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jay(at)horriblehyde.com Guest
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Posted: Tue Mar 30, 2010 4:05 am Post subject: Downed EAA Plane |
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An interesting thing about jamb-nuts; if we are thinking of the same thing
here. We call them 'half-nuts'; usually people place the full sized nut
under the half or jamb nut- I used to as well. However, the correct way is
to put the thin nut first - see
http://www.boltscience.com/pages/twonuts.htm
Jay
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longg(at)pjm.com Guest
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Posted: Tue Mar 30, 2010 6:00 am Post subject: Downed EAA Plane |
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Regardless of your ego, it's always good to read 43.13 part 1 & 2 when
building an airplane. It's written at a 9th grade level so little things
like that should not get by. They make a big deal on exposed threads for
studs, bolts etc. How many of you know the formula for how deep a stud
needs to be screwed in? It's so simple, if you can't see 2 threads, get
a longer bolt.
In areas where I can't frequently inspect potential loose nuts, I always
use Loctite and if I'm feeling particularly nervous I give the thread
and nut a thin coat of epoxy. There's lots of other neat stuff in the
43.13 like max number of washers, 3 and never use a jam nut more than
once - toss it.
It's your ass in the plane, so do it right.
Glenn
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jon(at)finleyweb.net Guest
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Posted: Tue Mar 30, 2010 6:25 am Post subject: Downed EAA Plane |
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Glenn,
Please explain the purpose of your "ego" comment.
Jon
DO NOT ARCHIVE
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longg(at)pjm.com Guest
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Posted: Tue Mar 30, 2010 6:54 am Post subject: Downed EAA Plane |
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Jon,
Ego may imply I know better than the book, or jeez, I'd have to walk all the way back to the shop for a longer bolt - I'll put it in on next time. Just like in flying, the macho attitude (John Kennedy) will get you into as much trouble as the resignation attitude. Build it and fly it by the book, then we have the right to complain to someone else.
Glenn
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rampil
Joined: 04 May 2007 Posts: 870
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Posted: Tue Mar 30, 2010 9:22 am Post subject: Re: Downed EAA Plane |
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Glenn,
Before you insult old ghosts, maybe you should read the 14 page
(if I recall correctly) NTSB report on John-Johns accident.
His flying endeavors were marked, in my opinion, by always trying
hard to do the right thing. I don't think he was cavalier or ego-driven
at all, just unlucky. He may not have had the aptitude for instrument
flight, but he tried hard, and attended the best IFR flight school in the
country at the time
http://ntsb.gov/ntsb/brief2.asp?ev_id=20001212X19354&ntsbno=NYC99MA178&akey=1
It was his sister-in-law's fault!
I am not now, nor have I ever been a fan of the Kennedy dynasty, tho
I did admire Jack and Bobby!
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_________________ Ira N224XS |
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longg(at)pjm.com Guest
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Posted: Tue Mar 30, 2010 10:40 am Post subject: Downed EAA Plane |
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You're joking right? His head was bigger than the airplane. That was his
MO. He was all about driving that thing out into the dark on his own. As
you may remember he turned down the offer of the CFI going along with
him.
What he did was let one small mistake build up into a giant one -
especially with family on board. Get-there-itis got him. If he had flown
by the book and did what he learned at the best IFR schools at first
entry into IMC or simply darkness he would have turned right around and
gone back inland.
He is now the butt of every CFI example of what happens to a pilot when
orientation is lost. Sure one can be unlucky, but I don't buy that in
his case.
I suppose we'll never really know.
Glenn
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simon(at)synchdes.com Guest
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Posted: Tue Mar 30, 2010 11:36 am Post subject: Downed EAA Plane |
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Glen and Ira,
What I've always wondered about with the fatal John-John flight was "why didn't he turn on the autopilot and let it fly him in IMC to his destination?" Didn't his Saratoga have autopilot? He must have been distracted by the two passengers on board, who had a lot to talk about. I've flown into dark areas before I had my instrument rating, and it scared the holy hel out of me-enough to fly back into VMC.
I've never been a fan of the Kennedy dynasty either. I have a t-shirt with a picture of Ted Kennedy and O.J. Simpson on it. Below it, it says "Vodka and OJ."
