Zenith-Archive.digest.vol-cb

January 22, 2001 - February 20, 2001



      I
      > locate the strobe power packs; on the spar, on an internal rib, on the
      > inside of the tip rib?
      > Regards,
      > Roger Tunsley
      > CH601HDS
      > www.casterbridge.com
      >
      >
      
      
      
________________________________________________________________________________
From: "Chuck Deiterich" <cfd(at)tstar.net>
Subject: Re: Kit Planes on Discovery
Date: Jan 22, 2001
Its also on the Dish Network Satellite for regular TV's. ----- Original Message ----- From: P. Owens <powens(at)inwave.com> Sent: Monday, January 22, 2001 2:11 PM Subject: Zenith-List: Kit Planes on Discovery > > Dear Friends, > I was interested in this program also but it was not listed in my > area either, so I went to the web site and discovered the WINGS > DISCOVERY channel is DIGITAL ONLY! So I guess if we want to see it we > either have to get digital service or write a lot of letters to the > Discovery channel telling them we want to see it on the regular > channel. How about it guys, do we want to see the program on regular > tv? If so we need a write in campaign. > Phil Owens > CH-801 N84349 Builder > > > > > > > ________________________________________________________________________________
From: SkyKingN(at)aol.com
Date: Jan 23, 2001
Subject: Re: Zenith-List Digest: 6 Msgs - 01/20/01
Placed power supply at wing tip, saved running all the harnesses back through to cabin, also, keeps the sending unit away from the radios. Use sheilded wire for returns to panels ,feed source. keep the work simple, will be flying sooner. regards, sky. ________________________________________________________________________________
From: "Chuck Deiterich" <cfd(at)tstar.net>
Subject: Re: Zenith-List Digest: 6 Msgs - 01/20/01
Date: Jan 23, 2001
And if you use anchor nuts on the fiber glass wing tips you can get to the power supplies with out drilling rivets. ----- Original Message ----- From: <SkyKingN(at)aol.com> Sent: Tuesday, January 23, 2001 12:21 AM Subject: Re: Zenith-List: Re: Zenith-List Digest: 6 Msgs - 01/20/01 > > Placed power supply at wing tip, saved running all the harnesses back through > to cabin, also, keeps the sending unit away from the radios. Use sheilded > wire for returns to panels ,feed source. keep the work simple, will be flying > sooner. regards, sky. > > ________________________________________________________________________________
From: "Ivan Rosales" <ingenieros(at)netservice.com.mx>
Subject: gear slides
Date: Jan 23, 2001
Hi guys: I think this was discussed before but couldn't find it in the archives. I'm in the process of drilling the center wing bottom skin to the rear ribs. The draft manual says that you have to clamp a 3/4 " tube between the gear slides to get the proper distance between them but if a do so the 6L3-1 that has to go between the slides will not fit. Seems like the part 6L3-1 was made from .5 to 1 mm too narrow. Should I file the gear slides? Has anyone encountered a similar problem? Thanks in advance. Ivan Rosales 601 HD From Kit Mexico City ________________________________________________________________________________
Date: Jan 23, 2001
From: Douglas Corarito <dougc(at)infoequipt.com>
Subject: Discovery Wings Channel Zenith Show Videotaped!
Hi everyone, I have the show on VHS. I'm too lazy to disconnect/reconnect both my VCRs to make a dupe. Keeping with the lazy theme, I didn't edit out the commercials either, so have that finger on the FF button of your remote. Why is it that I pay extra for Discovery Wings and I'm forced to sit through a myriad of commercials? Seesh! If you'd like to barrow my copy for your own personal viewing :-) let me know. Please contact me directly at : dougc(at)infoequipt.com and we'll make arrangements. -- mailto:dougc(at)INFOequipt.com http://www.infoequipt.com ________________________________________________________________________________
Date: Jan 23, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: gear slides
I took off the tube from a gear leg and used it to gauge the separation of the slides. I installed the top L stiffeners as prescribed. Then, I riveted a temporary piece of aluminium to the bottom of the slides (I saw that trick on someonelse's web site) to make the spacing fixed. It worked well. Michel --- Ivan Rosales wrote: > > > Hi guys: > I think this was discussed before but couldn't find > it in the archives. > I'm in the process of drilling the center wing > bottom skin to the rear ribs. > The draft manual says that you have to clamp a 3/4 " > tube between the gear > slides to get the proper distance between them but > if a do so the 6L3-1 that > has to go between the slides will not fit. Seems > like the part 6L3-1 was > made from .5 to 1 mm too narrow. Should I file the > gear slides? Has anyone > encountered a similar problem? Thanks in advance. > Ivan Rosales > 601 HD From Kit > Mexico City ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Yahoo! Auctions - Buy the things you want at great prices. http://auctions.yahoo.com/ ________________________________________________________________________________
From: "fhulen" <fhulen(at)gabs.net>
Subject: Fogging canopy
Date: Jan 23, 2001
In Bill's recent "I did it" posting about his first flight, he mentions that his canopy fogged up, and that he turned on the exhaust fan and it cleared right up. In one of the aviation magazines that I receive it listed a "Top 12 things" checklist of things that they thought should be included in every instrument panel design. A "defrost vent" on the front screen was on that list. This brings forth a question that I had been meaning to post. Do any of you have this, what's your experience, and of those of you that don't have this vent, have you run into times when the front canopy fogged up to a point that you needed or wished that you had this mentioned vent? Thanks Fred Getting close to hanging the 3300 engine.... ________________________________________________________________________________
From: Newdude(at)aol.com
Date: Jan 23, 2001
Subject: Re: 601HDS KIT FOR SALE
where are you located??? ________________________________________________________________________________
From: "Vince Veltri" <Vijan(at)home.com>
Subject: Re: 601HDS KIT FOR SALE
Date: Jan 23, 2001
Sarasota, FL ----- Original Message ----- From: <Newdude(at)aol.com> Sent: Tuesday, January 23, 2001 9:17 PM Subject: Re: Zenith-List: 601HDS KIT FOR SALE > > where are you located??? > > > > > > ________________________________________________________________________________
From: "Barry Mayne" <bazmay(at)ozemail.com.au>
Subject: Re: Fogging canopy
Date: Jan 24, 2001
G'day Fred, No I don't have a demisting vent for the screen and don't really know if it's needed. The bubble gets a lot of handprints and other stuff on it and I clean it pretty often. I use an anti static cleaning solution which stops dust clinging to the canopy and also has the added advantage of eliminating fogging. Take it for what it's worth. Barry Mayne HDS Jabiru 3300 ----- Original Message ----- From: fhulen <fhulen(at)gabs.net> Sent: Wednesday, January 24, 2001 1:18 PM Subject: Zenith-List: Fogging canopy > > In Bill's recent "I did it" posting about his first flight, he mentions that > his canopy fogged up, and that he turned on the exhaust fan and it cleared > right up. In one of the aviation magazines that I receive it listed a "Top > 12 things" checklist of things that they thought should be included in every > instrument panel design. A "defrost vent" on the front screen was on that > list. This brings forth a question that I had been meaning to post. Do any > of you have this, what's your experience, and of those of you that don't > have this vent, have you run into times when the front canopy fogged up to a > point that you needed or wished that you had this mentioned vent? > Thanks > Fred Getting close to hanging the 3300 engine.... > > ________________________________________________________________________________
Date: Jan 23, 2001
From: Carlos Sa <wings1(at)videotron.ca>
Subject: Re: Fogging canopy
Hello, Fred I had an experience just this weekend that relates to your question. It was a Cessna 152, not a Zodiac, but I think it applies. Temperature was -10 C. I flew with my wife - my first passenger, her first flight in a small A/C. We took our time getting prepared, adjusting the seats, getting the map in position, etc. When I started taxiing, the windshield was not only fogged, but frosted. It was not too difficult to clear it, and after a few minutes with the engine running, it got completely clear. The 152 has a small air vent next to the windshield. Could be much bigger, but it works. I believe the same would have happened in a 601. Bottom line: I'll definitely have a defrost vent in my 601. Cheers Carlos > In Bill's recent "I did it" posting about his first flight, he mentions that > his canopy fogged up, and that he turned on the exhaust fan and it cleared > right up. In one of the aviation magazines that I receive it listed a "Top > 12 things" checklist of things that they thought should be included in every > instrument panel design. A "defrost vent" on the front screen was on that > list. This brings forth a question that I had been meaning to post. Do any > of you have this, what's your experience, and of those of you that don't > have this vent, have you run into times when the front canopy fogged up to a > point that you needed or wished that you had this mentioned vent? > Thanks > Fred Getting close to hanging the 3300 engine.... ________________________________________________________________________________
Date: Jan 23, 2001
From: Mike Fothergill <mfothergill(at)sympatico.ca>
Subject: Re: Fogging canopy
Fred; I installed the exhaust fan on the bulkhead at the rear of the baggage shelf to coolthings off in summer but found that it defogged the canoy in winter very well. It is a 12 volt computer type fan. Mike fhulen wrote: > > > In Bill's recent "I did it" posting about his first flight, he mentions that > his canopy fogged up, and that he turned on the exhaust fan and it cleared > right up. In one of the aviation magazines that I receive it listed a "Top > 12 things" checklist of things that they thought should be included in every > instrument panel design. A "defrost vent" on the front screen was on that > list. This brings forth a question that I had been meaning to post. Do any > of you have this, what's your experience, and of those of you that don't > have this vent, have you run into times when the front canopy fogged up to a > point that you needed or wished that you had this mentioned vent? > Thanks > Fred Getting close to hanging the 3300 engine.... > ________________________________________________________________________________
From: "Mell" <kitplane(at)tradezone.com>
, ,
Subject: First Flight Profile
Date: Jan 23, 2001
Hi, When it was time for the first flight of our Glasair III, we were lucky enough to have the assistance of a NAASA test pilot. We came up with a first flight profile check list that some of you may be able to adapt to your first flight. Hope it helps. You can find it at this link. http://www.kitplaneforum.com/ubb/Forum29/HTML/000001.html Trip Mellinger Glasair III N196G ________________________________________________________________________________
From: "Randy L. Thwing" <n4546v(at)mindspring.com>
Subject: 701 Plans corrections, corrections?
Date: Jan 23, 2001
701 Listers: After a long lull, I am trying to get started again on my 701 plans built project. The first thing I did was dowloaded the 13 pages, 227 paragraphs of manual and plans corrections from the ZA site. I am up to the point of laying out the rear fuselage so I reviewed the corrections pertaining to pages 7F00 through 7F3 and found what I believe to be errors as follows: Par. 109: "Side Channels 7F5-3" should be 7F5-2 Par. 110: "8C5-3" should be 7C5-3 Par. 113: "line AA" should be AE I need help confirming the following: Par. 119, the first two sentences say: "7F3 Note: the distance from A to B is 3050 measured along the EDGE OF THE SKIN. In the kit these distances are set along the aircraft center line". I just don't see how the above is possible, the rear top skin layout (7F2-1) is with a 3050 centerline measurement between points AB plus a 20 mm overhang for a total of 3070 as shown on the plans, as the top sheet edges are obviously a longer run than the centerline, there is no way the sheet side measurements can be "3050". Shouldn't the layout of the rear fuselage, as shown at the top of 7F3, be done from the centerline of the top skin and transfered to the side skins, Brought down perpendicular to line AE on the side skins, and the measurements shown at the bottom of the side skins, between points CD are approximations only (as the last three aft measurements are noted). What am I missing here? Regards, Randy L. Thwing, 701 plans ________________________________________________________________________________
From: "Robert Loer" <rloer(at)mighty.net>
Subject: CH 701 plans for sale
Date: Jan 24, 2001
Check them out at: http://www.barnstormers2000.com/show_ads.asp?CategoryPlans%2DBuilt&MainCatExperimental&startwith0&first1 also aluminum for wings, .020 not .016. rloer(at)mighty.net ________________________________________________________________________________
Date: Jan 24, 2001
From: brentbattles(at)pipeline.com (Brent Battles)
Subject: Re: Fogging canopy
I'm reminded of Chris Heintz' poor-man's air conditioning option - a #2 pencil slipped under the front canopy seal. Seems like this would work well for defrosting too. Brent Battles N16BZ 64 Hrs 185 Landings ________________________________________________________________________________
From: "Chuck Deiterich" <cfd(at)tstar.net>
Subject: Re: JABIRU ENGINES
Date: Jan 24, 2001
Ashley, I am building a Zenith 701 and already have the Jabiru 2200 motor mount. Out of curiosity what does the FF (without mount but with a 2200 nose bowl) kit for the 701 cost and what would the shipping costs be for it and later an engine. Thanks, C. Deiterich Bertram, TX 78605 USA ----- Original Message ----- From: Ashley & Margaret Johnston <Jabiru.nz(at)xtra.co.nz> Sent: Wednesday, November 22, 2000 2:41 PM Subject: Zenith-List: JABIRU ENGINES > > Members, > > It is firstly a home builder and sport flyer that I am writing to your group > with some information many may find interesting. > I have been privileged to represent Jabiru Pty Ltd in New Zealand since > bringing the first Jabiru Aircraft here almost six years ago. Presently > Jabiru Engines are available and landed at most world Custom Clearance > Airports at:- > > 2200 cc 80 hp @ $6400 US > 3300 cc 120 hp @ $9450 US > > All Engines are shipped fully insured and fitted complete with:- > Oil Cooler > Full exhaust system including in Cowl muffler > Starter and Starter Solenoid > Alternator and Voltage Regulator > VDO Oil Pressure Sender > VDO Oil Temperature Sender > > Zenair FF Kits are available for 601(with Cowls for both Engines) > Zenair FF Kits are also avaibable for 701 (no Cowls) > > Kindest regards > > Ashley Johnston > > Jabiru New Zealand (064) 3 302 7197 > > ________________________________________________________________________________
Date: Jan 25, 2001
From: Peter Chapman <pchapman(at)ionsys.com>
Subject: Re: Fogging canopy
At 09:18 PM 23-01-2001 , you wrote: >instrument panel design. A "defrost vent" on the front screen was on that >list. This brings forth a question that I had been meaning to post. Do any >of you have this, what's your experience, and of those of you that don't >have this vent, have you run into times when the front canopy fogged up to a >point that you needed or wished that you had this mentioned vent? While I've made some winter flights with little problem, on a flight a couple weeks ago (at just under the freezing point) there was extensive fogging while warming up the engine and starting to fly. Keeping a good airflow through the cabin cleared it up after some minutes of flight, but having air ducted right to the windscreen infront of the pilot would probably work much faster. With a 16 gal fuselage tank and a full set of instruments (& wires & hoses) there's little space available for any ductwork in my plane. In a search of the archives I've kept, I found only a couple mentions of defrost vents. Mike Fothergill already mentioned how he handles it. Alan Newell in Calgary, Alberta installed a duct from his cabin heating system, but at the time he wrote, he hadn't flown it much in cold weather. (He has a Soob and so used an oil cooler core with electric fans for cabin heat.) Darryl West, also of Calgary, had a nice approach that avoided ductwork and provided airflow on the canopy, even if it wasn't hot air. In his 1996 builder's report (available through the Zenith list-of-builders web page) he wrote: >I also put a 2" computer fan flush >to the top of the dash in front of the pilot side to serve as a defroster >(just prevents breath condensing there).. When I asked him about it by email, part of his reply was: > I am happy with the computer fan defroster thru 2 winters and some >humid summer mornings. It does not have any hot air ducting feeding it, >but it seems to do the trick anyway. With no SCAT ducting to it, it >doesn't take up to much space beneath the top of the dash just in front >of the pilot. Calgary is usually pretty dry (more so than Toronto, I >suspect), but I have seen the fan make a difference several times. Of >course, this is only helpful for internal condensation, not exterior >icing. Being electric instead of ram-air, it can be run prior to engine >startup when the canopy is closed and condensation is likely.. Ventilation fans with clip mountings and cigarette lighter plugs are available for cars. For a quick remedy I wondered about adapting one of them, although they might be too cheap and weak to be useful. Peter Chapman Toronto, ON 601 HDS / 912 / C-GZDC ________________________________________________________________________________
From: "Bill Morelli" <billvt(at)together.net>
Subject: Bing Carbs
Date: Jan 25, 2001
A fellow EAA member and I were discussing Bing carbs tonight. He has an Avid Flyer on ski's with a Rotax XXX (two stroke) that I have forgotten the number of. It has Bing 54 carbs. He (Frank) was telling me that in the winter (cold here in Vermont) he has to change carb jets to richen up the mixture. If he doesn't, his exhaust gas temp goes above the recommended limit. My questions are: 1 - Is that a concern for those of us running Bing carbs on the Stratus, Rotax 912, etc? 2 - Why do the Bing carbs not require carb heat? Or do they actually require carb heat and we simply don't put it on??? The information I received from Stratus and ZAC for the engine installation made no mention of carb heat? Regards, Bill N812BM - CH601 HDS - Stratus - 2.1 flight hours, 11 landings ________________________________________________________________________________
Date: Jan 25, 2001
From: Phil Raker <phadr2(at)yahoo.com>
Subject: Re: Bing Carbs
No, Bill. Two-stroke engines are very sensitive to fuel/air mixture. So much so that changes in air density from temperature variations, and, of course, altitude changes, cause the need to re-jet carburetors for the previling conditions. This is true for almost any type of vehicle which uses a two-stroke engine. Most notable among those are ultralight aircraft and snowmobiles (I work for Polaris). Four-stroke engines are not nearly as sensitive to fuel/air mixture as are the two strokes. You should have no reason to worry about your Rotax 912/914 or Stratus with Bing carbs. Phil R. - HDS Stratus; on wheels, too cold to work in unheated shop in NW MN --- Bill Morelli wrote: > > > A fellow EAA member and I were discussing Bing carbs > tonight. He has an Avid > Flyer on ski's with a Rotax XXX (two stroke) that I > have forgotten the > number of. It has Bing 54 carbs. He (Frank) was > telling me that in the > winter (cold here in Vermont) he has to change carb > jets to richen up the > mixture. If he doesn't, his exhaust gas temp goes > above the recommended > limit. > > My questions are: > > 1 - Is that a concern for those of us running Bing > carbs on the Stratus, > Rotax 912, etc? > > 2 - Why do the Bing carbs not require carb heat? Or > do they actually require > carb heat and we simply don't put it on??? > > The information I received from Stratus and ZAC for > the engine installation > made no mention of carb heat? > > Regards, > Bill N812BM - CH601 HDS - Stratus - 2.1 flight > hours, 11 landings > > > > through > > http://www.matronics.com/archives > http://www.matronics.com/emaillists > > Matronics! > > > > > Yahoo! Auctions - Buy the things you want at great prices. http://auctions.yahoo.com/ ________________________________________________________________________________
From: Z4T143(at)aol.com
Date: Jan 25, 2001
Subject: 801 Wing Lessons Learned Summary
A few weeks ago, I requested lessons learned on the 801 Wing from those of you who have "graduated" from the wings portion of this kit. I received a number of very good comments, which I've compiled and posted on our web site. http://www.geocities.com/z4t143/wing_builders_lessons.html Thanks to all who contributed. Hope this is useful to other 801'ers. Dave Zilz St. Peters MO e-mail: z4t143(at)aol.com web site: www.geocities.com/z4t143/ ________________________________________________________________________________
From: "Larry McFarland" <larrymc(at)qconline.com>
Subject: Re: Bing Carbs
Date: Jan 25, 2001
Bill, The two stroke is dependant upon the oil in the fuel for lube and cooling and because of this, running lean would cause the engine to overheat. Four cycle engines are affected by lean mixtures, but not to the same extent. Just idling the 2-stroke causes the engine to want to seize up if it is not run-up occasionally, even when landing. Exhaust gas temps are more a consideration in the air cooled Lycoming and Continentals than the water cooled Subaru and Rotax 912. Carb heat is a matter which I hope someone will provide us both an answer. Larry C. McFarland ----- Original Message ----- From: Bill Morelli <billvt(at)together.net> Sent: Thursday, January 25, 2001 8:02 PM Subject: Zenith-List: Bing Carbs > > A fellow EAA member and I were discussing Bing carbs tonight. He has an Avid > Flyer on ski's with a Rotax XXX (two stroke) that I have forgotten the > number of. It has Bing 54 carbs. He (Frank) was telling me that in the > winter (cold here in Vermont) he has to change carb jets to richen up the > mixture. If he doesn't, his exhaust gas temp goes above the recommended > limit. > > My questions are: > > 1 - Is that a concern for those of us running Bing carbs on the Stratus, > Rotax 912, etc? > > 2 - Why do the Bing carbs not require carb heat? Or do they actually require > carb heat and we simply don't put it on??? > > The information I received from Stratus and ZAC for the engine installation > made no mention of carb heat? > > Regards, > Bill N812BM - CH601 HDS - Stratus - 2.1 flight hours, 11 landings > > ________________________________________________________________________________
Date: Jan 25, 2001
From: Mike Fothergill <mfothergill(at)sympatico.ca>
Subject: Re: Bing Carbs
Bill Morelli wrote: > > > A fellow EAA member and I were discussing Bing carbs tonight. He has an Avid > Flyer on ski's with a Rotax XXX (two stroke) that I have forgotten the > number of. It has Bing 54 carbs. He (Frank) was telling me that in the > winter (cold here in Vermont) he has to change carb jets to richen up the > mixture. If he doesn't, his exhaust gas temp goes above the recommended > limit. Yes, I had to readjust the carbs on the two-stroke incold weather.> > My questions are: > > 1 - Is that a concern for those of us running Bing carbs on the Stratus, > Rotax 912, etc? The carb on the 912 is a different model. It has some altitude compensation built in. The 912 also does not rely as much on fuel for cooling. > > 2 - Why do the Bing carbs not require carb heat? Or do they actually require > carb heat and we simply don't put it on??? On the 912, the carbs are usually buried back in the cowl where the air is warmer. I measured 4 degrees. They don't get ram air either. I am still very careful about getting the engine right up to temp before launching. Mike UHS Spinners 601HDS 912S > > The information I received from Stratus and ZAC for the engine installation > made no mention of carb heat? > > Regards, > Bill N812BM - CH601 HDS - Stratus - 2.1 flight hours, 11 landings > ________________________________________________________________________________
Date: Jan 25, 2001
From: Collins <collins(at)pali.com>
Subject: Re: Bing Carbs
Interesting to note is that the Zac 912S FWF _does_ include carb heat. I did hear a reason why but I don't remember it. Bob Collins Sunnyvale CA Bill Morelli wrote: > > > A fellow EAA member and I were discussing Bing carbs tonight. He has an Avid > Flyer on ski's with a Rotax XXX (two stroke) that I have forgotten the > number of. It has Bing 54 carbs. He (Frank) was telling me that in the > winter (cold here in Vermont) he has to change carb jets to richen up the > mixture. If he doesn't, his exhaust gas temp goes above the recommended > limit. > > My questions are: > > 1 - Is that a concern for those of us running Bing carbs on the Stratus, > Rotax 912, etc? > > 2 - Why do the Bing carbs not require carb heat? Or do they actually require > carb heat and we simply don't put it on??? > > The information I received from Stratus and ZAC for the engine installation > made no mention of carb heat? > > Regards, > Bill N812BM - CH601 HDS - Stratus - 2.1 flight hours, 11 landings > ________________________________________________________________________________
From: "Jim Frisby" <marslander(at)hotmail.com>
Subject: Re: Bing Carbs
Date: Jan 25, 2001
Concerning the mixture problem with Rotax engines at altitude, a local ultralight builder and instructor here in Alaska has developed (and I think patented) an inflight mixture control system for them. Here's his web page, you might have to write to him to get specifics on the mixture control. It works well enough that he and another ultralight flyer flew over Mt. McKinley (20320 feet) in trikes with rotax power. Jim Frisby http://www.arcticsparrowaircraft.com/ ________________________________________________________________________________
From: "Dave Austin" <daveaustin2(at)sprint.ca>
Subject: Carb heat on 912 Rotax
Date: Jan 26, 2001
Purely experience, but I've flown in all weathers and temps down to -10C many times. I have never had any hint of carb icing while flying in any weather condition, probably due to the carbs on the 912 being at the rear in a pressurized and heated airflow. HOWEVER, I was running up the aircraft two weeks ago with O/T around -3C WITHOUT the upper cowl on, and after ten minutes the engine started to run rough and would not accellerate. Sudden movement of the throttle in and out cleared the problem for a minute or two and it then came back. My conclusion from this unscientific situation and test is that Bings will ice up, given the right conditions. They were really bad on my Triumph TR3 many years ago! Dave Austin 601HDS daveaustin2(at)sprint.ca ________________________________________________________________________________
Date: Jan 26, 2001
From: Dick Baner <db8(at)mtco.com>
Subject: Re: Bing Carbs
Bill, Bing carbs can ice up just like any venturi apparatus but they are not normally provided with heated air because previouslythey typically ran on aircraft not operated in icing type of weather or in snowmobiles where icing produced less dramatic results. If you fly in the type of high humidity/cool air conditions that promote icing you may want to consider providing heated air or buying the electric carb heater to install on the bings. I think California Power Systems CPS, has them in their catalogue. The business about changing jets certainly applies as cold air is denser than warm air and thus provides more "air" for the same amount of gas provided by the jetting and thus the mixture is leaned resulting in higher EGT and ultimately higher CHT although water cooling makes cylinder temps less of a problem. Dick Baner Bill Morelli wrote: > > A fellow EAA member and I were discussing Bing carbs tonight. He has an Avid > Flyer on ski's with a Rotax XXX (two stroke) that I have forgotten the > number of. It has Bing 54 carbs. He (Frank) was telling me that in the > winter (cold here in Vermont) he has to change carb jets to richen up the > mixture. If he doesn't, his exhaust gas temp goes above the recommended > limit. > > My questions are: > > 1 - Is that a concern for those of us running Bing carbs on the Stratus, > Rotax 912, etc? > > 2 - Why do the Bing carbs not require carb heat? Or do they actually require > carb heat and we simply don't put it on??? > > The information I received from Stratus and ZAC for the engine installation > made no mention of carb heat? > > Regards, > Bill N812BM - CH601 HDS - Stratus - 2.1 flight hours, 11 landings > ________________________________________________________________________________
Date: Jan 26, 2001
From: "Chesterman Farm Equipment Inc." <inquire(at)chesterman.on.ca>
Subject: Re: Bing Carbs
Also Zenair designs draw hot air from inside the cowl at all times so in a way they have permanent carb heat. I also have a snowmobile dealership and can say that rejetting a 701 for temperature is not as necessary as it should be because of always drawing heated air. Radiator covering is much more common than a rejet. dave Chesterman Phil Raker wrote: > > > No, Bill. > Two-stroke engines are very sensitive to fuel/air > mixture. So much so that changes in air density from > temperature variations, and, of course, altitude > changes, cause the need to re-jet carburetors for the > previling conditions. This is true for almost any > type of vehicle which uses a two-stroke engine. Most > notable among those are ultralight aircraft and > snowmobiles (I work for Polaris). > Four-stro > > > > 1 - Is that a concern for those of us running Bing > > carbs on the Stratus, > > Rotax 912, etc? > > > > 2 - Why do the Bing carbs not require carb heat? Or > > do they actually require > > carb heat and we simply don't put it on??? > > > > The information I received from Stratus and ZAC for > > the engine installation > > made no mention of carb heat? > > > > Regards, > > Bill N812BM - CH601 HDS - Stratus - 2.1 flight > > hours, 11 landings > > > > > > > > through > > > > http://www.matronics.com/archives > > http://www.matronics.com/emaillists > > > > Matronics! > > > > > > > > > > > > Yahoo! Auctions - Buy the things you want at great prices. > http://auctions.yahoo.com/ > -- Chesterman Farm Equipment Inc. PO Box 572, Tillsonburg, ON N4G 4J1 TEL (519) 842-5977 FAX (519) 842-9228 http://www.chesterman.on.ca ________________________________________________________________________________
From: charles.long(at)gm.com
Date: Jan 26, 2001
Subject: Bearing Material for Landing Gear
There has been some discussion of suitable materials for landing gear bearings. Allison's has had good success with a material called Aurum JCF3030 manufacured by Mitsui Chemicals. The local rep is Chris Chapman at Allegany Plastics, phone number 412-741-4416. This material needs to be molded first into a puck shape. It can then be machined to the proper dimensions. Aurum has very good wear properties and an expansion rate similar to steel. ________________________________________________________________________________
Date: Jan 26, 2001
From: "P. Owens" <powens(at)inwave.com>
Subject: Bing Carbs
Dear Phil, I am not an expert on the Rotax but may I pass along some two cycle experience I have had with a Bultaco motorcycle which may relate to your problem as well. When I initially purchased the bike in 1969 the manufacturer recommended a specific type of oil which I used for about a year. I found the engine difficult to start and had the usual smoke associated with two stroke engines. Although it ran fine once started I wan unable to kick start it. I was introduced to AMSOIL 2 Cycle oil which was recomended to blend at between 50:1 and 100:1 opposed to the manufacturers 32:1. With that simple change I have been able to kick start the engine with the first or second kick and have noted a significant increase in performance and NO SMOKE. I still have the bike today and have yet to overhaul the engine. I have been very satisfied with this product and company and if you wish additional information please let me know direct and I will mail you info. I sincerely hope this will be of some assistance to you. Phil Owens CH-801 Builder N84349 ________________________________________________________________________________
From: "Jim Ingram" <jimingerman1(at)home.com>
Subject: Re: 801 Wing Lessons Learned Summary
Date: Jan 26, 2001
Sarcasm Alert ;>) heres a site you might want to visit www.capslockoff.com re. "COULDN'T YOU HAVE SENT THAT DIRECTLY TO DAVE ?????" ________________________________________________________________________________
From: "Bill Morelli" <billvt(at)together.net>
Subject: Re: Bearing Material for Landing Gear
Date: Jan 26, 2001
I used UHMWP for my nose gear bearings, main gear bearings and gear slides as did several other builders. Wouldn't you know now that I am finished building I would come across a product that would have probably been better. In the McMaster-Carr catalog they sell Oil Impregnated UHMWP! Says that it is self lubricating and can be used for chain guides or similar applications. Probably would have been nice to use. Regards, Bill - N812BM - HDS - Stratus - Flight time 5.1 - Landings 14 >There has been some discussion of suitable materials for landing gear >bearings. Allison's has had good success with a material called Aurum JCF3030 >manufacured by Mitsui Chemicals. The local rep is Chris Chapman at Allegany >Plastics, phone number 412-741-4416. This material needs to be molded first >into a puck shape. It can then be machined to the proper dimensions. Aurum >has very good wear properties and an expansion rate similar to steel. ________________________________________________________________________________
Date: Jan 27, 2001
From: Mike Slaughter <mslaughter(at)interhop.net>
Subject: 912 Carb Heat
Hi Guys, Here's my take on the carb heat question with the 912 in the 601. Mike Fothergill and I have nearly 2000 hours of flying time between our two aircraft, and we have discussed the carb ice/need for carb heat question during many, many hangar flying (read beer) sessions. Although we frequently fly together in the same air conditions, we also forge ahead on our own singular, long (sometimes 1000 plus miles) cross-countries. This provides us with a fair amount of real time been-there-done-that-flying data. Neither of us, in all ranges of temps and humidity-including the carb ice ideal range- have ever had a cough in the 912. Mike F. mentioned in a previous post that he did a temperature differential experiment and compared outside air temp vs. air temp at the carb intake inside the cowl. He found the air at the carb intake area measured about 4C difference to the OAT. We came to the conclusion that as long as you stick to the Zenair cowl design, then the higher air temp at the carb intake is essentially feeding the carbs pre-heated air all the time-thus precluding the need for carb heat. During the final paper work required to register the aircraft in Canada as an amatuer-built (experimental in the US), we were required to provide a letter from Zenair stating that carb heat was not required on the 601 series, if the aircraft was built to Zenair specs. We have long realized that feeding outside air at cooler temps to the carbs would improve engine performence-possibly to a considersable extent in some conditions-but just haven't got around to bashing aluminum (Mike F. calls it "tin-bashing") and forming the neccesary channels and baffling to feed outside air to the carbs. Then, of course, we would need to make the switch box to feed warm air for carb heat from the muffler shroud, and retrofit the control on the instrument panel....and so on, and so on.... The question becomes, how much of a performance increase would you see compared to the trouble of making the conversion to outside air and carb heat? And, is that increase worth the worry of remembering to applying carb heat every 15 mins? Cheers, Mike S. ________________________________________________________________________________
From: "Jeff Small" <zodiacjeff(at)email.msn.com>
Subject: Re: I did it !!!!!!!!
