A Test Quiz On Basic Aircraft Landing Gear System
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If the liquid level gauge in vapor- cycle cooling system indicates a low freon charge, the system should
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Not be operated until freon and oil have been added
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Be operated for a period of time to reach a stable condition and then the freon level rechecked
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Be operated and pressure check performed
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Explore the fundamentals of aircraft landing gear systems through this focused quiz. Assess your understanding of system components, operation issues, and maintenance practices crucial for safe and efficient aircraft operation.
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- 2.
Where does the breakage of control cable wires occur most frequently?
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Breakage usually occurs where the cables are swaged to turnbuckle and ball terminals
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Breakage usually occurs where cable pass over pulleys and through fairleads
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Breakage sites are unpredictable and usually occur randomly anywhere along the length of a cable
Correct Answer
A. Breakage usually occurs where cable pass over pulleys and through fairleadsExplanation
Breakage of control cable wires occurs most frequently where the cable passes over pulleys and through fairleads. This is because these areas experience high levels of stress and friction, which can lead to wear and tear on the cable. The constant movement and rubbing against the pulleys and fairleads can cause the cable to weaken and eventually break. Therefore, it is important to regularly inspect and maintain these areas to prevent breakage and ensure the proper functioning of the control cable system.Rate this question:
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- 3.
What controls the inflation sequence in a pneumatic deicer boot system?
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Vacuum pump
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Distributor valve
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Shuttle- valve
Correct Answer
A. Distributor valveExplanation
The distributor valve controls the inflation sequence in a pneumatic deicer boot system. It is responsible for distributing air pressure to different sections of the deicer boots in a specific sequence, ensuring that they inflate and deflate in the correct order. This helps to remove ice and frost from the aircraft's surfaces effectively, improving its performance and safety.Rate this question:
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- 4.
Which condition would be most likely to cause excessive vacuum in vacuum system?
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Vacuum relief valve spring weak
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Vacuum relief valve improperly adjusted
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Vacuum pump over speed
Correct Answer
A. Vacuum relief valve improperly adjustedExplanation
If the vacuum relief valve is improperly adjusted, it means that it is not set to the correct pressure level to release excess vacuum. This can cause the valve to remain closed even when there is excessive vacuum in the system. As a result, the vacuum pressure will continue to build up, leading to excessive vacuum in the vacuum system.Rate this question:
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- 5.
After installation of a rebuilt hydraulic hand pump, it is found that the handle cannot be moved in the pumping direction (pressure stoke). The most likely cause is an incorrectly installed
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Hand pump inport check valve
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Inport/outport orifice check valve
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Hand pump outport check valve
Correct Answer
A. Hand pump outport check valveExplanation
The most likely cause for the handle of the hydraulic hand pump not being able to move in the pumping direction (pressure stroke) after installation is an incorrectly installed hand pump outport check valve. The outport check valve is responsible for allowing fluid to flow out of the pump in the desired direction, and if it is installed incorrectly, it can block the flow of fluid and prevent the handle from moving.Rate this question:
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- 6.
Chattering of the hydraulic pump during operation is an indication
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That air is entering the pump
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That the main system relief valve is sticking open
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Of low accumulator preload
Correct Answer
A. That air is entering the pumpExplanation
The chattering of the hydraulic pump during operation indicates that air is entering the pump. This can be deduced because chattering is often caused by the presence of air bubbles in the hydraulic fluid. When air enters the pump, it can disrupt the smooth flow of the fluid, leading to vibrations and chattering noises. Therefore, the correct answer is that air is entering the pump.Rate this question:
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- 7.
What will be the result of the instrument static pressure line become disconnected inside a pressurized cabin during cruising flight?
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The altimeter will read low and the airspeed indicator will read high
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The altimeter and airspeed indicator will both read high
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The altimeter and airspeed indicator will both read low
Correct Answer
A. The altimeter and airspeed indicator will both read lowExplanation
If the instrument static pressure line becomes disconnected inside a pressurized cabin during cruising flight, the altimeter and airspeed indicator will both read low. This is because the static pressure line is responsible for providing the necessary air pressure to these instruments for accurate readings. Without the proper static pressure, both instruments will underestimate the altitude and airspeed, resulting in lower readings.Rate this question:
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- 8.