Simon Ramirez
Do Not Archive
On 3/30/2010 2:34 PM, longg(at)pjm.com (longg(at)pjm.com) wrote: [quote] [quote]--> AeroElectric-List message posted by: <longg(at)pjm.com> (longg(at)pjm.com) You're joking right? His head was bigger than the airplane. That was his MO. He was all about driving that thing out into the dark on his own. As you may remember he turned down the offer of the CFI going along with him. What he did was let one small mistake build up into a giant one - especially with family on board. Get-there-itis got him. If he had flown by the book and did what he learned at the best IFR schools at first entry into IMC or simply darkness he would have turned right around and gone back inland. He is now the butt of every CFI example of what happens to a pilot when orientation is lost. Sure one can be unlucky, but I don't buy that in his case. I suppose we'll never really know. Glenn --
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MauleDriver(at)nc.rr.com Guest
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Posted: Tue Mar 30, 2010 11:36 am Post subject: Downed EAA Plane |
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You must be joking. I've read the report and analysis of the report
several times. Lot's to learn there but I never got enough info to know
that his "head was bigger than the airplanes" or "that was his MO".
He screwed up and I've caught myself with a dismissive smile while
describing the incident to others. I'll try harder to check myself in
the future.
There but for the grace of whoever, goes I. Thinking I'll never be
subject to a simliar set of circumstances takes a pretty big head.
I agree, we'll never know,
Bill Watson
longg(at)pjm.com wrote:
[quote]
You're joking right? His head was bigger than the airplane. That was his
MO. He was all about driving that thing out into the dark on his own. As
you may remember he turned down the offer of the CFI going along with
him.
What he did was let one small mistake build up into a giant one -
especially with family on board. Get-there-itis got him. If he had flown
by the book and did what he learned at the best IFR schools at first
entry into IMC or simply darkness he would have turned right around and
gone back inland.
He is now the butt of every CFI example of what happens to a pilot when
orientation is lost. Sure one can be unlucky, but I don't buy that in
his case.
I suppose we'll never really know.
Glenn
--
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ceengland(at)bellsouth.ne Guest
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Posted: Tue Mar 30, 2010 12:23 pm Post subject: Downed EAA Plane |
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I'm no engineer, & don't even plan to stay in *any* motel at S&F, but it
will take more than a web site to convince me those instructions are
correct. If I'm following their instructions correctly, the preload on
the bolt will only be 25-50% of design (could easily wind up being even
less) & the only spot with 100% of the preload will be the threads
between the nuts.
The deal on that bridge will need to be a lot better to get my
attention.
Charlie
On 3/30/2010 7:01 AM, Jay Hyde wrote:
[quote]
An interesting thing about jamb-nuts; if we are thinking of the same thing
here. We call them 'half-nuts'; usually people place the full sized nut
under the half or jamb nut- I used to as well. However, the correct way is
to put the thin nut first - see
http://www.boltscience.com/pages/twonuts.htm
Jay
--
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nuckolls.bob(at)aeroelect Guest
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Posted: Tue Mar 30, 2010 1:16 pm Post subject: Downed EAA Plane |
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At 03:16 PM 3/30/2010, you wrote:
<ceengland(at)bellsouth.net>
I'm no engineer, & don't even plan to stay in *any* motel at S&F, but
it will take more than a web site to convince me those instructions
are correct. If I'm following their instructions correctly, the
preload on the bolt will only be 25-50% of design (could easily wind
up being even less) & the only spot with 100% of the preload will be
the threads between the nuts.
I read the article with interest and a sense
of mystery. Slicing and dicing distribution of
total loads between two nuts, one of which
ISN'T INTENDED TO BE STRUCTURAL gives one pause
to ponder.
Consider the host of anti-loosening technologies
including toothed lock washers, winged lock washers
keyed to a shaft and bent up to capture flats of the
installed nut, distorted diameters designed to
multiply friction between nut and bolt, locking
goos and gunks, plastic or fiber inserts on the
nuts or even the bolts, cotter keys through drilled
or castellated nuts, and finally the lowly hunk
of safety wire.
The laws of physics including a study of basic machines,
coefficients of friction and sliding forces tending
to move down an inclined plane will show that no
threaded fastener torqued to design values will rotate
on its mate unless for some reason tension on the
bolt is relaxed or strong but transient forces
vibrations) tend to overcome the breaking coefficient
of friction in the threads is overcome.
None of the cited prophylactics against inadvertent
loosening of a threaded couple take any part
whatsoever in the structural task assigned to
the threaded fasteners. Hence I find it curious
that one takes the time to put up such an explanation
about some seemingly critical function of jam nuts
on the structural integrity of the joint.
I've never seen a jamb nut installed anywhere
but on top of the nut it is intended to restrain.
Further, I'll bet that installation torque values
are a tiny fraction of that assigned to the
structural nut. This is because the friction forces normal
to the structural nut are being opposed by addition
of the jam nut. Depending on how much slop there
is in the threads, total release of tension on the
could result in total loss of "jamb" between the
two nuts.
