The FAA
Aviation Mechanic - Airframe
test bank contains questions pertaining to
Landing Gear Systems
. The following list contains only a relatively small percentage of the pertinent
questions. Our software, which you are free to download now at no cost, will
generally contain a much more complete set of questions associated with this
test bank. This list is intended only to familiarize you in a general way with
the questions of the
Aviation Mechanic - Airframe
test bank.
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That said, while the following questions are intended
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We do not update this website as often as we update our software, which will
contain at any moment all questions that we have for a given test / topic. Therefore,
if you need to actually study for your test, instead of using the list below,
we strongly, strongly encourage you to download our GroundSchool
Aviation Mechanic - Airframe
written test prep software. Not only is it more complete and more up to date,
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| Sample Questions
from the FAA
Aviation Mechanic - Airframe
Test Bank |
- To prevent a very rapid extension of an oleo shock strut after initial compression resulting from landing impact,
- The metering pins in oleo shock struts serve to
- If it is determined that spongy brake action is not caused by air in the brake system, what is the next most likely cause?
- When bleeding aircraft brakes, one of the indications that the air has been purged from the system is
- An embossed letter ``H'' on an air valve core stem
- An automatic damping action occurs at the steer damper if for any reason the flow of high pressure fluid is removed from the
- What is one effect a restricted compensator port of a master cylinder will have on a brake system?
- The purpose of a sequence valve in a hydraulic retractable landing gear system is to
- When servicing an air/oil shock strut with MIL-5606 the strut should be
- If the extended longitudinal axis of the main landing gear wheel assemblies intersects aft of the aircraft, the wheels can be termed as having
- Extension of an oleo shock strut is measured to determine the
- If an airplane equipped with master cylinders and single disk brakes has excessive brake pedal travel, but the brakes are hard and effective, the probable cause is
- The left brake is dragging excessively on an airplane on which no recent brake service work has been performed. The most probable cause is
- When a properly operating fusible plug has allowed a tire to deflate, the tire should be
- What action, if any, should be taken when there is a difference of more than 5 pounds of air pressure in tires mounted as duals?
- When an empty shock strut is filled with fluid, care should be taken to extend and compress the strut completely at least two times to
- A landing gear position and warning system will provide a warning in the cockpit when the throttle is
- What device in a hydraulic system with a constant delivery pump allows circulation of the fluid when no demands are on the system?
- An O ring intended for use in a hydraulic system using MIL-H-5606 (mineral base) fluid will be marked with
-
(Refer to figure 10.)
The trunnion nut on an aircraft landing gear requires a torque of 320 inch-pounds. To reach the nut, a 2-inch straight adapter must be used on an 18-inch torque wrench. How many foot pounds will be indicated on the torque wrench when the required torque of the nut is reached?
- In most modern hydraulically actuated landing gear systems, the order of gear and fairing door operation is controlled by
The
list above contains 1/4 or less of the actual number of questions
and may not be up to date! Download
the software today to get access to all available questions. |
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