Zenith601-List Digest Archive

Mon 09/15/08


Total Messages Posted: 6



Today's Message Index:
----------------------
 
     1. 06:27 AM - Re: Re: Rear Spar attachment (jaybannist@cs.com)
     2. 07:25 AM - Re: Re: Rear Spar attachment (A.F.RUPP@att.net)
     3. 07:27 AM - Re: Re: Recently completed Fuel Gauge Question (Jim Belcher)
     4. 01:55 PM - Re: Rear Spar attachment (PatrickW)
     5. 05:25 PM - LSA OR EXPERIMENTAL (GLJSOJ1)
     6. 10:09 PM - Re: Re: Rear Spar attachment (Gary Gower)
 
 
 


Message 1


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    Time: 06:27:29 AM PST US
    Subject: Re: Rear Spar attachment
    From: jaybannist@cs.com
    Tim, Again, I meant no disrespect. At the time I was working on it, I wondered: Since there are actually two doublers (an angle and a plate) on the rear wing spar, why were there not doublers on the channel in the fuselage ? It seems to me that reinforcing that channel would be necessary to get any benefit from thickening the connector. Beyond that, the wing rear spar is stabilized in buckling by being riveted to the wing skins. The fuselage channel only has the bottom flange stabilized by riveting to the fuselage floor and the .025" upright channels. The point is that this is a very complex connection; and one that shouldn't be messed with, without a LOT of engineering analysis. I am assuming that the change in the angle of incidence of the 650 wing was the reason for the change to the connector plate; therefore, it really doesn't apply to the XL. Jay in Dallas -----Original Message----- From: Tim Juhl <juhl@avci.net> Sent: Sun, 14 Sep 2008 8:55 pm Subject: Zenith601-List: Re: Rear Spar attachment Jay, If it was confirmed that the bracket had been beefed up then my next question would have been to ask what had been done to the attaching structure. I'm not trying to add to the hysteria about the wing safety, but I have always considered the rear attachment to be a potential weak point. Since I will be working on that section soon I thought it would be good to investigate whether or not major changes had been made in that area that were adaptable to my XL. I've been away from building since early June so I am not as up to date on current events as I would like to be. Since I plan to get back to building soon I'm just trying to get up to speed. Tim -------- ______________ CFII Champ L16A flying Zodiac XL - Jabiru 3300A Working on fuselage Read this topic online here: http://forums.matronics.com/viewtopic.php?p 4326#204326 ________________________________________________________________________ Email message sent from CompuServe - visit us today at http://www.cs.com


    Message 2


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    Time: 07:25:57 AM PST US
    From: A.F.RUPP@att.net
    Subject: Re: Rear Spar attachment
    Tim, According to ZAC in the Summary of Changes in the Builders Update section of the Zenith website the forward and rear uprights geometry was changed to accomodate the angle of incidence change and thus the attach plate was changed. As Jay pointed out there were a series of changes in that area to accomodate the canopy and wing incidence changes. The drawings for the canopy latches are available as is a list of the changes from the 601XL to 650 on Zeniths Builders Update website. Al 601 XL -------------- Original message from jaybannist@cs.com: -------------- > Tim ...... > The point is that this is a very complex connection; and one that > shouldn't be messed with, without a LOT of engineering analysis. I am > assuming that the change in the angle of incidence of the 650 wing was > the reason for the change to the connector plate; therefore, it really > doesn't apply to the XL. > > Jay in Dallas > > -----Original Message----- > From: Tim Juhl > To: zenith601-list@matronics.com > Sent: Sun, 14 Sep 2008 8:55 pm > Subject: Zenith601-List: Re: Rear Spar attachment > > > Jay, > If it was confirmed that the bracket had been beefed up then my next > question > would have been to ask what had been done to the attaching structure. > working on that section soon I thought it would be good to investigate > whether > or not major changes had been made in that area that were adaptable to myXL > Tim > > -------- > ______________ > CFII > Champ L16A flying > Zodiac XL - Jabiru 3300A > Working on fuselage > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p 4326#204326 > > > > > > > > > > > > > > > > ________________________________________________________________________ > Email message sent from CompuServe - visit us today at http://www.cs.com > > > >


    Message 3


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    Time: 07:27:35 AM PST US
    From: Jim Belcher <z601@anemicaardvark.com>
    Subject: Re: Recently completed Fuel Gauge Question
    On Sunday 14 September 2008 19:24, Gig Giacona wrote: > > Unless something has changed there are no E-LSA 601/650 at this time except > the ones that received AW prior to the deadline for certifying > non-conforming "Fat Ultralights." > > The reason for this is the mfg of the kit must also be the mfg of the > conforming factory built S-LSA. > > For there to be a an E-LSA of the Zenith line then AMD is going to have to > offer a kit or ZAC is going to have to offer a complete airplane. > > That said the builder of a conforming E-LSA has almost no leeway. They must > follow the instruction pretty much to the letter. That is pretty much what I would have expected, but I wasn't sure about the status of the 601/650 as far as ELSA is concerned. The business relationship of AMD/Zenith is a bit fuzzy to me. Thanks for that clarification. It means that the 601/650 being built are experimental, and there is considerable leeway in how fuel measurement is done. Someone mentioned the problems on gauging the amount of fuel in the 15 gallon tanks. I note that the AMD version has 15 gallon tanks. I wonder how they did the measurement, and how accurate their indication of fuel level is? ============================================= Those who can, do. Those who can't, sue. ================================================ Jim B. Belcher BS, MS Physics, math, Computer Science A&P/IA Instrument Rated Pilot General Radio Telephone Certificate ================================================


    Message 4


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    Time: 01:55:55 PM PST US
    Subject: Re: Rear Spar attachment
    From: "PatrickW" <pwhoyt@yahoo.com>
    Tim Juhl wrote: > I get the impression that the rear spar attachment bracket on the 650 is made out of thicker material. Can anyone confirm that? Here's a picture, with a ruler held up against it. - Pat -------- Patrick 601XL/Corvair N63PZ (reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p 4451#204451 Attachments: http://forums.matronics.com//files/rearplate_202.jpg


    Message 5


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    Time: 05:25:51 PM PST US
    Subject: LSA OR EXPERIMENTAL
    From: "GLJSOJ1" <gljno10@hotmail.com>
    Hi all Getting ready to send off for the airworthy cert and I am planning to list it as EXPERIMENTAL-AIRPLANE-AMATEUR BUILT rather than going the light sport. The way I see it as long as my specification match the light sport regulations I am good to go. Email me off line if you want Thanks all gljno10@hotmail.com -------- 601XL N676L reserved ALMOST DONE CHESAPEAKE VA Read this topic online here: http://forums.matronics.com/viewtopic.php?p 4477#204477


    Message 6


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    Time: 10:09:08 PM PST US
    From: Gary Gower <ggower_99@yahoo.com>
    Subject: Re: Rear Spar attachment
    Thats about--- 0.1377949"--- :-)- Do not archive. --- On Mon, 9/15/08, PatrickW <pwhoyt@yahoo.com> wrote: From: PatrickW <pwhoyt@yahoo.com> Subject: Zenith601-List: Re: Rear Spar attachment <pwhoyt@yahoo.com> Tim Juhl wrote: > I get the impression that the rear spar attachment bracket on the 650 is made out of thicker material. Can anyone confirm that? Here's a picture, with a ruler held up against it. - Pat -------- Patrick 601XL/Corvair N63PZ (reserved) Read this topic online here: http://forums.matronics.com/viewtopic.php?p 4451#204451 Attachments: http://forums.matronics.com//files/rearplate_202.jpg =0A=0A=0A




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