2A655 Volume 3 Unit Review 1-60(Aircraft)

If a hydraulic system is found to be contaminated, draining the affected system should begin with the reservoir. The reservoir is the primary storage tank for hydraulic fluid in a hydraulic system. By draining the reservoir first, any contaminated fluid can be removed and replaced with clean fluid, preventing further contamination of the system. Additionally, draining the reservoir allows for inspection and cleaning of the reservoir itself, ensuring that it is free from any debris or contaminants that could potentially cause further issues in the system.

Overfilling the system reservoir can cause it to rupture. When the reservoir is filled beyond its capacity, the excess fluid puts pressure on the walls of the reservoir, potentially causing it to burst. This can lead to fluid leakage and damage to the surrounding components of the system. Therefore, it is important to observe the fluid level and avoid overfilling to prevent any potential rupture of the reservoir.

The next component to be checked would be the antiskid control box. Since the antiskid switch is ON and all circuit breakers are engaged, the issue is likely with the control box itself. By inspecting the control box, it can be determined if there is a malfunction or any other issue that is causing the antiskid system to be completely inoperative.

The trim system in the aircraft's roll axis compensates for any imbalance or external environmental conditions that affect stabilized flight. This system helps to adjust the aircraft's control surfaces to maintain a desired attitude and reduce the pilot's workload. By making small adjustments to the trim, the aircraft can counteract any imbalances or external factors that may cause it to roll off course, ensuring a more stable and controlled flight.

In an emergency, pulling the fire handles is the correct way to operate the shutoff valves of the engine-driven hydraulic pump. This is because pulling the fire handles will activate the fire suppression system, which includes shutting off the fuel flow to the engines and cutting off the hydraulic pump. This action helps to prevent further damage or potential fire hazards in the event of an emergency.

The Stratopower variable-volume pump uses a nutating plate to hold the pistons in contact with the cam plate. The nutating plate is a component that moves in a circular motion, causing the pistons to follow the contour of the cam plate. This allows for efficient pumping action and ensures that the pistons maintain contact with the cam plate throughout the pumping process. The use of a nutating plate in this pump design helps to optimize performance and reliability.

To change the direction of rotation of a hydraulic motor, the direction of fluid flow into the motor should be changed. Hydraulic motors rely on the flow of fluid to generate rotational motion. By reversing the direction of fluid flow, the motor will rotate in the opposite direction. This can be achieved by adjusting the valves or changing the configuration of the hydraulic system to redirect the fluid flow.

Variable-volume pumps do not require a separate pressure regulating device in the system because they have an integral compensator. This means that the pump is able to automatically adjust its output pressure based on the system's demand. The integral compensator allows the pump to maintain a consistent pressure without the need for an additional regulating device.

An internal snubber is a type of actuator that has the characteristic of slowing down the travel of the piston when it nears either end of the cylinder. This is achieved through the use of internal mechanisms that provide resistance or dampening effect, reducing the speed of the piston as it reaches the ends of the cylinder. This helps to prevent abrupt stops or impacts, ensuring smoother and more controlled movement of the actuator.

If the signal system fails to advance to MADE conditions upon contact with the receiving aircraft, a probable cause could be a malfunctioning or faulty signal coil. The signal coil is responsible for transmitting the necessary signals to advance the system, so if it is not functioning properly, it can prevent the system from advancing as it should.

The cargo door is retracted upward into the aft fuselage cavity by two hydraulic actuators. These actuators are responsible for the movement and retraction of the door. Having two actuators ensures that there is redundancy in the system, providing a backup in case one actuator fails. This redundancy is crucial for the safe operation of the cargo door, as any failure in the actuator could result in a malfunction or inability to retract the door properly.

In a typical electrically sequenced system, a microswitch is used to ensure proper sequencing. A microswitch is a small mechanical switch that is activated by a physical force, such as a lever or button. It is commonly used in control systems to detect and control the position or presence of an object. In the context of sequencing, a microswitch can be used to detect the completion of one task before initiating the next, ensuring that the system operates in the correct sequence.

