| The FAA
Aviation Mechanic - Airframe
test bank contains questions pertaining to
Sheet metal & Non-metallic Structures
. 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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Aviation Mechanic - Airframe
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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,
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Aviation Mechanic - Airframe
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| Sample Questions
from the FAA
Aviation Mechanic - Airframe
Test Bank |
- Which statement is true regarding a cantilever wing?
- When fabricating parts from Alclad 2024-T3 aluminum sheet stock,
- Rivet pitch is the distance between the
- Which of the following need not be considered when determining minimum rivet spacing?
- Heat treated rivets in the D and DD series that are not driven within the prescribed time after heat treatment or removal from refrigeration
- A sheet metal repair is to be made using two pieces of 0.040-inch aluminum riveted together. All rivet holes are drilled for 3/32-inch rivets. The length of the rivets to be used will be
-
(Refer to figure 3.)
Which is the grip length of the flush rivet?
- A DD rivet is heat treated before use to
- Joggles in removed rivet shanks would indicate partial
- The length of rivet to be chosen when making a structural repair that involves the joining of 0.032-inch and 0.064-inch aluminum sheet, drilled with a No. 30 drill, is
-
(Refer to figure 5.)
What is the flat layout dimension?
- The flat layout or blank length of a piece of metal from which a simple L shaped bracket 3 inches by 1 inch is to be bent depends upon the radius of the desired bend. The bracket which will require the greatest amount of material is one which has a bend radius of
- The most important factors needed to make a flat pattern layout are
- When bending metal, the material on the outside of the curve stretches while the material on the inside of the curve compresses. That part of the material which is not affected by either stress is the
- (Refer to figure 7.) What is dimension F?
Setback at D = .095
Setback at E = .068
Bend allowance at D = .150
Bend allowance at E = .112
- A well designed rivet joint will subject the rivets to
- The shop head of a rivet should be
- The Dzus turnlock fastener consists of a stud, grommet, and receptacle. The stud diameter is measured in
- Metal fasteners used with carbon/graphite composite structures
- When balsa wood is used to replace a damaged honeycomb core, the plug should be cut so that
- One method of inspecting a laminated fiberglass structure that has been subjected to damage is to
- A category of plastic material that is capable of softening or flowing when reheated is described as a
- The classification for fiberglass reinforcement material that has high resistivity and is the most common is
- The strength and stiffness of a properly constructed composite buildup depends primarily on
- When repairing large, flat surfaces with polyester resins, warping of the surface is likely to occur. One method of reducing the amount of warpage is to
- Fiberglass damage that extends completely through a laminated sandwich structure
- Which of the following, when added to wet resins, provide strength for the repair of damaged fastener holes in composite panels?
1. Microballoons.
2. Flox.
3. Chopped fibers.
- If an aircraft's transparent plastic enclosures exhibit fine cracks which may extend in a network over or under the surface or through the plastic, the plastic is said to be
- The coefficient of expansion of most plastic enclosure materials is
- When holes are drilled completely through Plexiglas, a
- Longitudinal (fore and aft) structural members of a semi monocoque fuselage are called
- A single lap sheet splice is to be used to repair a section of damaged aluminum skin. If a double row of 1/8-inch rivets is used, the minimum allowable overlap will be
- What is the minimum spacing for a single row of aircraft rivets?
- Which procedure is correct when using a reamer to finish a drilled hole to the correct size?
The
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Aviation Mechanic - Airframe
test bank, click here.
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