Date: Jan 27, 2001
>N812BM made it's first flight. Hey Bill, Holy cow! You've made 14 landings and I haven't said,"WOW, congratulations!" yet. As you may have gathered, fate has thrown me a little curve in the form of Hodgkin's disease. It's a treatable form and I have an airplane to finish so I will get through this, it'll just take a year longer. Doctors say it's very treatable form and we underwent first chemo yesterday. Feeling quite good today and looking forward to the "bald" look. Please copy anything you send to Fred to me, I've flying vicariously through you and it's a hoot. Loved the pixs of the mountain from 6000. I may not get back to every message, but they keep my spirits up. Keep a close eye on that canopy mechanism as I feel a sense of responsibility in that. Your comments are educational. Congrats again Jeff ________________________________________________________________________________
From: "Jeff Small" <zodiacjeff(at)email.msn.com>
Subject: Re: I did it !!!!!!!!
Date: Jan 27, 2001
>N812BM made it's first flight. Hey Bill, Holy cow! You've made 14 landings and I haven't added my congratulations. As you may have figured out, nature has thrown me a curve in the form of Hodgkin's disease. The docs say it's a treatable form, and since I have an airplane to finish, we'll get through this; will just take a year longer. Please keep me copied with everything you send Fred; I flying vicariously through you and it's a hoot. Loved the 6000 foot pixs. Keep a close eye on the canopy as I feel some responsibility here. Your comments will be educational here. I bet it seal a WHOLE lot better than ZAC's design in cold Vermont weather. Congrats again, Jeff ________________________________________________________________________________
From: "Jeff Small" <zodiacjeff(at)email.msn.com>
Subject: mistake
Date: Jan 27, 2001
List, Very sorry as those last two messages were intended for Bill and in a bit of confusion I sent to everyone. Mea culpa, sorry. Jeff ________________________________________________________________________________
Date: Jan 27, 2001
From: joe mock <airplane_04282(at)yahoo.com>
Subject: "Joe's" leaving
I tried to send this out earlier today, but I had some problems, so will try again. If it shows up twice-SORRY!!----- After last nights mail, "Joe" has decided to leave this site as there are so many people out there who suffer from "CLINTONitis" (that is- "the rules don't apply to me"). Matt Dralle has gone through a lot of hard work and spends many hours maintaining his site, only to have it abused, even though he prints the rules about once a month. "Joe" knows there are a lot of sincere builders out there who are looking for some good constructive information--to those, "Joe" wants to wish you the best of luck and "happy building". Also "Joe realizes that the few individuals who abuse this site have done as much to hurt homebuilding as this site has to help it out. Just check around and see how many people have dropped off. I can't help but wonder if ZAC would recommend this site on their 'zenithair' web page if they monitored this site to see all that goes on. I did try to leave the site a week ago, but I hit the wrong key (I guess). I will leave the site no later than 1 Feb 01. Again, to the sincere folks out there, I wish you the best of luck!! Happy Building- goodbye-- "Joe" Yahoo! Auctions - Buy the things you want at great prices. http://auctions.yahoo.com/ ________________________________________________________________________________
From: "Steve Danielson" <steved(at)nc.rr.com>
Subject: 701 Trailing edge rivets for slats, wing, and flaperon, need
bigger size
Date: Jan 27, 2001
I am about to close out my right slat, and I have a question about what size rivets to use on the upper trailing edge. The plans call for AN470A3-3 which is a 3/32 soft solid rivet. The problem is that some of the holes are slightly oversized at A4 size (1/8) due to a repair in progress. What is the correct size of soft solid rivet to get? Is it AN470A4-3? The 4 for 4/32 diameter? Besides the normal skins that are joined by these rivets (.016 to .025), in one section I am adding an extra strip of .016 for a repair, so the rivet would be joining this: (.025 to .016 to .016). For that section should I go up to -4 for the extra length on the rivet? Thanks to all rivet guru's... Steve Danielson http://home.nc.rr.com/danielson/ ________________________________________________________________________________
Date: Jan 27, 2001
From: "Jerry Latimer" <ljm10587(at)qwest.net>
Subject: Re: Bing Carbs
----- Original Message ----- From: "Collins" <collins(at)pali.com> Sent: Thursday, January 25, 2001 10:18 PM Subject: Re: Zenith-List: Bing Carbs > > Interesting to note is that the Zac 912S FWF _does_ include > carb heat. > I did hear a reason why but I don't remember it. > > Bob Collins > Sunnyvale CA I believe the reason that the ZAC 912S FWF kit includes carb is that the 912S actually draws its carb air from outside the aircraft. This is consistent with the other inputs on carb icing. Jerry Latimer 601HDS rear fuse complete. ________________________________________________________________________________
Date: Jan 27, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: 701 Trailing edge rivets for slats, wing, and flaperon,
need bigger size My experience with solid rivets is quite limited (limited to building the spars and the aileron bellcranks). About the rivet style... the AN470A series are the soft rivets (tensile strenght of 16,000 psi), while the AN470AD are stronger (tensile strenght of 38,000 psi). To determine adequate rivet length, install a rivet and check that it extends 1.5 times its diameter. An A3 rivet needs to extend 9/64" beyond the grip lenght. An A4 rivet needs to extend 3/16" beyond the grip length. The head needs to be formed to 1.5 times the diameter of the rivet (in diameter) and .5 times the diameter in thickness. So, it appears that you do need the A4-4. Not because of added 0.016", but rather because of increased rivet diameter (you need a rivet that is .2445" long). Michel --- Steve Danielson wrote: > > > I am about to close out my right slat, and I have a > question about what size > rivets to use on the upper trailing edge. The plans > call for AN470A3-3 which > is a 3/32 soft solid rivet. The problem is that some > of the holes are > slightly oversized at A4 size (1/8) due to a repair > in progress. What is the > correct size of soft solid rivet to get? > > Is it AN470A4-3? The 4 for 4/32 diameter? > > Besides the normal skins that are joined by these > rivets (.016 to .025), in > one section I am adding an extra strip of .016 for a > repair, so the rivet > would be joining this: (.025 to .016 to .016). For > that section should I go > up to -4 for the extra length on the rivet? > > Thanks to all rivet guru's... > > Steve Danielson > http://home.nc.rr.com/danielson/ ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Yahoo! Auctions - Buy the things you want at great prices. http://auctions.yahoo.com/ ________________________________________________________________________________
From: "David Tanner" <vk3auu(at)sympac.com.au>
Subject: Re: Beefed up bearings?
Date: Jan 28, 2001
My elevator bearings are showing no sign of wear after 150 hours. (Steel pin inside aluminium plate as per CH701 plans) David Tanner ----- Original Message ----- From: "Gary Liming" <gary(at)liming.org> Sent: Monday, January 22, 2001 5:34 AM Subject: Zenith-List: Beefed up bearings? > > > On the 801, and I would be willing to bet on the 701 and even the 601 as > well, the elevator is hinged with steel pins into an aluminum hinge > bracket. I have read that one of the more serious places for wear after a > few hundred hours is where steel rides against aluminum. > > My questions for the esteemed list members are: > > 1. Does this really matter? > > 2. Anyone used any kind of bushing on these places, and if so, what was > used and the source? > > 3. On the 801, there is a little horizontal play that one of our list > members filled with a nylon washer. Are there other places in any of the > kits where this is also appropriate? > > Thanks, > > Gary Liming > 801 builder ________________________________________________________________________________
Date: Jan 27, 2001
From: Jerry Jensen <jensenm(at)jps.net>
Subject: Jabiru
To any interested. Just picked up my Jabiru 3300 engine and firewall forward kit. Mark Sarkowsky asked me to let any one interested to know that he has a 601 FWF kit in stock and a Prince prop 58 x 48 for a 601 w/3300 engine. Jerry Jensen 601HDS tail feathers outer wings 80% fuselage done car out of garage and engine in ________________________________________________________________________________
Date: Jan 27, 2001
From: Jerry Jensen <jensenm(at)jps.net>
Subject: [Fwd: Jabiru]
Forgot to include email address it is mark(at)jabiruaircraft.com -------- Original Message -------- Subject: Jabiru Date: Sat, 27 Jan 2001 23:10:42 -0800 From: Jerry Jensen <jensenm(at)jps.net> To any interested. Just picked up my Jabiru 3300 engine and firewall forward kit. Mark Sarkowsky asked me to let any one interested to know that he has a 601 FWF kit in stock and a Prince prop 58 x 48 for a 601 w/3300 engine. Jerry Jensen 601HDS tail feathers outer wings 80% fuselage done car out of garage and engine in ________________________________________________________________________________
From: "fhulen" <fhulen(at)gabs.net>
Subject: Re: Jabiru
Date: Jan 28, 2001
Mark > Sarkowsky asked me to let any one interested to know that he has a 601 > FWF kit in stock and a Prince prop 58 x 48 for a 601 w/3300 engine. ++ I mentioned it to a friend of mine, he wants to know how much it will cost? Fred ________________________________________________________________________________
Date: Jan 28, 2001
From: Jerry Jensen <jensenm(at)jps.net>
Subject: Re: Jabiru
Fred, Your or your friend should contact Mark for prices. mark(at)jabiruaircraft.com Jerry Jensen > > > ++ I mentioned it to a friend of mine, he wants to know how much it will > cost? > Fred > ________________________________________________________________________________
Date: Jan 28, 2001
From: Bill Mileski <kmileski(at)attglobal.net>
Subject: 701 Trim Tab hinge riveting
Hi folks, Another quick question for builders who have installed a trim tab while building their elevator: The trim kit instructs (and I use that word loosely) the builder to rivet the trim tab hinge to the elevator trailing edge using A4 rivets of pitch 70. Elevlator plans call for the trailing edge to be riveted using 3/32" soft rivets of pitch 40. I'm wondering what the best way is to rivet the trailing edge together where the trim tab is attached. 1/8" soft rivets (of appropriate grip)? Avex pulled A4? As an aside, I've often wondered: Are the soft rivets used in the trailing edges because of their relative higher strength compared to pulled rivets, their lower profile, a combination of these, or an entirely different reason? Inquiring minds wanna know..couldn't find an answer to the trim tab question in the archives. Thank you, Bill Mileski Middletown, Rhode Island ________________________________________________________________________________
Subject: rudder upper bearing/tail horn question
Date: Jan 28, 2001
Thread-Topic: Zenith-List Digest: 13 Msgs - 01/27/01 Thread-Index: AcCJA1XGIRAN9xuoQu6w8goOh/G6jAAWJcXt
From: "Killion, Patrick" <pkillion(at)vitalz.com>
SGVsbG8sDQogDQpNeSBuYW1lIGlzIFBhdHJpY2sgS2lsbGlvbiBhbmQgSSBhbSBqdXN0IHN0YXJ0 aW5nIGFuIFhMIChmcm9tIGtpdCkuDQogDQpEb2VzIGFueW9uZSBoYXZlIGFkdmljZSBmb3IgY3V0 dGluZyBwaWVjZXMgbGlrZSB0aGUgdGFpbCBob3JuPyAgSSBkb24ndA0KaGF2ZSBhIGxvdA0Kb2Yg Y29tcGxleCB0b29scyBhbmQgSSBhbSBub3Qgc3VyZSBhYm91dCBob3cgdG8gbWFrZSB0aGUgY3V0 cy9zaGFwZXMgdG8NCm1ha2UNCnRoZSB0YWlsIGhvcm4gbG9vayByaWdodC4gICBUaGlzIHNlZW1z IGRpZmZpY3VsdC4gICBBcmUgdGhlcmUgbG90cyBvZg0Kb3RoZXIgcGllY2VzIGluDQp0aGUga2l0 IHRoYXQgbmVlZCB0aGlzIGtpbmQgb2Ygd29yaz8NCiANCkJUVyAtIGFueW9uZSBoYXZlIGFuIG9w aW9uaW9uIG9uIHRoZSByb3RvemlwPyAgaHR0cDovL3d3dy5yb3RvemlwLmNvbS8NClNlZW1zIGxp a2UgaXQgd291bGQgYmUgaGFuZHkgZm9yIHRoaXMgdHlwZSBvZiB0aGluZy4NCiANClBrDQo ________________________________________________________________________________
From: "Chuck Deiterich" <cfd(at)tstar.net>
Subject: Re: 701 Trim Tab hinge riveting
Date: Jan 27, 2001
Bill, I used Axex A4 rivets to hold both the trailing edge and the hinge (70 pitch), and used the solid 3/32 for the rest of the trailing edge (40 pitch). I suspect the solids are used because they are a lot cheaper. Beware of the soft solid rivets with a small dimple on the head, they are not soft but hard and I got several with my 701 kit. Chuck D. ----- Original Message ----- From: Bill Mileski <kmileski(at)attglobal.net> Sent: Sunday, January 28, 2001 12:49 PM Subject: Zenith-List: 701 Trim Tab hinge riveting > > Hi folks, > > Another quick question for builders who have installed a trim tab while > building their elevator: > The trim kit instructs (and I use that word loosely) the builder to > rivet the trim tab hinge to the elevator trailing edge using A4 rivets > of pitch 70. Elevlator plans call for the trailing edge to be riveted > using 3/32" soft rivets of pitch 40. I'm wondering what the best way is > to rivet the trailing edge together where the trim tab is attached. > 1/8" soft rivets (of appropriate grip)? Avex pulled A4? > > As an aside, I've often wondered: Are the soft rivets used in the > trailing edges because of their relative higher strength compared to > pulled rivets, their lower profile, a combination of these, or an > entirely different reason? > > Inquiring minds wanna know..couldn't find an answer to the trim tab > question in the archives. > > Thank you, > > Bill Mileski > Middletown, Rhode Island > > ________________________________________________________________________________
From: STEFREE(at)aol.com
Date: Jan 28, 2001
Subject: Mounting Stabilizer
Hi lIst, In the past I have read many posts regarding mounting the stabilizer and the distance from the leading edge of the stabilizer to th rear top bulk head. Can any of you out thive give measurements for how far your distance is in this location. I have read anywhere from"almost touching" to as much as a centimeter or so? IS there any consensus on this topic? Also on the same vane.....What are some methods that people used to ensure that the stabilizer was mounted "sqaure" the the center wing "Z" I have several ideas some of which I think suck. LOL Anyway, As always thanks for everyones help in advance. Steve PS This years Superbowl Pick is Ravens 17, Giants 10. Since I started building my plane I have yet to miss one......Maybe that is a sign! Hopefully be able to fly to next years! ________________________________________________________________________________
From: "Michael Brook" <walruss(at)optushome.com.au>
Subject: 701 Trim Tab hinge riveting
Date: Jan 29, 2001
well if it isn't my good friend bill. Hey bill, How is the plane building caper treating you. I went for the A4 pulled rivets on the elevator trim tab hinges. The trailing edge soft rivets are great. I would thing that they are used because of the low profile if you do them right. I have a LOT left over. and I've finished all my trailing edges. Although I'm told they are or can be used in the doors a bit. I'm at 490 hours at the moment and making the push to 500. Motivation is hard to come by. I'll be putting both fuselages together this week, as in joinging the rear fuselage and the forward fuse together. exciting stuff. -----Original Message----- From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com]On Behalf Of Bill Mileski Sent: Sunday, January 28, 2001 6:49 PM Subject: Zenith-List: 701 Trim Tab hinge riveting Hi folks, Another quick question for builders who have installed a trim tab while building their elevator: The trim kit instructs (and I use that word loosely) the builder to rivet the trim tab hinge to the elevator trailing edge using A4 rivets of pitch 70. Elevlator plans call for the trailing edge to be riveted using 3/32" soft rivets of pitch 40. I'm wondering what the best way is to rivet the trailing edge together where the trim tab is attached. 1/8" soft rivets (of appropriate grip)? Avex pulled A4? As an aside, I've often wondered: Are the soft rivets used in the trailing edges because of their relative higher strength compared to pulled rivets, their lower profile, a combination of these, or an entirely different reason? Inquiring minds wanna know..couldn't find an answer to the trim tab question in the archives. Thank you, Bill Mileski Middletown, Rhode Island ________________________________________________________________________________
From: "Jeff Green" <jegreen(at)cdc.net>
Subject: Trimming sheet metal
Date: Jan 28, 2001
Each of the fuselage skins on the 801 requires trimming on 3 or 4 sides. I've been using Wiss sheers to make a rough cut then a final cut. Then I've been filing the edge smooth and straight. The final result is good, but it takes a lot of work. Does anyone have a better and/or quicker way to do this? Jeff Green CH-801. Tail section done, working on fuselage. ________________________________________________________________________________
Date: Jan 28, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: Trimming sheet metal
My preferred approach is with a knife. I clamp the sheet with a straight edge and I mark the sheet with a knife a few times. Then, when I bend the sheet, it simply breaks appart. Smoothering of the cut is required (with file, sand paper and scotch brite). See some pictures.... http://www.pcperfect.com/mthobby/ch601/images/powing15.jpg http://www.pcperfect.com/mthobby/ch601/images/p6t3f.jpg http://www.pcperfect.com/mthobby/ch601/images/pmiscpart2.jpg With this approach, the cut is very nice. With scissors, it may be that I do not have a good technique, but there are always marks that remain showing where I was squeezing the scissors. Michel --- Jeff Green wrote: > > > Each of the fuselage skins on the 801 requires > trimming on 3 or 4 sides. > I've been using Wiss sheers to make a rough cut then > a final cut. Then I've > been filing the edge smooth and straight. The final > result is good, but it > takes a lot of work. > > Does anyone have a better and/or quicker way to do > this? ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Yahoo! Auctions - Buy the things you want at great prices. http://auctions.yahoo.com/ ________________________________________________________________________________
From: "Larry McFarland" <larrymc(at)qconline.com>
Subject: Re: Trimming sheet metal
Date: Jan 28, 2001
Jeff, I'd strongly suggest an air shear for less than $50.00 from Harbor Freight. It will allow you to follow an ink marker line on it's trace edge from a straight edge. Then you use the file for the last .005 for straightness. The Weiss shears are good for small parts, aileron ribs etc. A better process I've not yet tried is the router with a carbide tip and a guide edge. Then you only need the debur tool to break a sharp edge. I've been using my air shear for a year and have no reservations about the straight and flat cuts it makes. Best bang for the buck. Larry C. McFarland I'm bending nose skins for a scratch-built 601 HDS to fit wing ribs, then on to welding tanks and 2 years to go. ----- Original Message ----- From: Jeff Green <jegreen(at)cdc.net> Sent: Sunday, January 28, 2001 8:31 PM Subject: Zenith-List: Trimming sheet metal > > Each of the fuselage skins on the 801 requires trimming on 3 or 4 sides. > I've been using Wiss sheers to make a rough cut then a final cut. Then I've > been filing the edge smooth and straight. The final result is good, but it > takes a lot of work. > > Does anyone have a better and/or quicker way to do this? > > Jeff Green > CH-801. Tail section done, working on fuselage. > ________________________________________________________________________________
Date: Jan 28, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: Trimming sheet metal
I have tried it with a router also (for the spar webs). I obtained very good and precise result, but it was not exactly quick (lots of measurements, fixing metal and straight edge...) http://www.pcperfect.com/mthobby/ch601/chwspars.htm I think that for more casual cuts, the knife approach is faster and very good. For the spar web, the router approach allows to meet the .5mm tolerance quite easily once everything is fixed in position. Michel --- Larry McFarland wrote: > A better process I've not yet tried is the router > with a carbide tip and a > guide edge. Then you > only need the debur tool to break a sharp edge. ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Yahoo! Auctions - Buy the things you want at great prices. http://auctions.yahoo.com/ ________________________________________________________________________________
Date: Jan 28, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Press for bending nose skins...