The drive shaft torque test is the appropriate test to determine the amount of torque required to turn the pump driveshaft. This test specifically focuses on measuring the torque needed to rotate the driveshaft, providing valuable information about the pump's performance and efficiency. By conducting this test during bench checking, technicians can ensure that the pump is functioning properly and meets the required torque specifications.

Sequence valves are installed in a system to ensure that one operation is performed before the rest of the system can operate. This helps in maintaining a specific order or sequence of operations, preventing simultaneous or undesired actions. By controlling the flow of fluid, sequence valves allow for a systematic and organized functioning of the system, ensuring that each operation is completed before the next one begins.

A leakage test on a swivel joint should be performed for 2 minutes. This duration allows enough time to detect any potential leaks in the joint without wasting excessive time. It strikes a balance between ensuring the joint's integrity and efficiency in completing the test. A shorter duration may not provide enough time to identify leaks accurately, while a longer duration may be unnecessary and time-consuming.

The first thing you should check is the press to test feature of the bulb. This means that you need to press the bulb to see if it lights up, indicating that it is functioning properly. If the bulb does not light up, then it is likely faulty and needs to be replaced. This is important because the low-pressure warning light is crucial for indicating any issues with the engine pump, and a faulty bulb could lead to a failure in detecting potential problems.

After bleeding the power system and removing air bubbles, it is recommended to bleed out an additional one quart of fluid. This is necessary to ensure that all air pockets are completely eliminated from the system, as even small amounts of air can cause issues with the system's performance and efficiency. Bleeding out this additional amount of fluid helps to ensure that the power system is properly filled and functioning optimally.

The correct answer is the aft loadmaster's control panel. This panel is located at the back of the aircraft and allows the loadmaster to operate the cargo door and ramp manually. The forward loadmaster's control panel may not have the necessary controls for this operation, and the co-pilot's ADS panel is unrelated to cargo door and ramp operation.

If a brake line ruptures and the hydraulic fuse sets, it means that the hydraulic fuse will activate and stop the flow of hydraulic fluid. Therefore, the amount of hydraulic fluid lost will depend on the size of the brake line and the pressure at which the hydraulic system operates. Since the answer is 40(+10/-0) cubic inches, it suggests that in this scenario, approximately 40 cubic inches of hydraulic fluid will be lost.

As the drive shaft rotates on a Stratopower pump, the pistons move back and forth while the cylinder block remains stationary. This means that the pistons are responsible for creating the pumping action, while the cylinder block serves as a stable housing for the pistons.

A filter assembly with a differential pressure indicator operates based on the principle of measuring the difference between the pressure entering the filter element and the pressure leaving the filter element. This allows the operator to monitor the pressure drop across the filter, which indicates the level of contamination or clogging. By observing the differential pressure, the operator can determine when the filter needs to be cleaned or replaced to maintain optimal filtration efficiency.

If air bubbles are coming out of the accumulator end cap during an internal leakage test, it indicates that the piston is leaking. The piston is responsible for separating the gas and liquid in the accumulator, and if it is leaking, it allows gas to escape into the liquid side, causing air bubbles to be released from the end cap. This suggests that there is a problem with the piston's seal or integrity, leading to the leakage.

The correct answer is "be 300 lbs with no back pressure". This means that the spring tension of the relief valve would need to be 300 lbs in order to relieve the pressure of 1800 psi. The ball seat area of 1/6 sq. in is not relevant to determining the spring tension.

The correct answer is "unseat one pressure poppet and one return." This means that when the camshaft is rotated, it causes one pressure poppet and one return poppet to become unseated. This action allows fluid to flow through the valve in a specific direction, depending on the design and configuration of the valve.

When the pump low pressure warning light comes on and the pressure reading on the accumulator pressure gauge reads low, it indicates that there is a problem with the pump system. The engine driven pump is responsible for maintaining the pressure in the system, so it is the first component that should be suspected of malfunctioning. The low pressure warning light and low pressure reading on the gauge suggest that the pump is not functioning properly, causing a decrease in pressure. Therefore, the engine driven pump is the most likely component to be causing the issue.

