FREE AND STUDY GAMES ABOUT 8 AIRCRAFT LANDING G

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FREE AND STUDY GAMES ABOUT 8 AIRCRAFT LANDING G

EXAM QUESTIONS

Actual Qs and Ans Expert-Verified Explanation

This Exam contains:

-Guarantee passing score -81 Questions and Answers -format set of multiple-choice -Expert-Verified Explanation

Question 1: Debooster cylinders are used in brake systems primarily to

Answer:

reduce the pressure to the brake and increase the volume of fluid flow.Question 2: If it is determined that spongy brake action is not caused by air in the brake system, what is the next most likely cause?

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Deteriorated flexible hoses.

Question 3: Lockout deboosters are primarily pressure reducing valves that

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allow full debooster piston travel without fluid from the high pressure side entering the low pressure chamber.

Question 4: What should be checked when a shock strut bottoms during a landing?

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Fluid level.

Question 5: The metering pins in oleo shock struts serve to

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retard the flow of oil as the struts are compressed.Question 6: Instructions concerning the type of fluid and amount of air pressure to be put in a shock strut are found

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in the aircraft manufacturer's service manual.Question 7: The removal, installation, and repair of landing gear tires by the holder of a private pilot certificate on an aircraft owned or operated is considered to be

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preventive maintenance.Question 8: How long should you wait after a flight before checking tire pressure?

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At least 2 hours (3 hours in hot weather).Question 9: What action should be taken whenever maintenance is performed that will affect the landing gear system performance?

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The aircraft should be placed on jacks and a retraction test should be performed.Question 10: What is the minimum amount of time to wait for tires to cool before checking tire pressure?

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• hours.

Question 11: Which statement is true with respect to an aircraft equipped with hydraulically operated multiple-disk type brake assemblies?

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Do not set parking brake when brakes are hot.

Question 12: A flexible hydraulic hose identified as MIL-H-8788 will have a stripe running the length of the hose. This stripe is

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installed without excessive twisting.Question 13: An electric motor used to raise and lower a landing gear would most likely be a

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split field series-wound motor.Question 14: Exposure to and/or storage near which of the following is considered harmful to aircraft tires?

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Fuel, oil, ozone, electrical equipment, hydraulic fluid, and solvents.

Question 15: A hydraulic system referred to as a 'power pack' system will

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have all hydraulic power components located in one unit.

Question 16: The best safeguards against heat buildup in aircraft tires are

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short ground rolls, slow taxi speeds, minimum braking, and proper tire inflation.Question 17: What is the purpose of a compensating port or valve in a brake master cylinder of an independent brake system?

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Permits the fluid to flow toward or away from the reservoir as temperature changes.Question 18: A sleeve, spacer, or bumper ring is incorporated in a landing gear oleo shock strut to

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limit the extension stroke.

Question 19: Extension of an oleo shock strut is measured to determine the

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proper operating position of the strut.

Question 20: The hydraulic packing seals used in a landing gear shock strut are

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used only with a specific type of fluid.Question 21: A close inspection of a fusible plug reveals the core has experienced some deformation. What is the appropriate maintenance procedure?

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Replace all the fusible plugs.Question 22: A pilot reports that the brake pedals have excessive travel. A probable cause is

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lack of fluid in the brake system.Question 23: Excessive wear in the shoulder area of an aircraft tire is an indication of

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underinflation.Question 24: An automatic damping action occurs at the steering damper if for any reason the flow of high-pressure fluid is removed from the

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inlet of the steering damper.

Question 25: The primary purpose for balancing aircraft wheel assemblies is to

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prevent heavy spots and reduce vibration.Question 26: What is the function of a cam incorporated in a nose gear shock strut?

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Straightens the nosewheel.Question 27: On all aircraft equipped with retractable landing gear, some means must be provided to

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extend the landing gear if the normal operating mechanism fails.