Today's Message Index:
----------------------
 
     1. 06:18 AM - Re: Trailering The CH701 (Steve Hulland)
     2. 08:17 AM - Re: Tow Bar (Tim Juhl)
     3. 08:29 AM - Re: Trailering The CH701 (Robert L. Stone)
     4. 11:08 AM - Re: A special Zodiac XL 601 (Gig Giacona)
     5. 12:25 PM - Re: (no subject) cork adhesive (Chuck & Lana Maggart)
     6. 12:36 PM - Re: Tow Bar (Chuck & Lana Maggart)
     7. 01:32 PM - Re: Trailering The CH701 (Chris Wolf)
     8. 01:35 PM - Re: Trailering The CH701 (Chris Wolf)
     9. 01:53 PM - Re: Tow Bar (Robert L. Stone)
    10. 01:58 PM - Re: Trailering The CH701 (Dave Austin)
    11. 03:08 PM - Re: Re: A special Zodiac XL 601 (LarryMcFarland)
    12. 03:59 PM - First Flight (george may)
    13. 04:20 PM - Re: Trailering The CH701 (Joe and Joan)
    14. 04:23 PM - Re: First Flight (LarryMcFarland)
    15. 04:34 PM - Wrong terms for aluminum properties....  (LarryMcFarland)
    16. 04:38 PM - Re: First Flight (N5SL)
    17. 04:42 PM - splicing long 601xl wing parts (Maarten Versteeg)
    18. 04:53 PM - sheet aluminum source (Maarten Versteeg)
    19. 05:20 PM - Re: Tow Bar (Sigmo@aol.com)
    20. 05:39 PM - Re: splicing long 601xl wing parts (David Barth)
    21. 05:57 PM - On-line info on making and using form blocks - the results (Craig Payne)
    22. 06:00 PM - Re: splicing long 601xl wing parts (Paul Mulwitz)
    23. 06:11 PM - Re: sheet aluminum source (Paul Mulwitz)
    24. 06:37 PM - Re: Re: Tow Bar (Trevor Page)
    25. 06:59 PM - 601XL Nose Wheel axle assembly ? (Robin Bellach)
    26. 07:03 PM - Re: Tow Bar (Robert L. Stone)
    27. 07:12 PM - Re: First Flight (n801bh@netzero.com)
    28. 07:23 PM - Re: First Flight (Michael Valentine)
    29. 08:09 PM - Re: Trailering The CH701 (Steve Hulland)
    30. 08:11 PM - Re: Trailering The CH701 (Gary Gower)
    31. 10:04 PM - CH-750? (George Harris)
 
 
 
Message 1
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| Subject:  | Re: Trailering The CH701 | 
      
      Robert,
      Nope, not an Ex-Marine as they are only the ones who were discharged under
      less than honorable conditions. I am a Marine - retired at that. Ha!
      Attended a reunion of Marines in Corpus Christi Oct 3-9. Attendees included
      active duty from Cpl to Lt.Gen. and retirees from GySgt - Lt General and
      Marines who got out with less than 20 from PFC to GySgt. We are a great band
      of brothers.
      
      On the way to the airport to work on airplane. Have a grand day.
      
      DO NOT ARCHIVE
      -- 
      Semper Fi,
      Steven R. Hulland
      CH 600 Taildragger
      Amado, AZ
      
      This and all other incoming/outgoing email, attachments and replies scanned
      prior to opening/sending and uses an external firewall to help insure virus
      free email and attachments.
      
Message 2
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      --> Zenith-List message posted by: "Tim Juhl" <juhl@avci.net>
      
      My XL came with the newer nose gear with the welded stop ring.  Regardless, I'm
      thinking that Larry's collar mounted just above the nose wheel pant would be
      a good spot to attach a tow bar.  I've seen others where builders put a hole in
      the pants over the axle nut and make a tow bar that has cups on the end that
      will fit into the hole and over the nut.  Using the collar would reduce the risk
      of scratching up the pant.
      
      Regarding pushing the aircraft around by the prop..... the propeller manufacturers
      all say this is a no-no although I admit to being guilty of this to some extent.
      I haven't finished my XL but I have moved many heavier aircraft using
      a tow bar and a hand on the prop close to the hub.  Obviously you wouldn't want
      to pull on the prop tip.
      
      Also, Cessna came out with a service bulletin many years ago warning of damage
      potential to the spar or attachments in the horizontal stabilizer caused by folks
      pushing down on it to raise the nose so it could be moved around.   Remember,
      stabs are designed to handle a load distributed evenly over their surface,
      not at one or two points the size of a human hand.
      
      Tim
      
      Do not archive
      
      --------
      DO NOT ARCHIVE
      ______________
      CFII
      Champ L16A flying
      Zodiac XL - Working on wings
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=67947#67947
      
      
Message 3
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  | 
      
      
| Subject:  | Re: Trailering The CH701 | 
      
      Steve,
           I cannot say I am from a more glorious outfit but very effective 
      anyway.  I am retired US Air Force.  The only people who get into combat 
      in the USAF today is the officers.  The only positions on air crews 
      today that are filled by enlisted is radio operators and load masters.  
      They are on cargo aircraft only.  All tactical combat aircraft have an 
      all officer crew. During the second world war the situation was quite 
      different because the bulk of the crew of a B-17 or a B-24 were the 
      gunners.  The 8th Air Force conducting bombing operations over German 
      occupied areas of Europe suffered loses of up to 67% until the North 
      American P-51 Mustang became available.  After that loses to enemy 
      fighters went down to almost nothing.  I went in right after the war in 
      1946 and have never heard a shot fired except on the rifle range.
           Tell me what you are building and how far along you are.  I am 
      building a ZodiacXL with the Jabiru 3300 engine and expect to be 
      finished this November or December.  I have enclosed a picture.
      