During landing-gear retraction, the automatic brake actuator applies the brakes to stop wheel spin. This unit is responsible for automatically engaging the brakes when the landing gear is being retracted to prevent the wheels from spinning freely. The automatic brake actuator ensures that the wheels are properly controlled and do not rotate excessively during the retraction process, enhancing the safety and stability of the aircraft.

The minimum psi pressure in the return line to the reservoir would be 25. This is because the hydraulic reservoir is already pressurized to 25 psi, so the pressure in the return line would need to be at least the same in order for the fluid to flow back into the reservoir.

To determine if the seals on the piston of an accumulator are leaking, you should perform an internal leakage test. This test involves pressurizing the accumulator and then monitoring the pressure over a period of time. If the pressure decreases significantly, it indicates that there is internal leakage in the seals. This test helps to identify any potential issues with the seals and allows for timely maintenance or replacement to prevent further damage or failure of the accumulator.

Reducing the pressure to 75psi during the testing of a brake assembly simulates back pressure. Back pressure refers to the resistance or force exerted against the normal flow of fluid or gas in a system. In the context of a brake assembly, back pressure simulates the resistance or force that occurs when the brakes are applied, mimicking real-world conditions and allowing for accurate testing and evaluation of the brake system's performance.

Spoilers are used to augment the ailerons to achieve the roll rate commanded by the pilot or copilot. Spoilers are surfaces located on the wings that disrupt the airflow over the wings, reducing lift and increasing drag. By deploying spoilers on one wing while retracting them on the other, the aircraft can roll in the desired direction. This helps in controlling the roll motion of the aircraft during maneuvers and allows for precise control of the aircraft's bank angle.

The pilot should consult the appropriate fault isolation manual first. This manual provides specific instructions and procedures for troubleshooting and identifying the cause of a fault or issue. By consulting this manual, the pilot can follow the recommended steps to diagnose and rectify the problem with the roll input in the mechanical mode. It is an essential resource for troubleshooting and resolving any system-related issues.

The correct answer is gland nuts. Gland nuts are used to connect the tandem surge boots to the fuel tube weld assembly. They provide a secure and tight connection between the two components, ensuring that there are no leaks or loose fittings. Gland nuts are typically threaded onto the fuel tube and tightened to create a seal, effectively connecting the surge boots to the fuel tube weld assembly.

The relief valve prevents excessive pressure from building in the toggle actuators during breakaway of the air-refueling nozzle. This valve is designed to open and release pressure when it reaches a certain level, ensuring that the actuators are not damaged by excessive pressure.

When taking fluid samples on a hydraulic system that does not have bleeder ports, it is necessary to open line connections to take the sample. This is because without bleeder ports, there is no other way to access the fluid in the system. By opening line connections, the fluid can be extracted for sampling purposes. Removing and replacing the filters or taking the sample from the reservoir only would not provide an accurate representation of the fluid within the system.

The purpose of the fluid quantity system test is to test the indication system. This system is responsible for providing accurate and reliable information about the fluid levels in various components of the system. By testing the indication system, the functionality and accuracy of the fluid level indicators can be verified. This is important for ensuring the safe and efficient operation of the fluid quantity system, as it allows operators to monitor and maintain appropriate fluid levels during operation.

The break-in period is necessary to ensure proper operation of the newly-overhauled pump at all pressure and revolutions per minute settings. During this period, the pump is run at various speeds and pressures to allow the components to settle into their proper positions and ensure that they are functioning correctly. This helps to identify any potential issues or malfunctions before the pump is put into regular use, ensuring its reliability and efficiency.

Hydraulically actuated downlocks are components that aid in forcing the cargo door down. These downlocks use hydraulic power to secure and lock the cargo door in place, ensuring that it remains closed during flight. By using hydraulics, the downlocks are able to provide a strong and reliable force to keep the cargo door securely shut, even under high pressure or turbulence. This ensures the safety and integrity of the aircraft's cargo during flight.

