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Chris' Last Letter

 
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yak52



Joined: 25 Oct 2007
Posts: 50

PostPosted: Sat Jul 11, 2009 5:13 am    Post subject: Chris' Last Letter Reply with quote

"We appear to be fairly reassured that flutter is not an issue with cables at proper tension,
adding balances is not required."
 
Agreed.
 
 
 "On the other hand they need not be heavy or complex"
 
 
Agreed with the proviso that some real engineering would be necessary, including the possibility that additional GVT testng would be necessary. See the recomendations at the end of the GVT report done by Zenith's contractor.
 
" and then flutter mitigation would not require a specific cable tension (although flight control would certainly require some tension). If they are added the ailerons would certainly not flutter even with no tension, controls disconnected (the ultimate slack) flutter would then never be an issue, under any circumstances. "
 
 
Flutter mitigation, within the flight envelope, and a properly maintained airplane is already not an issue without adding additional structures. As there would have to be a specific cable tension maintained,  even with mass balanced ailerons, that would have to be checked as part of your maintainance schedule, you have gained nothing by the addition of the balanced ailerons except redundancy.
 
"Now I regard that as an improvement. I don't think the author was advocating for flight minus controls. "
 
Actually the author is on record as demanding that Zenith's  GVT testing be done with the control cables without tension. Try to imagine flying the Zenith without tension between the stick and the ailerons. Your problem would not be flutter if the cables loosened to zero in flight.
 
"If such a mod is approved, it should be optional,"
 
Agreed, but who will design and approve it.
 
 
" but any further attempt to vilify ZBAG simply because of this wording will only serve to further split the Zenith community"
 
ZBAG is a group of adults who sent the results unverified computer models to virtually every government regulating aircraft insisting that flutter was the cause of the crashes. They also haven't used the GVT testing rsults from Zenith to verify their model. They are big boys who should be able to stand their statements being analyzed.
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PostPosted: Sat Jul 11, 2009 6:03 am    Post subject: Chris' Last Letter Reply with quote

Hi Roger,

This one little part of your post caught my attention.

At 06:11 AM 7/11/2009, you wrote:
Quote:
you have gained nothing by the addition of the balanced ailerons
except redundancy.


I think my view of this situation would be better stated if you
changed the word redundancy to robustness.

We all know that the Zodiac XL is basically a very sound design that
meets not only the specific criteria of ASTM LSA standards but also
is desirable enough to have sold hundreds or thousands of copies to
builders and flyers. It has passed static load testing multiple
times. It has passed ground vibration testing. We don't know the
results of the other "Engineering design studies" since some have
been kept secret from the general public, but I think we can assume
there have been no "Smoking Guns" found to explain the real world
structure failures.

Nearly everyone who flies a Zodiac XL has a great experience with
it. However there have been enough fatal accidents involving
structural failure in flight that there is cause for alarm. So the
nature of the "Problem" with the XL is it lacks sufficient robustness
to have a great safety record instead of a pretty good one.

The XL design works fine in most cases. Some times in some unknown
set of conditions it fails to hold up. Stated differently: We need
to have more robustness in this design rather than a fix for a part
of the design which is broken.

The latest round of discussion of the aileron controls seems to
suggest that complete loss of aileron control due to slack cables is
an unthinkable situation. This is simply not true. Aileron control
is not required to allow for controlled flight.

There are three cables in the aileron control system. If any one of
them were severed then the tension in the system would be
removed. If it were the balance cable then the control stick would
still activate one of the ailerons when moved in either direction and
the pilot would be able to control movement about the aircraft's roll
axis. If either of the other cables (the ones going directly to one
wing) were severed, roll in one direction would still be controlled
and the other direction would be uncontrolled - as far as the aileron
system is concerned. However, roll in that direction and turning in
general would still be controllable through the rudder. Indeed if
the stick had no connection at all to the ailerons the rudder could
still be used to get the plane to fly in the direction desired by the
pilot. Yes, it would be uncoordinated flight, but that would only
make it a little bit uncomfortable for the occupants of the plane.

Put together this adds up to a robust system. Even complete loss of
aileron control leaves you with a controllable and flyable plane.

If loss of aileron cable tension leads to flutter and wing
separation, then the aileron cables become a critical system for
flight. Adding balance to the ailerons seems to change this by
removing any possibility of flutter when the aileron cable tension is
lost. This addition would restore some of the robustness to the
design that should have been there all along.

