide material, which is soft and non-damaging to the ducting. It allows for precise adjustments and helps to create a tight seal between the ducting components. A screwdriver, center punch, and ball peen hammer are not suitable for this task as they can cause damage to the ducting or result in misalignment.

Water can be used as a lubricant on a beaded channel clamp sleeve to ease installation. Water reduces friction between the sleeve and the surface, making it easier to slide the sleeve into place. It acts as a temporary lubricant that allows for smooth and effortless installation.

The pair of unused wires that are cut-off close to the turbine housing are typically used for diagnostic purposes during maintenance. This level of maintenance, known as depot maintenance, involves more extensive repairs and overhauls that are performed at a centralized facility. Therefore, the correct answer is depot.

The correct answer is water separator. In a fighter aircraft, the water separator is an air-conditioning component that prevents excessive moisture from reaching the cockpit. It separates the water vapor from the air, ensuring that only dry air enters the cockpit. This is important as excessive moisture can lead to fogging and reduce visibility in the cockpit, which can be dangerous during flight operations. Therefore, the water separator plays a crucial role in maintaining a clear and safe cockpit environment.

Engine bleed air is used in aircraft systems for various purposes, such as providing air for anti-icing, rain removal, and anti-G systems. However, it is not used for fire extinguishing. Fire extinguishing systems in aircraft typically rely on other methods, such as fire suppression agents or halon gas, rather than engine bleed air. Therefore, the correct answer is fire extinguishing.

When replacing gaskets used in aircraft ducting, it is important to remember to always replace the gasket each time it is removed. This is because gaskets can become worn or damaged over time, and reusing them may result in leaks or other issues. Therefore, it is necessary to install a new gasket to ensure proper sealing and prevent any potential problems in the ducting system.

The fan in the bleed air system cooling turbine and fan assembly prevents turbine over speeding. This is because the fan helps regulate the flow of air, ensuring that it does not exceed the safe operating speed of the turbine. By controlling the air flow, the fan prevents the turbine from spinning too fast and potentially causing damage or malfunctions.

When smoke or fumes are discharged from the air-conditioning system, the cockpit is ventilated with atmospheric air. This means that the air from outside the aircraft is used to remove the smoke or fumes from the cockpit, ensuring the safety and well-being of the crew and passengers. The other options, such as liquid air, compressed air, and conditioned air, are not suitable for ventilating the cockpit in such situations.

Engine bleed air check valves are installed to prevent the loss of bleed air. These valves are designed to ensure that the high-pressure bleed air from the engine does not escape unintentionally. By preventing the loss of bleed air, these check valves help maintain the proper functioning of various aircraft systems that rely on bleed air, such as air conditioning, pressurization, and anti-ice systems.

The anti-G suit is designed to prevent blood from pooling in the lower portions of the body. This pooling of blood can occur when a person is subjected to high G-forces, such as during rapid acceleration or maneuvers in an aircraft. The suit applies pressure to the lower body, helping to push blood back up towards the heart and prevent it from collecting in the legs and feet. By preventing blood pooling, the suit helps to maintain proper blood circulation and prevent symptoms like dizziness, loss of vision, or even loss of consciousness that can occur when blood flow to the brain is compromised.

Bleed air is usually taken from the compressor section of the engine. The compressor is responsible for compressing the incoming air before it enters the combustion chamber. This compressed air is then used for various purposes, such as aircraft pressurization, air conditioning, and anti-icing. Taking bleed air from the compressor section ensures that it is at a high enough pressure and temperature to be used effectively for these purposes.

When a compressible flange duct end becomes distorted, the correct corrective action is to reshape the duct flange ends to its original shape. This means that the distorted flange ends should be carefully manipulated and reshaped back to their original form. This is important for ensuring a proper seal and preventing any leaks or inefficiencies in the duct system.

The purpose of the anti-G suit system is to inflate the pilot's anti-G suit. This is important because during high G-force maneuvers, such as rapid acceleration or tight turns, blood tends to pool in the lower extremities and away from the brain. By inflating the anti-G suit, it applies pressure to the pilot's legs and abdomen, helping to prevent blood from pooling and thus reducing the risk of the pilot experiencing G-induced loss of consciousness.

Isobaric pressurization maintains a constant cabin pressure throughout the flight. This means that the pressure inside the cabin remains the same as the pressure at sea level, regardless of changes in altitude. This type of pressurization helps to ensure the comfort and safety of passengers by preventing rapid changes in pressure that can cause discomfort or health issues.

A water aspirator is used to create a greater cooling effect by spraying atomized water across the inlet of the bleed air system secondary heat exchanger. This device uses the Venturi effect to create a vacuum, which draws in and mixes the water with the air. As the water and air mix, the water evaporates and absorbs heat from the air, resulting in a cooling effect. This helps to efficiently cool the bleed air system secondary heat exchanger.

