3rd_quarter_07_Newsletter ELITE SDVCS Nuts And Bolts 07 02

User Manual: ELITE SDVCS

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The Southwest Region’s Airworthi-
ness FAASTeam would like to
thank you for taking a moment of
your time to read this newsletter.
The purpose of this newsletter is to
provide a means of sharing critical
safety information and items of
interest between the FAA Airwor-
thiness Safety Team and the avia-
tion industry’s Maintenance Tech-
nicians. Our goal is to provide you
with short articles that will help you
keep up with the rapidly changing
world of aviation maintenance, as
well as guidance on where to find
additional information when appli-
cable.
The newsletter will contain at least
one accident case study in each
edition that we hope will make you
think twice before you close that
panel during your next inspection.
We hope to provide you with arti-
cles that will be informative as well
as interesting.
In our “Ask The Feds” column,
you will be invited to ask ques-
tions about any issue or subject
that might be bothering you or
that you really just don’t quite
understand. We will do the
necessary research and share
the results with everyone in our
column.
Our column titled “Lucky’s
Corner” will contain an article
written by the one and only
Lucky Lougue from Air Sal-
vage of Dallas. (ASOD) If you
haven’t had the pleasure of
working with Lucky on an acci-
dent investigation, parts loca-
tion problem, or technical prob-
lem, then you’re in for a treat.
Lucky also conducts IA re-
newal seminars and is the “GO
TO GUY” for the FAA and the
NTSB.
The “Tech Forum” column will
contain little known interesting
technical tips and explanations
or advice concerning legal mat-
ters that we feel you should
know.
We hope to provide you with an
interesting read that might an-
swer some of those gray areas,
or provide a tune up on issues
you haven’t dealt with for a
while and occasionally, a ‘heads
up’ for what might be coming
down from the hill.
Remember, this is a newsletter
written by Mechanics for Me-
chanics.
Welcome To The SW Regions FAASTeam
Airworthiness Newsletter
Nuts And Bolts
Who Is The FAASTeam?
On October 1, 2006 the old
FAA Safety Program died and
the FAA Safety Team was
born. The FAASTeam is a
smaller group of hand picked
Safety Inspectors that have
been given the job of reducing
accidents by teaming up with
an elite group of FAASTeam
Representatives from the indus-
try. This is where you come in!
We hope to accomplish the
mission by using a comprehen-
sive data analysis system to
identify problem areas geo-
graphically and then use our
resources to correct those prob-
lems. Isn't that a refreshing
idea compared to the old shot-
gun approach? If you would
like to get involved, contact
your local FAASTeam Program
Manager. They are listed on
page 5.
FEDERAL AVIATION ADMINISTRATION
SAFETY TEAM
June 25, 2007
Issue: 1
If you are inter-
ested in safety
and would like to
help the
FAASTeam
spread the word
in your local
aviation culture,
we need to talk
to you. Contact
your local
FAASTeam Pro-
gram Manager.
See page 5.
Welcome 1
Who is the
FAASTeam ?
1
AMO’s Take Training
Seriously
2
Ask The Feds 2
Lucky’s Corner 3
Meet The Team 5
Tech Forum
5-6
Accident Case Study 4
Inside this issue:
AC 39-7C in paragraph 8. If
they had intended to give relief
to type certificated products
installed on experimental air-
craft it would have stated that
in the regulation. The 14 CFR
part 39 rule says in part, that
when an unsafe condition exists
in a product and is likely to
exist in other similar products,
an AD is issued. It’s all about
safety to the flying public. If
the FAA knows there is a safety
issue with a product, it is their
job by law to require people
that use that product to do
something to correct or mitigate
the unsafe condition. Big
brother has no control over
where that product gets used.
That’s why if that unsafe prod-
uct has an applicable AD note,
and it ends up on an experimen-
tal aircraft, in the interest of
safety to the public the AD
must be complied with.