Paul
XL grounded


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d.goddard(at)ns.sympatico
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PostPosted: Sat Jul 11, 2009 9:44 am    Post subject: Chris' Last Letter Reply with quote

It may be issued as a result of OTHER gov't's demands, it doesn't look like the U.S. gov't has much interest. If it isn't issued and or approved it would be fine with me if any individual designed their own and self-evaluated the result. If it works well other builders could use it. If Zenith saw no harm in it that would likely be the extend of factory approval but we'll see. Frankly i think flutter is now a dead issue, doesn't mean the airframe can't be improved. I would regard these balance as desirable but not high priority.

I see ZBAG as a bunch of interested and engaged owners, not an enemy. I don't believe they had much influence on the Gov't and I don't believe they've grounded anything. They MAY have had a very small part in getting a very small and so far unenforced recommendation made by a safety agency. I believe the actions of foriegn gov'ts and the accidents will have had much more influence. All in all I see ZBAG as exactly what they say they are, a group of interested builders. Mostly irrelevant to the rest of us, certainly not worth all the electrons and angst required to hate their guts the way most of the zenith builders have decided to. I would certainly analyse any "statement" made by the group as a whole as an official statement, but there has been none and unless they find something definitive I would not expect that. Any statements by a person who happens to be a member would hold no more weight than any other of the vast array of opinions I've read here. I encourage ZBAG to do their thing, so far I percieve them as irrelevant. I'm unsure who the author who wants the GVT done with slack cables is, but he's free to want anything. I want the accidents to stop, after that I want to understand the reason this airframe appears to have a disproportionate rate of failure. I bet my wish happens before his.

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JohnDRead(at)aol.com
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PostPosted: Sat Jul 11, 2009 1:55 pm    Post subject: Chris' Last Letter Reply with quote

How about we bag the Zbaggers and get on with life? Personally I have had it with their unfounded accusations of the 601.

John Read
CH701 - Elbert CO - Jabiru 3300

Phone: 303-648-3261
Fax: 303-648-3262
Cell: 719-494-4567


Looking for love this summer? Find it now on AOL Personals.
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jmaynard



Joined: 27 Feb 2008
Posts: 394
Location: Fairmont, MN (FRM)

PostPosted: Sat Jul 11, 2009 2:57 pm    Post subject: Chris' Last Letter Reply with quote

On Sat, Jul 11, 2009 at 05:57:51PM -0400, JohnDRead(at)aol.com wrote:
Quote:
How about we bag the Zbaggers and get on with life? Personally I have had
it with their unfounded accusations of the 601.

If I thought there was no foundation for the concerns, I wouldn't have sent
in my money to support the effort. Do you think that we're doing this out of
a desire to harm the Zenith family of companies? Why on earth would that be
something Zenith owners and builders would want to do?
--
Jay Maynard, K5ZC, PP-ASEL, CFI-SP http://www.conmicro.com
http://jmaynard.livejournal.com http://www.tronguy.net
Fairmont, MN (KFRM) (Yes, that's me!)
AMD Zodiac CH601XLi N55ZC http://www.tronguy.net/N55ZC.shtml


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Juan Vega Jr



Joined: 13 Jan 2009
Posts: 157

PostPosted: Sat Jul 11, 2009 3:11 pm    Post subject: Chris' Last Letter Reply with quote

Dave,
Of all the accidents, There were two, out of all that may have been remotely based on some flutter, but totally unproven. Look at each accident and prior to people seeing the wings fall off, something else occured, crap weather, engine quits, pilot buzzing the field, Even the one in Texas, the witness heard the engine quite, THEN something about the wing failing. The only one that is complete unknown, is the one at Sun N FUn. The rest had something happen right before the claimed flutter. ZBAG latched on to the flutter issue like a Pissed off pit bull. Because some guy claimed he saw flutter over flying a power plant, then couldnt repeat it. 1000 zodiacs flying, and maybe 2 accidents that arte maybe a flutter issue.

Where is the disproportionate failure issue? check out the number of accidents of other aircraft. 2 out of how many zodiacs? PULL EVERY NTSB Zodiac accident, and label the ones that were possible flutter or design issue! Maybe 2! And trhe tests and nath can't find it!

Build it right, fly it right , maintain it right, its a great plane.

Juan
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PostPosted: Sat Jul 11, 2009 3:15 pm    Post subject: Chris' Last Letter Reply with quote

John, I am not clear that they have made any accusations. I believe they have some areas of concern that they are investigating. Any absolute accusations might well have come from a member, or from someone else. Let them do their thing. So far I don't believe they have harmed anyone, on the other hand, unexplained failures have. I hope they keep looking, maybe they'll help find an answer.
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PostPosted: Sat Jul 11, 2009 3:22 pm    Post subject: Chris' Last Letter Reply with quote

I don't believe they are out to harm anybody Jay, I believe you/they are
doing their best to satisfy themselves that their aircraft are as good as
they can be. Not sure how ZBAG got tagged an enemy that must be attacked at
every turn, miht be that old "If yer not with us, yer agin us us!!" crap.