A "tap test" is conducted to find damage in a
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Composite inspection
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Sheet metal inspection
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Both composite and sheet metal inspection
Correct Answer
A. Composite inspectionExplanation
A "tap test" is conducted to find damage in a composite inspection. This is because composite materials, which are made up of different layers of materials bonded together, can have hidden damage such as delamination or internal cracks. By tapping on the surface of the composite material, inspectors can listen for changes in sound that may indicate the presence of damage. In contrast, sheet metal inspections typically involve visual inspections or the use of non-destructive testing methods such as ultrasonic testing or dye penetrant inspection.Rate this question:
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- 9.
A loud hammering noise in a hydraulic system having an accumulator usually indicates
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Too low or nor preload in the accumulator
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Too much preload in the accumulator
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Air in the fluid
Correct Answer
A. Too low or nor preload in the accumulatorExplanation
A loud hammering noise in a hydraulic system with an accumulator usually indicates that there is too low or no preload in the accumulator. The accumulator is responsible for storing hydraulic energy and releasing it when needed. If there is insufficient preload in the accumulator, it will not be able to effectively store and release this energy, causing the hammering noise.Rate this question:
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- 10.
Upon completion of the landing gear extension cycle, the green light illuminated and the red light remained lit. What is the probable cause
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Short in the up limit switch
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Short in the down limit switch
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Short in the gear safety switch
Correct Answer
A. Short in the up limit switchExplanation
A short in the up limit switch could be the probable cause for the green light to illuminate and the red light to remain lit after the completion of the landing gear extension cycle. This short circuit could be preventing the down limit switch or the gear safety switch from functioning properly, causing the red light to stay on.Rate this question:
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- 11.
Excessive wear on both of the side of the control cable pulley grove is evidence of
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Pulley misalignment
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Cable misalignment
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Excessive cable tension
Correct Answer
A. Pulley misalignmentExplanation
Excessive wear on both sides of the control cable pulley groove indicates that the pulley is not properly aligned. When the pulley is misaligned, it causes the cable to rub against the sides of the groove, leading to excessive wear. This can occur due to incorrect installation or damage to the pulley itself. Cable misalignment or excessive tension may cause wear on only one side of the groove, making them incorrect explanations in this case.Rate this question:
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- 12.
Which statement regarding an aircraft instrument vacuum system is true?
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If the air to each vacuum instrument is connected to a common atmospheric pressure manifold, the system generally will be equipped with instrument filters only
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Vacuum systems are generally more effective at high altitudes than positive pressure systems
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Dry- type vacuum pump with carbon vanes are susceptible to damage form solid airborne particles particles and must take in only filtered air
Correct Answer
A. Dry- type vacuum pump with carbon vanes are susceptible to damage form solid airborne particles particles and must take in only filtered air -
- 13.
If and aircraft shock strut (air/ oil type) bottoms upon initial landing contact, but functions correctly during taxi, the most probably cause is
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Low fluid
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Low air charge
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A restricted metering pin orifice
Correct Answer
A. Low fluidExplanation
If an aircraft shock strut bottoms upon initial landing contact but functions correctly during taxi, the most probable cause is low fluid. This means that there is not enough hydraulic fluid in the shock strut to properly absorb the impact of landing. As a result, the strut reaches its limit and bottoms out upon initial contact. However, during taxi, the strut functions correctly because it does not experience the same level of impact as during landing.Rate this question:
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- 14.
Movement of the cockpit control toward the nose down position during operation check of the elevator trim tab system will cause the trailing edge of the trim tab to move in which direction?
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Upward, regardless of elevator position
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Downward, regardless of elevator positon
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Downward if the elevator is in the UP position and upward if the elevator is in the down position
Correct Answer
A. Upward, regardless of elevator positionExplanation
When the cockpit control is moved toward the nose down position during the operation check of the elevator trim tab system, the trailing edge of the trim tab will move upward. This movement is independent of the position of the elevator.Rate this question:
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Our quizzes are rigorously reviewed, monitored and continuously updated by our expert board to maintain accuracy, relevance, and timeliness.
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Current Version
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Mar 21, 2023Quiz Edited by
ProProfs Editorial Team -
Jul 04, 2015Quiz Created by
Truonghungngoc
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