As a class of anti-rotation device, I think the
jamb nut is the least capable of them all. I think
I'd consider all the alternatives before stacking
a jamb nut on top of a joint with any responsibility
for keeping the airplane and its accessories whole.
Bob . . .
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endspeed(at)yahoo.com Guest
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Posted: Tue Mar 30, 2010 4:36 pm Post subject: Downed EAA Plane |
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Boy oh boy,
You know, aside from the whole celebrity mirage our country seems to have either fallen in love with, or to resent, you can't lose sight of the fact these are just people. So now we have jousted with the ghosts of celebrity in John Jr's instance and one projected his belief's about him on to him, probably because of jealousy, plain and simple. I had a best friend in college who actually went on to have business dealings personally with JFK, Jr. He told me when I asked that JFK, Jr. was a really nice person as was Caroline. He told me their mom did a great job raising them after their dad was murdered. So, put your People Magazine away and realize a pilot, who was a great guy from my insider info, succumbed to the same errors many pilots have and learn from the facts. Enough said.
Bob Sultzbach
Sent from my iPhone
On Mar 31, 2010, at 1:22, "rampil" <ira.rampil(at)gmail.com> wrote:
Glenn,
Before you insult old ghosts, maybe you should read the 14 page
(if I recall correctly) NTSB report on John-Johns accident.
His flying endeavors were marked, in my opinion, by always trying
hard to do the right thing. I don't think he was cavalier or ego-driven
at all, just unlucky. He may not have had the aptitude for instrument
flight, but he tried hard, and attended the best IFR flight school in the
country at the time
http://ntsb.gov/ntsb/brief2.asp?ev_id 001212X19354&ntsbno=NYC99MA178&akey=1
It was his sister-in-law's fault!
I am not now, nor have I ever been a fan of the Kennedy dynasty, tho
I did admire Jack and Bobby!
--------
Ira N224XS
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=292377#292377
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pwmac(at)sisna.com Guest
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Posted: Tue Mar 30, 2010 4:37 pm Post subject: Downed EAA Plane |
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Bob,
You are correct. The application of a jam nut for locking is only applicable when one cannot wrench on the other end of the bolt. And never in a critical application. An example that comes to mind is a big relay where the bolt is molded into the plastic.
Its interesting that some tend to focus on how many threads are showing instead of "is the thing torqued with a locking feature nut". Mechanical locking nuts are favored (some call Pinch nuts). The castellated nut does not have my favor since the holes seldom meet my needs. Safe enough if torqued properly. The nylon nuts (called elastic stop nuts) are applicable for non critical places with no heat. Otherwise loctite in cool environs is also good and comes in several degrees of anti rotation sticky ness.
Paul
==========
At 02:15 PM 3/30/2010, Robert L. Nuckolls, III" wrote:
[quote]As a class of anti-rotation device, I think the
jamb nut is the least capable of them all. I think
I'd consider all the alternatives before stacking
a jamb nut on top of a joint with any responsibility
for keeping the airplane and its accessories whole.
Bob .[b]
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MauleDriver(at)nc.rr.com Guest
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Posted: Tue Mar 30, 2010 5:54 pm Post subject: Downed EAA Plane |
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I like the phrase, "aside from the whole celebrity mirage...". Nice.
Bill
Robert Sultzbach wrote:
Quote: |
Boy oh boy,
You know, aside from the whole celebrity mirage our country seems to have either fallen in love with, or to resent, you can't lose sight of the fact these are just people. So now we have jousted with the ghosts of celebrity in John Jr's instance and one projected his belief's about him on to him, probably because of jealousy, plain and simple. I had a best friend in college who actually went on to have business dealings personally with JFK, Jr. He told me when I asked that JFK, Jr. was a really nice person as was Caroline. He told me their mom did a great job raising them after their dad was murdered. So, put your People Magazine away and realize a pilot, who was a great guy from my insider info, succumbed to the same errors many pilots have and learn from the facts. Enough said.
Bob Sultzbach
do not archive
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user9253
Joined: 28 Mar 2008 Posts: 1927 Location: Riley TWP Michigan
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Posted: Wed Mar 31, 2010 4:22 am Post subject: Re: Downed EAA Plane |
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Quote: | The laws of physics including a study of basic machines, coefficients of friction and sliding forces tending to move down an inclined plane will show that no threaded fastener torqued to design values will rotate on its mate unless for some reason tension on the bolt is relaxed or strong but transient forces vibrations) tend to overcome the breaking coefficient of friction in the threads is overcome. |
I agree. The only advantage of using a jam nut that I see is that if the load on the bolt is relaxed, the two nuts will still be tight against each other. On non-aviation projects, I have used two nuts with a lock washer between them and never had them come loose.
Joe
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