The FAA
Aviation Mechanic - Airframe
test bank contains questions pertaining to
Assembly and Rigging
. 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.
Did you know? Despite their claims of completeness,
the FAA test banks provided by several other online test preparation sources
are woefully incomplete. Read more about the
situation here. Our GroundSchool FAA written test preparation software generally
contains a much more up to date and complete question set and in no way suffers
from such deficiencies. In fact, it's the best way to prepare for your FAA written
test, period.
That said, while the following questions are intended
as a general familiarization tool, this list may not be up-to-date nor accurate.
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,
but it also includes answers and explanation and has many features to make your
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| Sample Questions
from the FAA
Aviation Mechanic - Airframe
Test Bank |
- In rotorcraft external-loading, the ideal location of the cargo release is where the line of action passes
- In a hovering helicopter equipped with a tail rotor, directional control is maintained by
- Which statement is correct concerning torque effect on helicopters?
- Wing dihedral, a rigging consideration on most airplanes of conventional design, contributes most to stability of the airplane about its
- An airplane which has good longitudinal stability should have a minimum tendency to
- An airplane is controlled directionally about its vertical axis by the
- If the right wing of a monoplane is improperly rigged to a greater angle of incidence than designated in the manufacturer's specifications, it will cause the
- Improper rigging of the elevator trim tab system will affect the balance of the airplane about its
- Buffeting is the intermittent application of forces to a part of an airplane. It is caused by
- The correct dihedral angle can be determined by
- Where is fuselage station No. 137 located?
- When inspecting a control cable turnbuckle for proper installation, determine that
- When a fiber or nylon insert-type, self-locking nut can be threaded on a bolt or stud through the insert with only the fingers, it should be
- After repairing or re covering a rudder, the surface should be rebalanced
- Excessive wear on both of the sides of a control cable pulley groove is evidence of
- Which statement concerning the 100-hour inspection of an airplane equipped with a push pull tube type control system is true?
- The purpose of spring tabs or servo tabs is to
- If the travel of an airplane's controls is correct but the cables are rigged exceptionally tight, what probable effect will this have when flying the airplane?
-
(Refer to figure 8.)
Identify the cable that is used in primary control systems and in other places where operation over pulleys is frequent.
- Why is it generally necessary to jack an aircraft indoors for weighing?
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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