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vol 3 LO
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  • 問題数 79 • 8/29/2023

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    問題一覧

  • 1

    high strength and stiffness in composite-bonded materials is a result of the

    concept of the cross-plied lamination

  • 2

    what is the indentifying plot for aramid materials

    yellow

  • 3

    what is a characteristic of graphite materials

    ultra-high stiffness

  • 4

    nidirectional fabrics have the highest possible structural properties in fabric composite construction as a result of having

    straight and uncrimped fibers

  • 5

    what assential function does a resin matrix not preform

    carry the primary load of high-strength material

  • 6

    the process where viscous materials undergo a chemical reaction to generate a rigid structure is referred to as

    curing

  • 7

    hat type of adhesive is most often used as a lightweight splice material for honeycomb core section splice repairs

    foam

  • 8

    when storing advanced composite materials in cold storage, what is the maximum temp permitted

    0 degree

  • 9

    cutting large batches of material into smaller sections the first time it is thawed is a process known as

    kiting

  • 10

    adding too much catalyst to your matrix produces what is known as a

    hot mixture

  • 11

    when mixing a liquid matrix, the components should be

    blended together slowly

  • 12

    what must you do prior to using the triple-beam scale

    zero the scale

  • 13

    the recommended vacuum pressure, measured in inches of mercury, for curing a repair is

    15inHg-28inHg

  • 14

    liquid moisture present in honeycomb sandwich assemblies is usually detectable by

    x-ray

  • 15

    in a field environment, mitigate the effects of any moisture not removed during the drying process by using cure temp of or below

    210

  • 16

    what kind of ply lay-up would a laminate with a ply orientation of 45,53,-45,-45, 53,45

    angle

  • 17

    what can you do to help ease the reading of the ply orientation in a graphite repair site

    wet sand with 400 grit sandpaper

  • 18

    first element of patch preparation is generating a

    patch drawing

  • 19

    you would use a drill bushing and guide when drilling advanced composite laminates to ensure holes are drilled perpendicular to the surface and prevent

    wobble

  • 20

    to compensate for the stresses of flexing in flight, the minimum required panel gap is

    .010

  • 21

    which work procedure do you normally perform first when making a minor repair to a laminated fiberglass panel

    clean the damaged area thoroughly with an approved solvent

  • 22

    when making a minor repair to a laminated fiberglass panel, what is normally the tire work procedure you use

    mix the resin according to the applicable tech order

  • 23

    what is the first step of scarf repair

    removed and paint or coating

  • 24

    when repairing a minor metal-bonded honeycomb assembly skin delaminating, you can prevent core damage when drilling holes for the resin injection by using a

    drill stop

  • 25

    how are the thermocouples positioned when repairing a metal-bonded honeycomb repair

    equally spaced around the repair

  • 26

    LO technologist gives an aircraft the ability to defeat radar, thermal, acoustical

    visual

  • 27

    the main purpose of making an aircraft LO is to increase the aircraft’s

    survivablity

  • 28

    the acronym RADAR stands for

    radio detection and ranging

  • 29

    what is radar cross section

    the size of an object as measured by radar

  • 30

    radar cross section is typically measured in square

    meters

  • 31

    ondensation trains, glints and paint schemes are sources of which radar signature

    visual

  • 32

    what type of aircraft signature source is generated by energy backscatter

    radar cross section

  • 33

    at is the most important factor for radar cross section reduction on an object

    shape

  • 34

    which reduction strategy uses painting an aircraft to match primary mission

    visual

  • 35

    when you located damage during an insp you will record length, width, depth/height, classification and

    orientation

  • 36

    what LO verification tier is a whole body near field measurement

    3

  • 37

    during a repair layout, what tool would you use to create or measure an angle

    protractor

  • 38

    the best way to crest a straight line when cutting radar absorbent meter oak is to use

    steel ruler

  • 39

    arranging all aircraft details so that they coincide with the outer mold line angle of the aircraft is called

    platform alignment

  • 40

    what alignment shape is widely used because it allows for smaller repair areas

    saw-tooth

  • 41

    when developing a repair in a good platform alignment, you would align your repair with the aircraft

    butt line

  • 42

    what do you resistive properties of the loaded core of a radar-absorbing structure do to the electromagnetic energy entering it