I am done with the press I built to bend the nose skins of my 601 HD and I would like to make it available to any builder that would like to use it. Because of its size (of the press), this offer targets the builders around Montreal area. The steel tube and wood channel (to form the skin) are not included as they were borrowed from a friend. But I can explain what they are. For a picture of the press, go to: http://www.pcperfect.com/mthobby/ch601/images/powing20.jpg Seen on: http://www.pcperfect.com/mthobby/ch601/chowings2.htm oh... Shipping not included Michel ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Yahoo! Auctions - Buy the things you want at great prices. http://auctions.yahoo.com/ ________________________________________________________________________________
From: "tom tiedman" <ttiedman(at)hotmail.com>
Subject: Re: Trimming sheet metal
Date: Jan 28, 2001
I prefer the offset head style of Wiss hand shears as you can make very long cuts on very large parts much more easily than you can with the regular straight head style Wiss hand shears. The metal being cut just keeps on feeding right past the offset head with no problems. The biggest, thickest part I've cut out with them comfortably was the .040 center spar web. They will cut .063 also, but it is quite a chore and a real hand-killer! My offset head Wiss shears cost me $13.00 and can be found at any home supply or hardware store. You have to file and sand the edges after cutting with them, as their cutting edges are slightly serrated for easy cutting. Tom 601HD (worried for the past few weeks about mistakenly riveting inboard right wing rib at 150mm instead of 130mm. Still don't know how that happened! I've been religiously following the "measure twice, cut once" rule from the start, only its been more like measure 10 times and cut once. Been racking my brain for a solution, and thought I might end up having to rebuild the entire right wing, but then it finally dawned on me that I'll just mount the inboard left wing rib at 150mm also. That should keep the rivet lines on the skins identically spaced on both wings anyway... and so it goes)! >From: Michel Therrien <mtherr(at)yahoo.com> >Reply-To: zenith-list(at)matronics.com >To: zenith-list(at)matronics.com >Subject: Re: Zenith-List: Trimming sheet metal >Date: Sun, 28 Jan 2001 19:11:56 -0800 (PST) > > >I have tried it with a router also (for the spar >webs). I obtained very good and precise result, but >it was not exactly quick (lots of measurements, fixing >metal and straight edge...) > >http://www.pcperfect.com/mthobby/ch601/chwspars.htm > >I think that for more casual cuts, the knife approach >is faster and very good. For the spar web, the router >approach allows to meet the .5mm tolerance quite >easily once everything is fixed in position. > >Michel > >--- Larry McFarland wrote: > > A better process I've not yet tried is the router > > with a carbide tip and a > > guide edge. Then you > > only need the debur tool to break a sharp edge. > > >===== >---------------------------- >Michel Therrien CH601-HD > http://pages.infinit.net/mthobby > http://www.pcperfect.com/mthobby/ch601 > >Yahoo! Auctions - Buy the things you want at great prices. >http://auctions.yahoo.com/ > > ________________________________________________________________________________
Date: Jan 28, 2001
From: Norris <rnorris4(at)earthlink.net>
Subject: Re: Mounting Stabilizer
Mine is almost touching, about 2-3mm. To square the HS to center wing, I measured from outboard trailing edge of rear wing spar to outboard leading edge of HS. After drilling holes, about 1mm difference left to right. For level, I leveled center wing spar, then HS to match. Rob Norris No progress since the baby arrived, but trying to get there. STEFREE(at)aol.com wrote: > In the past I have read many posts regarding mounting the stabilizer and the > distance from the leading edge of the stabilizer to th rear top bulk head. > Can any of you out thive give measurements for how far your distance is in > this location. I have read anywhere from"almost touching" to as much as a > centimeter or so? IS there any consensus on this topic? > > Also on the same vane.....What are some methods that people used to ensure > that the stabilizer was mounted "sqaure" the the center wing "Z" I have > several ideas some of which I think suck. LOL ________________________________________________________________________________
From: "Peter Ferguson" <pfergus2(at)tampabay.rr.com>
Subject: Anyone flying a Jabiru 3300 yet ?
Date: Jan 29, 2001
Hi folks- I am interested in the Jabiru 3300 for my 601 HDS. Has anyone flown one yet and what are the performance figures on this? Has the distributor been easy to work with ( In the USA ) and did the FWF kit work "fit" as planned? Any help at this time would be much appreciated. Thanks in advance. Peter Ferguson 601 HDS TD with 68 3/8% done and 52% to go! ________________________________________________________________________________
From: "Matthew Mucker" <mmucker(at)airmail.net>
Subject: Trimming sheet metal
Date: Jan 29, 2001
Larry, What kind of volume do you get from your air compressor? Have you found that to be adequate? I'm looking at compressors and don't know how much I need. I know the riveter won't take much air, but I keep wondering about those air shears. -Matt > -----Original Message----- > From: owner-zenith-list-server(at)matronics.com > [mailto:owner-zenith-list-server(at)matronics.com]On Behalf Of Larry > McFarland > Sent: Sunday, January 28, 2001 9:08 PM > To: zenith-list(at)matronics.com > Subject: Re: Zenith-List: Trimming sheet metal > > > > > Jeff, > I'd strongly suggest an air shear for less than $50.00 from Harbor > Freight. It will allow you > to follow an ink marker line on it's trace edge from a straight > edge. Then > you use the file for > the last .005 for straightness. The Weiss shears are good for > small parts, > aileron ribs etc. > A better process I've not yet tried is the router with a carbide tip and a > guide edge. Then you > only need the debur tool to break a sharp edge. I've been using my air > shear for a year and > have no reservations about the straight and flat cuts it makes. > Best bang > for the buck. > Larry C. McFarland > I'm bending nose skins for a scratch-built 601 HDS to fit wing > ribs, then on > to welding tanks > and 2 years to go. > > ----- Original Message ----- > From: Jeff Green <jegreen(at)cdc.net> > To: > Sent: Sunday, January 28, 2001 8:31 PM > Subject: Zenith-List: Trimming sheet metal > > > > > > Each of the fuselage skins on the 801 requires trimming on 3 or 4 sides. > > I've been using Wiss sheers to make a rough cut then a final cut. Then > I've > > been filing the edge smooth and straight. The final result is > good, but it > > takes a lot of work. > > > > Does anyone have a better and/or quicker way to do this? > > > > Jeff Green > > CH-801. Tail section done, working on fuselage. > > > > ________________________________________________________________________________
From: charles.long(at)gm.com
Date: Jan 29, 2001
Subject: Aerodynamics Simulation
Have been working on an aerodynamics simulation for the HDS the last month or so. It's just about ready to go. Waiting for some feedback from ZAC. Thanks to Peter Chapman for his helpful suggestions. This simulation can be of great value in selecting Engine and Prop combinations. All that's left to do is check the accuracy of the calculations. For those of you already flying, could you please provide the following information on your aircrafts performance. It would be very helpful. Will provide the completed spreadsheet to those who are interested. Thanks for your help in advance! Empty Weight - lbs: Test Weight - lbs: Test Altitude, MSL - ft: Engine Model: Max Rated Power - hp: Max Ground Speed (average of two runs in opposite directions to factor out wind) - mph: Max Climb Rate @90mph IAS - ft/min: Engine Idle Sink Rate @80mph IAS - mph: Any info on drag related items would also be helpful ________________________________________________________________________________
From: "Larry McFarland" <larrymc(at)qconline.com>
Subject: Re: Trimming sheet metal
Date: Jan 29, 2001
Matt, I bought a 6.5 HP-60 Gal -2 cyl vertical tank unit for the garage and put it on casters for cleaning. The air shear cannot get ahead of it and I think any compressor that's set to 90 psi and offers NLT 4 SCFM would do. The shear will cut two lengths of .025, 8' long before kicking in to refill at the 90 psi level. Larry ----- Original Message ----- From: Matthew Mucker <mmucker(at)airmail.net> Sent: Monday, January 29, 2001 9:56 AM Subject: RE: Zenith-List: Trimming sheet metal > > Larry, > > What kind of volume do you get from your air compressor? Have you found > that to be adequate? I'm looking at compressors and don't know how much I > need. I know the riveter won't take much air, but I keep wondering about > those air shears. > ________________________________________________________________________________
From: "Michael Brook" <walruss(at)optushome.com.au>
Subject: Trimming sheet metal
Date: Jan 30, 2001
my experiience is that a 13CFM compressor is about the right size that you want. If you want to do any spray painting of your machine you will need this as a minimum. You want to have a large reciever tank on your compressor as well. It will run much less frequently and for a shorter duration thus allowing you to spend more time in peace, trying to figure out what the hell the plans mean. -----Original Message----- From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com]On Behalf Of Matthew Mucker Sent: Monday, January 29, 2001 3:57 PM Subject: RE: Zenith-List: Trimming sheet metal Larry, What kind of volume do you get from your air compressor? Have you found that to be adequate? I'm looking at compressors and don't know how much I need. I know the riveter won't take much air, but I keep wondering about those air shears. -Matt > -----Original Message----- > From: owner-zenith-list-server(at)matronics.com > [mailto:owner-zenith-list-server(at)matronics.com]On Behalf Of Larry > McFarland > Sent: Sunday, January 28, 2001 9:08 PM > To: zenith-list(at)matronics.com > Subject: Re: Zenith-List: Trimming sheet metal > > > > > Jeff, > I'd strongly suggest an air shear for less than $50.00 from Harbor > Freight. It will allow you > to follow an ink marker line on it's trace edge from a straight > edge. Then > you use the file for > the last .005 for straightness. The Weiss shears are good for > small parts, > aileron ribs etc. > A better process I've not yet tried is the router with a carbide tip and a > guide edge. Then you > only need the debur tool to break a sharp edge. I've been using my air > shear for a year and > have no reservations about the straight and flat cuts it makes. > Best bang > for the buck. > Larry C. McFarland > I'm bending nose skins for a scratch-built 601 HDS to fit wing > ribs, then on > to welding tanks > and 2 years to go. > > ----- Original Message ----- > From: Jeff Green <jegreen(at)cdc.net> > To: > Sent: Sunday, January 28, 2001 8:31 PM > Subject: Zenith-List: Trimming sheet metal > > > > > > Each of the fuselage skins on the 801 requires trimming on 3 or 4 sides. > > I've been using Wiss sheers to make a rough cut then a final cut. Then > I've > > been filing the edge smooth and straight. The final result is > good, but it > > takes a lot of work. > > > > Does anyone have a better and/or quicker way to do this? > > > > Jeff Green > > CH-801. Tail section done, working on fuselage. > > > > ________________________________________________________________________________
From: "Jim Frisby" <marslander(at)hotmail.com>
Subject: Re: Trimming sheet metal
Date: Jan 29, 2001
Larry, You mentioned "The air shear ..." I've searched the archive, and can't seem to find anything else about this tool. Could you help me track down a source? Thanks Jim Frisby ________________________________________________________________________________
Date: Jan 29, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
Subject: Re: Trimming sheet metal
Jim Frisby wrote: > > Larry, > You mentioned "The air shear ..." > I've searched the archive, and can't seem to find anything else about this > tool. Could you help me track down a source? > Thanks > Jim Frisby > Hey Jim, Harbor Freight....Pistol Grip or Straight: $49.95(Free Shipping)......1-800-423-2567 ( http://www.harborfreight.com ) Good Luck John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: "Alan Newell" <anewell(at)canuck.com>
Subject: Re: Fogging canopy
Date: Jan 29, 2001
Fred: I installed defrost vents in my 601 and I'm glad that I did. The set up is very much like a car. I have a heater box that hold a radiator 9actually it's an oil cooler rad but plumbed to my engine cooling system. The box has two outlets that go to two defrost vents and two flaps that direct air to the cockpit foot area. A panel mounted cable control opens the foot vents and closes the defrost vents via butterfly type valves in the outlets. Air is supplied by two 12 volt fans. I can run one or both fans at three different speed settings. I have the canopy frost over in the winter until the engine warms up but then it clears quickly. I once ran into freezing drizzel while flying a Cherokee in the circuit and had a really hard time seeing to land so I made sure that I had a good source of warm air for the canopy in my HDS. Regards, Alan Newell, Calgary, Alberta, Canada ---------- > From: fhulen <fhulen(at)gabs.net> > To: Zenith List > Subject: Zenith-List: Fogging canopy > Date: January 23, 2001 7:18 PM > > > In Bill's recent "I did it" posting about his first flight, he mentions that > his canopy fogged up, and that he turned on the exhaust fan and it cleared > right up. In one of the aviation magazines that I receive it listed a "Top > 12 things" checklist of things that they thought should be included in every > instrument panel design. A "defrost vent" on the front screen was on that > list. This brings forth a question that I had been meaning to post. Do any > of you have this, what's your experience, and of those of you that don't > have this vent, have you run into times when the front canopy fogged up to a > point that you needed or wished that you had this mentioned vent? > Thanks > Fred Getting close to hanging the 3300 engine.... ________________________________________________________________________________
Date: Jan 30, 2001
From: "J. Davis" <jd(at)lri.sjhc.london.on.ca>
Subject: Ontario --> Oshkosh route suggestions
Greetings... I am starting to organize a flight of several advanced ultra-light aircraft from London, ON, CA to Oshkosh, WI this summer. Not having flown there before, I would like to hear any suggestions regarding route, friendly airfields along the way, border crossing, etc. We plan to camp overnight at least once, more likely, twice, making the final hop to Wittman an easy one. We need to avoid built-up areas (ie., cities like Detroit) and probably most controlled airspace. I would especially like to hear from one of the Challenger drivers who made to trip last year (and, incidentally, thank them for pioneering the recent changes in regulations which now allow ULA's with appropriately licensed pilots to cross over into the US). I currently have the Detroit and Chicago sectionals. What is the American equivalent of our Flying Farmers? That would be a good resource for us. Keep in mind that we cruise at about 65 Kts, have about 3 hours of usable [auto] fuel, prefer grass to asphalt. We plan on having ground support, as well, a radio/gps equipped van. Thanks in advance for any suggestions/opinions/ideas. -- Regards, J. C-IGGY, CH701, ~100 hrs. | J. Davis, M.Sc. (comp_sci) | email: jd(at)uwo.ca | | SysMgr, research programmer | voice: (519) 646 6100 x64166 | | Lawson Research Institute | fax: (519) 646 6135 | | London, Ontario | lriweb.sjhc.london.on.ca/~jd | The other day, I was walking my dog around my building...on the ledge. Some people are afraid of heights. Not me, I'm afraid of widths. --- Steven Wright ________________________________________________________________________________
Date: Jan 30, 2001
From: Mike Fothergill <mfothergill(at)sympatico.ca>
Subject: Re: Ontario --> Oshkosh route suggestions
Hi J; Having done this flight in a Merlin in 91, I can vouch for the VFR route around Chicago shown on the Chicago VTA chart. We flew into St Clair County (Port Huron) to clear customs after filing flight plan from Sarnia. Overnighted just east of Chicago, then flew into the VFR circuit at Oshkosh. For this ,you need radio. If no radio, you have to go into UL circuit at less than 500 ft. Scary! Route from Baldwin, Ont. was Stratford, Sarnia, Port Huron(St Clair CO.), Griffith, East Troy and Oshkosh. There are lots of airports to stop at depending on your range limits. Make sure that you have lots of fuel going into Oshkosh to allow for holds. Mike UHS Spinners "J. Davis" wrote: > > > Greetings... > > I am starting to organize a flight of several advanced ultra-light > aircraft from London, ON, CA to Oshkosh, WI this summer. Not having > flown there before, I would like to hear any suggestions regarding route, > friendly airfields along the way, border crossing, etc. We plan to camp > overnight at least once, more likely, twice, making the final hop to > Wittman an easy one. We need to avoid built-up areas (ie., cities like > Detroit) and probably most controlled airspace. > > I would especially like to hear from one of the Challenger drivers who > made to trip last year (and, incidentally, thank them for pioneering the > recent changes in regulations which now allow ULA's with appropriately > licensed pilots to cross over into the US). I currently have the Detroit > and Chicago sectionals. What is the American equivalent of our Flying > Farmers? That would be a good resource for us. Keep in mind that we cruise > at about 65 Kts, have about 3 hours of usable [auto] fuel, prefer grass to > asphalt. We plan on having ground support, as well, a radio/gps equipped > van. > > Thanks in advance for any suggestions/opinions/ideas. > > -- > Regards, J. > C-IGGY, CH701, ~100 hrs. > > | J. Davis, M.Sc. (comp_sci) | email: jd(at)uwo.ca | > | SysMgr, research programmer | voice: (519) 646 6100 x64166 | > | Lawson Research Institute | fax: (519) 646 6135 | > | London, Ontario | lriweb.sjhc.london.on.ca/~jd | > > The other day, I was walking my dog around my building...on the ledge. Some > people are afraid of heights. Not me, I'm afraid of widths. > --- Steven Wright > ________________________________________________________________________________
Date: Jan 30, 2001
Subject: Re: Fogging canopy
From: Grant Corriveau <gfcorriv(at)total.net>
on 1/29/01 10:25 PM, Alan Newell at anewell(at)canuck.com wrote: ... > I have a heater box that hold a radiator 9actually > it's an oil cooler rad but plumbed to my engine cooling system. Alan, I like the concept as I imagine that the heater core is pretty small.. yes/no?... could you give me an estimate of the dimensions? I've searched for car heater cores, but they're pretty bulky. Does the oil cooler rad provide enough heat exchange for the cold Calgary winters? Thanks, Grant ________________________________________________________________________________
Date: Jan 30, 2001
From: Dick Baner <db8(at)mtco.com>
Subject: Re: Ontario --> Oshkosh route suggestions
Two of the fellows in our local ultralight club flew a two place challenger to s&f last spring and back. They went from central Illinois so their route may not do you much good. If you want to know how to contact them by phone send me a note off line. Dick Baner, subaru 701 "J. Davis" wrote: > > Greetings... > > I am starting to organize a flight of several advanced ultra-light > aircraft from London, ON, CA to Oshkosh, WI this summer. Not having > flown there before, I would like to hear any suggestions regarding route, > friendly airfields along the way, border crossing, etc. We plan to camp > overnight at least once, more likely, twice, making the final hop to > Wittman an easy one. We need to avoid built-up areas (ie., cities like > Detroit) and probably most controlled airspace. > > I would especially like to hear from one of the Challenger drivers who > made to trip last year (and, incidentally, thank them for pioneering the > recent changes in regulations which now allow ULA's with appropriately > licensed pilots to cross over into the US). I currently have the Detroit > and Chicago sectionals. What is the American equivalent of our Flying > Farmers? That would be a good resource for us. Keep in mind that we cruise > at about 65 Kts, have about 3 hours of usable [auto] fuel, prefer grass to > asphalt. We plan on having ground support, as well, a radio/gps equipped > van. > > Thanks in advance for any suggestions/opinions/ideas. > > -- > Regards, J. > C-IGGY, CH701, ~100 hrs. > > | J. Davis, M.Sc. (comp_sci) | email: jd(at)uwo.ca | > | SysMgr, research programmer | voice: (519) 646 6100 x64166 | > | Lawson Research Institute | fax: (519) 646 6135 | > | London, Ontario | lriweb.sjhc.london.on.ca/~jd | > > The other day, I was walking my dog around my building...on the ledge. Some > people are afraid of heights. Not me, I'm afraid of widths. > --- Steven Wright > ________________________________________________________________________________
Date: Jan 30, 2001
From: "J. Davis" <jd(at)lri.sjhc.london.on.ca>
Subject: Re: Fogging canopy
Here in ON, Princess Auto has a wide range of this type of heater. Pricing varies according to size/number of fans but the one I will use someday was ~$100. Better pricing during summer months ;') >> on 1/29/01 10:25 PM, Alan Newell at anewell(at)canuck.com wrote: >> ... >> > I have a heater box that hold a radiator 9actually >> > it's an oil cooler rad but plumbed to my engine cooling system. >> >> Alan, I like the concept as I imagine that the heater core is pretty small.. >> yes/no?... could you give me an estimate of the dimensions? >> >> I've searched for car heater cores, but they're pretty bulky. Does the oil >> cooler rad provide enough heat exchange for the cold Calgary winters? >> >> Thanks, >> Grant >> >> >> >> >> Regards, J. | J. Davis, M.Sc. (comp_sci) | email: jd(at)uwo.ca | | SysMgr, research programmer | voice: (519) 646 6100 x64166 | | Lawson Research Institute | fax: (519) 646 6135 | | London, Ontario | lriweb.sjhc.london.on.ca/~jd | Why is the alphabet in that order? Is it because of that song? The guy who wrote that song wrote everything. --- Steven Wright ________________________________________________________________________________
Date: Jan 30, 2001
From: Gerald Applefeld <jerryvmd(at)blazenet.net>
Subject: Help-electrical
I need suggestions from the list--building 601HD--in process of wiring panel and FFW. Using Bob Nichols drawings--also an EA81--from previous postings it seems most people put the battery behind the seats for weight/balance. Is this the best? If so, I'll be running #1 AGW wire from the battery contactor near the battery to the starter relay on the engine side of the firewall. Where is the best postion to run the wire and ground? 1.I've considered thru the rear Z under the seats and thru the spar but means multiple holes and grommets and removing the seat pan for access. 2. Thru side seat back support along the side fuselage (under the top longeron doubler)-over the vertical fuselage stiffeners to firewall. 3. Thru center armrest area-under control cables-thru spar-between rudder pedals to firewall Please-any suggestions--can't proceed to wire panel until this is solved---Thanks Jerry ________________________________________________________________________________
From: "Bill Morelli" <billvt(at)together.net>
Subject: Re: Help-electrical
Date: Jan 30, 2001
Jerry, I have a Stratus Soob with two 18 ah batteries behind the passenger seat. These batteries weight about 12 lbs each. My CG came out right on the money. I also have 8 gallon header and 10 gallon LE tanks. I used #4 wire from the battery to the contactor (near the battery) and then up to the starter. I ran the cable under the upper right longeron doubler (I have it protected with spiral wrap). I have no trouble cranking the Soob all day with this setup. I think that #1 wire is major overkill. Regards, Bill - N812BM - HDS (tri)- Stratus - Flight Hours 5.9 - Landings 16 >I need suggestions from the list--building 601HD--in process of wiring >panel and FFW. Using Bob Nichols drawings--also an EA81--from previous >postings it seems most people put the battery behind the seats for >weight/balance. Is this the best? If so, I'll be running #1 AGW wire >from the battery contactor near the battery to the starter relay on the >engine side of the firewall ________________________________________________________________________________
From: "Chuck Sonberg" <2408s@cox-internet.com>
Subject: Re: Help-electrical
Date: Jan 30, 2001
I placed my battery behind the seat because of cg problems. I used #2 welding wire as it is relatively inexpensive and contains many more strands and has a great sheath. I also went with 16 gauge wire for all my wiring so I could use 10 amp breakers throughout. I used 3 colors only with red - hot, black - ground, and white - sender. Be sure to mark each wire at both ends - really big help when chasing any future problems. Chuck 601HDS 15 hrs 35 landings ----- Original Message ----- From: "Gerald Applefeld" <jerryvmd(at)blazenet.net> Sent: Tuesday, January 30, 2001 4:51 PM Subject: Zenith-List: Help-electrical > > I need suggestions from the list--building 601HD--in process of wiring > panel and FFW. Using Bob Nichols drawings--also an EA81--from previous > postings it seems most people put the battery behind the seats for > weight/balance. Is this the best? If so, I'll be running #1 AGW wire > from the battery contactor near the battery to the starter relay on the > engine side of the firewall. Where is the best postion to run the wire > and ground? 1.I've considered thru the rear Z under the seats and thru > the spar but means multiple holes and grommets and removing the seat pan > for access. 2. Thru side seat back support along the side fuselage > (under the top longeron doubler)-over the vertical fuselage stiffeners > to firewall. 3. Thru center armrest area-under control cables-thru > spar-between rudder pedals to firewall > Please-any suggestions--can't proceed to wire panel until this is > solved---Thanks > Jerry > > ________________________________________________________________________________
Date: Jan 31, 2001
Subject: Fiberglass tips on Horizontal Stabilizer
From: "Tom Wood" <twood(at)ucf.k12.pa.us>
I offer a tip on attaching the fiberglass tips. The plans do not mention it but I epoxy a .025 strip 20mm wide on the inside of the fiberglass tips before drilling holes for attachment to the HS. The tips are less likely to develop cracks if the rivets pull on the aluminum rather than the fiberglass. This procedure is recommended in the RV -4 plans. All you need to do is rough up the fiberglass with 36 grit paper and use a two part epoxy for an adhesive. ________________________________________________________________________________
Date: Jan 31, 2001
From: Carlos Sa <wings1(at)videotron.ca>
Subject: Minister's Delegates-Recreational Aviation (Canada)
This is of interest (primarily) to Canadian builders: http://www.md-ra.com/ Mandate of Minister's Delegates-Recreational Aviation (MD-RA) MD-RA is a Transport Canada external delegation of authority program operated on behalf of the Department of Transport. MD-RA is responsible for amateur built aircraft only. MD-RA inspectors perform inspections on aircraft under construction and, upon completion, issue the initial Special Certificate of Airworthiness and a flight authority with certain restrictions. Once the aircraft is complete and flying, the files are transferred to the Department of Transport. The site does not look complete, but there is a good deal of interesting information there. Cheers Carlos ________________________________________________________________________________
From: "The Meiste's" <meiste(at)essex1.com>
Subject: Cork (again)
Date: Jan 31, 2001
List, I know it's been hashed about plenty here in the past but I was just wondering if anyone out there has found a usable substitute yet to isolate the 16 gallon main header tank other than cork? I'm getting ready to attempt this step and was wondering about some kind of rubber instead. From my past experiences with cork it would seem that in 5 to 10 years it would have to be redone. Anyway just wondering if anyone has heard if there was anything new worth looking at? Kelly Meiste 601 HD ________________________________________________________________________________
From: "David Tanner" <vk3auu(at)sympac.com.au>
Subject: Re: Cork (again)
Date: Feb 01, 2001
I used cork floor tile, if that is not durable, I don't know what is. David Tanner ________________________________________________________________________________
From: "Shay King" <shaking(at)eircom.net>
Subject: Fuel hose/ 701 wing tank access
Date: Feb 01, 2001
Dear List, I'm installing my first wing tank at the moment [701 -extended range] and I'm worried about the problem of access after the wing is closed up. I'm using the black rubber hose supplied with the kit by CZAW. Does anyone know the life of this hose? Does anyone have any clever ideas about access panels to the wing tank fittings? Regards, Shay King. ________________________________________________________________________________
From: Sjl219(at)aol.com
Date: Feb 01, 2001
Subject: Re: Fuel hose/ 701 wing tank access
I put an access hole between the root rib and the #1 rib, offset of course, so that I could get tools up there to change the hose and maintain the filter screen. Don't forget to provide a doubler. Stan L. CH701 from kit in fifth year of construction (400 hours ??**& %$??) ________________________________________________________________________________
Date: Feb 01, 2001
From: Rich <rich(at)carol.net>
Subject: Re: Fuel hose/ 701 wing tank access
As far as access... I'm making a 100mm x 70mm hole, big enough for my hands to get into with a wrench. I'll then make a cover with a lip to clip inside the skin & a quarter-turn wingnut to hold the cover in place. So easy to get to that I can also check this as part of every preflight. Inspection holes slightly weaken the area so, per ZAC, whenever inspection holes are cut into the skin another piece the same thickness or thicker, the shape of the hole, should be riveted to the inside to strengthen the area. I'll have to dimple the skin & the stiffener to make nice flush rivets so my cover will be flush. Rich 801 Shay King wrote: > > > Dear List, > I'm installing my first wing tank at the moment [701 -extended range] > and I'm worried about the problem of access after the wing is closed up. > I'm using the black rubber hose supplied with the kit by CZAW. Does > anyone know the life of this hose? Does anyone have any clever ideas > about access panels to the wing tank fittings? > > Regards, > Shay King. > ________________________________________________________________________________
From: "Carl Bertrand" <cgbrt(at)mondenet.com>
Subject: Re: Fuel hose/ 701 wing tank access
Date: Feb 01, 2001
Shay, I installed my wing-root skins with rivnuts. Its a five minute job to remove them and voila you have access to the wing root area for your attach fittings,tanks and other connections. Also saves taking the wings off to change the windshield. Happy flying, Carl -----Original Message----- From: Shay King <shaking(at)eircom.net> Date: February 1, 2001 4:55 PM Subject: Zenith-List: Fuel hose/ 701 wing tank access > >Dear List, >I'm installing my first wing tank at the moment [701 -extended range] >and I'm worried about the problem of access after the wing is closed up. >I'm using the black rubber hose supplied with the kit by CZAW. Does >anyone know the life of this hose? Does anyone have any clever ideas >about access panels to the wing tank fittings? > >Regards, >Shay King. > > ________________________________________________________________________________
From: "Peter Ferguson" <pfergus2(at)tampabay.rr.com>
Subject: * New Bulletin from Zenith *
Date: Feb 03, 2001
All 601 owners and builders should go to the Zenith Builders Pages on the web and check the latest bulletin issued by Chris Heintz. It refers to the splice plates used to join the wings to the center section. Some plates have been drilled erroneously ( short edge margin ). This could lead to cracking or failure of the splice joint. Peter Ferguson 601HDS TD ________________________________________________________________________________
From: "Daniel Pelletier" <pelletie1(at)hotmail.com>
Subject: Re: Wiring diagrams
Date: Feb 03, 2001
Hi list, Is anybody have wiring diagram for Vansaircraft RV'S gauge, please contact or send by E-mail. Regards Daniel Pelletier 601HDS\SOOB > > ________________________________________________________________________________
Date: Feb 03, 2001
From: Fernando Garzon <garzon(at)nets.com>
Subject: Airlink Quick build kits
I am looking for builders who are using Airlink quickbuild kits, particularly for the CH 701. I am interested in a fast build of a 701 (I would probably just buy one assembled if the FAA would let me) with a 912 S engine. I would appreciate any info on experiences with the company, i.e. delivery time, quality of workmanship, financial dealing etc. The variability of quality and the bankruptcy rate in the experimental aircraft industry are both very large so I put a lot of merit in customer experiences. Thanks, Fernando ________________________________________________________________________________
From: "David Tellet" <telletdl(at)erols.com>
Subject: Drop Tank?
