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All 601XL grounded in Netherlands
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David X



Joined: 10 Jan 2006
Posts: 154
Location: Princeton, NJ, USA

PostPosted: Fri Nov 14, 2008 4:26 pm    Post subject: All 601XL grounded in Netherlands Reply with quote

My purpose in posting this is to make information available to builders and owners. This may affect your periodic or annual inspection. Attention should be given to the wing rear attach points at the wing root and the cable tensions, particularly the ailerons.

I am not speculating, but simply conveying what I was told over the phone by the FAA and NTSB. I'm conveying this in my own words. Nothing in this post are official NTSB findings.

I received two calls today, one from the FAA and another from the NTSB. They wanted me to be aware of the grounding of all 601XL in Netherlands. The aircraft in question was built by Czech Aircraft Works. There are perhaps 2 in the US that were build by CZAW. One was crashed by my friend in Virginia (the NTSB preliminary report indicated that there was no fuel in the wing tanks, fuel lines or carburetor bowls). I own the only remaining 601XL in the US built by CZAW.

The issues of concern that were conveyed to me by the FAA and NTSB were aileron flutter (NTSB) and wing folding (FAA). There has not been a conclusion by the NTSB regarding the wing folding incidents. The aileron flutter is a point of interest but it is not known whether it is a factor in the Dutch crash. Although your aircraft was probably not built by CZAW, I think the information would apply to the 601XL design in general.

The thought/concern conveyed to me is that a flutter condition could cause a wing failure if torsional (twisting) forces were high enough. The main spar was not designed to withstand torsional forces and depends on the rear wing mounts to prevent twisting.

This is not something unique to the 601XL but a possible condition in any aircraft with unbalanced control surfaces. By unbalanced, I mean that there is no counter-weight in aileron, elevator or rudder to keep them in a neutral position absent any outside force (such as air flow or control inputs). The 601XL does not exhibit flutter so long as the cable tensions are correct. There is also a very generous margin +/- 5 lbs.

I was told that the engineers at the NTSB have reviewed the 601XL design and by all indications it is a 6G aircraft (theoretical) and is as advertised by the designer. Of course, it is rated much lower for margin of safety. I was told that there were no major concerns about the design. The potential for flutter seemed to be their main focus.

The only other information I was given was to make sure that the POH had the correct calibrated air speeds. Calibrated speeds are preferred over indicated (the latter varying depending on density altitude, temperature and altitude).

I have flown my 601XL for 300+ hours. I also flew it coast to coast over the Rockies twice and I have had zero issues whatsoever with aileron flutter. Years ago, after hearing about the wing folding incidents, I spot painted the the rear spar connection points and the main spar attach points as a way to detect any shift. I have seen zero shift in 3 years of flying.

Linked below are service bulletins issued by Dutch and AMD that apply to this particular situation. I've included a few links that speak to this situation.

http://www.zenairulm.com/News/pdfdocs/ZE-2008-01.pdf

http://www.newplane.com/Service_Letters_Bulletines/SAFETY_ALERT_october_29_2008.pdf

http://www.zenairulm.com/News/index_files/Page349.htm

http://www.zenairulm.com/News/index_files/Page350.htm


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Last edited by David X on Fri Nov 14, 2008 10:31 pm; edited 6 times in total
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PostPosted: Fri Nov 14, 2008 5:11 pm    Post subject: All 601XL grounded in Belgium Reply with quote

"There are perhaps 2 in the US that were build by CZAW."

I thought that the Xl that went down in Florida near Sun-n-fun was also a
CZAW plane?

NTSB:

<quote>
NTSB Identification: NYC08FA158
Accident occurred Monday, April 07, 2008 in Polk City, FL
Aircraft: Chech Aircraft Works SPOL SRO CH 601 XL RTF, registration: N357DT
Injuries: 1 Fatal.

This is preliminary information, subject to change, and may contain errors.
Any errors in this report will be corrected when the final report has been
completed.