      Bob Stone
        ----- Original Message ----- 
        From: Steve Hulland 
        To: zenith-list@matronics.com 
        Sent: Sunday, October 15, 2006 8:17 AM
        Subject: Re: Zenith-List: Trailering The CH701
      
      
        Robert,
        Nope, not an Ex-Marine as they are only the ones who were discharged 
      under less than honorable conditions. I am a Marine - retired at that. 
      Ha! Attended a reunion of Marines in Corpus Christi Oct 3-9. Attendees 
      included active duty from Cpl to Lt.Gen. and retirees from GySgt - Lt 
      General and Marines who got out with less than 20 from PFC to GySgt. We 
      are a great band of brothers.
      
        On the way to the airport to work on airplane. Have a grand day.
      
        DO NOT ARCHIVE
        -- 
        Semper Fi,
        Steven R. Hulland
        CH 600 Taildragger
        Amado, AZ
      
        This and all other incoming/outgoing email, attachments and replies 
      scanned prior to opening/sending and uses an external firewall to help 
      insure virus free email and attachments. 
      
      
Message 4
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  | 
      
      
| Subject:  | Re: A special Zodiac XL 601 | 
      
      --> Zenith-List message posted by: "Gig Giacona" <wr.giacona@cox.net>
      
      I too am concerned with the change in metals. Quoting the are of the site that
      talks about budget. I get the following Google translation. Now I don't what the
      properties of those are but they weren't what the designer intended.
      
      
      > The Kit made with plate 5052 - H38 has all the Stringers, of the wings, profundor
      and stabilizer made in aluminum 2024 T-3.
      > 2-S I can vender the Kit so that it has the project, in case that you I want
      I can buy, or you yourselves purchase for the Internet, costs 390 dollars, +,
      this gives to the guarantee to be in day with the designer and is demanded the
      Invoice in the hour of you to make the document of the airplane.
      
      
      --------
      W.R. "Gig" Giacona
      601XL Under Construction
      See my progress at www.peoamerica.net/N601WR
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=67966#67966
      
      
Message 5
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  | 
      
      
| Subject:  | Re: (no subject) cork adhesive | 
      
      The cork strips with my kit had adhesive applied tape to the cork which 
      worked great.
      
      Chuck Maggart
      XL/Jabiru in paint
      
Message 6
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      Bob, I would not recommend "pushing on the tail" especially if you have 
      untrained helpers.  I have seen factory built aircraft damaged that way 
      and the Zodiac is lighter.  
      
      I bought a tow bar for a Piper Cherokee from AS&S and added a 4130 steel 
      plate on the nose wheel fork.  The plate picks up the forward two bolt 
      holes in the fork and I drilled two holes in the plate to mate with the 
      tow bar.  It is the same setup used on Cherokees and Tri-Pacers.  I am 
      considering extending the tow bar about a foot to make it easier to 
      reach under the nose.
      
      Chuck Maggart, St. Louis
      XL in paint
      
Message 7
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  | 
      
      
| Subject:  | Re: Trailering The CH701 | 
      
      --> Zenith-List message posted by: Chris Wolf <cwolf41@comcast.net>
      
      On Sat, 14 Oct 2006 17:39:13 -0700, Steven Hulland wrote:
      
      >Chris,
      >I have an enclosed utility trailer. I lock the safety chains to my vehicle
      >and they are firmly attached (plus lock) to the tounge. I also use another
      >lock as the safety pin that holds the ball hitch lever in the down position.
      >Finally, if on a trip that requires the trailer to be at a motel, etc. I
      >take a tire boot and lock one of the tires. Takes a couple of extra minutes
      >to hook things up, but I have never lost the trailer - or any other.
      >
      >Also have a small 1/4 ton ex-USMC utility trailer with a pintal hitch. Lock
      >the safety chains, but don't worry about the hitch part - most people do not
      >have a pintel and cannot steal it.
      >
      >Last resort, if I see them stealing it, I simply shoot. Seems to work well.
      >Ha!
      >
      >DO Not Archive
      
      Good advice.  Thanks!
      
      Chris Wolf
      cwolf41@comcast.net
      
      
Message 8
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  | 
      
      
| Subject:  | Re: Trailering The CH701 | 
      
      --> Zenith-List message posted by: Chris Wolf <cwolf41@comcast.net>
      
      On Sat, 14 Oct 2006 22:26:06 -0700 (PDT), Gary Gower wrote:
      
      >To trailer the 701 fuselage is better to have the fuselage kind of a "take
      >off" position. 
      >This is with the front wheel raised as little and tied up over a stool type
      >support in the trailer floor and also a tie in the tail hook.  Off course
      >with the main gears well tied and movement free.
      >This way the trailer not need to be too tall.  
      
      Very clever!  Do you happen to know how tall the fuselage is, in this
      "takeoff" position?
      
      >The wings will be safe in a hamoc type support to the side walls.  The
      >hamoc support we made it from strips of  carpets (samples from a carpet
      >store)  carefully passed betwen the wing and the slats.   The wings will
      >be movement free with straps to the wall.   the wall will  have strips of
      >foam and heavy cloth to protect the wings.
      
      Sounds like a good system.
      
      >This, of course is a two or three person task, for the volume of the parts,
      >not the weight.
      >
      >Hope this helps.
      >
      >Saludos
      >Gary Gower.
      
      Very helpful.  Thanks!
      
