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Equipment Reliability
Institute
ERI News - your reliability newsletter
August 2003 - volume
12
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Hello,
everyone!
This issue starts off with some ideas by Rob
Poltz concerning saving money, a subject which should interest
everyone. By expending effort "up front" you save many
times more money in future years. Rob will expound on his ideas
September 15-17 here at Santa Barbara.
Are you feeling hot, humid and dusty this August?
You're uncomfortable, but probably not in danger; Dave
Douthit details the dangers being experienced by your newest
printed circuit cards.
Bob Renz of General Dynamics
- Advanced Information Systems at Bloomington, Minnesota, offers
some practical suggestions to those who operate electrodynamic shakers.
He also comments on Wayne's answer (last issue) to a reader-asked
question on accelerometers.
Please, readers, ask questions. You can e-mail
us or you can also visit our message boards at ERI
website or at vibrationandshock.com.
Best wishes,
Wayne Tustin
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What is
the Cost of Unreliability?
by Robert Poltz
As consumers, we purchase products, expecting
that they will work correctly the first time we try them and every
time thereafter. But we are sometimes disappointed. Fortunately,
however, the product usually comes with a warranty and we return
it to the place of purchase for a refund or credit. This scenario
works nine times out of ten, on average. If not, we usually chalk
the purchase up to experience and never go back to that manufacturer
again.
But, what if you are that manufacturer, trying
to sell good, reliable products to the public? Companies that pay
attention to Reliability and Quality succeed. Those that don't,
fail. It is as simple as that.
In electronics, Hewlett Packard, Sony and Pioneer
come to mind. Each name engenders immediate association with quality
and reliability of their products. Consumers return to the brand
name for subsequent purchases because they trust these companies
to produce the best bang for their buck.
In automobiles, we have BMW and Daimler-Chrysler
(Mercedes-Benz) identified as tops in their respective fields because
of high reliability and quality standards of excellence.
These are brands I trust and have used for
twenty years. In all likelihood, I'll purchase another of their
products in the near future. Your experience with other manufacturers
may differ from mine, but my point is that consumer loyalty is based
upon trust in products. Reliability of design is essential to creating
such consumer confidence. Quality is the implementation of that
design in manufacturing and delivery to the consumer.
Barringer [1] writes that "the
cost of improvement efforts are more productive when motivated from
the top-down rather than the bottom-up, because it is a top management-driven
effort for improving costs." Management steers the company,
and top management are at the helm. Decisions flow downward to supporting
organizations within the corporate structure to implement these
ideas.
Cost of unreliability programs are the spearhead
for reliability improvement. Appropriate questions are:
- Where within the organizational structure
is the cost problem(s) located?
- What magnitude is the problem(s), are all
business units affected, how can the problem areas be contained?
- What are the principal causes of these
problems, funding cutbacks, labor shortages, scheduling, transportation?
A useful management tool for predicting product
success/failure) is the Life Cycle Costing Model, LCC. Each of the
aforementioned areas is an integral part of the various models.
Dhillon and Reiche [2] co-authored a book entitled Reliability
and Maintainability Management and in chapter 13, "Life
Cycle Costing and Warranties" they discuss the need and uses
of LCC.
Life Cycle Cost enables management to:
- choose between competing manufacturers,
products and services
- compare costs of alternative approaches
to meet a specific need
- make equipment replacement decisions
- stimulate orderly planning and scheduling
- gain control over ongoing program costs
The general mathematical model for LCC is:
LCC = kD + kRD + kOS +
kP
KD is the cost of disposal
KRD is the cost of research and development
KOS is the cost of operation and support
KP is the cost of production
Within the context of Reliability, all these
are of great interest throughout the life of the product or system.
Each element plays a significant part in the design for reliability
equations from Infant Mortality, Useful Life and Wearout of the
product.
Systems Effectiveness is an index of value
used to evaluate product/system designs as a measure of desirability
to create satisfaction divided by the price of the item (Ireson
1996). Systems Effectiveness uses the LCC as the quantity of price
and uses effectiveness as the quantity measure of results received.
