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Nose gear bungees

 
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grs-pms(at)comcast.net
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PostPosted: Sun Oct 08, 2006 12:04 pm    Post subject: Nose gear bungees Reply with quote

Could the deterioration of the nose gear bungees be related to heat under the cowl? Particularly in installations where the muffler is close to the bottom of the bungee? Anyone try to shield the bungee from radiated heat?

George

Do not archive

[quote][b]


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mfothergill(at)sympatico.
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PostPosted: Sun Oct 08, 2006 2:42 pm    Post subject: Nose gear bungees Reply with quote

Hi;
The nose gear is subject to wear due to rotation for steering, both in
the air and on the ground. It is also bounced more. Make sure that you
smooth out the welds where the bungee passes around the 3/4" tubes.
Mike
UHS Spinners

George Swinford wrote:
Quote:
Could the deterioration of the nose gear bungees be related to heat
under the cowl? Particularly in installations where the muffler is
close to the bottom of the bungee? Anyone try to shield the bungee from
radiated heat?

George

Do not archive







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peterd(at)metec.co.nz
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PostPosted: Sun Oct 08, 2006 5:46 pm    Post subject: Nose gear bungees Reply with quote

Hi George,
I did make up a heat shield (see attached image) to deal with the issue of radiated and circulated heat after engine shut-down. FWIW, I have yet to prove any benefit, but it was simple to do at the time.

Tail winds

Peter Dunning
CH601HD/6-3884/912S
[quote] ---


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xl(at)prosody.org
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PostPosted: Sun Oct 08, 2006 10:02 pm    Post subject: Nose gear bungees Reply with quote

I just replaced my nose gear bungee at 400 hours.
The outer cover was frayed and some of the rubber
bands were cut. I ordered the new 1080 bungee from
Zenith. It wasn't clear to me which one to order from
Aircraft Spruce, so I went with the 'safe one'.
The new bungee must be about 1" longer because now
I have about a 1/2" gap at the top of the steel plate.
I had no gap before the replacement. The bungee is
about the same diameter and it works so I'll go with it.

I have no heat shield and the old bungee did not look
like it was affected adversely by the engine + exhaust heat.

I tried the bungee replacement tool sold by Travis, of
Kobush Welding and Machining, LLC. It did not work for
me. It could not get a grip under the bungee and it did damage
the old bungee when I tried to use the tool to remove the
bungee. I was reluctant to use it to install the new bungee.
I found that I didn't need it anyway. And the instructions
were poor. For example, no mention of having to remove the gear
to drop it enough to remove the old bungee. Yes, that is obvious,
so why isn't it in the instructions?? I sent an email to
Travus a week ago telling him that the tool did not work for
me and asking him if I could return it. I did not get a reply
yet.....

To get the front gear back in place I used a rachet strap
around the front gear and the main gear. I let gravity
do the work of compressing the bungee.

BTW, I use two 60 pound sand bags on the elevator to lift
the nose when I need to work on the front gear.
These are the same sand bags I used to put 240 pounds in
the passenger seat for gross weight flight testing.
The couple of dollars/bag weren't wasted.

Joe E
N633Z (at) BFI
CH601XL, 400 hours (677 hours to go before flight time = build time)
Jabiru 3300, Sensenich 49x64 wood prop


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klaus(at)utdallas.edu
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PostPosted: Mon Oct 09, 2006 10:56 am    Post subject: Nose gear bungees Reply with quote

Hi,

The nose gear bungees seem to fail because of the small diameter of the
four tubes where the bungee makes an almost-180 deg turn. In my case, the
muffler is in the area of the bungee, but twice the failure came from
fraying
at one of the tubes. A simple fix of the small-diameter problem does not
seem possible, and replacing the bungee every 500 hours may be the
most convenient solution.