Date: Feb 03, 2001
Perhaps I'm being premature and overly complicated with this, but I am concerned about placement of fuel and/or baggage and center of gravity in the 601HD. I'm not too keen on the idea of all that gas above my feet, but I have a feeling that the wing tanks will push the CG too far aft (my passenger and I aren't lightweights). Has anyone considered a streamlined belly tank or belly baggage space? This could probably be put forward of the wing locations and would still separate the fuel from the passengers. Any thoughts? Telling me I'm crazy is okay, you wouldn't be the first. David Tellet, 601HD working on tail. ________________________________________________________________________________
From: "Mell" <kitplane(at)tradezone.com>
, ,
Subject: Builders Neat Web Site
Date: Feb 03, 2001
Hello! If any of you guys need/want a web site for your kitplane project or airplane you can create one easily here and get listed with other homebuilders: http://www.kitplanesite.com/cgi-bin/creator/creator.cgi It's pretty cool... check it out! :) Mell ________________________________________________________________________________
Date: Feb 03, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: Drop Tank?
I did not consider a belley tank, but I did have the same concerns as you do. I elected to install wing tanks. These tanks are installed in the leading edge of the outboard wings (ahead of the spar and compartment baggages). The baggage compartments can still be used. See: http://www.pcperfect.com/mthobby/ch601/images/PFuel01.jpg I estimated the CG by using the data from one of my friend's place and making changes in weight positioning (I plan for a heavier instrument panel than him, more forward gas CG and lighter engine--he uses an EA-82). In his plane, the battery is in the rear fuselage. so not archive --- David Tellet wrote: > > > Perhaps I'm being premature and overly complicated > with this, but I am > concerned about placement of fuel and/or baggage and > center of gravity in > the 601HD. I'm not too keen on the idea of all that > gas above my feet, but > I have a feeling that the wing tanks will push the > CG too far aft (my > passenger and I aren't lightweights). > > Has anyone considered a streamlined belly tank or > belly baggage space? This > could probably be put forward of the wing locations > and would still separate > the fuel from the passengers. > > Any thoughts? Telling me I'm crazy is okay, you > wouldn't be the first. > > > David Tellet, 601HD working on tail. ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Get personalized email addresses from Yahoo! Mail - only $35 a year! http://personal.mail.yahoo.com/ ________________________________________________________________________________
From: "tom tiedman" <ttiedman(at)hotmail.com>
Subject: Re: * New Bulletin from Zenith *
Date: Feb 03, 2001
Zenith sent me a letter in the mail explaining the splice plate problem and solutions... even offering free materials for the fix... new aluminum splice plates (or steel, if your edge distances are too minimal). I thought that was very nice of them to do, and you all will probably be getting the same letter shortly if you watch your mail. This sort of thing reassures me that I made the right choice by using 1/4" plate for all 4 splice plates, as the specified 1/8" and 3/16" splice plates with only 11.2mm edge distance never looked or felt quite right to me. I'm using thicker (1/8", instead of .063) and longer rear zee splice plates also. In building from plans, I found the proper edge distances to be very easy to obtain. I can't imagine anybody could end up with only 6mm to 10mm of edge distance on their splice plates, like the Zenair letter warns about. It would also be very disheartening to think that any factory pre-drilled kit splice plates might have come from the factory with only 6 to 10mm of edge distance on such critical parts. At any rate, watch your mailboxes. Tom >From: "Peter Ferguson" <pfergus2(at)tampabay.rr.com> >Reply-To: zenith-list(at)matronics.com >To: >Subject: Zenith-List: * New Bulletin from Zenith * >Date: Sat, 3 Feb 2001 08:12:50 -0500 > > > >All 601 owners and builders should go to the Zenith Builders Pages on the >web and check the latest bulletin issued by Chris Heintz. It refers to the >splice plates used to join the wings to the center section. Some plates >have >been drilled erroneously ( short edge margin ). This could lead to cracking >or failure of the splice joint. > >Peter Ferguson >601HDS TD > > ________________________________________________________________________________
From: "tom tiedman" <ttiedman(at)hotmail.com>
Subject: Re: Drop Tank?
Date: Feb 03, 2001
Hi David, I've been thinking about belly, or even under-wing mounted fuel tanks similar in shape to the belly baggage pod on the Bowers Fly-baby, that could be jettisoned in an emergency several seconds before touchdown, so I could recover them from the same field I crash-land in. I suppose wing-mounting wouldn't help CG as much as the adjustable location of a belly tank would, but either way, they all would be dropable for minimizing any post-crash fire. Still working on wing skeletons, so drop tanks are just a distant thought at this time, but you are not alone in your thinking. Tom >From: "David Tellet" <telletdl(at)erols.com> >Reply-To: zenith-list(at)matronics.com >To: >Subject: Zenith-List: Drop Tank? >Date: Sat, 3 Feb 2001 14:39:37 -0500 > > >Perhaps I'm being premature and overly complicated with this, but I am >concerned about placement of fuel and/or baggage and center of gravity in >the 601HD. I'm not too keen on the idea of all that gas above my feet, but >I have a feeling that the wing tanks will push the CG too far aft (my >passenger and I aren't lightweights). > >Has anyone considered a streamlined belly tank or belly baggage space? >This >could probably be put forward of the wing locations and would still >separate >the fuel from the passengers. > >Any thoughts? Telling me I'm crazy is okay, you wouldn't be the first. > > >David Tellet, 601HD working on tail. > > ________________________________________________________________________________
Date: Feb 03, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
Subject: Re: Drop Tank?
David Tellet wrote: > > Perhaps I'm being premature and overly complicated with this, but I am > concerned about placement of fuel and/or baggage and center of gravity in > the 601HD. I'm not too keen on the idea of all that gas above my feet, but > I have a feeling that the wing tanks will push the CG too far aft (my > passenger and I aren't lightweights). > > Has anyone considered a streamlined belly tank or belly baggage space? This > could probably be put forward of the wing locations and would still separate > the fuel from the passengers. > > Any thoughts? Telling me I'm crazy is okay, you wouldn't be the first. > > David Tellet, 601HD working on tail. > I'm thinking of designing and adding a set of drop tanks to the wings. Very similar to what they had on the P-51D mustang's. Would look kool and give me an extra 5 gallons each... No, your not crazy...You show signs of intelligence. People that think should never think they are crazy. John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: "Bill Morelli" <billvt(at)together.net>
Subject: Re: * New Bulletin from Zenith *
Date: Feb 03, 2001
WARNING!!! My kit has the splice plates that don't meet spec. !!!!!!!!!! I went to the Zenith builders pages and printed out this latest bulletin from Chris with regard to the splice plates. Today was a beutiful day here albeit cold and I was ready to fly but instead decided to check my splice plates to see if I have the described problem. First of all, there is no way to measure them without removing them. I spent about four hours pulling the plates and taking the measurements. I have an HDS so my splice plates are all 1/8" thick 6061. The bad news is that all four of my plates failed the measurement criteria. The front plates meet the edge distance minimum of 10 mm but the sizes of the plates are not as drawn by 2 to 3 mm. The closest any of the 3/8" holes get to the edge on the front plates is 12 mm. The back plates fail the edge distance measurement as well as the size measurement. Agin the size is off by 2 to 3 mm but the 3/8" holes to edge is NO GOOD. The closet one is a scant 8 mm from the edge!!!! The eight 3/8" holes on the rear plates have edge distances of 10, 9.5, 9, 9.5, 9, 9, 8, 10 So according to the bulletin, I will need two new front plates made from 6061 (since the edge distance is OK) and I will need two new rear plates made from 4130N steel since the edge distances are bad. This aircraft was built from a kit. I took delivery on 5/22/1998 so this problem goes back quite some time. My kit serial number is 6-3798. I will call Nick Monday and request the new plates and I will stay grounded until they are installed. Regards, Bill N812BM - HDS (tri) - Stratus - 5.9 flight hours - 16 landings > >All 601 owners and builders should go to the Zenith Builders Pages on the >web and check the latest bulletin issued by Chris Heintz. It refers to the >splice plates used to join the wings to the center section. Some plates have >been drilled erroneously ( short edge margin ). This could lead to cracking >or failure of the splice joint. ________________________________________________________________________________
Date: Feb 03, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
"engines-list(at)matronics.com" , "zenith-list(at)matronics.com"
Subject: ACS Cable Tension Meter
Does anyone know how to use the Aircraft Spruce Cable Tension meter. Darn thing has no instructions.... -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
Date: Feb 03, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
Subject: Re: * New Bulletin from Zenith *
Bill Morelli wrote: > This aircraft was built from a kit. I took delivery on 5/22/1998 so this > problem goes back quite some time. My kit serial number is 6-3798. > I will call Nick Monday and request the new plates and I will stay grounded > until they are installed. > > Regards, > Bill N812BM - HDS (tri) - Stratus - 5.9 flight hours - 16 landings Has anyone found these plate to show where when they did their conditional inspections. From the sounds of it, this could be a fleet wide problem. That rear plate does not have the room to keep the holes in proper check... -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: "The Meiste's" <meiste(at)essex1.com>
Subject: Re: ACS Cable Tension Meter
Date: Feb 03, 2001
> Does anyone know how to use the Aircraft Spruce Cable Tension meter. > Darn thing has no instructions.... ++++++ Hi John, I have the ACS cable tensionmeter CT-1 (hope that's the model you have). Mine did come with instructions, & I'll gladly send them to you. But to get you going it basically is operated by hooking the bottom right tab over the cable, and then pushing on the button at the end of the spring lever. You keep pushing on the bottom until the tab on the lower left touches the cable. At that point you read the cable tension on the scale. I just did this a few weeks ago on my plane. My cables seemed a little to tight with the ZAC spec of 30 - 40 LBS. I asked Nick about this, and he is now recommending to tension cables to only 25 - 35 LBS. Let me know if you would like me to send you the actual instructions. Kelly Meiste 601 HD ________________________________________________________________________________
Date: Feb 03, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
Subject: Re: ACS Cable Tension Meter
The Meiste's wrote: > > > Does anyone know how to use the Aircraft Spruce Cable Tension meter. > > Darn thing has no instructions.... > > ++++++ > Hi John, > I have the ACS cable tensionmeter CT-1 (hope that's the model you have). > Mine did come with instructions, & I'll gladly send them to you. But to get > you going it basically is operated by hooking the bottom right tab over the > cable, and then pushing on the button at the end of the spring lever. You > keep pushing on the bottom until the tab on the lower left touches the > cable. At that point you read the cable tension on the scale. > I just did this a few weeks ago on my plane. My cables seemed a little to > tight with the ZAC spec of 30 - 40 LBS. I asked Nick about this, and he is > now recommending to tension cables to only 25 - 35 LBS. > Let me know if you would like me to send you the actual instructions. > > Kelly Meiste > 601 HD > Hey Kelly, Thank you...Your instructions seem very clear and now I see how it should work.....I'm going to give it a try in the morning. If I have any questions I'll drop a note..... -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: "fhulen" <fhulen(at)gabs.net>
Subject: Splice plates
Date: Feb 04, 2001
Well..... my rear splice plates failed the 10mm minimum dimension too and due to the position that Zenith has drilled the holes through the spar and outer wings, the dimensions of the splice plate has to use every single millimeter of the material size in order not to fail the measurement test. Have any of you received the replacement parts and instructions on how we are supposed to drill the holes to match the existing holes in the wings spars? Looks like that would have to be a very exacting process in order to maintain the shear pressure evenly on all bolts. For the record, my kit was received in September of 97. Fred (should hang the Jabiru 3300 engine within this next week) ________________________________________________________________________________
From: "Bill Morelli" <billvt(at)together.net>
Subject: Re: Splice plates
Date: Feb 04, 2001
Fred, I have not spoken to ZAC yet. I plan on calling nick first thing tomorrow (Monday) to request new plates and instructions. I am not sure what the drilling instructions will entail but I suspect that we will need to use the old plates as a template and clamp them to the new plates? The other thing I might do with the steel replacements is to have them powder coated to prvent rust. Stainless would be nicer but I doubt ZAC will provide plates in stainless. What a bummer!!!!! Bill >Well..... my rear splice plates failed the 10mm minimum dimension too and >due to the position that Zenith has drilled the holes through the spar and >outer wings, the dimensions of the splice plate has to use every single >millimeter of the material size in order not to fail the measurement test. >Have any of you received the replacement parts and instructions on how we >are supposed to drill the holes to match the existing holes in the wings >spars? Looks like that would have to be a very exacting process in order to >maintain the shear pressure evenly on all bolts. For the record, my kit was >received in September of 97. >Fred (should hang the Jabiru 3300 engine within this next week) ________________________________________________________________________________
From: "The Meiste's" <meiste(at)essex1.com>
Subject: Re: ACS Cable Tension Meter
Date: Feb 04, 2001
John ... try sliding a peace of paper between the cable and the tab on the lower left as you push on the lever button. When I feel the paper getting pinched between the cable & tab I know that's my reading. Seems to work a little better than eyeballing it. Good Luck! Kelly ________________________________________________________________________________
Date: Feb 04, 2001
From: Phil Raker <phadr2(at)yahoo.com>
Subject: Re: Drop Tank?
No, David. You're not crazy! I've also considered an external fuel tank. I'm trying to decide whether to use a "ready made" drop tank type or a "conformal pod" of my own design (maybe similar to the CH801 cargo pod but only for fuel). Either one would be hung underneath the fuselage, probably mounted to the lower longerons and would be adjustable (a little bit) to position the CG as required. I'm looking at about a 10-gallon capacity to augment my standard 8-gallon firewall tank. That should give about a 3-hour range with reserves. At 100+ knots cruise, that'll give useful cross-country abilities. I plan to keep and use the wing lockers for non-liquid baggage. Phil R.; N556P, HDS/Stratus, on wheels, too cold to work, unheated shop in NW MN --- David Tellet wrote: > Has anyone considered a streamlined belly tank or > belly baggage space? > Any thoughts? Telling me I'm crazy is okay, you > wouldn't be the first. > Get personalized email addresses from Yahoo! Mail - only $35 a year! http://personal.mail.yahoo.com/ ________________________________________________________________________________
From: "fhulen" <fhulen(at)gabs.net>
Subject: Re: Splice plates
Date: Feb 04, 2001
> I am not sure what the drilling instructions will entail but I suspect that > we will need to use the old plates as a template and clamp them to the new > plates? The other thing I might do with the steel replacements is to have > them powder coated to prvent rust. Stainless would be nicer but I doubt ZAC > will provide plates in stainless. > What a bummer!!!!! > Bill ++ Ah.... Powder coating the steel plates, good idea. I may be wrong but in regard to the stainless steel, I don't think it meets the same strength as the 4130 steel. Fred ________________________________________________________________________________
From: "tom tiedman" <ttiedman(at)hotmail.com>
Subject: Re: Splice plates
Date: Feb 04, 2001
I don't think I'd be brave enough to powder coat wing splice plates. The powder coating finishes I have seen appear to me to be similar to encasing your parts in a "plastic-like" shell a couple of mm thick. I don't think I'd be able to inspect the metal plates for cracks, etc. if they were so thickly hidden from view by the powder coating. I would think that a thin coat of any zinc-based primer on steel splice plates would be much better for visual inspection as well as corrosion resistance... zinc being the sacrificial lamb to corrosion that it is, the steel and aluminum wouldn't even notice being next to each other with that zinc in between... at least not for 40 or 50 years. Tom >From: "fhulen" <fhulen(at)gabs.net> >Reply-To: zenith-list(at)matronics.com >To: >Subject: Re: Zenith-List: Splice plates >Date: Sun, 4 Feb 2001 10:45:25 -0600 > > > > I am not sure what the drilling instructions will entail but I suspect >that > > we will need to use the old plates as a template and clamp them to the >new > > plates? The other thing I might do with the steel replacements is to >have > > them powder coated to prvent rust. Stainless would be nicer but I doubt >ZAC > > will provide plates in stainless. > > What a bummer!!!!! > > Bill > >++ Ah.... Powder coating the steel plates, good idea. I may be wrong but >in regard to the stainless steel, I don't think it meets the same strength >as the 4130 steel. >Fred > > ________________________________________________________________________________
From: "Robert Isaacs" <bob999(at)worldnet.att.net>
Subject: Fuel return line
Date: Feb 04, 2001
I hope someone can give me a little direction reguarding the fuel return line. I am Installing a Multi-Port-Fuel-Injected engine in my Zodiac 601XL which has leading edge tanks, I'm am gravity feeding a 2gal header/surge tank from the 3/8" tee line coupled wing tanks. I am using a duel electric fuel pumps out of the header tank w/ 1/4" line feeding the fuel rails. The big question is should I have my fuel return line going back to the header tank or teed back to the 2 leading edge tanks? Has body worked this issue before or any susgestions would be helpfur. Bob ZODIAC N601XL ________________________________________________________________________________
Date: Feb 04, 2001
From: Phil Raker <phadr2(at)yahoo.com>
Subject: Re: Splice plates
Fred: It all depends on which stainless alloy you're talking about. Some are stronger than 4130, some not. Many are tougher, and some "stainless" alloys are not even very corrosion resistant. PHR; N556P, HDS/Stratus --- fhulen wrote: I may be wrong but > in regard to the stainless steel, I don't think it > meets the same strength as the 4130 steel. > Fred Get personalized email addresses from Yahoo! Mail - only $35 a year! http://personal.mail.yahoo.com/ ________________________________________________________________________________
From: "Jim Ingram" <jimingerman1(at)home.com>
Subject: Re: Fuel return line
Date: Feb 04, 2001
Save yourself a lot of hassle and run your return line to the header tank. This is one of the (few) good things about having a header tank that you want to take advantage of. Jim Ingram Yamhill, Oregon CH801 mazda 13B working on engine conversion ----- Original Message ----- From: "Robert Isaacs" <bob999(at)worldnet.att.net> Sent: Sunday, February 04, 2001 9:56 AM Subject: Zenith-List: Fuel return line > > I hope someone can give me a little direction reguarding the fuel return > line. I am Installing a Multi-Port-Fuel-Injected engine in my Zodiac > 601XL which has leading edge tanks, I'm am gravity feeding a 2gal > header/surge tank from the 3/8" tee line coupled wing tanks. I am using > a duel electric fuel pumps out of the header tank w/ 1/4" line feeding > the fuel rails. > The big question is should I have my fuel return line going back to the > header tank or teed back to the 2 leading edge tanks? > Has body worked this issue before or any susgestions would be helpfur. > > Bob > ZODIAC N601XL > > ________________________________________________________________________________
From: "Jim Ingram" <jimingerman1(at)home.com>
Subject: Re: Fuel return line
Date: Feb 04, 2001
I guess I should add that even more important than the fuel return itself IMO is the line from the header tank to the FI pumps and on to the fuel rail and even the rail itself. Keep this path as cool as possible. Theoretically, if you keep this path shielded from heat well enough you dont need a retun line.But, I'll have a return line AND well shielded fuel line on mine regardless of theory. ----- Original Message ----- From: "Jim Ingram" <jimingerman1(at)home.com> Sent: Sunday, February 04, 2001 10:54 AM Subject: Re: Zenith-List: Fuel return line > > Save yourself a lot of hassle and run your return line to the header tank. > This is one of the (few) good things about having a header tank that you > want to take advantage of. > Jim Ingram > Yamhill, Oregon > CH801 mazda 13B working on engine conversion > > ----- Original Message ----- > From: "Robert Isaacs" <bob999(at)worldnet.att.net> > To: > Sent: Sunday, February 04, 2001 9:56 AM > Subject: Zenith-List: Fuel return line > > > > > > > I hope someone can give me a little direction reguarding the fuel return > > line. I am Installing a Multi-Port-Fuel-Injected engine in my Zodiac > > 601XL which has leading edge tanks, I'm am gravity feeding a 2gal > > header/surge tank from the 3/8" tee line coupled wing tanks. I am using > > a duel electric fuel pumps out of the header tank w/ 1/4" line feeding > > the fuel rails. > > The big question is should I have my fuel return line going back to the > > header tank or teed back to the 2 leading edge tanks? > > Has body worked this issue before or any susgestions would be helpfur. > > > > Bob > > ZODIAC N601XL > > > > > > ________________________________________________________________________________
From: "HOLCOMBE" <holcombe(at)oregonfast.net>
Subject: Re: Splice plates
Date: Feb 04, 2001
Corosion resistance is one thing, fatigue resistance is another. Ask the designer. Richard ________________________________________________________________________________
From: "Jeff & Marcia Davidson" <jdavidso(at)fcc.net>
Subject: Robert Nuckolls seminar
Date: Feb 04, 2001
fyi The AeroElectric's annual seminar on aircraft electrical systems in George and Becki's facilities near Ft. Worth has been scheduled for the weekend of March 24/25, 2000. A reservation form has been posted at http://www.aeroelectric.com/FtWorth.html ________________________________________________________________________________
From: "fhulen" <fhulen(at)gabs.net>
Subject: Re: Splice plates
Date: Feb 04, 2001
Just like flying..... we need to "See and Avoid". Now that I have read the comments about powder coating the splice plates, "I SEE", and I will "Avoid" that as a potentual problem. I'll stick with the suggestion to stay with the 4130 steel and protect it with primer. The good advice from this group never ceases to amaze me. Thanks Fred ________________________________________________________________________________
Date: Feb 04, 2001
From: Dick Baner <db8(at)mtco.com>
Subject: Re: Fuel return line
Bob, I am in the midst of working out this exact problem so my theories are untested. At the moment I am set up to return to one of the wing tanks and let the two tanks level each other but am now concerned after discussion on this list that the leveling function will not work. The only solution seems to be what you suggest. In my case I will have to add a tank , one or two gallon, in the fuselage to put fuel into from the wing tanks and then pump the return into it. Everyone I have checked this out with says that the header tank will handle the job with little problem with air bubbles from the return. One thing different is that I was told that the fuel rails will need 3/8 line even though the return is large enough at 5/16. Dick Baner Robert Isaacs wrote: > > I hope someone can give me a little direction reguarding the fuel return > line. I am Installing a Multi-Port-Fuel-Injected engine in my Zodiac > 601XL which has leading edge tanks, I'm am gravity feeding a 2gal > header/surge tank from the 3/8" tee line coupled wing tanks. I am using > a duel electric fuel pumps out of the header tank w/ 1/4" line feeding > the fuel rails. > The big question is should I have my fuel return line going back to the > header tank or teed back to the 2 leading edge tanks? > Has body worked this issue before or any susgestions would be helpfur. > > Bob > ZODIAC N601XL > ________________________________________________________________________________
Date: Feb 04, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Rear Fuselage question...