The "Effectiveness equation, therefore,
is the product of the chance that equipment or systems will be available
to perform its duty, it will operate for a given time without failure,
it is repaired without excessive loss maintenance time and it can
perform its intended production activity according to the standard."[3]
As related to engineering, each element of
the effectiveness equation is premised on data that varies by product
and specifies a probability of success between 0 and 1.
Within the RAMS disciplines there are Availability,
which deals with whether an item is up and running and available
for service. Reliability, which deals with whether an item
fails over a time interval and predicts the odds of failure vs success.
And then there is Maintainability, which concerns itself
with the duration of maintenance activity that will restore an item
to service. Often overlooked is Capability, which deals with
productive output of a product or system, or how well it performs
compared to some specification.
In summary, one must look at all aspects of
all factors contributing to the success/failure of a product. Try
to develop a global perspective of events within your organization,
identify potential weaknesses in structure and plan for success
by using forecasting models. Invite a Reliability expert to provide
quantification data for these models through detailed systems analyses.
These
topics are the subjects of my upcoming seminar/workshop, September
15-17, 2003, in Santa Barbara. For more information or registration,
click
here.
Bibliography
[1] Barringer, "Cost of Unreliability"
http://www.barringer1.com/cour.htm
[2] Dhillon and Reiche, "Reliability and Maintainability Management",
Van Nostrand Reinhold, 1985.
[3] Barringer, "Life Cycle Costs & Reliability for Process
Equipment", 1996.
Robert Poltz is Reliability Consultant,
President and CEO of Design
Analytx International, worldwide leader in reliability of design
analyses of high tech systems. For more information about Robert
or to contact him, click
here.
(back to the top)
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The True
Cost of COTS
The sure sign of momentum is when a movement
acquires its own acronym. The current enthusiasm for commercial
off the shelf technology is known as COTS, and one avionics expert
suggests it may be prudent to rein in the present enthusiasm.
In the rush from shelf to application, David
Douthit cautions, "It is impossible to produce a high-reliability
product without accurate and thorough environmental testing."
In this respect Douthit, owner/manager of
a Mesa, Arizona-based avionics reliability consulting firm, LoCan,
LLC, seems to be recalling the dictum of 19th century British prime
minister Benjamin Disraeli to "make haste slowly." Or,
rather, temper the enthusiasm with testing.
It may be useful to highlight certain trends,
by way of establishing the basis for Douthit's concerns. For one
thing, the military market for electronics is shrinking and military
specifications for reliability of components no longer apply. An
entire infrastructure that once guided component reliability for
both military and commercial application has dried up like a hail
pellet on a slab of sun-baked asphalt.
Ever thinner, ever more vulnerable
For another, airplanes and other military vehicles are being outfitted
with electronics and wiring that may degrade during service. Printed
circuit boards come to mind as one primary example. To be sure,
they pack performance into a small space, but how is it done? The
circuits are layered on top of one another, 25 or more in a board
just slightly thicker than a tenth of an inch. As Douthit pointed
out, "This overall reduction in spacing and thickness, combined
with the increased density of the circuits, increases the sensitivity
of printed circuit assemblies to moisture and ionic contamination."
Ionic contamination is the process of metal erosion when electrically
charged microscopic particles are deposited on the metal's surface.
Integrated circuits, once packaged in ceramic,
are now more often encased in polymer resins, giving rise to another
acronym, PEMs, for plastic encapsulated microcircuits. Unlike rock-hard
ceramic, these materials are vulnerable to penetration by contaminants
and, worse, by moisture.
Coatings, designed in part to prevent penetration,
introduce another variable. More than 400 different materials are
now being used as coatings. There is a huge variation in their coefficients
of thermal expansion. If not accounted for, electrical components
can become detached or damaged, especially if coatings with higher
thermal expansion characteristics are used in areas of the vehicle
likely to experience significant shifts in temperature.
The dust devil
When packing density goes up, so does the circuitry's potential
to generate heat. Designers have resorted to forced-air cooling
to carry away the heat. As in all things, there are side effects.