    weakens it

  • 43

    dissipating an energy current over the whole surface of the aircraft is purpose of the

    conductive layer

  • 44

    corrosion-inhibiting primer is recommended to be used as a barrier between LO coating and metal structure because of

    dissimilar metal potential

  • 45

    LO platforms use composite materials because they do not reflect radar and are

    nonconductive

  • 46

    ceramics are used as insulation on aircraft because the do not corrode, are heat resistant, and

    lightweight

  • 47

    radar-absorbing materials’ at a given frequency depends on its thickness and

    composition

  • 48

    a dielectric radar-absorbing materials’ reformable is based on the type of dielectric material, electrical loading and

    thickness

  • 49

    hat type of sheet is an R-card

    resistive

  • 50

    the R-card is typically bonded to the radar-absorbing structure or embedded weiteren composite materials that are

    radar transparent

  • 51

    hat is the result a hot sealant mixture

    premature bond failure

  • 52

    what type of materials are used to provide a smooth transition between two surfaces that have a mismatched height

    fairing

  • 53

    when assessing LO material defects, you must accurately identify width, depth, heigh, length, orientatio, classification of damage and

    location

  • 54

    extreme heat expands the radar absorbing material, breaking down the adhesive bond and causes

    bobbles

  • 55

    corrosion is an serious problem for stealth aircraft because LO coatings

    can hide the initial stages

  • 56

    extensive repair is usually required on LO materials when corrosion becomes visibly evident by showing

    bubbles and disbonds

  • 57

    while using a pneumatic scraper to remove LO coatings, what type of trajectectory must you use to prevent delaminations in the composite structure

    low

  • 58

    when using a pneumatic scraper to remove LO coating around the edge of a panel, the direction you should scrape is from an

    interior point and work out toward the edge

  • 59

    what tool do you use t remove filler material from gaps and seams on LO aircfraft

    nonmetallic pick

  • 60

    in order to safeguard the sensitivity of the material when discarding excess RAM you may have to use disposal equipment such as industrial shredders, hand-held cutting devices and

    incinerators

  • 61

    the term that describes the systematic removal of LO coating in a way that ensures a smooth transition between layers is

    racetracking

  • 62

    transitioning between an original coating and new coating by overlapping alternating paints is called

    tie-in

  • 63

    you should incorporate larger that’s minimum dimensions during your removal layout to allow for

    sanding imperfections

  • 64

    sand a coating layer until the layer below is visible is called a burn

    throught

  • 65

    what can occur if the conductive elements of a coating are left exposed and unprotected for an extended period of time in a hot and humid enviroment

    oxidation

  • 66

    what determines the aircraft surface temp that must be maintained for specific material application

    manufacturer’s instruction

  • 67

    the solvent wipe cleaning step for composite materials to omitted

    when authorized by aircraft tech order

  • 68

    to ensure that flex primer will adhere to the surface of RAM scuff sand the surface of the RAM with

    medium-to-fine grade sandpaper

  • 69

    what material is used for its adhesion-improving and corrosion-inhibiting properties

    primer

  • 70

    the exterior finish of the aircraft minimizes the moisture intrusion and provides ultraviolet protection for

    resin and materials

  • 71

    e most effective roller covers for the application of primer are made form

    ultra high - density foam

  • 72

    when applying sheet-type RAM you must consider surface area, shape, available equipment and

    contour

  • 73

    when applying RAM with PSA you roll it down with a rubber-wheeled roller to

    remove air bobbles

  • 74

    how can you prevent moisture and condensation from degrading the performance of filler material that has been removed from cold storage

    allow the material to acclimate in the sealed manufacturer’s containers

  • 75

    zip cords are installed around panels some panels to aid in gap filler

    removal

  • 76

    the most effective way to apply primer to panels seams during small repairs is to use a/an

    fantail artist brush

  • 77

    when a repair requires uniform pressure across the bonded surface you will use a

    contact vacuum bag system

  • 78

    inspection without the aid of diagnostic equipment of the procedures being preformed is

    visual process verify

  • 79

    Echt iCal verify of aerodynamic smoothness can be accomplished through the use of feeler gauges, pit depth gauges and

    optical tools