I thought it would be an easy thing to attach 6F1-1, the fuselage bottom skin, and 6F1-2, the end skin together today... Well, when I positioned them as shown in the plans, I checked the alignment and to my surprise, the line is not straight on each side. I did some calculations and found that the angle inside the end skin is of 9.517 degrees while the same angle on the main bottom skin is 11 degrees. If we extend a line from the edge of bottom skin on the end skin, the natural line would be 7mm inside the end skin (not on the edge). How do you deal with this? Do you make the longeron 6F1-3 curved as the assembly or do you have a rivet line at a variable edge distance from the bottom skin?... or both? I verified actual measures and they match theoritical mesures that I determined with some trigonometric functions. Michel ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Get personalized email addresses from Yahoo! Mail - only $35 a year! http://personal.mail.yahoo.com/ ________________________________________________________________________________
Date: Feb 04, 2001
From: Rich <rich(at)carol.net>
Subject: Re: Fuel return line
It's true that returning fuel to one tank will not level out the 2nd. I tried it. (Unless you have a 2" or larger diameter crossover) But I also tried returning the fuel to a tee & the tee evenly brought the fuel to each tank. I had it run for 30 minutes like this & the levels were always even. This will work as long as everything is equal for both sides (lengths, diameters, etc.). I won't be using a header tank. I bought the Andair fuel selector with return & will be sending the fuel back to the tanks. Rich 801 Dick Baner wrote: > > > Bob, I am in the midst of working out this exact problem so my theories are > untested. At the moment I am set up to return to one of the wing tanks and let > the two tanks level each other but am now concerned after discussion on this > list that the leveling function will not work. The only solution seems to be > what you suggest. In my case I will have to add a tank , one or two gallon, in > the fuselage to put fuel into from the wing tanks and then pump the return into > it. Everyone I have checked this out with says that the header tank will handle > the job with little problem with air bubbles from the return. One thing > different is that I was told that the fuel rails will need 3/8 line even though > the return is large enough at 5/16. Dick Baner > > Robert Isaacs wrote: > > > > > I hope someone can give me a little direction reguarding the fuel return > > line. I am Installing a Multi-Port-Fuel-Injected engine in my Zodiac > > 601XL which has leading edge tanks, I'm am gravity feeding a 2gal > > header/surge tank from the 3/8" tee line coupled wing tanks. I am using > > a duel electric fuel pumps out of the header tank w/ 1/4" line feeding > > the fuel rails. > > The big question is should I have my fuel return line going back to the > > header tank or teed back to the 2 leading edge tanks? > > Has body worked this issue before or any susgestions would be helpfur. > > > > Bob > > ZODIAC N601XL > > > ________________________________________________________________________________
From: "Robert Isaacs" <bob999(at)worldnet.att.net>
Subject: Re: Fuel return line
Date: Feb 04, 2001
I don't know why you would need to use a fuel ine larger the the origional design by the Mfr. My EA-82T engine was fed by a 1/4" and a 1/4" return. I figured 3/8" supply and 1/4" return would suffice. The only concern I have is whether or no the pressured return line would back up into the 3/8" gravity system at idle or lean fuel consumption. ----- Original Message ----- From: "Dick Baner" <db8(at)mtco.com> Sent: Sunday, February 04, 2001 8:34 PM Subject: Re: Zenith-List: Fuel return line > > Bob, I am in the midst of working out this exact problem so my theories are > untested. At the moment I am set up to return to one of the wing tanks and let > the two tanks level each other but am now concerned after discussion on this > list that the leveling function will not work. The only solution seems to be > what you suggest. In my case I will have to add a tank , one or two gallon, in > the fuselage to put fuel into from the wing tanks and then pump the return into > it. Everyone I have checked this out with says that the header tank will handle > the job with little problem with air bubbles from the return. One thing > different is that I was told that the fuel rails will need 3/8 line even though > the return is large enough at 5/16. Dick Baner > > Robert Isaacs wrote: > > > > > I hope someone can give me a little direction reguarding the fuel return > > line. I am Installing a Multi-Port-Fuel-Injected engine in my Zodiac > > 601XL which has leading edge tanks, I'm am gravity feeding a 2gal > > header/surge tank from the 3/8" tee line coupled wing tanks. I am using > > a duel electric fuel pumps out of the header tank w/ 1/4" line feeding > > the fuel rails. > > The big question is should I have my fuel return line going back to the > > header tank or teed back to the 2 leading edge tanks? > > Has body worked this issue before or any susgestions would be helpfur. > > > > Bob > > ZODIAC N601XL > > > > ________________________________________________________________________________
From: "David Tanner" <vk3auu(at)sympac.com.au>
Subject: Re: Fuel return line
Date: Feb 05, 2001
Hi Dick, I'm not too sure why you need a return line, seems to me to be an unnecessary complication. I have flown mine for 160 hours without one. The only thing that happens is that on a hot day, the fuel in the system seems to boil when I shut the engine down and this pressurises the line from the electric pump to the carbys. A friend of mine had trouble with the return line from the header tank to the main tank in a Kitfox having an "airlock" and this resulted in pressure building up above the fuel in the header tank and it would run dry, so it would seem that your header tank also need to have a vent back to the top of one of the fuel tanks as well. David ----- Original Message ----- From: "Dick Baner" <db8(at)mtco.com> Sent: Monday, February 05, 2001 12:34 PM Subject: Re: Zenith-List: Fuel return line > > Bob, I am in the midst of working out this exact problem so my theories are > untested. At the moment I am set up to return to one of the wing tanks and let > the two tanks level each other but am now concerned after discussion on this > list that the leveling function will not work. The only solution seems to be > what you suggest. In my case I will have to add a tank , one or two gallon, in > the fuselage to put fuel into from the wing tanks and then pump the return into > it. Everyone I have checked this out with says that the header tank will handle > the job with little problem with air bubbles from the return. One thing > different is that I was told that the fuel rails will need 3/8 line even though > the return is large enough at 5/16. Dick Baner > > Robert Isaacs wrote: > > > > > I hope someone can give me a little direction reguarding the fuel return > > line. I am Installing a Multi-Port-Fuel-Injected engine in my Zodiac > > 601XL which has leading edge tanks, I'm am gravity feeding a 2gal > > header/surge tank from the 3/8" tee line coupled wing tanks. I am using > > a duel electric fuel pumps out of the header tank w/ 1/4" line feeding > > the fuel rails. > > The big question is should I have my fuel return line going back to the > > header tank or teed back to the 2 leading edge tanks? > > Has body worked this issue before or any susgestions would be helpfur. > > > > Bob > > ZODIAC N601XL > > > > ________________________________________________________________________________
Date: Feb 04, 2001
From: "Jerry Latimer" <ljm10587(at)qwest.net>
Subject: Re: * New Bulletin from Zenith *
I just checked out my splice plates. Front splice plates are fine. Rear splice plates fail. My edge distance ranged from 8.5mm to 10mm. The rear plate actually fits very loosely in the outboard wing section and are approximately 4mm shorter than the drawings. It appears that whoever radiused the plates so that they would fit the spar, took off way to much material. Some data on my aircraft: recieved kit November 1999 Serial number 6-4141 Spar was built by factory November 1998 Plates have a ZAC work order number of "MWO # 7583-4" Jerry Latimer CH601HDS all flying surfaces complete, center wing complete, and just riveted up the rear fuse. ----- Original Message ----- From: "John Tarabocchia" <zodiac.builder(at)verizon.net> Sent: Saturday, February 03, 2001 6:06 PM Subject: Re: Zenith-List: * New Bulletin from Zenith * > Bill Morelli wrote: > > > This aircraft was built from a kit. I took delivery on 5/22/1998 so this > > problem goes back quite some time. My kit serial number is 6-3798. > > I will call Nick Monday and request the new plates and I will stay grounded > > until they are installed. > > > > Regards, ________________________________________________________________________________
Date: Feb 04, 2001
From: Jim and Lucy <jpollard(at)mnsi.net>
Subject: Re: Fuel return line
Hi Bob It seem to me that a gravity fed header tank would not work very well due to the fact that there is not very much difference in the level of the wing tanks and the header tank. A fairly small obstruction of many different kinds will block the gravity feed to your header tank. Where is your header tank, on the floor in front of the spar? If that is the case you may also be planning to have those buzzy high pressure fuel pumps in there with you. May be kind of irritating listening to them all the time. There also may be a problem where if your wing tanks are not vented exactly the same, one will run down at a different rate than the other. Since you got two pumps anyway, why not put one by each wing tank and leave out the header tank. If the line from the tank will not backflow due to the design of the pump or check valves you could switch tanks simply by switching one pump on and the other pump off. No valves needed for this part of the system although you may need a valve where each line enters the cabin for emergency shut off. Now the fuel return part. Its probably better to send the tank then to send it to a Tee just before the pump. Running on the ground for a while before takeoff could build up allot of bubbles in the fuel if the same fuel is racing around and round the loop. The fuel rail is in a hot area of the engine area usually. Better to send it back to the tanks. That way you know you always have cool liquid fuel flowing to your injectors all the time. Especially at takeoff. Quite allot of fuel runs though those return lines so you will need a valve to direct it to the desired wing tank. A regular 3 way valve can do this. This is simular to what I am doing only I don"t have the return fuel problem with a carb. Jim Pollard ch601hds ea81 wing tanks only working on rad and lights. > >I hope someone can give me a little direction reguarding the fuel return >line. I am Installing a Multi-Port-Fuel-Injected engine in my Zodiac >601XL which has leading edge tanks, I'm am gravity feeding a 2gal >header/surge tank from the 3/8" tee line coupled wing tanks. I am using >a duel electric fuel pumps out of the header tank w/ 1/4" line feeding >the fuel rails. >The big question is should I have my fuel return line going back to the >header tank or teed back to the 2 leading edge tanks? >Has body worked this issue before or any susgestions would be helpfur. > >Bob >ZODIAC N601XL ________________________________________________________________________________
Date: Feb 04, 2001
From: Norris <rnorris4(at)earthlink.net>
Subject: Re: Rear Fuselage question...
Bend the longerons to follow the edge, keeping a constant edge distance. There is a note explaining this in step 11 of the rear fuselage assembly document downloaded from the builder's page of the Zenair website. Rob Norris Been there, done that. > I thought it would be an easy thing to attach 6F1-1, > the fuselage bottom skin, and 6F1-2, the end skin > together today... > > Well, when I positioned them as shown in the plans, I > checked the alignment and to my surprise, the line is > not straight on each side. I did some calculations > How do you deal with this? Do you make the longeron > 6F1-3 curved as the assembly or do you have a rivet ________________________________________________________________________________
From: "RUSSELL JOHNSON" <entec1(at)pld.com>
Subject: Re: Rear Fuselage question...
Date: Feb 05, 2001
----- Original Message ----- From: Michel Therrien <mtherr(at)yahoo.com> > I thought it would be an easy thing to attach 6F1-1, > the fuselage bottom skin, and 6F1-2, the end skin > together today... When I spliced mine together, I drew a centerline down the middle of each part and used that to align the two pieces. The edges of the sheets will not be perfectly straight with each other. Place the rivet line in the center of the lower longeron. This will be at a varying distance from the edge of 6F1-2. Once it is assembled it won't even be noticeable. I checked my wing splice plates, looks like the rear ones will need to be replaced. Hope I can find a local machinest that has a set of transfer punches. Russell Johnson / 601-HDS ________________________________________________________________________________
From: "Eric Ingraham" <iflyul(at)hotmail.com>
Subject: Re: Airlink Quick build kits
Date: Feb 05, 2001
I'm not currently doing business with them but plan to use their interior when I get to that point......I've known Danny for some time and he's a sraight up kind of guy......He's been around the kit plane business for a number of years and does beautiful work........His glass work is second to none as are his interiors.........You won't be disapointed..........Eric ________________________________________________________________________________
Date: Feb 06, 2001
From: Dejan Vucinic <n713z(at)mail.com>
Subject: splice plates: me too
My splice plates' symptoms are pretty much exactly as described in other messages. Looks like ZAC's jig (assuming they are using one) was barely within tolerances, and then whoever filed the plates down to size was too trigger-happy so there's a 2mm gap to the extrusion and 8mm edge distance on the upper outboard holes. Batch MWO #7656-9, picked up in May '99. I'd gladly pay a reasonable fee if someone has access to equipment that can properly transfer the original holes. Small business, anyone? :) Dejan Vucinic N713Z(at)mail.com FREE Personalized Email at Mail.com Sign up at http://www.mail.com/?sr=signup ________________________________________________________________________________
From: "Steven J. Devine" <steve(at)tzogon.com>
Subject: Re: splice plates: machine shop?
Date: Feb 06, 2001
I have an excellent relationship with a local/online machine shop... I am talking to them now about the possibility of them making up new plates for anyone who is interested. Will post further details when they become available. ----- Original Message ----- From: "Dejan Vucinic" <n713z(at)mail.com> Sent: Tuesday, February 06, 2001 11:23 AM Subject: Zenith-List: splice plates: me too > > I'd gladly pay a reasonable fee if someone has access to > equipment that can properly transfer the original holes. > Small business, anyone? :) > > Dejan Vucinic > N713Z(at)mail.com ________________________________________________________________________________
From: mhodges(at)sprintmail.com
Subject: Four Seater Zenith anyone?
Date: Feb 06, 2001
This may already have been distributed on the list, I'm a little behind in my reading (and building, but lets not go there!) Zenith CH640 and 4 seater CH2000 to be announced at Sun and Fun http://accumcomm.net/~ch2000/News.htm from the http://www.newplane.com site. Mitch Hodges CH601HDS Powder Springs, GA "Really I am building, my drill is just really slow" ________________________________________________________________________________
From: Z4T143(at)aol.com
Date: Feb 06, 2001
Subject: Wing Tip Light Installation Options - 801
I have heard significant discussion about mounting strobe and nav lights. =A0There seems to be two schools of thought: 1) Mount Strobe generators in the fuselage and route high voltage wires to strobes and 2) mount strobe generators on outboard wing ribs to avoid high voltage wiring past the fuel tanks. Can anyone provide the pros and cons of these two methods? Does anyone have any good or bad experience with either installation? Dave Zilz St. Peters MO e-mail: z4t143(at)aol.com web site: www.geocities.com/z4t143/ ________________________________________________________________________________
From: "Thilo Kind" <m_tkind(at)sprynet.com>
Subject: Fogging canopy
Date: Feb 06, 2001
Hi folks, sorry for my late reply to this subject, but I was out of the country for a while with no access to e-mail. It was very lousy and cold, when I pulled the plane out the outer week. As soon as I closed the canopy it began to fog. However, after starting the engine and turning on the warm air (air over muffler / Rotax 912 with two air vents in the instrument panel) it took only a few minutes to clear again. No problems in flight. Thilo Kind spent some serious money for an electrical AH. Anybody interested in a vacuum AH and a venturi (both new)? > -----Original Message----- > From: owner-zenith-list-server(at)matronics.com > [mailto:owner-zenith-list-server(at)matronics.com]On Behalf Of fhulen > Sent: Tuesday, January 23, 2001 9:19 PM > To: Zenith List > Subject: Zenith-List: Fogging canopy > > > In Bill's recent "I did it" posting about his first flight, > he mentions that > his canopy fogged up, and that he turned on the exhaust fan > and it cleared > right up. In one of the aviation magazines that I receive it > listed a "Top > 12 things" checklist of things that they thought should be > included in every > instrument panel design. A "defrost vent" on the front > screen was on that > list. This brings forth a question that I had been meaning to > post. Do any > of you have this, what's your experience, and of those of you > that don't > have this vent, have you run into times when the front canopy > fogged up to a > point that you needed or wished that you had this mentioned vent? > Thanks > Fred Getting close to hanging the 3300 engine.... > > ________________________________________________________________________________
Date: Feb 06, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Hello from Michel Therrien
Hi Peter! I did not read from you for a long time... Are you still building your CH601? How are you progressing? I tried to access your web site, but it appears to be removed... On my side, I am doing quite well, but I don't work as much as I would like on the project. Later, Michel ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Yahoo! Auctions - Buy the things you want at great prices. http://auctions.yahoo.com/ ________________________________________________________________________________
From: "HOLCOMBE" <holcombe(at)oregonfast.net>
Subject: Re: Wing Tip Light Installation Options - 801
Date: Feb 06, 2001
I mounted mine (701) in the wing tips and found the wireing simpler, in part, because I did not have to shield the high voltage wires all the way out from the fuselage. Wing tip lights can include the rear white marker light and it is not necessary to wire back to the tail and mount a light in the rudder. Richard ----- Original Message ----- From: <Z4T143(at)aol.com> Sent: Tuesday, February 06, 2001 4:19 PM Subject: Zenith-List: Wing Tip Light Installation Options - 801 > > > I have heard significant discussion about mounting strobe and nav lights. >There seems to be two schools of thought: 1) Mount Strobe generators in t> he > fuselage and route high voltage wires to strobes and 2) mount strobe > generators on outboard wing ribs to avoid high voltage wiring past the fuel > tanks. > > Can anyone provide the pros and cons of these two methods? Does anyone have> > any good or bad experience with either installation? > > Dave Zilz > St. Peters MO > e-mail: z4t143(at)aol.com > web site: www.geocities.com/z4t143/ > > ________________________________________________________________________________
From: "The Meiste's" <meiste(at)essex1.com>
Subject: Splice plates
Date: Feb 06, 2001
My 601 HD also has the bad plates. Fronts are 11 1/2 mm at the worst. Backs are 8 1/2 at the worst. Kit was picked up Jan 99 Kit # 6-3934, & MWO # 7253-4HD Still haven't heard from ZAC yet (they must be notifying the oldest planes first). Kelly Meiste ________________________________________________________________________________
From: "Thilo Kind" <m_tkind(at)sprynet.com>
Subject: I did it !!!!!!!!
Date: Feb 06, 2001
Hi Bill, just came back from a long trip from overseas (270 e-mail in my inbox...) and run across your first flight announcement. Congratulations! Believe me, I know exactly, how you feel. It's a great flying machine. Keep the blue side up Thilo Kind Thilo Kind m_tkind(at)sprynet.com ________________________________________________________________________________
Date: Feb 07, 2001
Subject: 601 XL flaps
From: "Tom Wood" <twood(at)ucf.k12.pa.us>
Can someone help me with a question? My plans call for each flap to be 2080 mm in length at the longest point before cutting the inboard edge. Each flap measures 2200mm long as received from Zenith. Why? Did I miss something? ________________________________________________________________________________
From: "Gary & Cindy" <cingar(at)mtco.com>
Subject: Stratus Installation
Date: Feb 07, 2001
I'm new to the list. I just received my firewall fwd kit from Zenair and my Subaru from Stratus. As is the case more and more as I get further along, information and prints are very poor at best. I'm searching for someone that has already completed this installation and has taken photo's of each step. I would be more than happy to pay the processing costs for a set of these photo's. Also interested in ideas for cabin heat. Thanx, Gary ________________________________________________________________________________
From: "Weston, Jim" <Jim.Weston@delta-air.com>
Subject: Splice plates
Date: Feb 07, 2001
Boy, everyone is reporting bad splice plates. Doesn't anyone have good ones. I plan to inspect mine this weekend. Jim Weston McDonough, Ga. -----Original Message----- From: The Meiste's [mailto:meiste(at)essex1.com] Sent: Tuesday, February 06, 2001 9:16 PM Subject: Zenith-List: Splice plates My 601 HD also has the bad plates. Fronts are 11 1/2 mm at the worst. Backs are 8 1/2 at the worst. Kit was picked up Jan 99 Kit # 6-3934, & MWO # 7253-4HD Still haven't heard from ZAC yet (they must be notifying the oldest planes first). Kelly Meiste ________________________________________________________________________________
From: "fhulen" <fhulen(at)gabs.net>
Subject: Re: Splice plates
Date: Feb 07, 2001
I plan to inspect mine this weekend. > > Jim Weston ++ The area that seems to be failing most of the inspections on the HDS is the first three bolt holes going through the center wing section at the top on the rear plate. Fred ________________________________________________________________________________
From: "Jeff & Marcia Davidson" <jdavidso(at)fcc.net>
Subject: Splice plates
Date: Feb 07, 2001
Evidently, the problem has been around a while. The rear splice plates on my 1994 vintage HD wings have edge distances that vary from 8.5 to 14 also. Jeff Davidson ________________________________________________________________________________
From: "Thilo Kind" <m_tkind(at)sprynet.com>
Subject: RE: Fogging canopy
Date: Feb 07, 2001
Hi Michel, no, the venturi is not a good solution. I mounted mine underneath the cowling - agreeable not the best spot. I get enough vacuum only in straight and level flight at 120 mph. That's not good enough. Besides, the venturi looks ugly and is probably a big drag contributing part. For the records: I only run an AH on the 4" venturi - both are on sale, if anybody is interested.. Thilo Kind > -----Original Message----- > From: Michel Therrien [mailto:mtherr(at)yahoo.com] > Sent: Tuesday, February 06, 2001 9:55 PM > To: m_tkind(at)sprynet.com > Subject: RE: Fogging canopy > > > Do I understand right that the venturi does not work > on the 601? I know that Bruce Brockius tried in > various positions and could not get satisfying > results... > > This said, you should consider selling it on e-Bay... > Normally, selling price relatively high. > > Regards, > > Michel > > > --- Thilo Kind wrote: > > > > > > Hi folks, > > > > sorry for my late reply to this subject, but I was > > out of the country for a > > while with no access to e-mail. > > > > It was very lousy and cold, when I pulled the plane > > out the outer week. As > > soon as I closed the canopy it began to fog. > > However, after starting the > > engine and turning on the warm air (air over muffler > > / Rotax 912 with two > > air vents in the instrument panel) it took only a > > few minutes to clear > > again. No problems in flight. > > > > Thilo Kind > > > > spent some serious money for an electrical AH. > > Anybody interested in a > > vacuum AH and a venturi (both new)? > > > > > > > -----Original Message----- > > > From: owner-zenith-list-server(at)matronics.com > > > [mailto:owner-zenith-list-server(at)matronics.com]On > > Behalf Of fhulen > > > Sent: Tuesday, January 23, 2001 9:19 PM > > > To: Zenith List > > > Subject: Zenith-List: Fogging canopy > > > > > > > > > > > > > > In Bill's recent "I did it" posting about his > > first flight, > > > he mentions that > > > his canopy fogged up, and that he turned on the > > exhaust fan > > > and it cleared > > > right up. In one of the aviation magazines that I > > receive it > > > listed a "Top > > > 12 things" checklist of things that they thought > > should be > > > included in every > > > instrument panel design. A "defrost vent" on the > > front > > > screen was on that > > > list. This brings forth a question that I had been > > meaning to > > > post. Do any > > > of you have this, what's your experience, and of > > those of you > > > that don't > > > have this vent, have you run into times when the > > front canopy > > > fogged up to a > > > point that you needed or wished that you had this > > mentioned vent? > > > Thanks > > > Fred Getting close to hanging the 3300 > > engine.... > > > > > > > > > > > > > > through > > > > http://www.matronics.com/archives > > http://www.matronics.com/emaillists > > > > Matronics! > > > > > > > > > > > > > ===== > ---------------------------- > Michel Therrien CH601-HD > http://pages.infinit.net/mthobby > http://www.pcperfect.com/mthobby/ch601 > > __________________________________________________ > Yahoo! Auctions - Buy the things you want at great prices. > http://auctions.yahoo.com/ > ________________________________________________________________________________
From: "Thilo Kind" <m_tkind(at)sprynet.com>
Subject: Splice Plates
Date: Feb 07, 2001
Hi group, I have some problems downloading the memo about the splice plate issue from ZAC's webpage - get only the first and half of the second page. Next comes a error message. Can anybody e-mail me the drawings? Thanks Thilo Kind ________________________________________________________________________________
Date: Feb 08, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
Subject: Web Site Update....