The use of sandbags on the horizontal stabilizer to lift the nose gear
is not
such a good idea. One might argue that this okay since the horizontal
stabilizer/elevator must lift the nose gear on takeoff. But
when the plane rotates on takeoff, the wings already
carry almost all of the weight of
the airplane. Thus, the horizontal stabilizer/elevator force
needed for rotation on takeoff is much, much
smaller than the force needed to lift the nose gear while parked.
Cessna some years ago had failures of the horizontal stabilizer
spar of the 152 because people would push down on the elevevator to lift
the nose gear when parking the plane in a tight spot.

Best wishes,

Klaus Truemper

--
Klaus Truemper
Professor Emeritus of Computer Science
University of Texas at Dallas
Erik Jonsson School of Engineering and
Computer Science EC31
P.O. Box 830688
Richardson, TX 75083-0688
(972) 883-2712
klaus(at)utdallas.edu
www.utdallas.edu/~klaus


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xl(at)prosody.org
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PostPosted: Mon Oct 09, 2006 9:32 pm    Post subject: Nose gear bungees Reply with quote

I don't want to win a Darwin award - save me from that.

I place the sandbags at the root of the elevator, not at the outboard
ends. I will not use the sandbags if it will cause damage. I obviously,
don't think that placing 120 pounds of sand on the root of the elevator
will damage the elevator. I want to know if I'm wrong. Two G steep turns
must place more than 120 pounds of apparent weight on the elevator. I
agree that in flight the CG is forward of the landing gear and less force
is needed to lift the nose. But, on takeoff I tend to pull to lift the nose,
the 601XL is nose heavy, and that must take about the same force as
lifting the nose at rest - the wheels are still on the ground. The
'weight' on the elevator needed to rotate the nose during takeoff must be
close to 120 pounds. The wing is carrying some of the weight, but the
engine still must be lifted.

I have a structural engineering type friend whom I will ask to do some
calculations. I'd like some calculations to show how much apparent weight
is on the elevator at takeoff and in a 2G turn. He has examined the wings
and has found that the 6G loading design is accurate.

Joe E
N633Z (at) BFI
CH601XL 400 hours (and hoping for more)
do not archive

P.S. I will use O2 above 12,500 feet, I've been to 17,400.
On Mon, 9 Oct 2006, Klaus Truemper wrote:
Quote:

......snip
The use of sandbags on the horizontal stabilizer to lift the nose gear
is not such a good idea. One might argue that this okay since the
horizontal stabilizer/elevator must lift the nose gear on takeoff. But
when the plane rotates on takeoff, the wings already carry almost all
of the weight of the airplane. Thus, the horizontal stabilizer/elevator
force needed for rotation on takeoff is much, much smaller than the
force needed to lift the nose gear while parked. Cessna some years ago
had failures of the horizontal stabilizer spar of the 152 because
people would push down on the elevevator to lift the nose gear when
parking the plane in a tight spot.
Best wishes, Klaus Truemper


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p.mulwitz(at)worldnet.att
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PostPosted: Tue Oct 10, 2006 2:36 am    Post subject: Nose gear bungees Reply with quote

It seems to me that holding the tail down with the tie down ring
would be certain to be safe.

Paul
XL fuselage
do not archive


Quote:
I don't want to win a Darwin award - save me from that.

I place the sandbags at the root of the elevator, not at the outboard
ends. I will not use the sandbags if it will cause damage. I obviously,
don't think that placing 120 pounds of sand on the root of the elevator
will damage the elevator. I want to know if I'm wrong. Two G steep turns
must place more than 120 pounds of apparent weight on the elevator. I
agree that in flight the CG is forward of the landing gear and less force
is needed to lift the nose. But, on takeoff I tend to pull to lift the nose,
the 601XL is nose heavy, and that must take about the same force as
lifting the nose at rest - the wheels are still on the ground. The
'weight' on the elevator needed to rotate the nose during takeoff must be
close to 120 pounds. The wing is carrying some of the weight, but the
engine still must be lifted.