If you read FAR part 39 again,
with an open mind this time,
you will notice that there are
no words like “except for prod-
ucts installed on aircraft that
have been issued an experimen-
tal airworthiness certificate”, or
any other language that gives
relief from an applicable air-
worthiness directive. This is
not an area that has received
much attention from the FAA
Inspector staff, but we expect it
may make it to the front lines
with the influx of light sport
aircraft many of which have
type certificated products in-
stalled.
I always say “nothing happens
until something happens”. Just
think what might happen if an
experimental aircraft augers in
with your name in the logs for
the last condition inspection,
and the investigation reveals
the engine quit due to non com-
pliance with an applicable AD.
That’s food for thought.
The Aviation Maintenance
Technician Awards Program
for calendar year 2006 (AC65-
25C) offers a Diamond Award
Certificate of Excellence to
those aviation companies who
lead the industry in a measur-
able commitment to training.
To qualify, a minimum of 50%
of eligible employees must be
recipients of individual FAA
training awards in any given
year.
Additionally, a company that
has received an AMT award for
100% of its eligible employees
will receive a Diamond Award
Special Recognition Plaque
from FAA headquarters. For
information on the 2007 awards
program, see AC 65-25D since
the qualifications have
changed.
The following is a list of those
elite companies that realize that
a well trained technician is an
asset that will return the cost of
training many times over. For
the award year 2006:
Diamond Award Special Rec-
ognition Plaque:
Raytheon Aircraft Svcs.-SAT
Air Logistics LLC - ARA
Diamond Award Certificate
of Excellence:
San Antonio Aerospace-SAT
Chromalloy – SAT
Marathon Oil Co.-HOU
Texas Aviation Services-
FTW
Aramco Associated Co.
IAH
Petrolium Helicopters - LFT
Aeroframe Svcs. - CWF
Tarrant Co. College - FTW
Bombardier Bus. Jet Solu-
tions - DAL
This question was submitted by
an A&P / IA from the DFW
Metroplex area that occasion-
ally does condition inspections
on Experimental aircraft. He
asks, “Do Airworthiness direc-
tives apply to engines or pro-
pellers installed on experimen-
tal amateur built aircraft?
ANSWER: Yes.
This has been a controversial
subject for years. People as-
sume that because part 43 does
not apply to experimental air-
craft that AD’s are not applica-
ble. Wrong, it starts in 14 CFR
part 91.403(a) which says in
part, the owner or operator
must maintain the aircraft in an
airworthy condition including
compliance with part 39. Then
we go to , 14 CFR Part 39
where the whole subject of
AD’s is covered, and there is
no relief given in the rule for
experimentally certificated
aircraft. This is also covered in
Ask The Feds
Aviation Maintenance Organizations In The Southwest Region
Take AMT Training Seriously
Nuts And Bolts ISSUE: 1
Do Airworthiness
Directives apply to
engines and
propellers installed
on experimental
amateur built
aircraft?
Page 2
EAA Southwest Fly In
Hondo, Texas June 1,
2007
AAR - Oklahoma City
GE On Wing Support - DAL
Gulfstream Aerospace - DAL
CBP/L-3 Comm./Vertex - HDC
Citation Svc. Center - SAT
Helicomb - TUL
Nordam Repair Div. - TUL
Aircraft And Turbine Support -
TUL
Page 3
IA Renewal
It’s Your Choice On How To Renew, So Make The Best Of It
The purpose of this article is to help clarify the renewal process for Inspection Authorizations. As with anything
there are pros and cons. Last March the FAA passed a change in the renewal process, we are no longer required to
renew our Inspection Authorizations every year. To save time and money as far as the FAA budget goes, IA’s will
renew their Inspection Authorizations every two years, on odd numbered years. This change blind sided most of us,
including me. Once announced, I got busy to find out what this really meant to me as an Inspection Authorization
holder. When I got through with the research, I was blown away by the fact that the only change would be that my Au-
thorization would be renewed every two years instead of every year. This part sounds good, but don’t get too excited
yet. There is more to the story! As far as the requirements for renewal each year, nothing has changed. Under section
65.93 (c) (1) (5), you still have to "Qualify" for "EACH" preceding 12 calendar month period to be eligible to renew
your Authorization at the two year interval. To “Qualify” everyone knows that you can renew strictly on activity, having
signed off on at least 4 Annuals each year, having signed off on 8 Major Repairs and/or Alterations, 1 Progressive In-
spection, attend an approved Renewal Course or everyone’s favorite, "The Delightful Oral with the FAA". If you didn’t
“Qualify” by March 31 of that calendar year, you would not be able to exercise the privilege of using your Inspection
Authorization after that date and would be in Violation of Far 65.93 if you did.