      Chris Wolf
      cwolf41@comcast.net
      
      
Message 9
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  | 
      
      
      
      Chuck,
           I would like to see a picture of your set-up and also can you 
      furnish me with the part number of the tow bar you got from AS&S.
      
      Bob Stone
        ----- Original Message ----- 
        From: Chuck & Lana Maggart 
        To: Zenith List 
        Sent: Sunday, October 15, 2006 2:35 PM
        Subject: Re: Zenith-List: Tow Bar
      
      
        Bob, I would not recommend "pushing on the tail" especially if you 
      have untrained helpers.  I have seen factory built aircraft damaged that 
      way and the Zodiac is lighter.  
      
        I bought a tow bar for a Piper Cherokee from AS&S and added a 4130 
      steel plate on the nose wheel fork.  The plate picks up the forward two 
      bolt holes in the fork and I drilled two holes in the plate to mate with 
      the tow bar.  It is the same setup used on Cherokees and Tri-Pacers.  I 
      am considering extending the tow bar about a foot to make it easier to 
      reach under the nose.
      
        Chuck Maggart, St. Louis
        XL in paint
      
      
Message 10
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  | 
      
      
| Subject:  | Re: Trailering The CH701 | 
      
      --> Zenith-List message posted by: "Dave Austin" <daveaustin2@can.rogers.com>
      
      Of course, with the aircraft in the takeoff position, at hiway speed there
      will be no weight on the trailer or its' wheels so it will tow rather
      easily..
      Dave Austin  601HDS - 912, Spitfire Mk VIII
      Do not archive
      
      
Message 11
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  | 
      
      
| Subject:  | Re: A special Zodiac XL 601 | 
      
      --> Zenith-List message posted by: LarryMcFarland <larry@macsmachine.com>
      
      
      Gig,
      5052-H38 aluminum is used for deep press container segments and it gets 
      more resistant during the work done on it.
      We're talking pots and cookware here.  In aircraft speak, other than a 
      fuel tank it's application would be limited. As it gets stressed, it
      work hardens.  Not a product I'd want to put into actual wing structure 
      as its elongation is less than half that of 2024-T3 and 6061-T6
      aluminum for aircraft structures.   Ultimate is approx 42K for all 
      three, but 5052-H38 has elongation of 7000 psi, where the 2024-T3 and
      6061-T6 have 17000 psi elongation properties.  This speaks to the 
      durability over long term for structural loading.
      I used 5052-H32 for my header and wing tanks, and at .040, it's a little 
      softer, but excellent for a fuel tank, welding, forming etc.
      
      Larry McFarland - 601HDS at www.macsmachine.com
      
      Gig Giacona wrote:
      
      >--> Zenith-List message posted by: "Gig Giacona" <wr.giacona@cox.net>
      >
      >I too am concerned with the change in metals. Quoting the are of the site that
      talks about budget. I get the following Google translation. Now I don't what
      the properties of those are but they weren't what the designer intended.
      >
      > 
      >  
      >
      >>The Kit made with plate 5052 - H38 has all the Stringers, of the wings, profundor
      and stabilizer made in aluminum 2024 T-3.
      >>2-S I can vender the Kit so that it has the project, in case that you I want
      I can buy, or you yourselves purchase for the Internet, costs 390 dollars, +,
      this gives to the guarantee to be in day with the designer and is demanded the
      Invoice in the hour of you to make the document of the airplane.
      >>    
      >>
      >
      >
      >--------
      >W.R. "Gig" Giacona
      >601XL Under Construction
      >See my progress at www.peoamerica.net/N601WR
      >
      >
      >  
      >
      
      
Message 12
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  | 
      
      
      
      --> Zenith-List message posted by: "george may" <gfmjr_20@hotmail.com>
      
      
      Well folks, this list has helped to launch another Zodiac.  On Saturday 
      morning at about 9:00AM, N221GM launched off for its first flight.  Sky was 
      crystal clear, winds calm, and the foliage of New England outstanding.  Take 
      off occurred after about a 450 foot run with a climbout at 85mph.  I'm using 
      a dynon system for EFIS and forgot to set it up with VSI, so my best guess 
      is that the climb was about 600-700fpm.  No attempt was made for a max 
      climb, just a relatively gently one.  I climbed to 2500ft, took a deep 
      breath, enjoyed the secenery for a couple of minutes and gently circled the 
      field checking out pitch, roll and yaw.  With everything in the green engine 
      wise the only issued appeared to be the need for continuous back pressure on 
      the elevator which could not be trimmed out.  Speed was 95-100mph
        Since the preflight plan was take off, climb to 2500, circle for control 
      checks and land,  it was time to start the drop back to pattern altitute for 
      landing.  I still had the need for significant back pressure on the stick.  
      Luckily as the speed dropped to 65-70mph the backpressure required also 
      dropped making the landing approach a lot less exciting than I thought at 
      first it might be. Knowing I had to continue to hold back stick , I extended 
      the downwind leg figuring it would give me more time for the final lineup.  
      All went well.  The zodiac is a really well behaved plane, and was very 
      stable through the base and final.  I came over the fence at 65mph and 
      settled right on the numbers. Full stop was in about 350feet
      
        All suggestions for fixes to alleviate the elevator backpressure are 
      appreciated.  Since the pressure varied with speed, I assume it is probably 
      a misalignment of incidence between the wing,fuse and/or stab.  I'll be 
      checking that out on Monday.
      
      Thanks to everyone on the list for your comments, suggestions and help  
      especially to list member Jeff Paris for the familiarization flight.
      