Douthit maintains that too little attention has been devoted to
airflow patters inside the boxes housing these components. Venturi
effects, he maintains, can cause very high rates of airflow. More
is not necessarily better. The higher airflow can increase up to
a hundredfold the rate at which dust is deposited on delicate components.
Not only is the dust a fire hazard, it can conduct electricity,
leading to intermittent short circuits and computer failures.
Industry experts now recognize a finer grain
of dust, made possible by improvements in measuring technology.
Once measured in the range of .01 to 2 microns, a new "ultra
fine" class involves particles ranging from .002 to .01 microns
- extending the scale of smallness by a factor of five.
Thin circuits under thin coatings, blanketed
by thin layers of contaminating dust - these are just three factors
affecting reliability of printed circuit boards.
Wiring has its own trilogy of threats. Douthit
points out that thinner insulation has been used to save weight
on wiring. Again, for every benefit there is a countervailing problem.
Aromatic polyimide insulation is weakened by water. The water removed
during the manufacturing process makes this type of insulation a
sponge when exposed to high humidity and water condensation in service.
With thinner insulation of any type, more care must be paid to preventing
dents, crimps, nicks, gouges, sharp bends and pressure points, which
can break already thin insulation.
Crimp-type wire connectors pose another problem.
Although protective coatings are often used, crimped connections
can become casualties of corrosion. Even "gold to gold"
contacts are not immune, Douthit claims. "Gold plated contacts
usually have a layer of nickel under the gold. If the gold is worn
and the nickel is exposed, oxidation will cause serious intermittent
problems," Douthit maintains. Single sided crimp connections
are best soldered, whenever practical, to provide the strongest
barrier against breach, he suggests.
As it all of this weren't enough, these problems
are exacerbated in harsh environments. Indeed, SWAMP is the telling
acronym for severe weather and moisture prone areas of the aircraft
deemed the greatest threat to the safe functioning of electronics
- the leading and trailing edges of the wings, landing gear wells,
and the juncture of wings to fuselage.
Corrosive cocktail
These areas mark the front lines of exposure. Remove inert nitrogen,
which constitutes 80 percent of the atmosphere, and what remains
is a corrosive cocktail of oxygen, moisture and contaminants. At
atmospheric pressure, a downpour of this cocktail's molecules (400
x 1014 to be more exact, or 400 followed by 14 zeroes) will strike
a square centimeter (0.4 square inches) every second, Douthit calculates.
In a typical urban environment, the constituent compounds include
chlorine, iodine, trace metals, sulfuric acid, nitric acid, hydrochloric
acid, sulfates, nitrates and, in coastal areas, airborne sea salt.
Up to 50 percent of the summertime haze, often found in the skies
over the northeastern United States, is a combination of sulfuric
and nitric acids.
Moisture is a superb solvent and catalyst,
abetting the penetration of corrosive compounds through a coating
as far as the metal surface. The higher the humidity, the worse.
At 60 percent relative humidity, the moisture forming on the surface
of an electrical component may be only 2-4 molecules thick, but
at 80 percent humidity, the layer may be 5-20 molecules thick. At
or above a thickness of five molecules, the moisture layer is the
same chemically as bulk water. In some situations, a thicker layer
can facilitate more energetic chemical reactions. "Microscopic
points of attack will have already been started because many of
the particles carry water with them when they are deposited,"
Douthit observed.
These dour details all feed into the COTS
conundrum. "The primary issue is what is a harsh environment?"
Douthit said. Traditionally, three minimum conditions have applied:
- A relative humidity of 60 percent or higher,
- A temperature above 0º C (32º
F), and,
- A deposit rate of contaminants on the circuitry
surface exceeding 1.5 micrograms of salt, or its chemical equivalent,
per square centimeter during the expected lifetime of the product.
Of these criteria the last is the least certain,
because circuits of newer designs may be more subject to contamination.