On April 7, 2008 about 1700 eastern daylight time, a Czech Aircraft Works
SPOL SRO CH 601 XL RTF, N357DT, was substantially damaged when it impacted
trees and terrain following an uncontrolled descent near Polk City, Florida.
<endquote>

FAA database:

N357DT is Assigned

Aircraft Description

Serial Number 6-9733 Type Registration
Individual
Manufacturer Name CZECH AIRCRAFT WORKS SPOL SRO
Certificate Issue Date 11/28/2007
Model CH 601 XL RTF Status Valid
Type Aircraft Fixed Wing Single-Engine Type Engine
Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code
50777453
MFR Year 2005 Fractional Owner NO

-- Craig


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David X



Joined: 10 Jan 2006
Posts: 154
Location: Princeton, NJ, USA

PostPosted: Fri Nov 14, 2008 6:32 pm    Post subject: Re: All 601XL grounded in Belgium Reply with quote

I recall that there was a 3rd, but the NTSB seems to be under the impression that there were only two. Thank you for the info. I'll pass it along.

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David X



Joined: 10 Jan 2006
Posts: 154
Location: Princeton, NJ, USA

PostPosted: Fri Nov 14, 2008 10:33 pm    Post subject: Re: All 601XL grounded in Netherlands Reply with quote

To anyone who read this post before I edited it ... the country in question is the Netherlands, not Belgium.

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aerobat



Joined: 07 Nov 2008
Posts: 21
Location: UK

PostPosted: Sat Nov 15, 2008 5:36 am    Post subject: Re: All 601XL grounded in Netherlands Reply with quote

The aircraft is grounded by most European countries now, here in the UK about two dozen are affected.

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PostPosted: Sat Nov 15, 2008 8:14 am    Post subject: All 601XL grounded in Netherlands Reply with quote

As I understand it the XL was grounded in the UK due to worries about the
cable AD, not the Dutch action. What will the UK authorities do to decide
whether to let them fly again?

-- Craig

Do not archive

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Gig Giacona



Joined: 10 Jan 2006
Posts: 1416
Location: El Dorado Arkansas USA

PostPosted: Sat Nov 15, 2008 10:39 am    Post subject: Re: All 601XL grounded in Netherlands Reply with quote

David, I curious. Did they call you because you had a CZAW built aircraft?

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chris Sinfield



Joined: 28 Nov 2006
Posts: 270
Location: Sydney Australia

PostPosted: Sat Nov 15, 2008 8:34 pm    Post subject: Re: All 601XL NOT grounded in Australia Reply with quote

Some good news
in Australia the RAA has not grounded any XL's there is 1imported CZAW built aircraft and the rest are by zenith kits. We have a good Zenith XL network and he was notified of the aileron tension issues and checked his A/C. yes his cables were about 1/2 of what they should be. of note he had no flutter issues before with the lower tensions.

The RAA here are happy with us having the SB in our XL newsletter, the remainder of us are all builders of XL those finished and those still going. we built it we should know how to check it, maintain it.

Common sense to the RAA.
Chris.
Sydney
XL Jab3300


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Jugle



Joined: 04 Aug 2007
Posts: 47
Location: Victoria, Australia

PostPosted: Sun Nov 16, 2008 2:59 pm    Post subject: Re: All 601XL grounded in Netherlands Reply with quote

Can someone please clarify?

As I understand it the CZAW 601s have a lower MTOW and are built from lighter material in some areas, correct?

So, obviously the cable tensions need to be correct regardless, but does this mean the CZAW versions are more susceptible to the problem?

Glenn.


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601XL- Rudder, Stabiliser parts completed, Wing ribs, nose ribs done, 70% Fuselage parts made.
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PostPosted: Sun Nov 16, 2008 4:10 pm    Post subject: All 601XL grounded in Netherlands Reply with quote

Glenn,
You are correct about the materials and MTOW, so would it not be more a
risk to those who would load to US standards by mistake or assume the
aircraft
to be the same after the fact. This would be easier to understand if
they used Internet to read Zenith specifications. The casual thought that
these aircraft were the same construction might be a dangerous one for
the European built and Mfg aircraft.