      George May
      Zodiac 601XL  912s
      N221GM
      
      _________________________________________________________________
      Try the new Live Search today!  
      http://imagine-windowslive.com/minisites/searchlaunch/?locale=en-us&FORM=WLMTAG
      
      
Message 13
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  | 
      
      
| Subject:  | Re: Trailering The CH701 | 
      
      --> Zenith-List message posted by: "Joe and Joan" <jnjkimbell@hotmail.com>
      
      Chris, 3 months ago I trailered my ch 701 on a trailer behind my Motorhome 
      from FL to CA and Back, so I have do have  experience and knowledge of your 
      desire.  I would rather not discuss this on the list as I do not like to be 
      ridiculed or put down.  Please  contact me by telephone or at my email 
      jnjkimbell@hotmail.com
      ----- Original Message ----- 
      From: "Chris Wolf" <cwolf41@comcast.net>
      Sent: Saturday, October 14, 2006 2:34 PM
      Subject: Zenith-List: Trailering The CH701
      
      
      > --> Zenith-List message posted by: Chris Wolf <cwolf41@comcast.net>
      >
      >
      > I'm interested in doing extended trailering of a Zenith 701.
      >
      > I've been flying for many years, and I'm currently part owner of a Cessna
      > 182.  I also own a recreational vehicle which I love to travel in, around
      > the country.  But what I would really enjoy, is an airplane that I could
      > tow on a trailer behind my RV, stopping and flying wherever the scenery
      > looks interesting.  RVs seem to be towing every other kind of recreational
      > vehicle, these days, so why not an airplane?
      >
      > Obviously such an aircraft would have to have folding wings, which is why
      > I've been looking at the Zenith 701.  I took the rudder building workshop
      > for the 701, and thoroughly enjoyed it.  I think I would enjoy building 
      > the
      > 701.  I also took a ride in the 701, and was quite impressed with its
      > performance.
      >
      > I've seen pictures at the Zenith web site of a 701 on trailers.  One plane
      > was even being towed behind an RV, so it looks like I'm not the first guy
      > to get the idea.
      >
      > But is the 701 really suited for extensive trailering?  That folding wing
      > design looks like it was more intended to reduce hangar space, rather than
      > designed for zooming down the highway at 70 mph.  Those folding wings
      > constitute a large, flat surface of metal, high in the air.  How much side
      > gusting of wind could the plane endure before it was damaged, or worse 
      > yet,
      > caused the trailer to flip over?
      >
      > It's my understanding that the folded wings are only secured by a single
      > pivot bolt at the front, and slots in a plywood saddle at the back.  Is
      > this really enough to secure the wings for extended highway travel?
      >
      > I talked to Michael Heintz at Quality Sport Planes, in Cloverdale,
      > California, last week, while I was taking the rudder building workshop. 
      > He
      > said for extended trailering, the best method would be to remove the wings
      > entirely, and strap them to the bed of the trailer.  Then trailering would
      > be fine.
      >
      > Does anyone have any experience with extended trailering of the 701?  If
      > so, I would sure like to talk to you!
      >
      > I like the 701 very much.  However I'm also looking at a Kolb Mark III
      > Xtra.  It seems like Kolb planes get trailered quite a bit, while the 701
      > does not.  Perhaps there is a good reason?  The Kolb factory says their
      > aircraft was designed for folding and trailering, and the folded plane 
      > does
      > seem to look more solid and compact than the 701.  I also like the fact
      > that the Kolb does not use a wet wing, so unlike the Zenith, there is no
      > need to drain the fuel before folding the wings.
      >
      > If anyone has any suggestions or advice on this topic, I'd sure appreciate
      > hearing from you.  Thanks!
      >
      > Chris Wolf
      > cwolf41@comcast.net
      >
      >
      > 
      
      
Message 14
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  | 
      
      
| Subject:  | Re: First Flight | 
      
      --> Zenith-List message posted by: LarryMcFarland <larry@macsmachine.com>
      
      
      George,
      Congratulations on your first flight.  The adventure has just begun!
      
      Larry McFarland
      do not archive
      
      george may wrote:
      
      > --> Zenith-List message posted by: "george may" <gfmjr_20@hotmail.com>
      >
      >
      > Well folks, this list has helped to launch another Zodiac.  On 
      > Saturday morning at about 9:00AM, N221GM launched off for its first 
      > flight.  Sky was crystal clear, winds calm, and the foliage of New 
      > England outstanding. 
      >
      >  All suggestions for fixes to alleviate the elevator backpressure are 
      > appreciated.  Since the pressure varied with speed, I assume it is 
      > probably a misalignment of incidence between the wing,fuse and/or 
      > stab.  I'll be checking that out on Monday.
      >
      > Thanks to everyone on the list for your comments, suggestions and 
      > help  especially to list member Jeff Paris for the familiarization 
      > flight.
      >
      > George May
      > Zodiac 601XL  912s
      > N221GM
      >
      >
      
      
Message 15
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  | 
      
      
| Subject:  | Wrong terms for aluminum properties....  | 
      
      --> Zenith-List message posted by: LarryMcFarland <larry@macsmachine.com>
      
      Whoops,
      I mentally transposed % of elongation in 2 inch samples to KPSI.  The 
      following should have read 7% and 17% elongation
      respectively.  Fingers got ahead of the brain, again.............
      
      5052-H38 aluminum is used for deep press container segments and it gets 
      more resistant during the work done on it.
      We're talking pots and cookware here.  In aircraft speak, other than a 
      fuel tank it's application would be limited. As it gets stressed, it
      work hardens.  Not a product I'd want to put into actual wing structure 
      as its elongation is less than half that of 2024-T3 and 6061-T6
      aluminum for aircraft structures.   Ultimate is approx 42K for all 
      three, but 5052-H38 has elongation of 7 %, where the 2024-T3 and
      6061-T6 have 17 % elongation properties.  This speaks to the durability 
      over long term for structural loading.
      I used 5052-H32 for my header and wing tanks, and at .040, it's a little 
      softer, but excellent for a fuel tank, welding, forming etc.
      