Some new densely packed circuits feature a salt contamination limit
of 0.2 micrograms or less, roughly a sevenfold reduction in the
traditional limit. To Douthit, the wider application of inadequately
tested COTS technology represents a journey into unknown territory.
"The result is an increasing amount of intermittent failures,
which cannot be verified or confirmed as equipment ages."
The COTS conundrum
Result? The illusory cost savings associated with COTS technology
tends to be offset over time by the increased cost of trouble shooting
and maintenance.
Indeed, support for Douthit's concern comes
from two sources. Earlier this year, operators were warned that
epoxy molding compound containing phosphorous has led to instances
of internal electrical shorting. The May 2002 ADVISORY, published
by the Computer Aided Life Cycle Engineering (CALCE) office at the
University of Maryland, cautioned that phosphorous' affinity for
water led to "phosphorous particles bridging wire bonds,"
making it a "failure accelerator."
It seemed that the standard mesh size worked
for bromide, but not for phosphorous when the manufacturer switched
to its use as a substitute fire retardant. Since then, a finer mesh
has been used to sieve the material, but bromide-braced components
out in the system have demonstrated failures within 6 to 12 months
of operation.
This case illustrates that process control
tests used in production are not the same thing as reliability tests.
The second source of support for concern about
COTS comes from the Federal Aviation Administration (FAA). Its August
2001 review of COTS electronics in airborne systems, presented three
important points. The first is that building high reliability systems
using COTS can be more expensive than utilizing hardened hardware
built to military specifications. Second, the introduction of new
materials poses new reliability risks. The compatibility matrix
is approaching infinity.
Third, reliability research is much more fragmented
in the commercial sector than in the military community, and much
of the limited information that does exist is considered proprietary.
What is to be done? Douthit has a couple of
suggestions. More research on COTS component reliability under field
conditions is needed, he maintained. Of greater importance, he says,
"A new paradigm will be required."
"A central agency, such as the FAA, must
step up to provide the industry with a centralized source of information
on COTS components." Rubber-stamping of military standards
"tweaked" for commercial application represents not only
an "enormous conflict of interest" but also presents a
"major potential for disaster," Douthit asserted.
"Until proper test equipment and protocols
are developed, there is a huge 'black hole' in avionics reliability,"
he maintains.
A sobering statement in the FAA's report of
the enthusiasm for COTS buttresses Douthit's concern: "Commercial
market trends are rapidly diverging from the needs of safety critical
airborne systems."
The lesson du jour: when a cost saving looks
too good to be true, it probably is.
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Test Lab Musings
(part 1)
by Robert L. Renz
Vibration
and shock levels always seem to be increasing, so your shaker will
always be on the edge of its capacity. Be careful when designing
a fixture to watch its weight - paying the extra for magnesium up
front might make the difference between being able to run a profile,
or having to go to an outside lab.
There
is nothing as eternal as a test lab. We never really abandon anything,
we just move it to a different shelf. The old tape cassette deck
that we used to drive the shaker is kept on a shelf just in case
we ever need it again... The manual equalization panel that goes
back forever? On a shelf, right behind the antique spectrum analyzer
and right next to the boxes of new 5 1/4 floppy disks. Naturally,
the cassette tapes, the connecting cables, and the instruction manuals
were thrown out years ago. The new equipment goes on the most accessible
(and visible) shelves while the older equipment gradually crawls
deeper and deeper into the depths and shadows of the lab.
And
why is it that no one has ever standardized on the size for hardened
washers for the fixture bolts? Over the years, I've run into 3/8"
washers with OD's from 1/2" to 7/8", and thicknesses from
1/16" - 1/4". As challenging as this makes it when you
are trying to bolt down a fixture, it's even worse when you need
to use a fixture that turns out to be counterbored for a 1/2"
OD washer - and you can't find enough of them..... At that point,
I run the fixture to the machine shop and have them re-counterbored
to 7/8". Instead of having the machine shop make washers from
solid bar stock, I buy hardened washers off-the-shelf from a machine
tool supplies dealer at a cost of only about 50 cents each. Likewise
for bolts - Buy 'em by the box, and don't be afraid to throw them
away when they start to get beat up. And while we're at it, standardize
on one diameter bolt whenever possible, such as 3/8". And also,
limit yourself to either fine or coarse threads- one or the other.