Remember what’s important here — to renew!!!! You must meet renewal requirements by the end of the Cal-
endar year "EACH YEAR" (March 31) or you blew it. So, when you take a good look at this "2 Year Renewal Thing”
nothing has changed as far as renewal requirements for us, other than submitting the paperwork and getting renewed
every Odd Numbered year. So, my suggestion to you is to act as if nothing has changed and continue to fill out your
Renewal paperwork (FAA form 8610-1, not required but I recommend it) with your activity documented and/or continue
to attend the approved courses and stash your paperwork in a safe place so you can have it readily available at re-
newal time. Remember, if you can’t find it or produce it at renewal time, you’ve got a Big Problem! For further informa-
tion on this refer to AMT Magazines April 2007 article by Bill O’Brien on page 24.
Now that we’ve gotten all that out of the way, let’s talk about the advantages and disadvantages of how you
renew. By renewing your Inspection Authorization by activity alone, I believe you will miss out on one very important
thing! Continuing Education. This shows us what is happening in the field and industry!!!! That is where the Approved
Renewal Seminars come into play! Most ask themselves, why should I pay money and spend a full 8 hour day sitting
in a classroom listening to people talk and lecture when I already qualify to renew by activity??? To that I answer- For
the knowledge and updating of what we have learned in the past year from our own mistakes and successes and that
of others, that’s why. The FAA Approved Seminars strive to keep you updated on upcoming changes. Changes that
have already taken place and are in effect, whether it is regulations, processes, Airworthiness Directives, Improper
Maintenance techniques, log book sign-offs, paperwork changes and what caused the most accidents last year. Re-
newal through Seminars shares with you All of the combined errors, misjudgments, proper uses that are shared by
your fellow IA's. Instead of just acquiring the knowledge you gained last year through qualified activity, you now can
acquire so much more from your fellow IA’s as discovered by them, Industry and the FAA. Let’s face it; "SAFETY" is
the key word and focus behind the Seminars. It is your decision on how to renew. Think about being in a seminar with
150 to 200 IA’s with individual experience levels ranging from being an IA for 1 year to 40 years. Just think of how
much combined experience that is in one room that you now have access to just by being there!!!! It’s your choice on
how to renew, so make the best of it.
Lucky Louque, Air Salvage of Dallas
Lucky’s Corner
Nuts And Bolts ISSUE: 1
For the purpose of this column
we change the names of any
person involved and do not
release aircraft registration
information.
You know this scenario— New
student pilot buys a Beech
Skipper without a pre-purchase
inspection, (gets a heck of a
deal), and hires a flight instruc-
tor to teach him to fly it. After
a couple of flights, the flight
instructor tells the new student/
owner that he believes there is
something wrong with the
power output of this aircraft.
They take the aircraft to … let’s
use Joe. Joe is a good A&P/IA
that the instructor has used
before. Joe inspects the engine
in his one man shop and deter-
mines that the camshaft in the
little O-235-L2C has worn
down lobes and needs replace-
ment for the engine to develop
rated power. The new owner
agrees and work begins. Dur-
ing the repair process, Joe dis-
covers that the oil pump AD
was applicable and had not
been complied with and that
one magneto was totally
trashed and needed to be re-
placed as well as a timing gear
and all lifters. The owner
agreed to the additional work
and the parts were ordered.
During the reassembly process
and while waiting on parts, Joe
stuffed the crankcase and other
openings with industrial paper
towels (shop towels) to keep
dirt and bugs out of the engine
and he goes on working on
other aircraft. Sounds pretty
normal so far.