Doubt cable tensions had anything to do with the problems nor a solution
for the problems of concern either.

Larry McFarland 601HDS at www.macsmachine.com

Jugle wrote:
Quote:


Can someone please clarify?

As I understand it the CZAW 601s have a lower MTOW and are built from lighter material in some areas, correct?

So, obviously the cable tensions need to be correct regardless, but does this mean the CZAW versions are more susceptible to the problem?

Glenn.

--------
Glenn Andressen
601XL- Rudder, Stabiliser partially completed, Wing ribs, nose ribs done, numerous other parts made.



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Terry Phillips



Joined: 11 Jan 2006
Posts: 346
Location: Corvallis, MT

PostPosted: Sun Nov 16, 2008 6:01 pm    Post subject: All 601XL grounded in Netherlands Reply with quote

Glenn

You are right. CZAW 601XL's are lighter. But, they are lighter in only one
place: The landing gear.

CZAW used the composite gear sold by Aircraft Spruce. The Aircraft Spruce
landing gear is limited to 550 kg gross, which is less than the Zenair 600
kg (1320 lb) gross. However, I believe that some of the CZAW 601XL's that
made it to the US were registered with 600 kg gross. See:

http://www.aircraftspruce.com/catalog/lgpages/compositelg.php

Other than that, CZAW 601XL's are identical or even beefed up a bit
compared to the standard Zenair 601XL. I believe that all CZAW 601XL's use
the piano hinged aileron and incorporate the electric aileron trim option.
In fact, I believe that if you check with someone who owns a CZAW 601XL,
you'll find that the aileron piano hinge has been beefed up beyond the
standard Zenair piano hinge.

So, if the cable tension is more critical for the CZAW built 601XL's than
for the Zenair 601XL's (personally, I do not believe that it is), the
difference would evidently lie in the hinges or the trim option. (Note that
not all Zenair 601XL's have piano hinges or aileron trim tabs, while all
CZAW 601XL's apparently have those options.)

Terry
At 02:59 PM 11/16/2008 -0800, you wrote:
Quote:
Can someone please clarify?

As I understand it the CZAW 601s have a lower MTOW and are built from
lighter material in some areas, correct?

So, obviously the cable tensions need to be correct regardless, but does
this mean the CZAW versions are more susceptible to the problem?

Glenn


Terry Phillips ZBAGer
ttp44~at~rkymtn.net
Corvallis MT
601XL/Jab 3300 s .. l .. o .. o .. w build kit - Tail, flaps, & ailerons
are done; working on the wings
http://www.mykitlog.com/N47TP/


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Terry Phillips
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ttp44<at>rkymtn.net
Zenith 601XL/Jab 3300 slow build kit - Tail feathers done; working on the wings.
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alex_001



Joined: 14 Jan 2007
Posts: 61

PostPosted: Mon Nov 17, 2008 1:14 am    Post subject: Re: All 601XL grounded in Netherlands Reply with quote

I would like to point out that the 601xl that went down in the Netherlands was not a RTF CZAW it was a kit build (Kit was supplied by CZAW)

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tiethoff



Joined: 02 Sep 2008
Posts: 23

PostPosted: Mon Nov 17, 2008 7:46 am    Post subject: All 601XL grounded in Netherlands Reply with quote

CZAW XL's are lighter because the undercarriage gear is made out of carbon.
That's the ONLY difference. On some 601's flying in Europe the part of the
wing where you put your feet (on the black anti slip pieces) is a half
milimeter thicker. On each wing 40 x 80 cm.

Regards, Eric Tiethoff
The Netherlands.

--------------------------------------------------
From: "Jugle" <glenn(at)eastcoastit.net>
Sent: Sunday, November 16, 2008 11:59 PM
To: <zenith601-list(at)matronics.com>
Subject: Re: All 601XL grounded in Netherlands

Quote:


Can someone please clarify?

