We ran a cable to the vertical stabilizer point for a Jeanies'
Teenee, and friend Art crashed it.  The tail cone was damaged, and
Art was pi___d about loosing his plane.  Mark's right about the
rear spar attach.  Cable plan is good (IMHO).

Ron Freiberger
mailto: [email protected]

-----Original Message-----
From: [email protected] [mailto:[email protected]]On
Behalf Of Mark Langford
Sent: Wednesday, June 23, 2004 8:52 PM
To: KRnet
Subject: KR> seat belts and spar strength (dead horse alert!)

NetHeads,

There has been a lot of talk about seat belt brackets, bolt
diameters, etc
lately.  I just ordered my seat belts today from Hooker Harness,
and have
been forced to think about attachment in order to come up with the
proper
belt lengths.  The thing that concerns me most is the strength of
the aft
spar itself.  If you think about laying the thing out flat between
two
sawhorses with a 32" space between them, I'll bet a lot of you
would have
second thoughts about merely STANDING on the middle of it, much
less jumping
up and down on it.  I think the standard for seat belts is
something like
20g's, so if you weigh 200 pounds, and have a 200 pound passenger
with you
(half of both would be 200 at the center), imagine 4000 pounds out
there in
the middle of that spar (laid flat).  Do you think it would hold
it?  I'll
bet you big money it won't.

I stopped by my stress guy's office today, and talked him into
working out
the details for me (I'm more than just a little rusty).  We
assumed a 1" x
1" piece of spruce with 4000 pounds (pilot and passenger) of force
out in
the middle of that 32" span, neglecting the upper cap, and the
vertical
members and plywood connecting them to the "subject" lower cap
(somewhat
conservative).  The number we calculated was  192,000 psi applied
to that
spar cap's spruce material in a 20g crash.  The modulus of rupture
in static
bending is 9600 psi for aircraft grade spruce.  So my apprehension
of
walking on that spar would be justified.   Theoretically, 200
pounds would
break that 1x1, and that passes my "common sense" test.

Larry's idea of spanning the two caps with a bracket is a good
one, since it
calls both caps into play.  Using that bracket to span the caps,
and if
you're the optimistic type and assume that the shoulder belt and
lap belt
will play equal parts bearing the load, and you have no passenger,
then
there's only 25 pounds (200/8) acting out in the middle of each
cap, so the
spar would handle something closer to an 8g crash.  But I
seriously doubt
the shoulder belts do as much work as the lap belts do, so we're
probably
back to 6g's again, and that's with no passenger.

My point is that although bolt diameter and bracket material are
important
factors, you also need to make sure the spar itself can handle it.
Obviously the load of the seat belts needs to be shared with
something other
than the aft spar if you are preparing for a 20g crash.  The two
best ways I
can think of are a compression member connecting the main spar to
the aft
spar (connected to both caps of each), or a cable connected to
something
like the tailwheel block.  I know the cable thing will stir up the
usual
arguments, but I think that's exactly what I'm going to do...run
cables
from both center shoulder and center lap belt attachment points
back to the
something substantial in the tail (like the tailwheel block).

I know we've all heard of KR's torn to pieces in a crash, and the
guy walks
away with the rear spar belted to his butt, but those are not the
sort of
full frontal crash that this 20g standard is based on.  You say
you're not
going to worry about 20g frontal impacts because the chance of one
is
unlikely?  I don't blame you.  They are.  But then why worry about
bolt
diameter or brace strength for a 20g crash if the spar's not going
to take
it anyway?  And I'm not saying the cable strap is a 20g solution
either, but
that's what it'll take to make me comfortable, with minimal weight
gain.

Just thought I'd throw that out there.  There are lots of ways to
work this
problem, and you're welcome to work it the way you want to.  I
need to get
back to work if I'm going to fly to the Gathering.  I just wanted
to bring
it up...

Mark Langford, Huntsville, Alabama
N56ML "at" hiwaay.net
see KR2S project at http://home.hiwaay.net/~langford





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