The parts are received, most of
the paper towels (all but one)
are removed, and the engine is
reassembled. The engine is
serviced with the proper quan-
tity and grade of oil, test ran,
and checked for leaks. Nothing
abnormal noted and the mainte-
nance records receive an ap-
proval for return to service.
The owner is called and told the
aircraft is ready for delivery.
The flight instructor and a
friend, who was also a pilot,
show up and take delivery of
the aircraft for the owner. A
normal run up is accomplished,
followed by an uneventful take-
off. During level flight, the
pilot reported a loud metallic
sound and the propeller stopped
turning. The pilot initiated a
forced landing on a golf course.
During the roll out the aircraft
impacted trees and came to rest
upright. The two occupants
suffered only minor injuries.
The aircraft was determined by
the insurance company to be
totaled.
The post accident investigation
and engine teardown revealed
the following:
The #3 piston was not moving.
They were unable to remove
the #3 cylinder. After remov-
ing the #4 cylinder you could
see that the #3 connecting rod
cap was destroyed by heat and
the #3 crank journal was de-
stroyed by heat due to oil star-
vation.
Portions of an industrial paper
shop towel were discovered
throughout the crankcase. Re-
moval of the oil sump screen
showed it was completely
clogged with the same material.
The investigation led back to
Joe’s shop where matching
paper shop towels were discov-
ered. During the interview with
Joe, he admitted putting the
towels in the engine to keep out
dirt but thought he had gotten
them all out. Additionally,
there was no one available to
do a second inspection prior to
installing the cylinders.
This is clearly a case of ‘Failure
To Follow Procedures’. The
Lycoming direct drive overhaul
manual states in part “prior to
assembly all parts should be
cleaned to remove all traces of
preservative oil and any accu-
mulated foreign matter. I
think a shop towel qualifies as
foreign matter. You could also
call this a case of another FAA
favorite, ‘Failure to Properly
Inspect’. In either case, Joe
really messed up when he was
in fact trying to do a quality job
for his customer and be a re-
sponsible and professional me-
chanic. As a result of his inad-
vertent oversight, he destroyed
an aircraft, endangered the lives
of two airmen, and put a major
blemish on his record after
dealing with the FAA Inspec-
tor, and the aircraft owner is
still trying to get back the
money he paid for the work.
This case also smells like a
dose of “Human Factors”, an-
other FAA identified casual
factor in accidents. Perhaps Joe
was tired when he installed the
cylinders, maybe he was think-
ing about something else,
maybe there was poor lighting
in his shop, maybe the phone
was ringing off the wall and
distracting him, who knows.
We can all learn at Joe’s ex-
pense. If you work by yourself,
you might want to check your
work two or even three times
before closing.
Post Accident Engine Tear-
down Reveals
Paper Shop Towel in The
Crankcase
Accident Case Study — Failure To Follow
Procedures
Nuts And Bolts ISSUE: 1
The oil sump screen was
clogged with a shop towel.
Page 4
Experimental Special
Light Sport Aircraft
Page 5
The Southwest Region’s airworthiness FAASTeam is composed of four Program Managers. We are
located in Dallas, Oklahoma City, Baton Rough, and San Antonio. Each Program Manager is an A&P
Mechanic with IA, some are Parachute Riggers, Pilots and were DME’s, and we are all bi-lingual. We
speak FAA and Mechanic fluently. Except for Mr. Capone in Baton Rough, LA, he’s trilingual, he
speaks FAA, Mechanic, and a little Cajun. Please do not hesitate to contact us if you have a question
or an issue that you would like to discuss, or if you would like to join the FAASTeam as a Representa-
tive. Below is our contact information:
Brian Capone - Assistant Regional Manager -Baton Rough FSDO
Phone 225-932-5926 E-Mail - brian.t.capone@faa.gov
Mike Jordan - San Antonio FSDO
Phone 210-308-3312 E-Mail - michael.r.jordan@faa.gov
Barry Proctor - Dallas FSDO
Phone 214-902-1834 E-Mail - barry.g.proctor@faa.gov
Steve Keesey - Oklahoma City FSDO
Phone 405-951-4236 E-Mail - carl.s.keesey@faa.gov
Meet The Team
This article was contributed by Jim Sparks, (I’m not Kidding) an
avionics technician, a FAASTeam Representative, and a writer
for AMT magazine. Thank you Jim for the informative article.
