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