Wait until you have both fine and coarse threads in your lab, and
you're trying to set up for a test....
Many
labs use a battery-operated drill to run down / spin out fixture
attachment bolts, usually with a kluged adapter to adapt it all
to a hex wrench with a long enough drive to reach down into the
fixtures. Instead of using this pile of adapters, extensions, and
sockets held together with duct tape, it's a lot easier to use a
12" (or longer) hex wrench chucked directly up in the drill.
Can't find long wrenches? Check the Bondhus catalog or on line at
www.bondhus.com - they are in there (1/4 x 12" Balldriver Blades
are part number 3612, 5/16 x 12" Balldriver Blades are part
number 3613, 1/4 x 36" hex stock is part number 191912, and
5/16 x 36" hex stock is part number 191913). Your regular Bondhus
distributor can order them for you.
Rober L. Renz of General Dynamics - Advanced Information
Systems at Bloomington, Minnesota.
(back to the top)
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Questions
our readers have asked...
This section of our newsletter was created
for you, reader! Feel free to send questions or suggestions to the
webmaster.
One of our specialists will respond.
In our last issue, Wayne responded to the question
"How many accelerometers do I need?". Robert L. Renz wrote
back and would like to share his comments with us:
"Hello, Wayne.
As you said, the total can reach 12 very quickly.
In addition, though, we also have to consider
what type of test it is.
Are we evaluating a satellite module that will be very hard to get
to
after it is launched, or are we looking at an engineering prototype
that
will be back and forth to the vibe lab for many months? Is it in
our own
lab and under our control, or is it at an outside lab? Is the UUT
a
complicated unit, or is it a monolithic shape?
In some cases, our customer tells us what they
want to measure, which
simplifies the whole matter a lot. I always make sure that I have
extra
accelerometers & cables available in case one dies in mid test,
especially if the customer wants to witness the test.
If, however, you are instrumenting a MIL-STD-901
heavy shock test for
COTS equipment, you will discover that you need N+1 accelerometers,
where N is the number you have installed... The problem is that
every
accelerometer channel usually costs about $ 1000 per shot, so you
are
caught in the middle between engineering and the money people. I
usually
plan on about 12 accelerometers per shot, and try to get some of
them
positioned near the COTS equipment within the cabinet. Otherwise,
when
the COTS equipment goes obsolete and has to be replaced by something
else, you will have some idea what shock / vibe levels that the
replacement will have to handle. Remember, in a barge shot you will
have
the shock wave hitting the barge at angles approaching 45 degrees
vertically, so you will have to monitor side-side motion as well
as
up-down motion, which eats up a few more accelerometers."
Rober L. Renz of General Dynamics - Advanced
Information Systems at Bloomington, Minnesota.
(back to the top)
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Wayne's
new vibration and shock text |
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My new text is titled "Random Vibration and Shock Testing,
HALT, ESS and HASS". We're describing it as "A minimal-mathematics
introduction to the fundamentals of Random Vibration and Shock Testing,
HALT, ESS and HASS also Measurements, Analysis and Calibration,
with applications in the fields of aeronautical, automotive, seismic
and shipboard design and production". It is shown here, alongside
my 1984 text "Random Vibration in Perspective", which is updated
and greatly expanded.

Click
on the image to enlarge
The book will be approximately
300+ pages, letter size, hard cover and in color. It will include
a CD-ROM, which carries a number of video clips and animations that
illustrate vibratory and shock motion. One of my favorites shows
the highly repetitive motions inside an automobile engine. Another
shows cantilever beams responding to random vibration.
Prepublication
Sale
You can order the book for only $150 if your funds reach us by December
1, 2003. And we'll pay the shipping. After that the price
will be $250.00 + shipping.. We expect to ship by February 1, 2004.