As I understand it the CZAW 601s have a lower MTOW and are built from
lighter material in some areas, correct?

So, obviously the cable tensions need to be correct regardless, but does
this mean the CZAW versions are more susceptible to the problem?

Glenn.

--------
Glenn Andressen
601XL- Rudder, Stabiliser partially completed, Wing ribs, nose ribs
done, numerous other parts made.


Read this topic online here:

http://forums.matronics.com/viewtopic.php?p 14595#214595





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alex_001



Joined: 14 Jan 2007
Posts: 61

PostPosted: Mon Nov 17, 2008 8:13 am    Post subject: Re: All 601XL grounded in Netherlands Reply with quote

I have a little dent in my LH aileron ruder at the hinge area.
can someone give my advise if i should worry or if this could be caused by "flutter"

thank you


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alex_001



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PostPosted: Mon Nov 17, 2008 8:47 am    Post subject: Re: All 601XL grounded in Netherlands Reply with quote

Sabrina,
i send my pics to Michael H. and waiting for answer.
this 601xl is always kept in hangar and has about 70hrs

on a other issue i fitted some wing root fairings from Zenair in France looks real cool


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alex_001



Joined: 14 Jan 2007
Posts: 61

PostPosted: Mon Nov 17, 2008 8:57 am    Post subject: Re: All 601XL grounded in Netherlands Reply with quote

Sabrina,

on my friends 601xl (RTF CZAW) this plane was a former display plane at the Friedrichshafen Air Show in 2005 after the show the plane went back to CZAW, to have on the area where you have the anti slip tape on the top of the wing a 2nd skin riveted on the reason for this was during the exhibition so many people climbed in and out of the plane (also some females with pointed heels) that the skin was a bit sad to look at. And therefore CZAW riveted a 2nd skin over it (but i am not sure in what gauge) but this was ONLY to cover the dents that came from climbed show.


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Terry Phillips



Joined: 11 Jan 2006
Posts: 346
Location: Corvallis, MT

PostPosted: Mon Nov 17, 2008 9:16 am    Post subject: All 601XL grounded in Netherlands Reply with quote

Very good point, Sabrina. and a very interesting photo.

I wasn't aware of Alex's photo. Where did you find it, BTW? My search fails me in trying to locate it. Alex's photo points out a good example of a CZAW "beef up," i.e., the diagonal bracing in the fuselage side panels. I don't recall seeing that in my B-23. I believe that ZAC did copy that feature in the 650. It is probably a good idea and I will probably add it to my 601XL.

Regarding the skin thickness, one must also be aware that CH's designs also change over the years. Fortunately, ZAC has documented these changes on their website. See, e.g.,

http://www.zenithair.com/zodiac/xl/data/xl-update-3rd-ed-1st-rev-4-05.pdf

where you find the following:

6-B-3 04/05 REAR SIDE SKINS
1) new page layout: Moved 6B3-3 and 6B3-4 to drawing 6-B-1 (01/05)
2) 6B3-1 Rev. 2 change material thickness from t=.016” to t=.025” (12/04)
3) 6B3-2 deleted battery access option (area is now accessible through bottom access
panel) (12/04)
4) 6B3-6 Rev 1 new width at front and rear, changed 67 to 61 , 251 to 272mm (03/05)
5) New parts 6B3-7 and 6B3-8 piano hinge and bottom fuselage access panel. (12/04)
6) Re-positioned 6B1-7 between the Z and 6B5-2 (12/04)
note: the aft rivet line through the fairing 6G3-2 is the same rivet line through the piano
hinge and Z angle.(12/04)
7) Deleted Gusset 6B3-5 (01/05)
Cool Add nutplate 21075L3 (02/05)
9) Added A4 pitch 20 bottom skin 6B1-4 into 6B1-1 (02/05)
10) middle diagram: 340mm between rivets for the H.T frames (measured on center line)
(03/05)
11) top right diagram: riveting L angles to side skin 6B3-1 changed pitch from 60 to 40
(04/05)

Where I've colored item 2) to red for emphasis.