Hey Listers, I have updated my site with new pictures in the Cabin, Fuselage, and Firewall Forward sections. These include my Canopy Locking system that I devised from a simple home depot product. It also includes my fuel system and 0-200 installation and home made metal cowl..... Enjoy and good luck -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: "Steven J. Devine" <steve(at)tzogon.com>
Subject: Re: Splice Plates
Date: Feb 08, 2001
> I have some problems downloading the memo about the splice plate issue from > ZAC's webpage - get only the first and half of the second page. Next comes a > error message. Can anybody e-mail me the drawings? Download Acrobat 4.0 reader from Adobe... 3.0 (3.01...) is not compatible with the file and is producing this error message. Steve Steven J. Devine, President, Consultant, TZOGON Enterprises Incorporated President, EAA Chapter 136 (LWM/Merrimac Valley) steve@tzogon.com HAM Tech lic: N1YZJ http://www.tzogon.com http://www.tzogon.com/~steve/glass_cockpit http://www.tzogon.com/~steve/stolch801 ________________________________________________________________________________
From: "Dave Austin" <daveaustin2(at)sprint.ca>
Subject: Venturi on a 601
Date: Feb 08, 2001
Responding to the comment re use of a venturi on the 601, I've had my 4 inch unit since build, placed below the upper longeron and above the main spar on the passenger side. It has driven my AH well, and starts to spin up during takeoff. The AH is fully stabilized well before reaching 200 ft. The AH is a life-saver. The venturi is a real drag. Dave Austin 601HDS 912 with ARPLAST daveaustin2(at)sprint.ca ________________________________________________________________________________
From: STEFREE(at)aol.com
Date: Feb 08, 2001
Subject: Re: Splice Plates
Hey Bill, Could you pass those along to me as well? Thanks, Steven Freeman ________________________________________________________________________________
From: "Peter Ferguson" <pfergus2(at)tampabay.rr.com>
Subject: Jabiru FWF
Date: Feb 08, 2001
I have just received my FWF kit from Jabiru West. It was complete and packed so well, it could have carried fine china. The cowling is EXCELLENT ! The workmanship " A1 ". The engine mount matched the firewall and the airbox is neat. If you can't tell from this email, I am very happy. I had some hesitation in dealing with Mark Sarkowsky ( US agent for Jabiru ) because of some negative feed back I had received earlier. But Mark went the extra mile to reassured me and provided me with some other references. He sent some paper work for me to fill out and a list of what I should receive in the box. Five days later the FWF shows up and everything is in the box. It doesn't get better that that. Mark might be a little hard to get a hold of ( email is best ) but he is honest and I am not the least bit hesitant in dealing with him. Bad news, my splice plates ( rear ) need replacement " MWO 4959-3 ". Peter Ferguson 601HDS TD Largo FL ________________________________________________________________________________
From: "Michael Brook" <walruss(at)optushome.com.au>
Subject: joining fuselages together
Date: Feb 09, 2001
Hey guys, Sometimes I need to be reminded why building 2 701's at the same time isn't a good reason to be certified insane. Last night was one of those times. I've put the forward fuses onto the rear fuses. The first one took me about 7 hours to get tweeked up and I had a lot of angst and one sleepless night. Last night was the second go at the first one and it went together well. Using what I learnt from the first one I did the preperation on the second one and decided to give it a go. It went together in under an hour. Woooohhooooo Sooo.. now I have 2 beautiful looking fuselages downstairs ready to be fitted out and rivetted up. I'm kinda running out of room in my garage. hmmmm... THis is a good problem to have. So, for the members of the list with motivation difficulties. Build boldy and never fear the spills, for tis very few that know the rewards of flying the machine they built, over distant blue hills. Mike B. 2 701's simultaneously, 520hrs construction time, flying surfaces complete, fuses joined well and truely over the motivation hump.running out of room -----Original Message----- From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com]On Behalf Of STEFREE(at)aol.com Sent: Thursday, February 08, 2001 6:45 PM Subject: Re: Zenith-List: Splice Plates Hey Bill, Could you pass those along to me as well? Thanks, Steven Freeman ________________________________________________________________________________
From: "Robert Isaacs" <bob999(at)worldnet.att.net>
Subject: Re: Venturi on a 601
Date: Feb 08, 2001
Has anyone tried to use the manifold vacuum w/ a reserve tank for those using a Subaru engine I can't see why this won't work, you might have to supplement it with a 4" Venturi. Just asking? Any comments? Bob N601XL ----- Original Message ----- From: "Dave Austin" <daveaustin2(at)sprint.ca> Sent: Thursday, February 08, 2001 8:51 AM Subject: Zenith-List: Venturi on a 601 > > Responding to the comment re use of a venturi on the 601, I've had my 4 > inch unit since build, placed below the upper longeron and above the main > spar on the passenger side. It has driven my AH well, and starts to spin up > during takeoff. The AH is fully stabilized well before reaching 200 ft. > The AH is a life-saver. The venturi is a real drag. > Dave Austin 601HDS 912 with ARPLAST > daveaustin2(at)sprint.ca > > ________________________________________________________________________________
From: "Bill Morelli" <billvt(at)together.net>
Subject: Splice Plate Update
Date: Feb 08, 2001
I received my replacement splice plates yesterday from ZAC along with instructions and two drill guides and drill bits. Today I spent about four hours making the two new steel plates match my two rear aluminum plates. They came out perfectly. All 10 holes in each plate match the originals. I followed the ZAC instructions pretty much to the letter. The only thing I did differently was that ZAC said to drill all four 3/8" holes (with pilot holes using the drill guide) with the plate clamped to the OB spar. I only did that with one upper and one lower 3/8" hole. Then removed the plate and drilled the pilot hole which was a #7 size hole up to 3/8" using progressively larger bits till the 3/8" drill Then I simply bolted the new and old plate together through the 3/8" holes and pilot drilled all of the other holes on a drill press (using the drill guides supplied)which included the two remaining 3/8" and six 5/16" holes again stepping up in drill sizes until the final size was reached. I had some reservations about using he pilot hole and simply drilling in this stepped up fashion. I was assured by two A & P mechanics and a retired machinist the hangs out at the airport that the drills would self align as I drilled each succeeding size and they were 100% correct. I can put the old 6061 rear plate and new 4130 rear plate together and slip all 10 bolts in as snug as the originals supplied by ZAC. If anyone want the ZAC instructions to look over I can scan the document and e-mail it. I was going to change the front plates but decided not to at this time anyway ( I may never change them). The front plates all have good edge distance and are only slightly smaller (top to bottom) than the spec. shows. The edge distance on all the holes in the spars is OK. My new 4130 plates are at the paint shop getting primed and will go back in on Saturday. Hopefully I will be back in the air by Sunday. ZAC did not request that I send back these drill guides and bits but I probably will anyway so they can pass them on to someone else. Regards, Bill ________________________________________________________________________________
Date: Feb 08, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: Venturi on a 601
This was discussed on the AirSoob list a while ago... apparently it was affecting the performance of the engine either at idle or at speed, but I don't remember exactly. One interesting thing tough is that a different approach was discussed. Some tried putting a tube at an angle in the exhaust system to create a vacuum. It seems to work better. We would need to consult those archives to find more. Michel --- Robert Isaacs wrote: > > > Has anyone tried to use the manifold vacuum w/ a > reserve tank for those > using a Subaru engine I can't see why this won't > work, you might have to > supplement it with a 4" Venturi. > Just asking? Any comments? > > Bob > N601XL > ----- Original Message ----- > From: "Dave Austin" <daveaustin2(at)sprint.ca> > To: "Zenith list" > Sent: Thursday, February 08, 2001 8:51 AM > Subject: Zenith-List: Venturi on a 601 > > > > > > > Responding to the comment re use of a venturi on > the 601, I've had my 4 > > inch unit since build, placed below the upper > longeron and above the main > > spar on the passenger side. It has driven my AH > well, and starts to spin > up > > during takeoff. The AH is fully stabilized well > before reaching 200 ft. > > The AH is a life-saver. The venturi is a real > drag. > > Dave Austin 601HDS 912 with ARPLAST > > daveaustin2(at)sprint.ca > > > > > > > > through > > http://www.matronics.com/archives > http://www.matronics.com/emaillists > > Matronics! > > > > > ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Get personalized email addresses from Yahoo! Mail - only $35 a year! http://personal.mail.yahoo.com/ ________________________________________________________________________________
From: "Chuck Deiterich" <cfd(at)tstar.net>
Subject: Re: joining fuselages together
Date: Feb 08, 2001
Mike, How do you do it? I've got about 1400 hrs in my (just 1) 701 and have wings, tail, slats, flaperons and most of the rear fuselage and some of the front fuselage done. I sure hope that Zenith has figured out the geometry so the firewall will really be at 73 degrees to the horizontal reference line. Because I don't see any room to adjust the firewall. Chuck D. ----- Original Message ----- From: Michael Brook <walruss(at)optushome.com.au> Sent: Friday, February 09, 2001 12:45 AM Subject: Zenith-List: joining fuselages together > > Hey guys, > > Sometimes I need to be reminded why building 2 701's at the same time isn't > a good reason to be certified insane. Last night was one of those times. > > I've put the forward fuses onto the rear fuses. The first one took me about > 7 hours to get tweeked up and I had a lot of angst and one sleepless night. > Last night was the second go at the first one and it went together well. > Using what I learnt from the first one I did the preperation on the second > one and decided to give it a go. It went together in under an hour. > Woooohhooooo > > Sooo.. now I have 2 beautiful looking fuselages downstairs ready to be > fitted out and rivetted up. I'm kinda running out of room in my garage. > hmmmm... THis is a good problem to have. > > So, for the members of the list with motivation difficulties. > > Build boldy and never fear the spills, > for tis very few that know the rewards > of flying the machine they built, > over distant blue hills. > > Mike B. 2 701's simultaneously, 520hrs construction time, flying surfaces > complete, fuses joined well and truely over the motivation hump.running out > of room ________________________________________________________________________________
From: "fhulen" <fhulen(at)gabs.net>
Subject: Jabiru U.S. distribution
Date: Feb 09, 2001
I received a message this morning that indicated that Jabiru West might not be the U.S. distributor any longer. I went to the Jabiru webb site in Australia and sure enough, it says that Jabiru distrubution in the United States is being re-organized and that for now we should contact them. I had heard a rumor about a month ago that a big change was going to happen after the first of the year and that Jabiru owners would be very happy with what would be coming in the next few months. I checked the Jabiru West site and all pages are gone except one, that one saying that you can contact Mark Sarkowski by email. The rest of the site is gone. Fred Area 41 Snailworks ________________________________________________________________________________
Date: Feb 09, 2001
Subject: Re: 601 XL flaps
From: Michael R Fortunato <wizard-24(at)juno.com>
Don't know if you ever got your question answered, and I don't have the plans in front of me, so I may not be of much help...... But having built both my flaps, I seem to remember having to cut them to size, and leaving them a bit long until installing them against the fuselage, when the final cut can be made more precisely. Mike Fortunato 601XL Tail section, rear fuse, and left wing done. writes: > > Can someone help me with a question? > > My plans call for each flap to be 2080 mm in length at the > longest point > before cutting the inboard edge. Each flap measures 2200mm long > as > received from Zenith. Why? Did I miss something? > ________________________________________________________________________________
From: PWalsh8045(at)aol.com
Date: Feb 10, 2001
Subject: fuel filter...and oil
H What is everyone using for a fuel filter for the 912? I have been using a small clear plastic...filter from acsp...kind of a hard "sand" type. I recall reading somewhere not to use the paper type filters...so I havent...but it seems thats all there is really....so....any thoughts?... Also...what oil is best used with auto gas in the 912..in Texas.....and what weight...the manual is not too clear on this....I have been using a fully synthetic motorcycle oil with gear additive only...but cant find it anymore...certainly an auto parts store should have all we need..... Thanks in advance Patrick Walsh....200 + hrs...601 HD ________________________________________________________________________________
Date: Feb 10, 2001
From: Bill Izard <bill(at)izard.co.nz>
Subject: Re: fuel filter...and oil
Please remove me from your Mailing List. I`m get 40- 50 emails from your company each day ,all I want is Tailwind information Regards Bill Izard > >H > What is everyone using for a fuel filter for the 912? > I have been using a small clear plastic...filter from acsp...kind of a hard >"sand" type. I recall reading somewhere not to use the paper type >filters...so I havent...but it seems thats all there is really....so....any >thoughts?... > Also...what oil is best used with auto gas in the 912..in Texas.....and > what >weight...the manual is not too clear on this....I have been using a fully >synthetic motorcycle oil with gear additive only...but cant find it >anymore...certainly an auto parts store should have all we need..... > Thanks in advance >Patrick Walsh....200 + hrs...601 HD > > ------------------------- Izard Industries Ltd P.O.Box 477 Masterton New Zealand The Izard Family http://mysite.xtra.co.nz/~izard/page1.html Phone 64 6 3788862 Fax 64 6 3788649 Mobile 025 463 254 ________________________________________________________________________________
From: "Bill Morelli" <billvt(at)together.net>
Subject: Splice plate tooling
Date: Feb 10, 2001
Today I finished installing the new 4130 rear splice plates. Aircraft is all back together and will fly tomorrow weather permitting. I shipped the drill guides and drill bits I received from ZAC to Dejan Vucinic, N713Z(at)mail.com so he can use them next. If anyone wants them, contact Dejan and I'm sure he would be glad to pass them along. For you builders that are weight conscious, each 4130 rear plate weights 1.5 lbs more than the 6061 plate for an increase in gross weight of 3.0 lbs. Regards, Bill ________________________________________________________________________________
Date: Feb 11, 2001
From: Andrew SanClemente <ansancle(at)townisp.com>
Subject: Instrument Panel
Hi, For those of you that are flying or near so I have a question on your instrument panel layout (601 HDS). Most layouts have the nav-comms, gps, etc.. located in the middle or to the right. When flying with the center stick does this present a problem when needing to change settings on these instruments? Im doing my panel layout now and would really like to hear the comments of those who are flying, Thanks Andrew SanClemente 90% complete for 2 years now ;) ________________________________________________________________________________
From: "Steve Danielson" <steved(at)nc.rr.com>
Subject: Re: Instrument Panel - Radios on left with center stick?
Date: Feb 11, 2001
On my 701 the com radio and gps are on the left of the panel and the regular instruments and engine instruments were toward the center. At first I thought it looked wierd (I wasn't the original builder) but it worked out really great and feels totally natural to me now. When I am in a 152 or something it looks wierd to me now that all the instruments are jammed at the left side of the panel... I could do all the stuff with my left hand, radio, gps, and puch to talk, and keep my right hand on the stick. I too have wondered the same thing because I have seen plenty of our panels with all the radios and stuff in the middle. I wonder how I would change frequencies on a climbout from a controlled airport or something for example. Here is a picture of my panel: http://home.nc.rr.com/danielson/cockpit.jpg Steve Danielson http://home.nc.rr.com/danielson/ ----- Original Message ----- From: "Andrew SanClemente" <ansancle(at)townisp.com> Sent: Sunday, February 11, 2001 10:22 AM Subject: Zenith-List: Instrument Panel > > Hi, > For those of you that are flying or near so I have a question on your > instrument panel layout (601 HDS). Most layouts have the nav-comms, gps, > etc.. located in the middle or to the right. When flying with the center > stick does this present a problem when needing to change settings on these > instruments? Im doing my panel layout now and would really like to hear the > comments of those who are flying, > Thanks > Andrew SanClemente > > 90% complete for 2 years now ;) > > ________________________________________________________________________________
From: "The Meiste's" <meiste(at)essex1.com>
Subject: 601 Throttle Cable Stop
Date: Feb 11, 2001
Would anyone out there know why ZAC supplies two Throttle Cable Stops (6E5-2) with their FWF kit (for the tri-gear style 601)? I'm trying to install this today. I see on drawing 6E5 that it shows the Throttle Cable Stop installed on the firewall & angled up to the top shelf with an "L" joining all three parts. I just don't see where the second Throttle Cable Stop would be installed? Thanks to anyone who can comment on this! Kelly Meiste 601 HD Tri-Gear ________________________________________________________________________________
Date: Feb 11, 2001
Subject: Re: Instrument Panel
From: Jim <jashford(at)hawaii.rr.com>
Andrew, I have an in panel King Radio and Transponder located center with trans. at bottom. No problem with access in flight. I do have my portable Garmin GPS velcroed to the top of a pedestal from the panel to the floor. To read it, I have to bend a bit forward to see around the stick. If I have to make any changes in the entries, I "unstick" it from the velcro for easy access. You are getting close! Jim Ashford 601 HDS 912 tri ________________________________________________________________________________
Date: Feb 11, 2001
From: Rich <rich(at)carol.net>
Subject: Re: Venturi on a 601
Are you talking about using the manifold vacuum for the vacuum instruments like the DG, artificial horizon, etc.? Rich 801 Robert Isaacs wrote: > > > Has anyone tried to use the manifold vacuum w/ a reserve tank for those > using a Subaru engine I can't see why this won't work, you might have to > supplement it with a 4" Venturi. > Just asking? Any comments? > > Bob > N601XL > ----- Original Message ----- > From: "Dave Austin" <daveaustin2(at)sprint.ca> > To: "Zenith list" > Sent: Thursday, February 08, 2001 8:51 AM > Subject: Zenith-List: Venturi on a 601 > > > > > Responding to the comment re use of a venturi on the 601, I've had my 4 > > inch unit since build, placed below the upper longeron and above the main > > spar on the passenger side. It has driven my AH well, and starts to spin > up > > during takeoff. The AH is fully stabilized well before reaching 200 ft. > > The AH is a life-saver. The venturi is a real drag. > > Dave Austin 601HDS 912 with ARPLAST > > daveaustin2(at)sprint.ca > > > > > ________________________________________________________________________________
Date: Feb 12, 2001
From: Dejan Vucinic <n713z(at)mail.com>
Subject: tools, heavy splice plates
Received my new splice plates a few days ago, with instructions but no tools. I suppose ZAC ran out or stopped including tools when they realized the magnitude of the problem... Anyway, Bill Morelli has graciously offered to pass along the drills and drill guides he got from ZAC. If you'd like me to send you the tools when I finish my plates write me your snail-mail address at N713Z(at)mail.com. I must admit that I was taken by surprise when I was handed the package by the UPS person, so I measured the old and new plates. The original rear plates weigh just a tad under 600 grams. The two new 4130 ones are 1800 grams. Ouch! I wonder if a lightening hole or two is permissible in the center. --dv FREE Personalized Email at Mail.com Sign up at http://www.mail.com/?sr=signup ________________________________________________________________________________
Date: Feb 11, 2001
Subject: Re: Venturi on a 601
From: clydes-shop(at)juno.com
HI: Rich The use of manifold vacuum is too unreliable to use with gyros. They need to be kept real clean other wise the gyros are short lived ,I know because I am a retired Instrument Technician of 41 years experience. It works with vacuum pumps pumps or Venturi that use fans in front of it that is streamlined In remote areas > > Are you talking about using the manifold vacuum for the vacuum > instruments like the DG, artificial horizon, etc.? > > Rich > 801 > > > Robert Isaacs wrote: > > > > > > > Has anyone tried to use the manifold vacuum w/ a reserve tank for > those > > using a Subaru engine I can't see why this won't work, you might > have to > > supplement it with a 4" Venturi. > > Just asking? Any comments? > > > > Bob > > N601XL > > ----- Original Message ----- > > From: "Dave Austin" <daveaustin2(at)sprint.ca> > > To: "Zenith list" > > Sent: Thursday, February 08, 2001 8:51 AM > > Subject: Zenith-List: Venturi on a 601 > > > > > > > > > Responding to the comment re use of a venturi on the 601, I've > had my 4 > > > inch unit since build, placed below the upper longeron and above > the main > > > spar on the passenger side. It has driven my AH well, and > starts to spin > > up > > > during takeoff. The AH is fully stabilized well before reaching > 200 ft. > > > The AH is a life-saver. The venturi is a real drag. > > > Dave Austin 601HDS 912 with ARPLAST > > > daveaustin2(at)sprint.ca > > > > > > > > > > > > > > > Yours truly Clyde D. Ehlers ________________________________________________________________________________
From: "David Tanner" <vk3auu(at)sympac.com.au>
Subject: Radial Engine
Date: Feb 12, 2001
Members of the list might be interested to know that one Slepcev Storch is now flying with a 7 cylinder, 120 h.p. radial engine designed and made locally in Australia. My informant said that the Storch had a take off run of about 20 yards and then climbed out at 45 degrees. The engine has 2.8 litre capacity and if I remember right, swings a 75 inch propellor. I have no other details at the moment. David Tanner ________________________________________________________________________________
From: "Randy L. Thwing" <n4546v(at)mindspring.com>
Subject: 701, 7.F.6.1 rivet size & pitch
Date: Feb 11, 2001
Listers: I've finally restarted on my 701 project, could anyone advise the rivet size and spacing to attach part no. 7.F.6.1 to the rear fuselage lower skin? I can't seem to find it in the plans. I also need clarification regarding the rivet size used to attach the longerons to the rear fuselage skins. My location coordinates refer to a location on the plans measured from the printed borders, the first number is across from the left border and the second number is down from the top border in mm, like a road map. On plans sheet 7.F.6 at location (110, 215) is the note: "Longerons Rivets A4 pitch 40 (except splice + rear end). At location (220, 215) is the note: "rivets A5 pitch 40 (longerons top + bottom) shown within arrows like you switch to A5's for the forward portion at some point. Do you use A4 full length on the longerons or is there some point up front where you switch to A5? Started again and immediately stuck again. Regards, Randy L. Thwing, 701 plans ________________________________________________________________________________
Date: Feb 11, 2001
From: Elbie(at)aol.com (by way of Matt Dralle 925-606-1001 <dralle(at)matronics.com>)
Subject: Announcement
2/9/2001 Fellow Pilots and Builders: EM aviation is pleased to announce that the RiteAngle III Angle of Attack system is in production. I know this has been a long, long wait for some of you, however I will not sell a system that is not up to my standards. The long delay was partially caused by the total new design required after the RiteAngle 2000 system was terminated. The remainder of the delay was insuring the system met all our requirements such as both hot and cold environment testing. The first production group of systems off the line are being again extensively tested for approximately 2 weeks before we deliver any systems to insure there are no "bugs" appearing. When all production testing is accomplished I will ship according to who has sent in the order form via fax or US mail. (Again, DO NOT send your credit card number via e-mail! I DO NOT have a secure e-mail line.) If you want a spot in line for early delivery you can request this via e-mail, and mail your check or CC number. At present time I estimate 4- 10 weeks before your delivery, depending on when I receive your payment. To those of you who have been in correspondence with me for the last year, thanks for your belief in EM aviation's product, and soon you will have a product in your hands. I honor my correspondence of the quoted price. Current price $295 + mount & options see web site for information. www.riteangle.com Elbie Mendenhall President EM Aviation, LLC P NE Prairie Rd Brush Prairie WA 98606 360-260-0772 www.riteangle.com ________________________________________________________________________________
Date: Feb 11, 2001
From: Norris <rnorris4(at)earthlink.net>
Subject: Re: Splice plate tooling
Bill Morelli wrote: > For you builders that are weight conscious, each 4130 rear plate weights 1.5 > lbs more than the 6061 plate for an increase in gross weight of 3.0 lbs. Actually it results in an increase in empty weight. Gross weight stays the same. I need new rear plates also, but I don't know yet if I have to use the 4130 or can get away with Al. Does ANYONE have Zenair produced plates that meet the specs? Rob Norris One step forward, two steps back. ________________________________________________________________________________
From: Sjl219(at)aol.com
Date: Feb 12, 2001
Subject: Re: 701, 7.F.6.1 rivet size & pitch
Randy, Use A5 on the longeron splices (all four of them, of course) and use A5 on the forward longerons, starting from about the middle of the bottom access hole. Use A4 whenever A5 is not specified; thus rivet the 7F6-1 channel to the bottom of the rear fuselage with A4. Do not be discouraged! I have been working nearly since 1997 on my "four hundred hour" "easy to build" "first time builder" CH701. Stan - CH701/"everything finished" but the fuselage, engine and instruments...... ________________________________________________________________________________
From: "Chuck Deiterich" <cfd(at)tstar.net>
Subject: Re: 701, 7.F.6.1 rivet size & pitch
Date: Feb 12, 2001
Randy, From: Randy L. Thwing <n4546v(at)mindspring.com> > Listers: > I've finally restarted on my 701 project, could anyone advise the > rivet size and spacing to attach part no. 7.F.6.1 to the rear fuselage > lower skin? I can't seem to find it in the plans. use A4 pitch 40 I also need > clarification regarding the rivet size used to attach the longerons to > the rear fuselage skins. My location coordinates refer to a location on > the plans measured from the printed borders, the first number is across > from the left border and the second number is down from the top border > in mm, like a road map. On plans sheet 7.F.6 at location (110, 215) is > the note: "Longerons Rivets A4 pitch 40 (except splice + rear end). At > location (220, 215) is the note: "rivets A5 pitch 40 (longerons top + > bottom) shown within arrows like you switch to A5's for the forward > portion at some point. Do you use A4 full length on the longerons or is > there some point up front where you switch to A5? Use A4 pitch 40 on longerons except use A5 at longeron splices, on longerons forward of uprights 7.F.5.4, for horisontal tail attach brackets and lower rudder hinge 7.F.4.2. Bolts on upper rudder hinge. ZAC has a 701 construction manual update on their web site, but beware there are some typos. Chuck D. ________________________________________________________________________________
From: "Eric Ingraham" <iflyul(at)hotmail.com>
Subject: Re: Radial Engine
Date: Feb 12, 2001
Hi David.....the engine you're speaking of is the Rotec R-8000. It can be found at WWW.rotecradialengines.com.....You can E-mail them at cherna(at)netstra.com.au......The engine weighs 194 lbs all up.....seems a bit on the heavy side for a 701......You might want to check www.aviator.cc/engines.html..."Eric's Homebuilt Aircraft Engine Directory".........It's a great site with a lot of info.....Take care and fly safe.......Eric (no relation to the site listed above.....I only wish I could take credit for it......te Guy does a great job!) >From: "David Tanner" <vk3auu(at)sympac.com.au> >Reply-To: zenith-list(at)matronics.com >To: >Subject: Zenith-List: Radial Engine >Date: Mon, 12 Feb 2001 15:47:31 +1100 > > >Members of the list might be interested to know that one Slepcev Storch is >now flying with a 7 cylinder, 120 h.p. radial engine designed and made >locally in Australia. My informant said that the Storch had a take off run >of about 20 yards and then climbed out at 45 degrees. The engine has 2.8 >litre capacity and if I remember right, swings a 75 inch propellor. I have >no other details at the moment. > >David Tanner > > ________________________________________________________________________________
From: Sjl219(at)aol.com
Date: Feb 12, 2001
Subject: Re: 601 rivet size
Tom, when I started my 701 I called the factory and asked if it would be ok if I used A5s throughout. They asked me why I would want to do that. I said because then the airplane would be stronger. They took me apart! Bottom line: Chris Heintz knows what he's doing and part of the cost of our kits includes his expertise and there's a high probability that he has a better handle on stresses than most of us do. Now, at my local EAA chapter, all the old timers think pop rivets are for sissies and they wanted me to buck rivet the whole airplane; they also wanted me to use thicker skins and beef up the internal structures. In other words, they wanted me to turn the 701 into a Beechcraft. I determined then and there that I would build my airplane to the specs as exactly as I could and that the only "mods" I would consider would be nonstructural or aesthetic such as where the instruments go on my panel and where I mount the ELT. Well, for what it's worth, this is my opinion about rivets although I must say that emotionally, I sure like the heft of an A5 compared to an A4. stan. ________________________________________________________________________________
From: "Gary & Cindy" <cingar(at)mtco.com>
Subject: Re: 601 Throttle Cable Stop
Date: Feb 12, 2001
I just called on that one the other day...Talked to Nick...he said some had broken them when trying to make the bend. One is all that you use. He also said not to attach the choke cables as shown on drawings because the 90 deg bend after the firewall will make it too stiff. Gary -----Original Message----- From: The Meiste's <meiste(at)essex1.com> Date: Sunday, February 11, 2001 10:49 AM Subject: Zenith-List: 601 Throttle Cable Stop > >Would anyone out there know why ZAC supplies two Throttle Cable Stops >(6E5-2) with their FWF kit (for the tri-gear style 601)? >I'm trying to install this today. I see on drawing 6E5 that it shows the >Throttle Cable Stop installed on the firewall & angled up to the top shelf >with an "L" joining all three parts. I just don't see where the second >Throttle Cable Stop would be installed? >Thanks to anyone who can comment on this! > >Kelly Meiste >601 HD Tri-Gear > > ________________________________________________________________________________