      Larry McFarland - 601HDS at www.macsmachine.com
      do not archive
      
      
Message 16
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  | 
      
      
| Subject:  | Re: First Flight | 
      
      --> Zenith-List message posted by: N5SL <nfivesl@yahoo.com>
      
      George I'm happy for you!  Congratulations!  Thanks for the detailed description
      of your first flight.  I felt like I was up there with you!  
      
      I've heard of a few guys adjusting their horiz. Stab for the same reason you stated
      below.  I'd get some details from the actual guys before taking any action.
      
      
      Congratulations again!  
      
      Scott Laughlin
      601XL/Corvair
      Engine testing
      
      ----- Original Message ----
      From: george may <gfmjr_20@HOTMAIL.COM>
      Sent: Sunday, October 15, 2006 5:58:46 PM
      Subject: Zenith-List: First Flight
      
      --> Zenith-List message posted by: "george may" <gfmjr_20@hotmail.com>
      
      
      Well folks, this list has helped to launch another Zodiac.  On Saturday 
      morning at about 9:00AM, N221GM launched off for its first flight.  
      
      
Message 17
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  | 
      
      
| Subject:  | splicing long 601xl wing parts | 
      
      --> Zenith-List message posted by: Maarten Versteeg <maarten.versteeg@swri.org>
      
      Hello List,
      
      I nearly finished building the tail from kit(s) and am
      enjoying the building very much. Now I am getting closer
      to starting on the main wing and am considering jumping
      in the deep end by building it from scratch.
      There are 3 very long 11-12 feet bend parts in the wind.
      I read in the list archive and 601.org that the rear spar
      channel 6W7-1 can be spliced from two 6 feet parts.
      Through my EAA counselor I can access a 8 feet brake so
      that should work. The main spar has two caps (top 6W3-6
      and bottom 6W3-7) that are almost as long. I didn't find
      any mention of these parts, can these parts just be split
      in two ~6 feet sections since they are attached to the
      main spar and the wing skin or is some splicing needed ?
      
      Regards,
      	Maarten: 601xl tail almost finished
      	San Antonio, Texas
      	
      -- 
      
      
Message 18
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  | 
      
      
| Subject:  | sheet aluminum source | 
      
      --> Zenith-List message posted by: Maarten Versteeg <maarten.versteeg@swri.org>
      
      Hello List,
      
      Up to now I have build the 601xl tail using the kits
      and am very satisfied with these, but it seems like a
      real challenge to build at least some part completely
      from scratch. I could easily order the large 6061-T6
      aluminum wing sheets from Aircraft Spruce together with
      all the other needed parts. I have three questions:
      - Do they also have the correct rivets and what would
      the AS order number for A4 and A5 be?
      - Did anyone count the number of rivets in the main
      wings ?
      - Any suggestions on other sources, easier, cheaper,
      more local for this order with the large 4 x 12 '
      sheets including some that can't be rolled ?
      
      Regards,
      	Maarten: 601xl tail almost finished
      	San Antonio, Texas
      	
      -- 
      
      
Message 19
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  | 
      
      
      
      I tried several methods to mount a tow bar and since I'm not putting on the  
      wheel farings I just bought a standard cessna tow bar from aircraft spruce and
      
       it fits over the end of the wheel axel bolts. Works great.
      Mike Sigman
      N7092N 601XL
      
      13-01540 DELUXE CESSNA TOWBAR      
                 
      
Message 20
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  | 
      
      
| Subject:  | Re: splicing long 601xl wing parts | 
      
      --> Zenith-List message posted by: David Barth <davids601xl@yahoo.com>
      
      Hi Maarten.
      Chris Heintz said we could butt the spar cap angles up
      to one another (not spliced as per the rear spar) as
      long as the break in continuity is located away from
      the termination point of the front spar caps to
      prevent stress concentrations in that area. My spar
      cap angles have their break about 1 foot outboard of
      the front spar cap termination point. HOpe that
      answers your question. 
      David 
      
      --- Maarten Versteeg <maarten.versteeg@swri.org>
      wrote:
      
      > --> Zenith-List message posted by: Maarten Versteeg
      > <maarten.versteeg@swri.org>
      > 
      > Hello List,
      > 
      > I nearly finished building the tail from kit(s) and
      > am
      > enjoying the building very much. Now I am getting
      > closer
      > to starting on the main wing and am considering
      > jumping
      > in the deep end by building it from scratch.
      > There are 3 very long 11-12 feet bend parts in the
      > wind.
      > I read in the list archive and 601.org that the rear
      > spar
      > channel 6W7-1 can be spliced from two 6 feet parts.
      > Through my EAA counselor I can access a 8 feet brake
      > so
      > that should work. The main spar has two caps (top
      > 6W3-6
      > and bottom 6W3-7) that are almost as long. I didn't
      > find
      > any mention of these parts, can these parts just be
      > split
      > in two ~6 feet sections since they are attached to
      > the
      > main spar and the wing skin or is some splicing
      > needed ?
      > 
      > Regards,
      > 	Maarten: 601xl tail almost finished
      > 	San Antonio, Texas
      >
      
      David Barth
      601 XL Plansbuilder  15% done?
      Working on Wings
      www.ch601.org
      
      __________________________________________________
      
      
Message 21
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  | 
      
      
| Subject:  | On-line info on making and using form blocks - the results | 
      
      Thanks for all the pointers and instruction on making and using form blocks.
      The results are attached.
      