The temperature of conditioned air going to the crew compartment depends on the position of the cabin dual-temperature mixing valve. This valve controls the mixture of hot and cold air to achieve the desired temperature. By adjusting the position of the valve, the temperature of the conditioned air can be regulated accordingly.

The correct answer is that the leading edge section must be removed to replace the tube. This suggests that the attachment of the distribution duct (piccolo tube) to the leading edge section is such that it cannot be easily accessed or replaced without removing the leading edge section.

An orifice is a pressure and flow control device that restricts airflow. It is used to protect aircraft engines against air starvation by regulating the amount of air that enters the engine. By restricting the airflow, the orifice ensures that the engine receives a consistent and controlled supply of air, preventing any damage or issues that could arise from air starvation.

The important procedure that was overlooked is that the flange bolts were not torqued in the proper sequence. Torquing the bolts in the correct sequence is crucial to ensure even pressure and proper sealing of the flange. This could have resulted in a leak during the operational check.

A compressible flange is a type of high-pressure/high-temperature ducting that does not require a gasket. This type of flange is designed with a compressible material, such as rubber, that creates a tight seal when the flange is bolted together. The compressible material allows for flexibility and compensates for any irregularities or misalignments in the flange connection, eliminating the need for a separate gasket. This makes the compressible flange a convenient and cost-effective option for high-pressure/high-temperature applications.

The correct answer is "outlet temperature above 32°." The bleed air system water separator anti-icing system prevents the condenser bag from icing by maintaining the outlet temperature above 32°. This ensures that any moisture or water in the system does not freeze and cause blockages or damage.

The pressure to the floor heat ejector on a cargo aircraft floor heat system is regulated by the floor heat modulating and shutoff valve. This valve controls the flow of air to the ejector, which in turn controls the amount of heat being supplied to the cargo floor. By adjusting the position of the valve, the pressure to the ejector can be increased or decreased, allowing for precise regulation of the floor heat system. The other options, such as the floor heat shutoff valve, pneumatic control thermostat, and pneumatic temperature anticipator, do not have direct control over the pressure to the ejector and therefore are not correct answers.

During a ground pressure test, there is a risk that components may separate from the aircraft. To prevent this, the components need to be securely fastened. Tying them with a net or strap is the most effective way to ensure that they remain in place during the test. Double locking, anchoring with a chain, or removing the components before testing may not provide sufficient security and could lead to separation. Therefore, tying with a net or strap is the correct answer.

The correct answer is "results are within allowable limits." The pressure decay method is used to check for leakage in the bleed air system of an aircraft engine. In this case, the pressure dropped 30 psi in 11 seconds, which indicates that the leakage is within the allowable limits. If the leakage was dangerously excessive or if the test needed to be repeated, the pressure would have dropped at a faster rate.

A pressure regulator and shutoff valve is usually installed upstream of the flow control valve to remedy its limitations. This component helps regulate and control the pressure of the air flow, ensuring that it is at the desired level before entering the flow control valve. Additionally, the shutoff valve allows for complete shut off of the air flow when needed.

A pre-cooler assembly is a cooling package that is designed to lower the temperature of a fluid or gas. It is typically equipped with its own temperature control system to regulate and maintain the desired temperature. This system ensures that the fluid or gas being cooled is kept at the appropriate temperature for optimal performance and efficiency.

The average pilot can withstand a maximum of 6-7 Gs when wearing an anti-G suit. G-force is a measurement of the force of gravity on a body and can be experienced during high-speed maneuvers or acceleration. An anti-G suit is designed to counteract the effects of G-forces by applying pressure to the lower body, preventing blood from pooling in the lower extremities and helping to maintain blood flow to the brain. This allows the pilot to tolerate higher G-forces without losing consciousness or experiencing negative physiological effects.

The temperature and pressure of the aircraft engine in relation to the bleed air system are influenced by the engine throttle setting and the ambient temperature. The engine throttle setting determines the amount of air being drawn into the engine, which affects the temperature and pressure. The ambient temperature also plays a role in determining the temperature and pressure of the air entering the engine.

Bleed air leaks are permissible around valve shafts.

The small drill hole in the outlet of some engine bleed air shutoff valves serves to check the valve position. This hole allows the operator to visually inspect whether the valve is open or closed by observing the flow of air through the hole. It provides a simple and effective way to verify the position of the valve without the need for additional equipment or tools.

The load control valve is the component that determines the amount of bleed air bled from a gas turbine compressor (GTC). It regulates the flow of bleed air based on the load requirements of the system. The thermocouple measures temperature, the fuel control valve regulates fuel flow, and the bleed air control governor maintains constant pressure in the bleed air system. Therefore, the load control valve is the correct answer as it specifically controls the amount of bleed air.

