2106 Flashcards

1
Q

The term composite is used to describe two or more
materials that are combined to form a structure that is
much stronger than the individual components.

A

Composite Structure

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2
Q

The simplest composite is composed of two elements:

A

Matrix and Reinforcing Materials

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3
Q

is generally in a liquid form that
serves as a bonding substance.

A

Matrix

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4
Q

is a solid form that provide the primary structural strength to the composite structure when combined in
a matrix

A

Reinforcing Materials

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5
Q

This manual developed by the aircraft Manufacturers that includes information prepared for the AMT or technicians who performs work on units, components and system while they are installed on the airplane.

A

AIRCRAFT MAINTENANCE MANUAL.

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6
Q

a chemical additives that quicken cure, or chemical reactions.

A

Accelerator

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7
Q

A material that are mixed into a two –part resin system to improve the properties of the systems.

A

Additives

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8
Q

A substance that is applied to two mating surfaces to bond them together by surface attachments.

A

Adhesive

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9
Q

Fibrous materials embedded in a resin matrix. The term
ADVANCED applied those materials, which have superior strength and stiffness and the process in which they are manufactures

A

Advance Composite

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10
Q

The weight of the fiber reinforcement per unit area of tape of fabric.

A

Area Weight

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11
Q

The term composite is define in FAA AC 4-214. A combination of two or more materials (reinforcing elements, fillers, and composite matrix binder), differing in form or composite on on a macro-scale.

A

Composite

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11
Q

A manual developed BY THE COMPONENT manufacturer and frequently adopted by the airframe manufacturer. A CMM is most frequently not approved by the FAA. Blanket approval comes through the AMM and SRM.

A

Component Maintenance Manual

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12
Q

The resistance to resist the crushing force.

A

Compressive Strength

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13
Q

An impurity of foreign substance present in the materials or environment that affects one or more property es of the materials, particularly adhesion.

A

Contaminant

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14
Q

A compression damage of the core.

A

Core Crush

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15
Q

to change the physical properties of the material by chemical reaction, by the application of catalyst , heat and pressure , alone or in combination.

A

Cure

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16
Q

Individual fibers woven together to produce cloth.

A

Fabric

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17
Q

Single strands of materials used reinforcement because of its high strength and stiffness

A

Fiber

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18
Q

A require document which is produced by the manufacturer. It has the parts and their part numbers exploded for identification.

A

ILLUSTRATED PARTS CATALOG.

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19
Q

One Fabric resin layer that is bonded to adjacent layers in the curing process.

A

Laminate

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20
Q

Persons performing a repair or alteration under parts 121 and 135, or repair stations certificated under part 145. As used in this AC, this term includes Maintenance Repair Organization(MRO), certificated repair stations (CRS), and operators’ maintenance facilities.

A

Maintenance Organization

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21
Q

The alignment of the fibers to the baseline set by the manufacturer for the perpendicular component

A

Orientation

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22
Q

The length of time that the resin, mixed with catalyst will be in a workable state.

A

Pot Life

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23
Q

a manual which developed by the manufacturer to cover all items not listed as minor, maintenance , including instructions for structural repair, major component removal, installation and adjustment set up. Etch.

A

Structural Repair Manual

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24
The life span that a product will remain useful, and in FAA AC 43-214 define shelf life as the length of time a raw material may be in storage under specific conditions and still meet the requirements of the applicable material specification, also known as storage life.
Shelf Life
25
The cumulative length of time a material may be out of freezer storage, prior to curing, and still maintain the required processability characteristics and mechanical properties.
Out Life
26
Types of Reinforcing Materials
Fiber Glass, Aramid, Carbon, Boron, Ceramic
27
Is made from a small strands of molten silica glass that are spun together & woven into cloth.
Fiberglass
28
3 Common Types of Fiberglass
E-glass S-glass C-glass
29
is a registered trademark of the El DuPont company and its most widely used Aramid.
Kevlar
30
Grade of a Kevlar fibers
Kevlar grade 49 Kevlar grade 29 Kevlar grade 129
31
Is a very strong, stiff reinforcement and used for its rigid strength characteristics.
Carbon
32
are made by depositing the element boron on a thin filament of tungsten
Boron
33
are used when a high temperature application is needed.
Ceramic
34
A manufacturer can design a part by using different types of fiber combination (hybrid) to tailor a part for strength or to reduce cost.
Hybrids
35
What are the types of Hybrid
Intraply hybrid Interply hybrid Selective placement
36
utilize reinforcing material that is woven from two or more different fibers.
Intraply hybrid
37
uses two or more layers of different reinforcing materials that are laminated together.
Interply Hybrid
38
Fibers may be selectively place to give greater strength , flexibility or reduced cost.
Selective Placement
39
Fabric Style
1) Non-Woven Fabric/ Unidirectional Fabric 2) Woven fabric / BI DIRECTIONAL FABRIC 3) Mat
40
Manufacturers construct honeycomb from the ff:
* Aluminum * Kevlar * Carbon * Fiberglass * Paper * Steel
41
This core materials consist of six sided shape of a natural honeycomb, which provide a core with a very high strength to weight ratio
Honeycomb
41
is a paper impregnated material which is widely used as an advance composite core material
NOMEX
42
Kinds of a Resin systems
--Polyester resin systems -Epoxy resin systems -Polybutadiene resins Polyester resin systems
43
used heat to form and set the shape of the part permanently
Thermoset
44
Thermoplastic c resins use heat to form the part into the desired shape is heated a second time, it will flow to form another shape
Thermoplastics
45
Resin marix are two-part systems consisting of the ff:
Resin and Hardener/Curing agent
46
This fabric are woven together in a number of weaves and weights and are more resistant to fiber breakout, delamination, and more damage tolerant than unidirectional materials
Woven Fabric
47
This fiber orientation in which all of the major fibers run in onedirection , giving strength in that direction is known as the unidirectional or the non woven fabric.
Non Woven
48
plain, satin, crowfoot
Weaves
49
is measure in thousandths of an inch or millimeters
Thickness
50
is measured in ounces per square yards, or a gram per square meter
Weight
51
is the number of yarns per inch of width in the warp and fill direction
Count
52
s the yield or denier, twist and ply level
Yarn Construction
53
not as strong as a unidirectional or woven fabric , and therefore is not commonly used in a repair work.
Mat
54
is at 45 to a warp threads, and can be formed into contoured shapes .
Bias
55
The threads that run the length of the fabric as it comes off the bolt and designated at 0 , more threads and stronger than fill directions
Warp
56
Are those that run perpendicular to the warp fibers, designated as 90 and ____ are the threads that interweave with the warp threads.
Weft
57
It is parallel to the warp threads, and its been removed for all fabrication and repair works.
SELVAGE EDGE
58
are the fabrics that have the resin system already impregnated into the fabric.
Pre-preg
59
Parts of Honeycomb
Facesheet, adhesive and honeycomb
60
The two most common types of core materials utilized in sandwich construction
Honeycomb and foam cores