All Aircraft Must Be Grounded!
No, the title is not a catch phrase from a Railroad Executive’s conference. In
fact, it has to do with grounding as used in an electrical sense. Although in
some cases an aircraft is grounded when it is on the ground but there are grounds
when this assumption is not grounded. Perhaps Merriam Webster can shed some
light on this dilemma:
Ground is obtained when an object makes an electrical connection with
the earth: Ground is also referred to when a large conducting body such
as the metal structure of an aircraft is used as a common return for an
electric circuit and has a zero (or near zero) electrical potential.
There are of course positives and negatives (please excuse the pun) when using
aircraft structure as part of electrical circuits. On the plus side, elimination of
significant amounts of wire can be realized as only one wire is needed to feed
power to specific components and the return path can be through the airframe.
The down side is that many airframes are manufactured using aluminum which
Tech Forum
Nuts And Bolts ISSUE: 1
Steve Keesey -
FAASTeam Program
Manager
Berry Proctor -
FAASTeam Program
Manager
Mike Jordan -
FAASTeam Program
Manager
Brian Capone-
FAASTeam Asst.
Regional Manager
is a good conductor of electrical current. Copper wires equipped with cadmium plated terminal ends are often
attached to this aluminum structure using steel hardware. Just add water! Galvanic action occurs resulting in
corrosion.
Not only does corrosion pose a structural threat but it can impact the proper operation of electrical circuits. In
the world of glass cockpits where milliamp current flows are normal, milliohms of resistance can cause some
of the strangest electrical and avionic problems. Corroded grounds can also hamper operations in high current
draw systems as well. One of the leading causes of generator parallel problems is related to deteriorating elec-
trical connections resulting from exposure. In fact in some situations this can become a serious safety concern
as high resistance in an electrical circuit utilizing high current draw will result in heat being produced at the
corroded junction. In severe situations electrical arcing can result which produces a fire hazard.
Electrical bonding is another topic associated with grounds and requires as much awareness as the corrosion
issue. As the aircraft moves through the air there is constant contact with air molecules. This contact results
in an electron transfer from the air to the aircraft. In the event the aircraft does not have the ability to dis-
charge the excess electrons all or part of the aircraft will begin to build a significant electrical potential.
Once the charge is strong enough, an uncontrolled discharge will result and can cause radio interference as
well as cause physical damage to aircraft components.
Most airframe manufacturers will map the aircraft surfaces and design a route where static discharge can be
safely managed. This involves the use of bonding surfaces using a variety of methods including straps, wires,
enhanced electrical contact points and static dischargers. In addition, manufacturers generally build into their
maintenance programs a means of testing airframe electrical continuity as well as static discharge capabilities.
Care should always be taken when applying any product to an aircraft exterior. Certain commercial polishes
may not be electrostatic friendly and when applied to an otherwise well bonded aircraft will cause electrostatic
buildup and subsequent radio problems.
In addition to manufacturer’s recommended bonding checks, planning to have a periodic “Corona Discharge”
test accomplished will often pinpoint hard to find problem areas.
This process involves electrically grounding the aircraft and then bringing a wand that is charged to a very
high voltage within a close proximity of all exposed external surfaces. By monitoring the inductive discharge
rate a very accurate determination can be made as to what panels are conducting and which are not. Corona
discharge equipment cost upwards of $15,000 and is frequently owned by Maintenance and Repair Organiza-
tions (MRO). Testing on most general aviation aircraft can be accomplished within a short time and for a
nominal cost.
Who knows, perhaps the MRO will even have ground coffee without grounds that is provided by a well
grounded ground crew who have the grounds to get your aircraft off the ground.
Do you need to find or get information about any FAA office?
(click on the link below)
http://www.faa.gov/about/office_org
EAA Southwest Fly In
Hondo, Texas June 1,
2007

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