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mfryer

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Everything posted by mfryer

  1. For what aircraft? Featherlite can supply you with the strut. Most of the other major parts are available at http://www.eznoselift.com/pricelist.html
  2. Another option would be to use an electric actuator.
  3. Interesting. The ACS site says they have aluminium fittings also, but mine are steel. I purchased mine about a year and a half ago.
  4. I have two of the ACS belts for my long-ez project and the fittings are definatly steel.
  5. Well, I didn't complete the spar by new years. But it is done now.. The Long-EZ plans now call for the spar to be permenantly installed in the fuselage. I think however that I will hold off on that for now. With the spar and canard installed, my EZ takes up a huge amount of space in the shop. Instead I am considering skipping ahead and constructing the wings. With those out of the way I think I will cut down the size of the work table. Also I see some cozy and other long-ez folks are aligning the wings to the center spar before mounting it to the fuse. Any thoughts on this strategy? more photos at... http://flyingbackward.blogspot.com
  6. I saw this the other day. Looks interesting but may require some modification. http://cgi.ebay.com/NEW-ESSEX-AIRCRAFT-CONTROL-STICK-GRIP-COMPONENT_W0QQitemZ230422786816QQcmdZViewItemQQptZLH_DefaultDomain_0?hash=item35a644b300#ht_3890wt_722
  7. I beleve there is a scale .PDF of the templates in one of the threads
  8. mfryer

    Progress

    Marc, I hope you plan on having some redundancy. I am not sure what options are available for an auto confersion, but if you have a separate electrical systems for the ignition you would'nt nessisarily become a glider.
  9. That books looks like it about covers everything. Thanks
  10. Can any of you recomend some good books, or online resources that I can use to study aircraft engines?
  11. mfryer

    Day # 1

    In one of the cp issues, they discuss the temporary unavailibility of the 250 lb 1/4" foam. They did approve 1/4" plywood as a substitute.
  12. Prime rib here. And for the rest of us, a happy Festivus!!
  13. RAF used a few different techniques for spar cap layups, including the use of their uni cloth in the GU canard. At the time of the video, many techniques were still being perfected. I too was a little confused when I saw Burt and Mike laying up the spar cap with the cross weave. My understanding is that the spar cap material is designed to be used without the cross weave. The cross weave does not allow the uni fibers to lay as straight as they can be with the weave in place. If one examines the weave, it is very irregular and obviously only there to keep the roving in place until installation. The most latest RAF documentation (perhaps there is a CP article as well that I missed) that I can find is the Special performance canard (Roncz canard) instructions, that specifically mentions the removal of the "fine thread that is obviously not fiberglass" and the cross fibers. Perhaps there is a reason that fine thread is red. The procedure to remove the cross thread is not difficult and I cannot think of any reason to keep the cross fibers in place for spar cap layups. Spar jig: Good to know if found a new home, it would have been chopped up if you didn't take it. Be sure to measure everything again, I just want to make sure mine is the only plane flying crooked!
  14. I guess that makes sense. I usualy mix in small amounts as well, use it up in under 1/2 hour. I suppose what had me concerned is the time it takes to complete a large layup. My center section spar shear web took me over 5 hours to complete, what with phone ringing, santa and fire department stopping by, etc. But then you say "gel time", not "cure time". That there lies the fallicy of my origional comment. Marc, sounds like you are on to something with the local suppliers. I don't suppose you can russle up a cheap O-320 for me while your at it?
  15. It's been a little too cold here until just lately, so progress has been slow. Its been a tad warmer over the last few day so I managed to complete the center section spar shear web last evening. More photos of my center section spar progress are at: http://flyingbackward.blogspot.com
  16. For a large layup 3 hours is not a lot of time at all. It took me 5 hours to complete my center section spar sheer web. I don't think it would be very fun to have to hurry a large layup like that.
  17. mfryer

    Roncz Canard

    The "Special Performace Canard" (roncz) plans are included in the RAF Aircraft Encyclopedia (TERF) CDs. However the plans are not to scale. The TERF CDs are not free, they can be purchased from the terf website or search long-ez on eBay.
  18. This may be a stretch, but the Varieze origionaly had a VW engine. Update: after a little web searching that probably is not the answer....
  19. My bro picked up the aluminium angle from Alaska copper and brass for my landing gear brackets. Later he returned to find some 2024 stock and they didn't carry it, perhaps there stock fluctuates.
  20. The metals supplier I discovered is "Metal Supermarkets". They are located in Kent, Lakewood and Portland. www.metalsupermarkets.com
  21. I contacted Tacoma Screw, and they can supply AN hardware, but at about twice the cost of ACS and Wicks. You may have better luck with the salesman than me though. If you total up the cost of the AN hardware vs, other sources you probably will not save enough $$ to justify the time spent on this site justifying it . I did find a contact for 2024 aluminum and steel in Peirce and King county. The sales rep didn't think they could necessarily beat ACS prices but with shipping and time a factor they may be a good source. The sales rep also told me that they had a good contacts for small project machining. I will try and remember to bring the info home tomorrow. Also, one of the things that I find myselft wasting $$ on is shipping cost, particularly epoxy. The hazardous materials fee can really add up. Try ordering in larger quantities of foam, glass and epoxy where possible.
  22. Marc, are you considering starting you own project?
  23. Thanks for all of the input. I will not be inalling retracts and I plan to build my my spar as per the plans. I am using EZ-Poxy throughout my build, so I assume that there will be no inconpqtibiliy issuse with avgas.
  24. Materials arrive tomorrow for my center section spar. I have been combing through the CPs again and I think I have found all the updates. If anyone has any words of wisdom to share before I dive in, please let me know.
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