I have a structural engineering type friend whom I will ask to do some
calculations. I'd like some calculations to show how much apparent weight
is on the elevator at takeoff and in a 2G turn. He has examined the wings
and has found that the 6G loading design is accurate.

Joe E
N633Z (at) BFI
CH601XL 400 hours (and hoping for more)
do not archive

P.S. I will use O2 above 12,500 feet, I've been to 17,400.
On Mon, 9 Oct 2006, Klaus Truemper wrote:
>
> ......snip
> The use of sandbags on the horizontal stabilizer to lift the nose gear
> is not such a good idea. One might argue that this okay since the
> horizontal stabilizer/elevator must lift the nose gear on takeoff. But
> when the plane rotates on takeoff, the wings already carry almost all
> of the weight of the airplane. Thus, the horizontal stabilizer/elevator
> force needed for rotation on takeoff is much, much smaller than the
> force needed to lift the nose gear while parked. Cessna some years ago
> had failures of the horizontal stabilizer spar of the 152 because
> people would push down on the elevevator to lift the nose gear when
> parking the plane in a tight spot.
> Best wishes, Klaus Truemper


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JERICKSON03E(at)aol.com
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PostPosted: Tue Oct 10, 2006 10:12 am    Post subject: Nose gear bungees Reply with quote

In a message dated 10/10/2006 1:56:25 AM Central Daylight Time, xl(at)prosody.org writes:
Quote:
I place the sandbags at the root of the elevator,


Joe, Are you sure that you meant the elevator? Or was it the horizontal stabilizer?

I would avoid placing any weight on the elevator, or any of the movable control surfaces.

Jerry
[quote][b]


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xl(at)prosody.org
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PostPosted: Tue Oct 10, 2006 10:12 pm    Post subject: Nose gear bungees Reply with quote

Yes, I meant the stabilizer. I'm told it takes 2 - 60 pound
concrete blocks for a Piper TriPacer.

Joe E
N633Z (at) BFI
CH601XL 400 hours
do not archive
On Tue, 10 Oct 2006 JERICKSON03E(at)aol.com wrote:
Quote:
In a message dated 10/10/2006 1:56:25 AM Central Daylight Time,
xl(at)prosody.org writes:
'I place the sandbags at the root of the elevator,'
Joe, Are you sure that you meant the elevator? Or was it the horizontal
stabilizer?
I would avoid placing any weight on the elevator, or any of the movable
control surfaces.
Jerry


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Joined: 19 Jul 2006
Posts: 2704
Location: Campbellton, Newfoundland

PostPosted: Wed Oct 11, 2006 8:41 am    Post subject: Nose gear bungees Reply with quote

You could also make a rope saddle to fit over the fuselage in front of the
vertical stab. Put your weight on both sides. Use plenty of weight, no
sense in having it flop forward because some one dropped a feather on the
nose.

Noel

[quote] --


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planejim(at)bellsouth.net
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PostPosted: Thu Oct 12, 2006 3:20 pm    Post subject: Nose gear bungees Reply with quote

Mike,

I agree that tne nose gear bungee wears because of steering and the small
diameter of the tubes over which the bungee is stretched. I don't believe
the heat of the engine is the problem.

Jim Hoak

---


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PostPosted: Tue Oct 17, 2006 5:13 am    Post subject: Nose gear bungees Reply with quote

George and Listers,

My experience is that heat is not the reason for the nose gear bungee deterioration. In my opinion, FWIW, is that the wearing and fraying is due to bending the bungee over a small diameter tube along with a twisting motion during taxiing when the nose gear is moving up and down. Remember, the twisting motion, small as it is, goes on in flight too when you move the rudder pedals. I suggest that people don't get too concerned with some fraying of the outer threads of the bungee. The real problem arises when the rubber bands become exposed. Just my thoughs on this from my experiences.

Jim Hoak 601HD - 912UL - 532 hours.
[quote] ---


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