So, while I will readily agree with you that CZAW may have changed skin thicknesses, etc., over the years, I'm not yet ready to agree that their kit differs from ZAC except for the "beefing up" and the landing gear already cited. While their changes may (and I emphasize may because I don't have their design history) have lagged ZAC's would not be very suprising, because they would have had to react to whatever ZAC published.

If you can show me examples of "light weight" CZAW designs, materials, etc., that differ from ZAC's designs, I'm ready to admit your point.

Terry



At 07:01 AM 11/17/2008 -0800, you wrote:
Quote:
"But, they are lighter in only one place: The landing gear... Other than that, CZAW 601XL's are identical or even beefed up a bit compared to the standard Zenair 601XL. I believe" Terry

Terry,

Different CZAW 601XLs have different skin thicknesses, especially the kits as pointed out by Alex. The attached photo is of an EU CZAW kit. The QQ-A-250/11 does not designate a .025 skin, look up at the 0.016 in

6-B-3 08/05 specs .025 on the US version. .025 is 56% more AL than .016, so our rear fuselage skins alone weigh 56% more than the CZAW kit.

The FAA reads this list, we can't keep telling them that the all CZAW 601XL are built "identical" or "beefed up" compared to our aircraft if it is not necessarily true. They may start believing us.


Terry Phillips ZBAGer
ttp44~at~rkymtn.net
Corvallis MT
601XL/Jab 3300 s .. l .. o .. o .. w build kit - Tail, flaps, & ailerons are done; working on the wings
http://www.mykitlog.com/N47TP/ [quote][b]


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PostPosted: Mon Nov 17, 2008 9:42 am    Post subject: All 601XL grounded in Netherlands Reply with quote

Why is it that some of those, who know FOR SURE, swear that the European XLs are stronger and lighter than the US version; and others, who know FOR SURE, swear that the European XL is lighter and weaker than the US version; and still others, who know FOR SURE, swear that there is no difference? Someone, please 'splain how that can be to this poor ole country boy!

I AM just smart enough to know that all these positions (actually opinions) can't be true. I really hate to say it, but some of you either don't know what you are talking about, or you are lying, or both. Prove me wrong!

Jay in Dallas
Do not archive





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alex_001



Joined: 14 Jan 2007
Posts: 61

PostPosted: Mon Nov 17, 2008 9:45 am    Post subject: Re: All 601XL grounded in Netherlands Reply with quote

the difference i think the 601xl from CZAW also have is that the angle of attack of the wing is flatter because CZAW only uses Rotax engine and that engine is less heavy and therefor less front heavy and less lift required and also more speed archieved . i been told this by chip erwin on my visit to the czaw factory.

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PostPosted: Mon Nov 17, 2008 9:57 am    Post subject: All 601XL grounded in Netherlands Reply with quote

Hi Jay,

I agree with your question, but I would like to add another one.

How is it that the Dutch government has determined the design load
calculations indicate an error on the designer's part but the
Brittish government sees the same design as adequate?

I've been watching all these opinions by both qualified and
unqualified people for years and still I believe we don't know
anything at all about the structural failures. There are, however,
many people who are SURE they know what is wrong.

I am feeling good about Bill of Georgia's comments today about lose
cables. He is one of the people who have actually experienced the
vibrations and survived. His observation that his cables were loose
suggests to me that we should all keep a close watch on those cables.

Paul
XL getting close
do not archive
At 09:42 AM 11/17/2008, you wrote:
Quote:
Why is it that some of those, who know FOR SURE, swear that the
European XLs are stronger and lighter than the US version; and
others, who know FOR SURE, swear that the European XL is lighter and
weaker than the US version; and still others, who know FOR SURE,
swear that there is no difference? Someone, please 'splain how that
can be to this poor ole country boy!

I AM just smart enough to know that all these positions (actually
opinions) can't be true. I really hate to say it, but some of you
either don't know what you are talking about, or you are lying, or
both. Prove me wrong!

Jay in Dallas
Do not archive


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