      One might ask why I need two luggage shelf bulkheads. Well, the new one on
      the left is 5 mm wider than the old factory one on the right. Why 5 mm? That
      is long story that begins in 1999...
      
      -- Craig
      
Message 22
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  | 
      
      
| Subject:  | Re: splicing long 601xl wing parts | 
      
      --> Zenith-List message posted by: Paul Mulwitz <p.mulwitz@worldnet.att.net>
      
      Actually, I believe the angles on the main XL spar are around 12 feet 
      long.  I wouldn't splice them without designer approval.
      
      Paul
      XL fuselage
      
      At 04:41 PM 10/15/2006, you wrote:
      >--> Zenith-List message posted by: Maarten Versteeg 
      ><maarten.versteeg@swri.org>
      >
      >Hello List,
      >
      >I nearly finished building the tail from kit(s) and am
      >enjoying the building very much. Now I am getting closer
      >to starting on the main wing and am considering jumping
      >in the deep end by building it from scratch.
      >There are 3 very long 11-12 feet bend parts in the wind.
      >I read in the list archive and 601.org that the rear spar
      >channel 6W7-1 can be spliced from two 6 feet parts.
      >Through my EAA counselor I can access a 8 feet brake so
      >that should work. The main spar has two caps (top 6W3-6
      >and bottom 6W3-7) that are almost as long. I didn't find
      >any mention of these parts, can these parts just be split
      >in two ~6 feet sections since they are attached to the
      >main spar and the wing skin or is some splicing needed ?
      >
      >Regards,
      >         Maarten: 601xl tail almost finished
      >         San Antonio, Texas
      >
      >--
      >
      
      
Message 23
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  | 
      
      
| Subject:  | Re: sheet aluminum source | 
      
      --> Zenith-List message posted by: Paul Mulwitz <p.mulwitz@worldnet.att.net>
      
      Hi Maarten,
      
      I like your idea of making the wing skins from scratch.  I used ones 
      from the kit and had problems with the holes drilled at ZAC.  They 
      didn't match my rib structure.  You will face an interesting 
      challenge when it comes to bending the nose skin.  It should be 
      easier, though, than the spar cap angles.
      
      On the rivets, I think you would do best to order them from 
      ZAC.  They perform special qualification tests on them to get ones 
      better than the manufacturer guarantees.  They also know how many to 
      supply for the wings since that is what they put in the kits.  I 
      don't think Aircraft Spruce has anything close.
      
      One thing you might consider is ordering the completed spars from ZAC 
      (they actually get them from Zenair) and building the rest 
      yourself.  If you add in the nose skin and rear channel then you 
      won't have any long bending to do.  The fiberglass wing tips are 
      another candidate for ordering from ZAC.  The ones they supply are 
      difficult to fit, but it might be easier than laying up your own fiberglass.
      
      If you order the center wing section along with the spars, then they 
      will probably fit them together with the proper dihedral angle 
      (certainly if you ask).
      
      Paul
      XL fuselage
      
      
      At 04:52 PM 10/15/2006, you wrote:
      >--> Zenith-List message posted by: Maarten Versteeg 
      ><maarten.versteeg@swri.org>
      >
      >Hello List,
      >
      >Up to now I have build the 601xl tail using the kits
      >and am very satisfied with these, but it seems like a
      >real challenge to build at least some part completely
      >from scratch. I could easily order the large 6061-T6
      >aluminum wing sheets from Aircraft Spruce together with
      >all the other needed parts. I have three questions:
      >- Do they also have the correct rivets and what would
      >the AS order number for A4 and A5 be?
      >- Did anyone count the number of rivets in the main
      >wings ?
      >- Any suggestions on other sources, easier, cheaper,
      >more local for this order with the large 4 x 12 '
      >sheets including some that can't be rolled ?
      >
      >Regards,
      >         Maarten: 601xl tail almost finished
      >         San Antonio, Texas
      >
      >--
      >
      >
      
      
Message 24
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  | 
      
      
      
      For the life of me I can't figure out why some people think that  
      pulling a plane from the prop hub is a bad thing. After all, this is  
      where all the loads are from the prop during flight anyhow!!!
      
      I am however very careful to only grab the root of a blade when I  
      push/pull. I've made 2 tow-bars for my 601 so far and my second  
      attempt worked out much better since it's articulated. Total cost of  
      the parts was about $13 CND and 2 hours of cutting/welding and I'd  
      highly recommend making one since it makes directing the plane much  
      easier. Of course this is a nose gear plane so tail draggers will  
      have to figure out a tail wheel bar. Should be easy if you Google  
      some RV stuff.
      
      I'll try and post some pictures next time I go out to the hangar.
      
      Trev Page
      C-IDUS 601HD R912
      
      
Message 25
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  | 
      
      
| Subject:  | 601XL Nose Wheel axle assembly ? | 
      
      --> Zenith-List message posted by: "Robin Bellach" <601zv@ritternet.com>
      
      I don't understand how to properly fit/shim the front axle to achieve proper 
      spacing and tension on the wheel bearings. My wheel fork is 152mm wide 
      outside, 142mm inside. The wheel width overall at the bearings is about 75mm 
      and adding 62mm for the spacers = 137mm. That leaves about 5mm of slack. The 
      kit includes 2 AN960-1216 washers that I thought would go on the outside 
      under the castle nuts. Should these actually be on the inside of the fork to 
      take up that 5mm of slack, or should they be on the outside with and 
      additional pair on the inside? (I notice that 2 AN960-1216's total about 5mm 
      thick so seems would be about right.) How does one properly shim the 
      bearings and tighten the axle nuts to get the right tension on the wheel 
      bearings?
      