If electrical power is interrupted to the solenoid of an electrically-controlled, pneumatically-operated air-conditioning system shutoff valve that has a fail-safe feature, the valve will either open or close depending on the design requirements of the system. The fail-safe feature ensures that the valve will move to a specific position in the event of a power failure, which could be either open or closed depending on the desired safety mechanism of the system.

When fluid flows through an orifice, there is a loss of energy due to factors such as friction and turbulence. This loss of energy causes a decrease in pressure. Therefore, the outlet air pressure of an orifice is lower than the inlet pressure.

The lockout butterfly of the airflow regulator has an offset center of rotation, which means that the butterfly is not evenly balanced. When the butterfly is in the closed position, the offset center of rotation creates an unbalanced pressure that helps to keep the butterfly securely closed. Therefore, the correct answer is closed.

The function of the floor heat system pneumatic anticipator on a cargo type aircraft is to respond to rapid temperature changes. This means that the system is designed to detect sudden increases or decreases in temperature and adjust the floor heat accordingly. This is important in order to maintain a comfortable and safe temperature in the cargo area of the aircraft. The anticipator helps to prevent extreme temperature fluctuations and ensures that the floor heat system is responsive to changes in temperature.

The correct answer is "returns to the jet pump as recirculating air." When the bleed air is used for wing anti-icing, a portion of it is released overboard, while the remaining air is recirculated back to the jet pump. This recirculating air helps maintain the flow and pressure needed for the system to function properly.

Expansion joints in bleed air systems are best used on short runs of ducting. This is because expansion joints are designed to absorb the thermal expansion and contraction of the ducting caused by the high temperatures of the bleed air. Short runs of ducting experience less thermal expansion and contraction compared to long runs, making them more suitable for the use of expansion joints. Additionally, expansion joints are typically used in low-pressure ducting systems, as the high pressures in the system can cause the joints to fail. Therefore, short runs of low-pressure ducting are the ideal application for expansion joints in bleed air systems.

Low engine pressure ratio (EPR) refers to a lower than normal ratio between the pressure at the engine inlet and the pressure at the engine exhaust. In this case, the correct answer suggests that a clamp that has been improperly installed could be the cause of the low EPR. Improper installation of the clamp may result in a leak in the bleed air system, causing a decrease in pressure and subsequently leading to a low EPR.

An excessive pressure in the bleed air system can cause an unusually high cockpit temperature due to an over-speeding turbine. When the turbine spins too fast, it generates more heat, which can lead to higher temperatures in the cockpit. This can be caused by a malfunction or failure in the turbine's control system, resulting in an increase in pressure and speed.

The correct answer is "modulating valve, sensor, and temperature control circuit." The modulating valve helps regulate the flow of bleed air, while the sensor measures the outlet temperature. The temperature control circuit then adjusts the modulating valve based on the sensor readings to maintain a constant outlet temperature.

The system shutoff valve is the component that stops the flow of air to the air-conditioning system. It is responsible for controlling the flow of refrigerant and preventing it from entering the system when necessary, such as during maintenance or repairs. This valve is typically located near the compressor or in the high-pressure line, and it can be manually operated or controlled by the air-conditioning system itself. Its main function is to ensure the safety and efficiency of the air-conditioning system by allowing for proper maintenance and preventing damage to the system.

When the downstream air temperature of the bleed air air-conditioning system exceeds the predetermined temperature, the butterfly valve closes. In order to prevent any damage or overheating, a thermal switch is activated. This thermal switch will then open the flow control and shutoff valve component to allow for proper cooling and regulation of the air temperature.

During a cabin leakage test, the maximum allowable temperature of the air provided to the aircraft is 120°F. This temperature limit ensures that the test is conducted under realistic conditions and simulates the potential temperature variations that the aircraft may experience during normal operations. It helps to evaluate the performance of the cabin pressure control system and identify any potential leaks or issues that may affect the safety and comfort of the passengers and crew.

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The correct answer is 175 ± 10°F. This means that the water separator over temperature switch will actuate when the temperature reaches 175°F, with a tolerance of plus or minus 10 degrees. This allows for a range of temperatures between 165°F and 185°F for the switch to activate.

The cargo aircraft temperature control component that produces an electrical signal that causes the temperature control valve to increase or decrease compartment temperature as required to correct an unbalanced bridge condition is the temperature control box.

The timed pressure drop method determines cabin pressure leakage by measuring the pressure decrease. This means that the method calculates the difference in pressure before and after a certain period of time to determine the amount of leakage. By measuring the pressure decrease, it gives an accurate indication of the leakage rate in the cabin.

The correct answer is ACS pressure regulator and shutoff valve. The ACS pressure regulator and shutoff valve is responsible for maintaining the bleed air inlet pressure at 40 pounds per square inch gage (psig) on the bomber air-conditioning system (ACS). This valve regulates the flow of air into the system and shuts off the air supply when the desired pressure is reached. It ensures that the air-conditioning system operates at the correct pressure to provide effective cooling and ventilation.