From: "Vince Veltri" <vijan(at)home.com>
Subject: Airspeed Indicator for sale
Date: Feb 12, 2001
I sold my project and have a United Model 8100, True Airspeed Indicator with the range marks for a 601HDS silk screened. This is advertised in TAP for about $395. I will sell for $250. Vince ________________________________________________________________________________
From: "Darryl West" <rdwest(at)cadvision.com>
Subject: Re: Splice plate tooling
Date: Feb 12, 2001
I have not been able to produce a totally legible print from the 601-splice-plate.pdf file downloaded from Zenair's builder website. The light grey fine print dimensions on the sketches is very faint and missing some detail on the printout, making it difficult to read the number values, even on the best quality setting and blown up to 11"x17". The actual pdf file can be magnified on-screen to reveal all details, but not the print. Is everybody else having this problem also? Darryl ________________________________________________________________________________
From: "HOLCOMBE" <holcombe(at)oregonfast.net>
Subject: Re: 601 rivet size
Date: Feb 12, 2001
Follow the plans, all part of K.I.S.S. Try squeezing A-5s all day and see if the unneeded extra beef still looks so good. Richard ________________________________________________________________________________
From: "Daniel Pelletier" <pelletie1(at)hotmail.com>
Subject: Re: Airspeed Indicator for sale
Date: Feb 13, 2001
Hi Vince What the size of your True airspeed Daniel 601 HDS >From: "Vince Veltri" <vijan(at)home.com> >Reply-To: zenith-list(at)matronics.com >To: >Subject: Zenith-List: Airspeed Indicator for sale >Date: Mon, 12 Feb 2001 18:23:24 -0500 > > >I sold my project and have a United Model 8100, True Airspeed Indicator >with the range marks for a 601HDS silk screened. This is advertised in >TAP for about $395. I will sell for $250. Vince > > ________________________________________________________________________________
From: Sjl219(at)aol.com
Date: Feb 12, 2001
Subject: Re: 601 rivet size
Tom, visit my project website at http://hometown.aol.com/sjl219/index.html and you will clearly see why I fall into the category of "those who adhere strictly to the plans." stan CH701 ________________________________________________________________________________
From: "Vince Veltri" <vijan(at)home.com>
Subject: Re: Airspeed Indicator for sale
Date: Feb 12, 2001
Daniel, It fits a standard 3-1/8" hole. Vince ----- Original Message ----- From: "Daniel Pelletier" <pelletie1(at)hotmail.com> Sent: Monday, February 12, 2001 9:29 PM Subject: Re: Zenith-List: Airspeed Indicator for sale > > > Hi Vince > > What the size of your True airspeed > > Daniel 601 HDS > > > >From: "Vince Veltri" <vijan(at)home.com> > >Reply-To: zenith-list(at)matronics.com > >To: > >Subject: Zenith-List: Airspeed Indicator for sale > >Date: Mon, 12 Feb 2001 18:23:24 -0500 > > > > > >I sold my project and have a United Model 8100, True Airspeed Indicator > >with the range marks for a 601HDS silk screened. This is advertised in > >TAP for about $395. I will sell for $250. Vince > > > > > > ________________________________________________________________________________
From: "fhulen" <fhulen(at)gabs.net>
Subject: Re:Splice plate instruction printing
Date: Feb 12, 2001
> I have not been able to produce a totally legible print from the > 601-splice-plate.Is > everybody else having this problem also? > ++ Yes.... I finally went up to the upper left corner of my computer and clicked on "file" which brings down the options, clicked on "print" and up came the box with "properties". I clicked on "Properties" box and found after trying a print at better quality, that the only way to get a really great print was to move the quality button all the way over to best quality, then I got a great print. Fred ________________________________________________________________________________
Date: Feb 12, 2001
Subject: Re: Splice plate tooling
From: Jim <jashford(at)hawaii.rr.com>
Darryl, I had the same problem, so I e-mailed ZAC for the two drawings. Linda said, "they're in the mail" Jim Ashford 601 HDS > From: "Darryl West" <rdwest(at)cadvision.com> > Reply-To: zenith-list(at)matronics.com > Date: Mon, 12 Feb 2001 18:17:25 -0700 > To: > Subject: Re: Zenith-List: Splice plate tooling > > > I have not been able to produce a totally legible print from the > 601-splice-plate.pdf file downloaded from Zenair's builder website. The > light grey fine print dimensions on the sketches is very faint and missing > some detail on the printout, making it difficult to read the number values, > even on the best quality setting and blown up to 11"x17". The actual pdf > file can be magnified on-screen to reveal all details, but not the print. Is > everybody else having this problem also? > > Darryl > > > > > > ________________________________________________________________________________
Date: Feb 13, 2001
From: Mike Fothergill <mfothergill(at)sympatico.ca>
Subject: Re: Instrument Panel
Hi; Some suggestions re: radios. Keep the GPS and VHF separated as much as possible. The GPS's radiate a fair bit of noise. Box in the GPS in metal and make sure it is well grounded. Separate the coax from the VHF coax. I fyou find that you have to set the squelch on the VHF higher to cut out the noise when the GPS is on, then you have some work to do. Regards Mike UHS Spinners Andrew SanClemente wrote: > > > Hi, > For those of you that are flying or near so I have a question on your > instrument panel layout (601 HDS). Most layouts have the nav-comms, gps, > etc.. located in the middle or to the right. When flying with the center > stick does this present a problem when needing to change settings on these > instruments? Im doing my panel layout now and would really like to hear the > comments of those who are flying, > Thanks > Andrew SanClemente > > 90% complete for 2 years now ;) > ________________________________________________________________________________
Date: Feb 13, 2001
Subject: Zodiac 601 XL Sport Plane Catagory
From: "Tom Wood" <twood(at)ucf.k12.pa.us>
Does anyone know whether the 601XL zodiac will qualify for the proposed sport plane catagory? ________________________________________________________________________________
From: "Bill Steer" <bsteer(at)gwi.net>
Subject: Re: Zodiac 601 XL Sport Plane Catagory
Date: Feb 13, 2001
It doesn't appear that, with an advertised stall speed of 49 mph with flaps, it will meet the 44 mph stall speed criteria. Bill ----- Original Message ----- From: "Tom Wood" <twood(at)ucf.k12.pa.us> Sent: Tuesday, February 13, 2001 4:30 PM Subject: Zenith-List: Zodiac 601 XL Sport Plane Catagory > > Does anyone know whether the 601XL zodiac will qualify for the proposed > sport plane catagory? > > ________________________________________________________________________________
From: George Pinneo <George.Pinneo(at)trw.com>
Subject: Splice plate tooling
Date: Feb 13, 2001
My rear splice plates, 3/16" 6061, 1994-era, plates meet the specs mailed out by Chris H. GGP ________________________________________________________________________________
Date: Feb 13, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
"engines-list(at)matronics.com" , "zenith-list(at)matronics.com"
Subject: O-200 Woes
Today was the day I would start my used 0-200. Everything was checked, fuel, electrical, oil added. Well I sat in the cockpit and started to turn on the appropriate switches. I then pulled the handle for the pull starter. It turned several times and didn't fire up. Well it hasn't been running in over a year. I figured it would take a little working. Then I tried it again, while the starter was engaged , there was a loud bang and the prop stopped cold. I got out to investigate and found that the prop would not move. I got real nervous at this point. Once I realized that something was wrong internally I started to look for the likely suspect. I pulled the alternator off and found the the gear on the alternator broke off completely. This stopped the motor from turning. Then I looked to see if there was any more damage. Well I found, when I took the starter off, that the engaging gear was ground down very bad. I inspected the engine case gears and found that the starter gear had only a bit of grazing and really didn't look to bad. Now I'm left with a ton of questions. I called Wentworth Aircraft, where I purchased the engine, and they said they would replace any parts required. Which I found to be fair at this time. I also have some ground up metal from the ground starter gear on internal parts of the engine (gears, case and mag gears, ect.). How do I get these properly cleaned up. Or do I let the oil carry it away when I finally do get it started up. Any help or comments would be greatly appreciated. -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: "Schemmel, Grant" <Schemmel(at)utmc.aeroflex.com>
Subject: O-200 Woes
Date: Feb 13, 2001
John Having just finished my overhaul (under A&P supervision) I would recommend that you wash down the whole area with mineral spirits, which will go down into the sump. Then pull the sump off (not a big deal) and clean it out. You might want to pull the sump and inspect it before you wash it down too, just to see how much sludge is in there. Grant Schemmel 601HDS - O-200 -----Original Message----- From: John Tarabocchia [mailto:zodiac.builder(at)verizon.net] Sent: Tuesday, February 13, 2001 3:28 PM zenith-list(at)matronics.com Subject: Zenith-List: O-200 Woes Today was the day I would start my used 0-200. Everything was checked, fuel, electrical, oil added. Well I sat in the cockpit and started to turn on the appropriate switches. I then pulled the handle for the pull starter. It turned several times and didn't fire up. Well it hasn't been running in over a year. I figured it would take a little working. Then I tried it again, while the starter was engaged , there was a loud bang and the prop stopped cold. I got out to investigate and found that the prop would not move. I got real nervous at this point. Once I realized that something was wrong internally I started to look for the likely suspect. I pulled the alternator off and found the the gear on the alternator broke off completely. This stopped the motor from turning. Then I looked to see if there was any more damage. Well I found, when I took the starter off, that the engaging gear was ground down very bad. I inspected the engine case gears and found that the starter gear had only a bit of grazing and really didn't look to bad. Now I'm left with a ton of questions. I called Wentworth Aircraft, where I purchased the engine, and they said they would replace any parts required. Which I found to be fair at this time. I also have some ground up metal from the ground starter gear on internal parts of the engine (gears, case and mag gears, ect.). How do I get these properly cleaned up. Or do I let the oil carry it away when I finally do get it started up. Any help or comments would be greatly appreciated. -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: "Graham Byass" <gbyass(at)cygnus.uwa.edu.au>
Subject: Splice plate tooling
Date: Feb 13, 2001
Darryl It may be related to your printer - I tried printing it out on a good quality inkjet printer and had the same problems but when I used a laser printer all was revealed. Graham Byass Western Australia -----Original Message----- From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com]On Behalf Of Darryl West Sent: Tuesday, 13 February 2001 9:17 Subject: Re: Zenith-List: Splice plate tooling I have not been able to produce a totally legible print from the 601-splice-plate.pdf file downloaded from Zenair's builder website. The light grey fine print dimensions on the sketches is very faint and missing some detail on the printout, making it difficult to read the number values, even on the best quality setting and blown up to 11"x17". The actual pdf file can be magnified on-screen to reveal all details, but not the print. Is everybody else having this problem also? Darryl ________________________________________________________________________________
From: "Robert Isaacs" <bob999(at)worldnet.att.net>
Subject: Re: Venturi on a 601
Date: Feb 13, 2001
Yes, with the additional use of a vacuum reserve tank and check valve. ----- Original Message ----- From: "Rich" <rich(at)carol.net> Sent: Sunday, February 11, 2001 7:41 PM Subject: Re: Zenith-List: Venturi on a 601 > > Are you talking about using the manifold vacuum for the vacuum > instruments like the DG, artificial horizon, etc.? > > Rich > 801 > > > Robert Isaacs wrote: > > > > > > Has anyone tried to use the manifold vacuum w/ a reserve tank for those > > using a Subaru engine I can't see why this won't work, you might have to > > supplement it with a 4" Venturi. > > Just asking? Any comments? > > > > Bob > > N601XL > > ----- Original Message ----- > > From: "Dave Austin" <daveaustin2(at)sprint.ca> > > To: "Zenith list" > > Sent: Thursday, February 08, 2001 8:51 AM > > Subject: Zenith-List: Venturi on a 601 > > > > > > > > Responding to the comment re use of a venturi on the 601, I've had my 4 > > > inch unit since build, placed below the upper longeron and above the main > > > spar on the passenger side. It has driven my AH well, and starts to spin > > up > > > during takeoff. The AH is fully stabilized well before reaching 200 ft. > > > The AH is a life-saver. The venturi is a real drag. > > > Dave Austin 601HDS 912 with ARPLAST > > > daveaustin2(at)sprint.ca > > > > > > > > > > ________________________________________________________________________________
From: "Kent Brown" <kbplanner(at)email.msn.com>
Subject: Re: Splice plate tooling
Date: Feb 13, 2001
Just checked my splice plates, kit 6-4046, Nov '99, front plates OK, but will need the 4130 rear plates. Kent ----- Original Message ----- From: Norris <rnorris4(at)earthlink.net> Sent: Sunday, February 11, 2001 9:43 PM Subject: Re: Zenith-List: Splice plate tooling > > Bill Morelli wrote: > > > For you builders that are weight conscious, each 4130 rear plate weights 1.5 > > lbs more than the 6061 plate for an increase in gross weight of 3.0 lbs. > > Actually it results in an increase in empty weight. Gross weight stays > the same. I need new rear plates also, but I don't know yet if I have to > use the 4130 or can get away with Al. Does ANYONE have Zenair produced > plates that meet the specs? > > Rob Norris > One step forward, two steps back. > > ________________________________________________________________________________
From: "Kent Brown" <kbplanner(at)email.msn.com>
Subject: Re: Splice plate tooling
Date: Feb 13, 2001
I had same problem with two different printers, and finally just wrote the numbers on by hand. Kent ----- Original Message ----- From: Darryl West <rdwest(at)cadvision.com> Sent: Monday, February 12, 2001 5:17 PM Subject: Re: Zenith-List: Splice plate tooling > > I have not been able to produce a totally legible print from the > 601-splice-plate.pdf file downloaded from Zenair's builder website. The > light grey fine print dimensions on the sketches is very faint and missing > some detail on the printout, making it difficult to read the number values, > even on the best quality setting and blown up to 11"x17". The actual pdf > file can be magnified on-screen to reveal all details, but not the print. Is > everybody else having this problem also? > > Darryl > > ________________________________________________________________________________
Date: Feb 13, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
Subject: Re: O-200 Woes
"Schemmel, Grant" wrote: > > John > > Having just finished my overhaul (under A&P supervision) I would recommend that you wash down the whole area with mineral spirits, which will go down into the sump. Then pull the sump off (not a big deal) and clean it out. > > You might want to pull the sump and inspect it before you wash it down too, just to see how much sludge is in there. > > Grant Schemmel > 601HDS - O-200 > Hi Grant, Your suggestion mirrors what my mechanic suggested. The engine never really started. So I think that the particles are confined to the gear case area. After doing this I will have my mechanic take a look. If there is any evidence of particle going beyond the case, I will tear the whole thing down. At that point with the engine disassembled I think I will bite the bullet and overhaul it. I'm curious as to your own overhaul. I will definitely want to do it myself too. But I don't have the luxury of the airport and my A&P nearby. I have an overhaul manual and lots of people that I can get good advice from. Was it overly complicated or is just follow the manual. I have a good solid idea as to the way it should be done. But that isn't the same a experience. I would also like to do with new millennium cylinders. Also have the crank and cam sent out ot get reconditioned. Any tips would be greatly appreciated.... I would also like to that you for your suggestion... -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: "Thilo Kind" <m_tkind(at)sprynet.com>
Subject: Tach
Date: Feb 13, 2001
Hi folks, have a problem. I installed the Engine Information System (EIS)from Grand Rapid Technology in my 601 HDS with Rotax 912. The unit is performing as advertised; I can highly recommend it. Besides other parameters, the EIS shows the RPM of the engine. However, the EIS allows to select several different screen; not all of them show the RPM. 151 SQ from A/S made for the Rotax 912). This tach gets the signal from the same wire than the EIS. In the lower RPM range (below 3000 RPM) both units display the same RPMs. However, as soon as the RPM exceeds 3000 RPM, the needle of the Micro - 1000 goes immediately all the way around and stops at the 6 o'clock position. The EIS on the other hand works fine throughout the whole RPM range. I have no explanation for that. I tried already several options: - the RPM signal wire was replaced with a shielded wire - the EIS was disconnected (only the Micro - 1000 was connected) - the Micro - 1000 was exchanged against a new unit All measurements showed no success. Anybody with an idea? Anybody has an address, where I can contact the manufacturer? Thanks, folks Thilo Kind 25.1 hours so far - this a great flying machine Thilo Kind m_tkind(at)sprynet.com ________________________________________________________________________________
Date: Feb 13, 2001
From: Dick Baner <db8(at)mtco.com>
Subject: Re: Tach
Thilo, I suggest that you call Greg at EIS and explain your problem to him. Even though the problem does not seem to be with his instrument he is always very willing to work out problems for users and may be able to help. I am no one to give advice on electrical matters but I seem to recall that the tach settings can be extremely tricky and sometimes on what version of the instrument you have. Also some of the sender lines have resistors built into the line and could affect the other tach as you said the same source line went to both instruments. Anyway greg may have the answer on the tip of his brain and he is a pleasant guy to talk to in any event. Dick Baner Thilo Kind wrote: > > Hi folks, > > have a problem. I installed the Engine Information System (EIS)from Grand > Rapid Technology in my 601 HDS with Rotax 912. The unit is performing as > advertised; I can highly recommend it. > > Besides other parameters, the EIS shows the RPM of the engine. However, the > EIS allows to select several different screen; not all of them show the RPM. > 151 SQ from A/S made for the Rotax 912). This tach gets the signal from the > same wire than the EIS. In the lower RPM range (below 3000 RPM) both units > display the same RPMs. However, as soon as the RPM exceeds 3000 RPM, the > needle of the Micro - 1000 goes immediately all the way around and stops at > the 6 o'clock position. The EIS on the other hand works fine throughout the > whole RPM range. > > I have no explanation for that. I tried already several options: > - the RPM signal wire was replaced with a shielded wire > - the EIS was disconnected (only the Micro - 1000 was connected) > - the Micro - 1000 was exchanged against a new unit > > All measurements showed no success. Anybody with an idea? Anybody has an > address, where I can contact the manufacturer? > > Thanks, folks > > Thilo Kind > 25.1 hours so far - this a great flying machine > > Thilo Kind m_tkind(at)sprynet.com > ________________________________________________________________________________
Date: Feb 14, 2001
Subject: Re: O-200 Woes
From: Joey Powell <joeypowell(at)earthlink.net>
on 2/13/01 5:28 PM, John Tarabocchia at zodiac.builder(at)verizon.net wrote: > > > Today was the day I would start my used 0-200. Everything was checked, > fuel, electrical, oil added. Well I sat in the cockpit and started to > turn on the appropriate switches. I then pulled the handle for the pull > starter. It turned several times and didn't fire up. Well it hasn't > been running in over a year. I figured it would take a little working. > Then I tried it again, while the starter was engaged , there was a loud > bang and the prop stopped cold. I got out to investigate and found that > the prop would not move. I got real nervous at this point. Once I > realized that something was wrong internally I started to look for the > likely suspect. I pulled the alternator off and found the the gear on > the alternator broke off completely. This stopped the motor from > turning. Then I looked to see if there was any more damage. Well I > found, when I took the starter off, that the engaging gear was ground > down very bad. I inspected the engine case gears and found that the > starter gear had only a bit of grazing and really didn't look to bad. > > Now I'm left with a ton of questions. I called Wentworth Aircraft, > where I purchased the engine, and they said they would replace any parts > required. Which I found to be fair at this time. I also have some > ground up metal from the ground starter gear on internal parts of the > engine (gears, case and mag gears, ect.). How do I get these properly > cleaned up. Or do I let the oil carry it away when I finally do get it > started up. > > Any help or comments would be greatly appreciated. > > -- > > John W. Tarabocchia > > 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html > > Airframe 100% Complete... > Installing Wire and Engine... > > > > > > > If anyone knows a more reliable way to clean out an engine than taking it completely to pieces - I'd like to hear it! Joey Powell 801 kit to be collected next month ________________________________________________________________________________
Date: Feb 14, 2001
From: Mark Wood <mawood(at)zoo.uvm.edu>
Subject: Re: O-200 Woes
> > Having just finished my overhaul (under A&P supervision) I would > recommend that you wash down the whole area with mineral spirits, which > will go down into the sump. Then pull the sump off (not a big deal) and > clean it out. > Grant Schemmel > > 601HDS - O-200 > >Hi Grant, >Your suggestion mirrors what my mechanic suggested. .... >I'm curious as to your own overhaul. I will definitely want to do it >myself too. But I don't have the luxury of the airport and my A&P >nearby. I have an overhaul manual and lots of people that I can get good >advice from. >Was it overly complicated or is just follow the manual. I have a good >solid idea as to the way it should be done. But that isn't the same a >experience. I would also like to do with new millennium cylinders. Also >have the crank and cam sent out ot get reconditioned. > >Any tips would be greatly appreciated.... I would also like to that you >for your suggestion... >John W. Tarabocchia >601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html John I am rebuilding my O-200 as a winter project (I can do this in the basement rather than out in the cold garage) Aircraft Spruce has a video on rebuilding the O-200 which sells for $25. Not a bad price for some peace of mind. Mark Wood N221MW ________________________________________________________________________________
From: "Melanie @ Thilo Kind" <m_tkind(at)sprynet.com>
Subject: Re: Tach
Date: Feb 14, 2001
Hi Dick, I talked already with Greg. He indeed is a very helpful guy and very knowledagble, but couldn't help me with the tach. Best regards Thilo Kind ----- Original Message ----- From: Dick Baner <db8(at)mtco.com> Sent: Wednesday, February 14, 2001 12:38 AM Subject: Re: Zenith-List: Tach > > Thilo, I suggest that you call Greg at EIS and explain your problem to him. > Even though the problem does not seem to be with his instrument he is always > very willing to work out problems for users and may be able to help. I am no > one to give advice on electrical matters but I seem to recall that the tach > settings can be extremely tricky and sometimes on what version of the instrument > you have. Also some of the sender lines have resistors built into the line and > could affect the other tach as you said the same source line went to both > instruments. Anyway greg may have the answer on the tip of his brain and he is > a pleasant guy to talk to in any event. Dick Baner > > Thilo Kind wrote: > > > > > Hi folks, > > > > have a problem. I installed the Engine Information System (EIS)from Grand > > Rapid Technology in my 601 HDS with Rotax 912. The unit is performing as > > advertised; I can highly recommend it. > > > > Besides other parameters, the EIS shows the RPM of the engine. However, the > > EIS allows to select several different screen; not all of them show the RPM. TA > > 151 SQ from A/S made for the Rotax 912). This tach gets the signal from the > > same wire than the EIS. In the lower RPM range (below 3000 RPM) both units > > display the same RPMs. However, as soon as the RPM exceeds 3000 RPM, the > > needle of the Micro - 1000 goes immediately all the way around and stops at > > the 6 o'clock position. The EIS on the other hand works fine throughout the > > whole RPM range. > > > > I have no explanation for that. I tried already several options: > > - the RPM signal wire was replaced with a shielded wire > > - the EIS was disconnected (only the Micro - 1000 was connected) > > - the Micro - 1000 was exchanged against a new unit > > > > All measurements showed no success. Anybody with an idea? Anybody has an > > address, where I can contact the manufacturer? > > > > Thanks, folks > > > > Thilo Kind > > 25.1 hours so far - this a great flying machine > > > > Thilo Kind m_tkind(at)sprynet.com > > > > ________________________________________________________________________________
From: "Schemmel, Grant" <Schemmel(at)utmc.aeroflex.com>
Subject: O-200 Woes
Date: Feb 14, 2001
Hi John In my case, I bought an engine from a wrecked 150, and didn't get the logs with it, so because of that fact, and because I found oil in the mags I decided to do the teardown. Turns out to be a good thing too, as 3 of the 4 cylinders were cracked, with the 4th beyond limits. I ended up getting 4 new cyl. assys from ECI. It also pays to shop around for parts - I got a bunch of them from Don George Aircraft in Florida, some from Sacramento Sky Ranch, and some from El Reno Air, but they are pretty pricey. As to the process itself, I pretty much just followed the latest revision of the overhaul manual. I only had a few questions for my A&P while doing so. Mostly it's pretty straightforward, with the only real tricky part being the case reassembly. One bit of advice I got from my A&P I should pass on - instead of buying all the different gasketing compounds recommended by TCM, use Permatex Ultra Copper for most everything. It's good to 700F, makes a great seal, and cleans up pretty easily. I sent all of my internal steel parts off to Aircraft Specialties for magnafluxing and balancing (except the cam, which was beyond limits). I also sent the case off to Divco to be lapped and line bored, as my A&P says o-200's tend to get a bit larger in the center bearing area over time. They did a really nice job too. Replaced most of the parts recommended by the overhaul SB from the TCMLink website, and did all my parts cleaning with either mineral spirits or carb cleaner out in my garage. Everything else I did in my basement. Now that most everything is together, I have to find a way to get the engine back out to the garage. Hope this helps. Grant Schemmel -----Original Message----- From: John Tarabocchia [mailto:zodiac.builder(at)verizon.net] Sent: Tuesday, February 13, 2001 9:31 PM Subject: Re: Zenith-List: O-200 Woes "Schemmel, Grant" wrote: > > John > > Having just finished my overhaul (under A&P supervision) I would recommend that you wash down the whole area with mineral spirits, which will go down into the sump. Then pull the sump off (not a big deal) and clean it out. > > You might want to pull the sump and inspect it before you wash it down too, just to see how much sludge is in there. > > Grant Schemmel > 601HDS - O-200 > Hi Grant, Your suggestion mirrors what my mechanic suggested. The engine never really started. So I think that the particles are confined to the gear case area. After doing this I will have my mechanic take a look. If there is any evidence of particle going beyond the case, I will tear the whole thing down. At that point with the engine disassembled I think I will bite the bullet and overhaul it. I'm curious as to your own overhaul. I will definitely want to do it myself too. But I don't have the luxury of the airport and my A&P nearby. I have an overhaul manual and lots of people that I can get good advice from. Was it overly complicated or is just follow the manual. I have a good solid idea as to the way it should be done. But that isn't the same a experience. I would also like to do with new millennium cylinders. Also have the crank and cam sent out ot get reconditioned. Any tips would be greatly appreciated.... I would also like to that you for your suggestion... -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
Date: Feb 14, 2001
From: Keith Maloney <kmaloney(at)lsil.com>
Subject: Splice plates
I am scratch building but double checked my plates anyway. The larger holes that come in pairs seem to be the only ones covered by the service request. Mine are well within tolarence, but the last one of the top three smaller holes is down to 8mm due to the angle on the top of the plate. I've double checked the plans and everything is dimentionaly correct. Are the 3/16 plates supplied by Zenith this way or do they have more edge distance on that last top hole? I guess you could angle the line of holes to match the splice plate, but I kept mine in the center of the extrusion flange. Thanks, Keith Maloney ________________________________________________________________________________
From: "Randy L. Thwing" <n4546v(at)mindspring.com>
Subject: 701 rear fuselage bulkhead plans errors
Date: Feb 14, 2001
Listers: Could 701 builders please advise how they addressed the following: On plans page 7.F.2.3, the rear bottom fuselage skin is cut out 156 mm wide (78 x 2) at the location of the rear bulkhead (7.F.1.3) and cut out 247 mm wide (123.5 x 2) at the location of the front bulkhead (7.F.1.4), yet on plans page 7.F.1, they have you construct the rear bulkheads 6mm wider, 162 mm & 253 mm respectively. Of course once you attach the longerons (following the plans) to the bottom rear fuselage skin, it is 6mm too narrow and the bulkheads won't fit without jamming them in and creating a bulge. This is not addressed in the 240 plus corrections available from ZA. I am plans building so I can just scrap my perfectly good bulkheads I made according to the plans and build another set that will actually fit the fuselage. Could a kit builder measure these parts and fuselage widths as furnished by ZA and advise how they differ from the plans? Could other plans builders advise how they addressed this error? 6mm isn't much, but it's a fair distance to spread the longerons. All help is appreciated. Regards, Randy L. Thwing, 701 plans, started out strong but stalled by the plans again ________________________________________________________________________________
From: "tom tiedman" <ttiedman(at)hotmail.com>
Subject: Re: Splice plates
Date: Feb 14, 2001