          Robin, confused in AR
          N601ZV Zen-Vair 
      
      
Message 26
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  | 
      
      
      
      
Message 27
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  | 
      
      
| Subject:  | Re: First Flight | 
      
      A big congrats to you. The smile you have will last for weeks..
      do not archive
      
      
      Ben Haas
      N801BH
      www.haaspowerair.com
      
      -- "george may" <gfmjr_20@HOTMAIL.COM> wrote:
      --> Zenith-List message posted by: "george may" <gfmjr_20@hotmail.com>
      
      
      Well folks, this list has helped to launch another Zodiac.  On Saturday 
      
      
      morning at about 9:00AM, N221GM launched off for its first flight.  Sky 
      was 
      
      crystal clear, winds calm, and the foliage of New England outstanding.  
      Take 
      
      off occurred after about a 450 foot run with a climbout at 85mph.  I'm u
      sing 
      
      a dynon system for EFIS and forgot to set it up with VSI, so my best gue
      ss 
      
      is that the climb was about 600-700fpm.  No attempt was made for a max 
      
      climb, just a relatively gently one.  I climbed to 2500ft, took a deep 
      
      breath, enjoyed the secenery for a couple of minutes and gently circled 
      the 
      
      field checking out pitch, roll and yaw.  With everything in the green en
      gine 
      
      wise the only issued appeared to be the need for continuous back pressur
      e on 
      
      the elevator which could not be trimmed out.  Speed was 95-100mph
        Since the preflight plan was take off, climb to 2500, circle for contr
      ol 
      
      checks and land,  it was time to start the drop back to pattern altitute
       for 
      
      landing.  I still had the need for significant back pressure on the stic
      k.  
      
      Luckily as the speed dropped to 65-70mph the backpressure required also 
      
      
      dropped making the landing approach a lot less exciting than I thought a
      t 
      
      first it might be. Knowing I had to continue to hold back stick , I exte
      nded 
      
      the downwind leg figuring it would give me more time for the final lineu
      p.  
      
      All went well.  The zodiac is a really well behaved plane, and was very 
      
      
      stable through the base and final.  I came over the fence at 65mph and 
      
      settled right on the numbers. Full stop was in about 350feet
      
        All suggestions for fixes to alleviate the elevator backpressure are 
      
      appreciated.  Since the pressure varied with speed, I assume it is proba
      bly 
      
      a misalignment of incidence between the wing,fuse and/or stab.  I'll be 
      
      
      checking that out on Monday.
      
      Thanks to everyone on the list for your comments, suggestions and help  
      
      
      especially to list member Jeff Paris for the familiarization flight.
      
      George May
      Zodiac 601XL  912s
      N221GM
      
      _________________________________________________________________
      Try the new Live Search today!  
      
      http://imagine-windowslive.com/minisites/searchlaunch/?locale=en-us&FO
      RM=WLMTAG
      
      
      ========================
      ===========
      ========================
      ===========
      ========================
      ===========
      ========================
      ===========
      ========================
      ===========
      
      
      <html><P>A big congrats to you. The smile you have will last for weeks..
      </P>
      <P>do not archive<BR><BR><BR>Ben Haas<BR>N801BH<BR>www.haaspowerair
      .com<BR><BR>-- "george may" <gfmjr_20@HOTMAIL.COM>&
      nbsp;wrote:<BR>--> Zenith-List message posted by:
       "george may" <gfmjr_20@hotmail.com><BR><BR><BR>Wel
      l folks, this list has helped to laun
      ch another Zodiac.  On Saturday <BR>mornin
      g at about 9:00AM, N221GM launched off&nbs
      p;for its first flight.  Sky was <BR>
      crystal clear, winds calm, and the foliage
       of New England outstanding.  Take <B
      R>off occurred after about a 450 foot 
      ;run with a climbout at 85mph.  I'm&n
      bsp;using <BR>a dynon system for EFIS and&
      nbsp;forgot to set it up with VSI, so
       my best guess <BR>is that the climb&
      nbsp;was about 600-700fpm.  No attempt was
       made for a max <BR>climb, just a&nbs
      p;relatively gently one.  I climbed to&nbs
      p;2500ft, took a deep <BR>breath, enjoyed 
      the secenery for a couple of minutes 
      and gently circled the <BR>field checking 
      out pitch, roll and yaw.  With everyt
      hing in the green engine <BR>wise the 
      ;only issued appeared to be the need 
      for continuous back pressure on <BR>the el
      evator which could not be trimmed out.&nbs
      p; Speed was 95-100mph<BR>  Since the 
      ;preflight plan was take off, climb to&nbs
      p;2500, circle for control <BR>checks and 
      land,  it was time to start the 
      drop back to pattern altitute for <BR>land
      ing.  I still had the need for s
      ignificant back pressure on the stick. &nb
      sp;<BR>Luckily as the speed dropped to 65-
      70mph the backpressure required also <BR>droppe
      d making the landing approach a lot l
      ess exciting than I thought at <BR>first&n
      bsp;it might be. Knowing I had to con
      tinue to hold back stick , I extended
       <BR>the downwind leg figuring it would&nb
      sp;give me more time for the final li
      neup.  <BR>All went well.  The zodiac
       is a really well behaved plane, and&
      nbsp;was very <BR>stable through the base 
      and final.  I came over the fence&nbs
      p;at 65mph and <BR>settled right on the&nb
      sp;numbers. Full stop was in about 350feet
      <BR><BR>  All suggestions for fixes to&nbs
      p;alleviate the elevator backpressure are <BR>a
      ppreciated.  Since the pressure varied wit
      h speed, I assume it is probably <BR>
      a misalignment of incidence between the wi
      ng,fuse and/or stab.  I'll be <BR>checking
       that out on Monday.<BR><BR>Thanks to ever
      yone on the list for your comments, s
      uggestions and help  <BR>especially to lis
      t member Jeff Paris for the familiarizatio
      n flight.<BR><BR>George May<BR>Zodiac 601XL  91
      2s<BR>N221GM<BR><BR>____________________________________________________
      _____________<BR>Try the new Live Search today!
        <BR>http://imagine-windowslive.com/minisites/searchlaunch/?l
      ========================
      ========================
      nbsp;Use the Matronics List Features Navigator&
      Archive Search & Download, 7-Day Browse,&nb
      ========================
      =           &nb
      sp;  - NEW MATRONICS WEB FORUMS -<BR>
      ========================
      ========================
          - NEW MATRONICS LIST WIKI&nb
      ========================
      =           &nb
        Thank you for your generous support
      bsp;           &n
      bsp;       -Matt Dralle, Li
      ========================
      ====================<BR><BR><BR>
      <BR></P>
      