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Reference edition of 1001 CD Program
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Many of our readers are aware of ERI's 1001 Distance Learning Program
in vibration and shock technology. The participant receives a CD-ROM
that has some 3000 PowerPoint® slides in 31 lessons. At the
end of each lesson, the participant keys in answers to problems
and questions in the lesson "review", then attaches his
work to an e-mail to his "remote professor", Wayne Tustin. Wayne
personally reviews each lesson, sometimes asking the participant
for additional work. Eventually the participant receives his/her
Certificate of Completion. Details may be found at our website.
A few people
have told us "I don't want to perform 31 lessons and I don't need
your Certificate. How can I have the CD only?" Now you can purchase
the "Reference Edition" CD. Click
here to order one.
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| Change
notice 3 to MIL-STD 810 F |
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If your work involves environmental testing, whether for military
or for commercial applications, whether inside the USA or abroad,
you probably are aware of Military Standard 810, Military Standard
Environmental Test Methods for Aerospace and Ground Equipment.
Commonly identified as MIL-STD-810, (USAF), 810 was initially published
in June 1962.
Why commercial interest in 810? Largely because commercial interests
have few other sources for environmental test guidance. Many are
unwilling to spend the necessary money and effort to acquire their
own data on in-the-field usage, on transport and storage.
We urge you to visit the Developmental
Test Command website and possibly to download the Standard.
There is also a link to "The Evolution of USAF Environmental Testing"
by V. J. Junker, dating back to October 1965. This historic document
reaches even further back to the first Army Air Force specification
410656 dated 7 December 1945.
In the years since 1962, as 810 evolved, changes were made to the
document. When sufficient changes had accumulated, a new version
was published as 810A, 810B, etc. The current F version appeared
1 January 2000. Then Change Notice 1 appeared 1 November 2000, followed
by Change Notice 2 on 30 August 2002 and now by Change Notice 3
on 5 May 2003.
You may wish to read "MIL-STD-810F - its evolution and future"
by Herbert W. Egbert, formerly at Aberdeen Proving Ground, Maryland,
in TEST
Engineering & Management magazine, December/January 1999-2000.
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Vibration and Shock in Switzerland
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"Vibration and shock training surrounded by the Alps" is one way
to describe Markus Dumelin's event at Thun, Switzerland October
14-16. Details can be found here.
On the same dates, Wayne will offer similar
training at Newport, Rhode Island. Details can be found on our websites.
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| Vibration
and Shock courses coming up |
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Wayne Tustin will teach short courses in vibration testing, shock
testing, measurement, analysis, calibration, HALT, ESS and HASS
at the following locations:
Seattle,
Washington, August 12-14, 2003
Santa
Barbara, California, August 26-28, 2003
Detroit,
Michigan
October 8-10, 2003
Newport,
Rhode Island
October 14-16, 2003
Palatine,
Illinois
November 5-7, 2003
Chatsworth
(LA), CA November 19-21, 2003
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Announcements |
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AST Meeting
Where will you be the week of October 20-24? If you're interested
in Accelerated Stress Testing, click
here for details of this Seattle meeting.
Shock and Vibration Symposium
On October 27-31 the 74th annual Shock and Vibration Symposium will
meet in San Diego. Click
here for details. Wayne is to tutor on fixture design, fabrication
and usage.
Reliability Symposium
The CRMS Reliability Symposium will meet October 2003, in Ottawa,
Canada. Click
here to visit their website and get more information.
Acoustics Consultant Wanted
We'd like to hear from an acoustics consultant who is willing to
travel and to teach short courses to groups of engineers and consultants,
possibly in non-industrialized countries.
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Contact information |
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ERI - Equipment Reliability Institute
1520 Santa Rosa Ave.
Santa Barbara - CA - 93109
Tel: (805) 564-1260
Our
fax number:
(805) 966-7875
Wayne Tustin tustin@equipment-
reliability.com
Webmaster webmaster@equipment
- reliability.com
Websites
http://www.equipment-
reliability.com
http://vibrationand
shock.com
Copyright © 2000-2003 Equipment Reliability Institute.
All rights reserved.
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