Nose wheel steering shimmy dampening is effective when the valve plunger is in the neutral position. This means that the valve is neither extended nor retracted. In this position, the valve is able to effectively dampen any vibrations or oscillations in the nose wheel steering system, preventing shimmying.

When a power control cylinder is in manual mode, the bypass valve allows the fluid to flow from one side of the main actuator to the other. The bypass valve acts as a pathway for the fluid to bypass the main actuator, allowing for manual control of the power control cylinder.

A check valve is a type of orifice that allows normal speed of operation in one direction, but limits speed in the other direction. It is designed to allow fluid flow in one direction while preventing backflow in the opposite direction. This is achieved through a valve mechanism that opens when the fluid flows in the desired direction and closes when there is reverse flow or pressure. As a result, the check valve acts as a speed limiter, allowing fluid to flow freely in one direction but restricting its flow in the opposite direction.

Hydraulic flow regulators are devices that control the flow of fluid in a hydraulic system. They are designed to regulate the flow in one specific direction, allowing fluid to pass through in that direction while restricting or blocking flow in the opposite direction. This helps to control the speed and pressure of the fluid in the system, ensuring that it flows smoothly and efficiently. Therefore, the correct answer is "in one direction."

A pressure reducer hydraulic valve would be needed in this scenario to lower the system pressure to a subsystem. This valve is designed to regulate and decrease the pressure of the hydraulic fluid flowing through it, which would help prevent the actuator from overloading the airframe.

If the fire control handle on No. 3 engine is pulled and the suction shutoff valve closes but the pressure shutoff valve does not close, it suggests that the pressure shutoff valve is faulty. The fire control handle is designed to shut off both the suction and pressure valves in order to stop the flow of fuel to the engine during a fire. If the suction shutoff valve is closing properly but the pressure shutoff valve is not, it indicates that there is an issue with the pressure shutoff valve specifically.

A wooden dowel would be used to remove the sleeve from a selector valve body. This is because a wooden dowel is a non-abrasive and non-magnetic tool that can be used to gently tap or push the sleeve out of the valve body without causing any damage. The wooden dowel is preferred over a brass dowel or magnet in this case because it is less likely to scratch or magnetically attract any metal components, ensuring a safe and effective removal process.

Energizing the slipway door control valve to the open side will direct hydraulic pressure to both the open and close side of the door actuators. This means that when the control valve is energized, it will activate both sides of the door actuators, allowing them to open and close the slipway door as needed.

When accomplishing a piston seizure test on a hydraulic accumulator, it is important to ensure that the hydraulic pressure does not exceed 50 psig. This is because exceeding this pressure limit can result in a piston seizure, which can cause damage to the hydraulic system. Keeping the pressure below 50 psig ensures that the test is conducted safely and prevents any potential issues or damage.

The purpose of the proof pressure test while bench checking a reservoir is to check for deformation/failure. This test is conducted to ensure that the reservoir can withstand the maximum pressure it is designed for without any structural damage or failure. By subjecting the reservoir to a higher pressure than its normal operating pressure, any potential deformations or failures can be identified and addressed before the reservoir is put into service. This test helps ensure the reliability and safety of the reservoir during its operation.

The statement "shock strut conical bearings binding" is not a probable cause for the aircraft tending to steer only to the left. The shock strut conical bearings are responsible for absorbing shocks and providing stability to the landing gear, but they do not directly affect the steering of the aircraft. Dragging brakes and a metering valve malfunction can both cause the aircraft to steer to one side, as they can create uneven braking forces or affect the hydraulic system that controls the steering.

A manually-operated check valve is typically installed in the pressure line. This is because the purpose of a check valve is to allow fluid flow in one direction and prevent backflow. By installing it in the pressure line, it ensures that the fluid can only flow in the desired direction, maintaining the desired pressure in the system.

The selector valve in an automatic hydraulic actuating system is controlled manually by the operator. This means that the operator is responsible for manually selecting and operating the valve to control the flow of hydraulic fluid. This allows the operator to manually control the system and make adjustments as needed.