      
      <pre><b><font size=2 color="#000000" face="courier new,courier">
      
      
      </b></font></pre></body></html>
      
Message 28
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  | 
      
      
| Subject:  | Re: First Flight | 
      
      Great news George - congratulations.  I look forward to coming for a visit.
      
      Michael
      
      On 10/15/06, george may <gfmjr_20@hotmail.com> wrote:
      >
      > --> Zenith-List message posted by: "george may" <gfmjr_20@hotmail.com>
      >
      >
      > Well folks, this list has helped to launch another Zodiac.  On Saturday
      > morning at about 9:00AM, N221GM launched off for its first flight.  Sky
      > was
      > crystal clear, winds calm, and the foliage of New England
      > outstanding.  Take
      > off occurred after about a 450 foot run with a climbout at 85mph.  I'm
      > using
      > a dynon system for EFIS and forgot to set it up with VSI, so my best guess
      > is that the climb was about 600-700fpm.  No attempt was made for a max
      > climb, just a relatively gently one.  I climbed to 2500ft, took a deep
      > breath, enjoyed the secenery for a couple of minutes and gently circled
      > the
      > field checking out pitch, roll and yaw.  With everything in the green
      > engine
      > wise the only issued appeared to be the need for continuous back pressure
      > on
      > the elevator which could not be trimmed out.  Speed was 95-100mph
      >   Since the preflight plan was take off, climb to 2500, circle for control
      > checks and land,  it was time to start the drop back to pattern altitute
      > for
      > landing.  I still had the need for significant back pressure on the stick.
      > Luckily as the speed dropped to 65-70mph the backpressure required also
      > dropped making the landing approach a lot less exciting than I thought at
      > first it might be. Knowing I had to continue to hold back stick , I
      > extended
      > the downwind leg figuring it would give me more time for the final lineup.
      > All went well.  The zodiac is a really well behaved plane, and was very
      > stable through the base and final.  I came over the fence at 65mph and
      > settled right on the numbers. Full stop was in about 350feet
      >
      >   All suggestions for fixes to alleviate the elevator backpressure are
      > appreciated.  Since the pressure varied with speed, I assume it is
      > probably
      > a misalignment of incidence between the wing,fuse and/or stab.  I'll be
      > checking that out on Monday.
      >
      > Thanks to everyone on the list for your comments, suggestions and help
      > especially to list member Jeff Paris for the familiarization flight.
      >
      > George May
      > Zodiac 601XL  912s
      > N221GM
      >
      > _________________________________________________________________
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Message 29
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| Subject:  | Re: Trailering The CH701 | 
      
      Robert,
      CH 600. It will be ready to fly in a few weeks. I have the registration and
      am finishing a re-paint on instrument panel before scheduling the DAR. Hope
      to fly in Nov/Dec. Will send pictures  to everyone soon.
      -
      Semper Fi,
      Steven R. Hulland
      CH 600 Taildragger
      Amado, AZ
      
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Message 30
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| Subject:  | Re: Trailering The CH701 | 
      
      Hello Chris,
      
      Dont remeber right now how tall was...  But with the propeller in  a "Y" position,
      the rudder was just a little higher than the propeller.    A almost "normal"
      height enclosed trailer can be made.   
      
      Saludos
      Gary Gower
      do not archive.
      
      Chris Wolf <cwolf41@comcast.net> wrote: --> Zenith-List message posted by: Chris
      Wolf 
      
      On Sat, 14 Oct 2006 22:26:06 -0700 (PDT), Gary Gower wrote:
      
      >To trailer the 701 fuselage is better to have the fuselage kind of a "take
      >off" position. 
      >This is with the front wheel raised as little and tied up over a stool type
      >support in the trailer floor and also a tie in the tail hook.  Off course
      >with the main gears well tied and movement free.
      >This way the trailer not need to be too tall.  
      
      Very clever!  Do you happen to know how tall the fuselage is, in this
      "takeoff" position?
      
      >The wings will be safe in a hamoc type support to the side walls.  The
      >hamoc support we made it from strips of  carpets (samples from a carpet
      >store)  carefully passed betwen the wing and the slats.   The wings will
      >be movement free with straps to the wall.   the wall will  have strips of
      >foam and heavy cloth to protect the wings.
      
      Sounds like a good system.
      
      >This, of course is a two or three person task, for the volume of the parts,
      >not the weight.
      >
      >Hope this helps.
      >
      >Saludos
      >Gary Gower.
      
      Very helpful.  Thanks!
      
      Chris Wolf
      cwolf41@comcast.net
      
      
       		
      ---------------------------------
      
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