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		David X
 
  
  Joined: 10 Jan 2006 Posts: 154 Location: Princeton, NJ, USA
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				 Posted: Fri Nov 14, 2008 4:26 pm    Post subject: All 601XL grounded in Netherlands | 
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				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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 _________________ Zodiac 601 XL - CZAW Built - Rotax 912S
 
DO NOT ARCHIVE
  Last edited by David X on Fri Nov 14, 2008 10:31 pm; edited 6 times in total | 
			 
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		craig(at)craigandjean.com Guest
 
 
 
 
 
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				 Posted: Fri Nov 14, 2008 5:11 pm    Post subject: All 601XL grounded in Belgium | 
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				"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
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				 Posted: Fri Nov 14, 2008 6:32 pm    Post subject: Re: All 601XL grounded in Belgium | 
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				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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 _________________ Zodiac 601 XL - CZAW Built - Rotax 912S
 
DO NOT ARCHIVE | 
			 
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		David X
 
  
  Joined: 10 Jan 2006 Posts: 154 Location: Princeton, NJ, USA
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				 Posted: Fri Nov 14, 2008 10:33 pm    Post subject: Re: All 601XL grounded in Netherlands | 
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				To anyone who read this post before I edited it ... the country in question is the Netherlands, not Belgium.
 
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 _________________ Zodiac 601 XL - CZAW Built - Rotax 912S
 
DO NOT ARCHIVE | 
			 
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		aerobat
 
 
  Joined: 07 Nov 2008 Posts: 21 Location: UK
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				 Posted: Sat Nov 15, 2008 5:36 am    Post subject: Re: All 601XL grounded in Netherlands | 
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				The aircraft is grounded by most European countries now, here in the UK about two dozen are affected.
 
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		craig(at)craigandjean.com Guest
 
 
 
 
 
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				 Posted: Sat Nov 15, 2008 8:14 am    Post subject: All 601XL grounded in Netherlands | 
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				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
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				 Posted: Sat Nov 15, 2008 10:39 am    Post subject: Re: All 601XL grounded in Netherlands | 
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				David, I curious. Did they call you because you had a CZAW built aircraft?
 
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 _________________ W.R. "Gig" Giacona
 
601XL Under Construction
 
See my progress at www.peoamerica.net/N601WR | 
			 
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		chris Sinfield
 
 
  Joined: 28 Nov 2006 Posts: 270 Location: Sydney Australia
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				 Posted: Sat Nov 15, 2008 8:34 pm    Post subject: Re: All 601XL NOT grounded in Australia | 
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				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
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				 Posted: Sun Nov 16, 2008 2:59 pm    Post subject: Re: All 601XL grounded in Netherlands | 
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				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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 _________________ Glenn Andressen
 
601XL- Rudder, Stabiliser parts completed, Wing   ribs, nose ribs done, 70% Fuselage parts made. | 
			 
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		larry(at)macsmachine.com Guest
 
 
 
 
 
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				 Posted: Sun Nov 16, 2008 4:10 pm    Post subject: All 601XL grounded in Netherlands | 
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				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
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				 Posted: Sun Nov 16, 2008 6:01 pm    Post subject: All 601XL grounded in Netherlands | 
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				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
 
Corvallis, MT
 
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
 
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				 Posted: Mon Nov 17, 2008 1:14 am    Post subject: Re: All 601XL grounded in Netherlands | 
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				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
 
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				 Posted: Mon Nov 17, 2008 7:46 am    Post subject: All 601XL grounded in Netherlands | 
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				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
 
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				 Posted: Mon Nov 17, 2008 8:13 am    Post subject: Re: All 601XL grounded in Netherlands | 
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				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
 
 
  Joined: 14 Jan 2007 Posts: 61
 
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				 Posted: Mon Nov 17, 2008 8:47 am    Post subject: Re: All 601XL grounded in Netherlands | 
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				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
 
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				 Posted: Mon Nov 17, 2008 8:57 am    Post subject: Re: All 601XL grounded in Netherlands | 
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				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
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				 Posted: Mon Nov 17, 2008 9:16 am    Post subject: All 601XL grounded in Netherlands | 
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				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)
    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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 _________________ Terry Phillips
 
Corvallis, MT
 
ttp44<at>rkymtn.net
 
Zenith 601XL/Jab 3300 slow build kit - Tail feathers done; working on the wings. | 
			 
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		jaybannist(at)cs.com Guest
 
 
 
 
 
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				 Posted: Mon Nov 17, 2008 9:42 am    Post subject: All 601XL grounded in Netherlands | 
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				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
 
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				 Posted: Mon Nov 17, 2008 9:45 am    Post subject: Re: All 601XL grounded in Netherlands | 
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				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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		psm(at)att.net Guest
 
 
 
 
 
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				 Posted: Mon Nov 17, 2008 9:57 am    Post subject: All 601XL grounded in Netherlands | 
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				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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