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jmaynard



Joined: 27 Feb 2008
Posts: 394
Location: Fairmont, MN (FRM)

PostPosted: Sat Jul 11, 2009 3:31 pm    Post subject: Chris' Last Letter Reply with quote

On Sat, Jul 11, 2009 at 08:22:17PM -0300, Dave wrote:
Quote:
I don't believe they are out to harm anybody Jay, I believe you/they are
doing their best to satisfy themselves that their aircraft are as good as
they can be.

I can't speak for everyone involved, but that's certainly my motivation.

Quote:
Not sure how ZBAG got tagged an enemy that must be attacked at every turn,
miht be that old "If yer not with us, yer agin us us!!" crap.

I don't know either, but I'm getting goddamned tired of it.
--
Jay Maynard, K5ZC, PP-ASEL, CFI-SP http://www.conmicro.com
http://jmaynard.livejournal.com http://www.tronguy.net
Fairmont, MN (KFRM) (Yes, that's me!)
AMD Zodiac CH601XLi N55ZC http://www.tronguy.net/N55ZC.shtml


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PostPosted: Sat Jul 11, 2009 3:34 pm    Post subject: Chris' Last Letter Reply with quote

IRT "some guy claimed he saw flutter over flying a power plant, then
couldnt repeat it."
See below from my archives;
Tony Graziano; XL/Jab N493TG w 510 hrs to date
-
Hi Bill,Glad everything came out OK. Looks like you ran into some really
weird turbulence from the power-plant, giving you an "E" ticket ride. If
you were really experiencing wing or control surface flutter, your diving
and picking up speed should have exacerbated the problem with the amplitude
going divergent very rapidly, until something(s) bends or more likely breaks
off. Only saw this once in a film of a dynamic model in a wind tunnel - once
flutter started the entire model was gonzo in a second or two. Do you
recall experiencing any feed back in the stick/rudder?In 199 hours in my XL,
I have had some bumpy rides and the airplane has handled it ok - just glad I
always have my seat belt tight. I have also had some GREAT*, almost I would
have believed, GOOD*, landings and I agree the airplane is tough. *GREAT
Landing - Airplane is still flyable. GOOD Landing - You can walk away from
the airplane.Please let us know if you find anything after your in-depth
inspection. I kind of suspect you will not find anything amiss, but if you
do it would be a good data point for all of us for tailoring our structural
inspections. Tony Graziano XL; N493TG--------Ben, maybe I did not explain
well, but it was not control flutter. The
aileron did not move independent of the wing. What occurred is the whole
wing
fluttered with aileron moving with it., best regards,
Bill------------------------- Dear Thread Friends, I went flying this
afternoon. Took a fellow with me and
just wanted an hour in the clear blue. Conditions were perfect, clear, cool
and only a slight wind. The only big thing around much to see nearby is Lake
Juliette which has a big coal fired power station in the middle. Three huge
steam

towers that look like a nuclear power station. We flew around the lake about
two miles away at 5000 feet so my pal could get a good look see. On the down
wind side we flew into an invisible killer. We were doing above 140 when we
flew into it. Instantly the left wing fluttered at a fast pitch, aileron and
all

and it looked to be moving maybe two inched up and down. I figured a couple
seconds would break it off. I didn't have time to look around the passenger
to

see if the right wing was fluttering, but I suspect it was. I chopped power
and

did a hard diving wing over to the left and out of it. The flutter sound was
great even over my Lightspeed AN system and the whole thing probably last
maybe 5 or 6 seconds. I regained control out of the snap dive, maxing above
170

and flew slow and easy back to the field before I tested the controls.
Everything felt okay and I could see no wrinkles in the top skin so I
landed. Didn't

really have much choice. Upon inspection I found no sign of stress, no skin
deform, no paint cracked around rivets, nothing. I will take off all
inspection

panels for a close inspection this weekend and check bolts, controls, etc.,
but

I cannot believe such a prolonged violent movement of the wing did not
damage
something other than my pride. Two things learned. Don't fly anywhere near a
power station. Even at 5000 feet and miles away the invisible heat rises and
is

most extreme. Maybe intensified in cold weather. The other thing is the XL
is
very, very tough. Oh, there is a third thing. How could I have been so
stupid
not to know the first thing !! I am interested though in knowing why the
wings fluttered in this thermal? What theory of air dynamics would cause
this
extreme reaction? Was is just the level of heat and speed the invisible air
was

streaming past? This was my 90th flight in her and she made me proud again.
Best regards to you all,
Bill of Georgia
N505WP
601XL-3300
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