Hi Keith, I'm scratchbuilding mine also. That most inboard 5/16" hole you mention was the most difficult to get proper edge distance (on the smaller plate, because of the angle on the top edge of the splice plate). If I was at 11.2mm as in the plans, then I would wind up too close to the lower edge of the spar cap... and vice versa. I split the 29mm distance between the top edge of the plate and bottom edge of the spar cap at that bolt location, drew a center line, and to make double sure I didn't get too close to either edge, I then drew 5/16" parallel lines, with the previously drawn center line as their center line also. This was so I could watch as the drill bit bit, to make sure no part of the drill touched either parallel line. When done, The edge distances on that hole turned out to be about 10-1/4mm to the top edge of the splice plate, and 10-1/2mm to the bottom edge of the cap, so my drill did want to travel north a teeny bit. Using 1/4" splice plates, I am not concerned about the 10-1/4mm top edge distance at those two inboard bolt locations. In my 1993 plans, Chris says 10mm is minimum acceptable anyway, so I just squeaked by there! Drilling with proper edge distance was also simplified by having the smaller plates facing up when setting the wing dihedral and drilling your splice plate bolt holes. If you can keep the bolt holes in the smaller plates to proper edge distance while drilling, you know the larger plates underneath, hidden from view, will have proper edge distance, being that they are larger and all. I guess the only way to achieve the desired 11.2mm edge distance on that pesky inboard 5/16" bolt would be to decrease the angle of the wing dihedral. Not me, I'll keep the dihedral to plan, as I'm after a more stable, less touchy control feel. Hope this helps all the scratchbuilders. Tom >From: Keith Maloney <kmaloney(at)lsil.com> >Reply-To: zenith-list(at)matronics.com >To: "zenith-list(at)matronics.com" >Subject: Zenith-List: Splice plates >Date: Wed, 14 Feb 2001 09:41:39 -0700 > > > I am scratch building but double checked my plates anyway. The larger >holes that come in pairs seem to be the only ones covered by the service >request. Mine are well within tolarence, but the last one of the top >three smaller holes is down to 8mm due to the angle on the top of the >plate. I've double checked the plans and everything is dimentionaly >correct. Are the 3/16 plates supplied by Zenith this way or do they >have more edge distance on that last top hole? I guess you could angle >the line of holes to match the splice plate, but I kept mine in the >center of the extrusion flange. > >Thanks, >Keith Maloney > > ________________________________________________________________________________
From: "tom tiedman" <ttiedman(at)hotmail.com>
Subject: Re: Zodiac 601 XL Sport Plane Catagory
Date: Feb 14, 2001
Nope, HDS stall speed's too high. I'm hoping the HD qualifys, I think it will just squeak by. Tom >From: "Tom Wood" <twood(at)ucf.k12.pa.us> >Reply-To: zenith-list(at)matronics.com >To: zenith-list(at)matronics.com >Subject: Zenith-List: Zodiac 601 XL Sport Plane Catagory >Date: Tue, 13 Feb 2001 13:30:15 -0800 > > >Does anyone know whether the 601XL zodiac will qualify for the proposed >sport plane catagory? > > ________________________________________________________________________________
Date: Feb 14, 2001
From: Jerry Jensen <jensenm(at)jps.net>
Subject: Re: Splice Plate tooling
Received my rear splice plates from Zenith, without tooling but a list of tools that are needed. I would like to be placed on the list of builders who are sharing the tooling. I will then pass them on to the next builder. 601HDS, Jabiru 3300, 90% (??). Jerry Jensen ________________________________________________________________________________
From: "Schemmel, Grant" <Schemmel(at)utmc.aeroflex.com>
Subject: RE: O-200 Woes
Date: Feb 14, 2001
Hi John In my case, I bought an engine from a wrecked 150, and didn't get the logs with it, so because of that fact, and because I found oil in the mags I decided to do the teardown. Turns out to be a good thing too, as 3 of the 4 cylinders were cracked, with the 4th beyond limits. I ended up getting 4 new cyl. assys from ECI. It also pays to shop around for parts - I got a bunch of them from Don George Aircraft in Florida, some from Sacramento Sky Ranch, and some from El Reno Air, but they are pretty pricey. As to the process itself, I pretty much just followed the latest revision of the overhaul manual. I only had a few questions for my A&P while doing so. Mostly it's pretty straightforward, with the only real tricky part being the case reassembly. One bit of advice I got from my A&P I should pass on - instead of buying all the different gasketing compounds recommended by TCM, use Permatex Ultra Copper for most everything. It's good to 700F, makes a great seal, and cleans up pretty easily. I sent all of my internal steel parts off to Aircraft Specialties for magnafluxing and balancing (except the cam, which was beyond limits). I also sent the case off to Divco to be lapped and line bored, as my A&P says o-200's tend to get a bit larger in the center bearing area over time. They did a really nice job too. Replaced most of the parts recommended by the overhaul SB from the TCMLink website, and did all my parts cleaning with either mineral spirits or carb cleaner out in my garage. Everything else I did in my basement. Now that most everything is together, I have to find a way to get the engine back out to the garage. Hope this helps. Grant Schemmel -----Original Message----- From: John Tarabocchia [mailto:zodiac.builder(at)verizon.net] Sent: Tuesday, February 13, 2001 9:31 PM Subject: Re: Zenith-List: O-200 Woes "Schemmel, Grant" wrote: > > John > > Having just finished my overhaul (under A&P supervision) I would recommend that you wash down the whole area with mineral spirits, which will go down into the sump. Then pull the sump off (not a big deal) and clean it out. > > You might want to pull the sump and inspect it before you wash it down too, just to see how much sludge is in there. > > Grant Schemmel > 601HDS - O-200 > Hi Grant, Your suggestion mirrors what my mechanic suggested. The engine never really started. So I think that the particles are confined to the gear case area. After doing this I will have my mechanic take a look. If there is any evidence of particle going beyond the case, I will tear the whole thing down. At that point with the engine disassembled I think I will bite the bullet and overhaul it. I'm curious as to your own overhaul. I will definitely want to do it myself too. But I don't have the luxury of the airport and my A&P nearby. I have an overhaul manual and lots of people that I can get good advice from. Was it overly complicated or is just follow the manual. I have a good solid idea as to the way it should be done. But that isn't the same a experience. I would also like to do with new millennium cylinders. Also have the crank and cam sent out ot get reconditioned. Any tips would be greatly appreciated.... I would also like to that you for your suggestion... -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: "ron dewees" <rdewees(at)mindspring.com>
Subject: splice plates
Date: Feb 14, 2001
Hi fellow builders.. I have sent for my new plates and have read with interest the procedures for re-centering holes in new plates. I got a new Harbor Freight catalog today and saw an item I never noticed before. It was a self-centering hinge drill. I think it's for sinking hinge screws in the exact center of hinge plates on doors. It has a tapered brass collar around a 1/8" drill bit and does what we need to do.. center a small pilot hole in a second surface without danger of scoring the original hole. It was only $3.00 and I will send for it if others think it would do the job. Ron DeWees 601HDS/TD ________________________________________________________________________________
From: "Shay King" <shaking(at)eircom.net>
Subject: 701 wingtips
Date: Feb 14, 2001
Dear List, I'll soon be doing my first 701 wingtip. So far the dimensions given, with revisions, don't seem to make a lot of sense. Are the cut lines in the top and bottom skins meant to be straight or curved? Should the top and bottom skins end at the end of the tip rib? If anyone can give me a few tips, [pardon the pun], I'd be very grateful. Regards, Shay King. ________________________________________________________________________________
From: "L.D. Pahnke" <ldpahnke(at)netwitz.net>
Subject: Re: splice plates
Date: Feb 14, 2001
. I got a new Harbor Freight catalog today and saw an item I never noticed before. It was a self-centering hinge drill. Ron, I have this tool and believe it would be too small. Hinge screw holes are #10 and this tool is about that size. It would not center properly in a 3/8th in. hole in my opinion. A better investment for not much more would be Harbor Freights' set of transfer punches which are designed for this purpose. Doug ________________________________________________________________________________
From: "Bill Morelli" <billvt(at)together.net>
Subject: Re: splice plates
Date: Feb 14, 2001
Ron, My only concern with that is it may be difficult to keep the drill straight. You need to drill the first couple of pilot holes with the new plate clamped to the OB spar. Since you have to use hand drill I would be leary about making sure that everything is perfectly square. Seems like you could be slightly off with the tapered collar. With the drill guides that ZAC calls out, there is no danger of that happening as the drill guide fits snugly inside the 3/8" hole in the spar. Just my two cents worth. The drill guides from McMaster-Carr are about $7.00 each. Regards, Bill >It has a tapered brass collar >around a 1/8" drill bit and does what we need to do.. center a small >pilot hole in a second surface without danger of scoring the original >hole. It was only $3.00 and I will send for it if others think it would >do the job. >Ron DeWees ________________________________________________________________________________
From: "fhulen" <fhulen(at)gabs.net>
Subject: Re: splice plates
Date: Feb 14, 2001
> The drill guides from McMaster-Carr are about $7.00 each. > Regards, > Bill ++ Bill, how serviceable will these guides and things be after being used, handed off to another builder, and so forth, on and on. Assuming each builder only needs to do rear plates, that's 20 holes per builder. 6 builders X 20 holes will be 120 holes through this guide. Will the guides be likely to hold close enough tolerances by the time it gets to the 6 th. builder, or even further on down the line? Fred ________________________________________________________________________________
From: Sjl219(at)aol.com
Date: Feb 14, 2001
Subject: Re: 701 rear fuselage bulkhead plans errors
Randy, I'm building from kit. My skins were dimensioned as per plans. Also, my bottom skin had pilot holes to locate the placement of 7.F.1.4 and 7.F.1.3. All I had to do was drill through the center of the flanges to establish bulkhead placement. This is apparently idiot proofed, right?? Here's what happened. When I attached the side skins to the bulkheads, the bulkheads seemed to be too narrow for the fuselage position that ZAC committed me to by virtue of the predrilled bottom skin. I had to reposition the bulkheads slightly at the top in order to get an acceptable rivet seating. Now, I'm left with a bulkhead-to-bulkhead distance greater than the plans call for. Since the stabilizer supports MUST be attached with A5 rivets ON the bulkhead rivet lines, I have no latitude to move these supports to and fro. Without this latitude, I cannot "trap" the stabilizer mounting flanges with proper edge distance for the bolt holes. My solution will be to make WIDER stabilizer supports with a few extra rivets added. IMHO, the kit has some "problems" in this area also! If I were you, I'd just use common sense and build a couple of bulkheads that fit YOUR fuselage and will properly accept YOUR stabilizer supports based on YOUR stabilizer flange measurements. Stan ________________________________________________________________________________
From: "Bill Morelli" <billvt(at)together.net>
Subject: Re: splice plates
Date: Feb 14, 2001
Fred, The guides appeared to be made out of some sort of hardened steel but I honestly can't say how long they would last. I just looked in the McMaster-Carr catalog. They are actually called drill bushings. The description says they are made from case hardened steel with a Rockwell C scale hardness of 62-65. Of course that means nothing to me. Regards, Bill - 8.2 flight hours - 18 landings >++ Bill, how serviceable will these guides and things be after being used, >handed off to another builder, and so forth, on and on. Assuming each >builder only needs to do rear plates, that's 20 holes per builder. 6 >builders X 20 holes will be 120 holes through this guide. Will the guides >be likely to hold close enough tolerances by the time it gets to the 6 th. >builder, or even further on down the line? >Fred > > ________________________________________________________________________________
From: Sjl219(at)aol.com
Date: Feb 14, 2001
Subject: Re: 701 wingtips
Shay, The lines ARE meant to be curved. There are "problems" with the plan coordinates according to Nick. But I didn't know that at the time I built my wings. I ended up adding an "L" to the end of the wingtip extension to bring it out far enough to "catch" the skin (based on the erroneous data points I had). So, in the end, my wings are a bit longer than called for. But there are no real "forces" acting up way out there so what the heck, the tips are unlikely to fall off. My experience was that it took me over 20 hours to build the first wing tip and about 8 hours to complete the other one. If you talk to Nick, he may tell you what he told me - just to draw a gentle curve from the end of the wingtip extension to the rear spar. That's not much to go on, I know. If you use the coordinates from the plans, you'll have to "extend" the wingtip extension. Be very careful building these wingtips - I inadvertantly built some washout into one of mine because, with nothing "solid" out there to "anchor" things building gets tricky. Just ONE extra rib out there would have made all the difference in the world for a firsttime builder like me. I see a really big trim tab hanging off my future airplane! stan. ________________________________________________________________________________
From: "ron dewees" <rdewees(at)mindspring.com>
Subject: Re: splice plates
Date: Feb 14, 2001
THanks Doug, I wondered if it would be large enough. Ron ----- Original Message ----- From: "L.D. Pahnke" <ldpahnke(at)netwitz.net> Sent: Wednesday, February 14, 2001 3:14 PM Subject: Re: Zenith-List: splice plates > > . I got a new Harbor Freight > catalog today and saw an item I never noticed before. It was a > self-centering hinge drill. > > Ron, I have this tool and believe it would be too small. Hinge screw holes > are #10 and this tool is about that size. It would not center properly in a > 3/8th in. hole in my opinion. A better investment for not much more would > be Harbor Freights' set of transfer punches which are designed for this > purpose. Doug > > ________________________________________________________________________________
From: "Chuck Deiterich" <cfd(at)tstar.net>
Subject: Re: 701 wingtips
Date: Feb 14, 2001
Shay, I made a sample tip skin out of cardboard, and kept trimming it till it fit then transferred to metal. The wing top and bottom skins end at the curved L's at the tip. Chuck D. ----- Original Message ----- From: Shay King <shaking(at)eircom.net> Sent: Wednesday, February 14, 2001 4:34 PM Subject: Zenith-List: 701 wingtips > > Dear List, > I'll soon be doing my first 701 wingtip. So far the > dimensions given, with revisions, don't seem to make a lot of sense. > Are the cut lines in the top and bottom skins meant to be straight or > curved? > Should the top and bottom skins end at the end of the tip rib? > If anyone can give me a few tips, [pardon the pun], I'd be very > grateful. > > Regards, > Shay King. > > ________________________________________________________________________________
From: "ldpahnke" <ldpahnke(at)netwitz.net>
Subject: Re: splice plates
Date: Feb 14, 2001
Hi All: I am not sure I understand the criteria for requesting 4130 plates vs. 6061 alum. plates for replacement. I have a good copy of the announcement from the web site but do not think I understand it properly. What I think I am reading is that if the d distance on the spar extrusions is between 6.0-9.9mm then the 4130 is called for. Is this d distance on the spar extrusions or on on the splice plates? If it is the spar extrusions where is the "inside edge"? Would there be any benefit to keeping the original plates and making up a doubler plate in addition.Thanks for the help Doug. ________________________________________________________________________________
Date: Feb 14, 2001
From: "Lanny A. Phillips" <lanny(at)alltel.net>
Subject: Re: 701 rear fuselage bulkhead plans errors
The skin is cut 3mm less on each side because that is about the amount of radius on each longeron. When skin is riveted to longeron the radius will give you the extra 3mm on each side. Lanny A. Phillips 701Z "Randy L. Thwing" wrote: > > Listers: > Could 701 builders please advise how they addressed the following: On > plans page 7.F.2.3, the rear bottom fuselage skin is cut out 156 mm wide (78 > x 2) at the location of the rear bulkhead (7.F.1.3) and cut out 247 mm wide > (123.5 x 2) at the location of the front bulkhead (7.F.1.4), yet on plans > page 7.F.1, they have you construct the rear bulkheads 6mm wider, 162 mm & > 253 mm respectively. Of course once you attach the longerons (following the > plans) to the bottom rear fuselage skin, it is 6mm too narrow and the > bulkheads won't fit without jamming them in and creating a bulge. This is > not addressed in the 240 plus corrections available from ZA. I am plans > building so I can just scrap my perfectly good bulkheads I made according to > the plans and build another set that will actually fit the fuselage. Could > a kit builder measure these parts and fuselage widths as furnished by ZA and > advise how they differ from the plans? Could other plans builders advise > how they addressed this error? 6mm isn't much, but it's a fair distance to > spread the longerons. All help is appreciated. > Regards, > Randy L. Thwing, 701 plans, started out strong but stalled by the plans > again > ________________________________________________________________________________
From: "HOLCOMBE" <holcombe(at)oregonfast.net>
Subject: Re: 701 wingtips
Date: Feb 14, 2001
I second the, "just use common sense". I made everything fit then didn't dare go back to the plans to see if I did it right. Richard ________________________________________________________________________________
From: "HOLCOMBE" <holcombe(at)oregonfast.net>
Subject: Re: 701 wingtips
Date: Feb 14, 2001
Make the fiberglass tips fit nicely and look good, then cut the aluminum to fit Richard ________________________________________________________________________________
From: "David Tanner" <vk3auu(at)sympac.com.au>
Subject: Re: 701 rear fuselage bulkhead plans errors
Date: Feb 15, 2001
I seem to remember having a bit of trouble with one or both of those rear bulheads. The clue is to build the fuse first, then when you build the stab, you can make the supports to fit. The same goes for the wing attachments. The dimensions on the fuse do not quite agree with the dimensions on the wings, so dont finish the inboard end of the wings until you have finished the fuse. Also, do not drill the mounting holes for the slats until you are ready to mount the slats to the leading edges of the wings. Also, do not mount your battery until you have EVERYTHING finished and have done a preliminary weight and balance, if you have an extended bagage compartment, you probably need to put it just behind the large inspection door if you use a 912. It could end up just about anywhere with other engines, just make sure you keep the CoG well away from the forward limit or you will find out what wheelbarrowing is the first time you land with the flaps and the power off.. (Been there, done that) David Tanner CH701 912UL 160 hours flying ________________________________________________________________________________
From: "Barry Mayne" <bazmay(at)ozemail.com.au>
Subject: splice plates
Date: Feb 16, 2001
Just a quick question to all on the list, What is the situation if you are not on the internet or subscribe to the newsletter, has ZAC going to notify all builders about the splice plates or are they relying on the grapevine to let everyone know. I am obviously on the list and use the internet but what if I wasn't ? ZAC haven't sent me anything about it and I only found out by information passed on to me by a builder who exchanges information with me on engines. I know of three builders down here in Australia who are not on the internet or use the newsletter and I have no contact info on them so I don't know if they are aware of the problem. Interesting to hear how many of you guys have actually been contacted by ZAC. Barry Mayne HDS Jabiru 3300 ________________________________________________________________________________
From: "George Swinford" <grs-pms(at)mindspring.com>
Subject: Light-Conducting Fibers
Date: Feb 15, 2001
Hello, Zenith builders: Does anyone know of a source of inexpensive light-conducting glass or acrylic fibers? I'm looking for 20 to 25 inch lengths to conduct light for illumination, not for optical data transmission, so the optical quality needn't be too high. Also, I need a source of information telling me how to work with such fibers. Any help will be much appreciated. The intended application is non-electric fuel gauging. George Swinford ________________________________________________________________________________
Date: Feb 15, 2001
From: Rich <rich(at)carol.net>
Subject: Re: Venturi on a 601
Is there some kind of blow by or dirt that would come from the intake manifold to dirty up the gyros? Vacuum line filters on both sides of the instruments can be used as well as a regulator. But I guess the engine would register it as some kind of manifold leak & may have problems. Unless It can be tuned to compensate. How much vacuum does an intake manifold for an O-360 produce anyway? Has any thought been given to this? Rich clydes-shop(at)juno.com wrote: > > > HI: Rich > The use of manifold vacuum is too unreliable to use with gyros. They > need to be kept real > clean other wise the gyros are short lived ,I know because I am a retired > Instrument Technician of 41 years experience. It works with vacuum pumps > pumps or Venturi that use fans in front of it that is streamlined In > remote areas > > > > Are you talking about using the manifold vacuum for the vacuum > > instruments like the DG, artificial horizon, etc.? > > > > Rich > > 801 > > > > > > Robert Isaacs wrote: > > > > > > > > > > > Has anyone tried to use the manifold vacuum w/ a reserve tank for > > those > > > using a Subaru engine I can't see why this won't work, you might > > have to > > > supplement it with a 4" Venturi. > > > Just asking? Any comments? > > > > > > Bob > > > N601XL > > > ----- Original Message ----- > > > From: "Dave Austin" <daveaustin2(at)sprint.ca> > > > To: "Zenith list" > > > Sent: Thursday, February 08, 2001 8:51 AM > > > Subject: Zenith-List: Venturi on a 601 > > > > > > > > > > > > > Responding to the comment re use of a venturi on the 601, I've > > had my 4 > > > > inch unit since build, placed below the upper longeron and above > > the main > > > > spar on the passenger side. It has driven my AH well, and > > starts to spin > > > up > > > > during takeoff. The AH is fully stabilized well before reaching > > 200 ft. > > > > The AH is a life-saver. The venturi is a real drag. > > > > Dave Austin 601HDS 912 with ARPLAST > > > > daveaustin2(at)sprint.ca > > > > > > > > > > > > > > > > > > > > > > > > > > > Yours truly > Clyde D. Ehlers > ________________________________________________________________________________
From: "fhulen" <fhulen(at)gabs.net>
Subject: Re: splice plates
Date: Feb 15, 2001
> Barry, > My first notice about the splice plates was a letter received in the mail. > Yours is probably on a boat somewhere betwen Oz and Hawaii. > Cliff ++ Seems to be hit-and-miss. I heard about a letter received by a local builder in my area about 2 weeks ago, but I have never received one. Fred ________________________________________________________________________________
Date: Feb 15, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
Subject: Re: splice plates
Barry Mayne wrote: > > Just a quick question to all on the list, > What is the situation if you are not on the internet or subscribe to the > newsletter, has ZAC going to notify all builders about the splice plates or > are they relying on the grapevine to let everyone know. I am obviously on > the list and use the internet but what if I wasn't ? ZAC haven't sent me > anything about it and I only found out by information passed on to me by a > builder who exchanges information with me on engines. I know of three > builders down here in Australia who are not on the internet or use the > newsletter and I have no contact info on them so I don't know if they are > aware of the problem. > > Interesting to hear how many of you guys have actually been contacted by > ZAC. > > Barry Mayne HDS Jabiru 3300 > Interesting point. I'm a scratch builder and I definitely haven't receive a notice. Come to think of it, I don't think that the factory could give a dam about us plans buyers. Funny though' when I called to purchase supplies such as rivets and small items, they don't mind talking to me then. I also love the looks I get at the tent at Sun-N-Fun when I say Hello to Nick Heintz and introduce myself as a scratch builder. I would have thought I had tree heads or something. Are there any other scratch builders that get that feeling? Just my observation...... Hey Barry.....You like that Jabiru. What this dawn 0-200 is going to cost me now, I could have bought the 3300 and the firewall forward kit. Oh--Well, You live and you learn.... John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
Date: Feb 15, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
"engines-list(at)matronics.com" , "zenith-list(at)matronics.com"
Subject: 0-200 Woes......
Well after quite a bit of good information from fellow listers, my mechanic, and my DAR (also A&P). I decided to tear down the case. After careful inspection, I found that the metal fragments from the starter gear, did travel beyond the accessory case. I found metal on the rear piston bases, the rear connecting rods, and the crankshaft. I weighed my options, taking into consideration my financial situation, work involved, and the time SMOH, and decided to tear the motor down, clean all internal parts, and inspect for damage. I will re-assemble the case with all new gaskets. I will have to replace the crankshaft gear which is the gear the starter clutch gear tore into. I decided to do the top end with new OEM cylinder assemblies. The cheapest way to go at this time, yet keep a good piece of mind. Any thoughts would be very welcome. Thanks to all that sent me all that valuable information and suggestions. -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: "Randy L. Thwing" <n4546v(at)mindspring.com>
Subject: "Z" ' s around bottom fuse access 701
Date: Feb 15, 2001
701 Listers: I am just about ready to rivet traverse members to my lower rear fuselage skin. Plans sheet no. 7.F.6 shows 2 pieces of "z" located on the sides of the bottom skin access opening, example is at plan coordinates (185,177). I cannot find a measurement specifiying how far outboard these z's should be positioned. They don't seem to interact with other parts so I could just pick a distance and it looks like it would probably work, but if others who have been this way before have an opinion on where they should be located, I would appreciate the benefit of their experience. Regards, Randy L. Thwing, 701 plans, 60 hp Franklin, 50.0001 complete ________________________________________________________________________________
From: "Matthew Mucker" <mmucker(at)airmail.net>
Subject: splice plates
Date: Feb 15, 2001
> > Interesting point. I'm a scratch builder and I definitely > haven't receive a > notice. Come to think of it, I don't think that the factory > could give a dam > about us plans buyers. Um.... if you didn't buy splice plates from Zenith, why would they bother telling you about a manufacturing defect? :) ________________________________________________________________________________
From: "Graham Byass" <gbyass(at)cygnus.uwa.edu.au>
Subject: splice plates
Date: Feb 16, 2001
Barry For what it is worth I am a scratch builder in Australia BUT I did buy the spars and splice plates from ZAC and I have not heard from ZAC yet. I have not got around to checking the splice plates yet but the odds are that they will be out of spec. Sometimes I think that the mail from the US comes to Australia via camel train through Moscow of something similar. Graham Byass -----Original Message----- From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com]On Behalf Of Barry Mayne Sent: Friday, 16 February 2001 11:14 Subject: Zenith-List: splice plates Just a quick question to all on the list, What is the situation if you are not on the internet or subscribe to the newsletter, has ZAC going to notify all builders about the splice plates or are they relying on the grapevine to let everyone know. I am obviously on the list and use the internet but what if I wasn't ? ZAC haven't sent me anything about it and I only found out by information passed on to me by a builder who exchanges information with me on engines. I know of three builders down here in Australia who are not on the internet or use the newsletter and I have no contact info on them so I don't know if they are aware of the problem. Interesting to hear how many of you guys have actually been contacted by ZAC. Barry Mayne HDS Jabiru 3300 ________________________________________________________________________________
From: "Michael Brook" <walruss(at)optushome.com.au>
Subject: "Z" ' s around bottom fuse access 701
Date: Feb 16, 2001
I take it you are refering to the 2 longitudinal member thats go on either side of the access door. The access door is approximately 500mm wide. You really only have to put the Z's wide enough for teh door. I put my z spacing at 560mm wide AT THE RIVETLINES, so that I have an inch or so either side of the rivetlines. I'm going to be putting the door on with rivnuts so that it can be easily removed if a problem comes up. Teh purpose of the z's is simply to transfer the load that is carried in the skin to the transverse member to the frame in such a way that the access hole and panel doesn't take any excess load that could fail the skin. BAD BAD THING in a semi monocoque structure. Hope this helps, mike 2 planes, 2 701's from kits 525 hours, working on fuses. -----Original Message----- From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com]On Behalf Of Randy L. Thwing Sent: Friday, February 16, 2001 5:15 AM Subject: Zenith-List: "Z" ' s around bottom fuse access 701 701 Listers: I am just about ready to rivet traverse members to my lower rear fuselage skin. Plans sheet no. 7.F.6 shows 2 pieces of "z" located on the sides of the bottom skin access opening, example is at plan coordinates (185,177). I cannot find a measurement specifiying how far outboard these z's should be positioned. They don't seem to interact with other parts so I could just pick a distance and it looks like it would probably work, but if others who have been this way before have an opinion on where they should be located, I would appreciate the benefit of their experience. Regards, Randy L. Thwing, 701 plans, 60 hp Franklin, 50.0001 complete ________________________________________________________________________________
Date: Feb 16, 2001
From: Douglas Corarito <dougc(at)infoequipt.com>
Subject: 701 Dedalius Wings
Has anyone considered the Dedalius wings for their 701? I'm wondering why you did/didn't decide to go with the wings. Does anyone know anybody that's flying with this system? I'm interested in knowing performance numbers. -- Doug INFOequipt,Inc. dougc(at)infoequipt.com http://www.infoequipt.com ________________________________________________________________________________
From: SEAL2CC(at)aol.com
Date: Feb 16, 2001
Subject: Re: splice plates
In a message dated 2/16/01 5:58:03 AM Eastern Standard Time, billvt(at)together.net writes: << I was never notified of the splice plate issue. I heard about it on this e-mail list and then went to the ZAC builders pages. I subscribe to the newsletter but did not see any mention of the problem in the last newsletter. >> Same situation here... Chris Carey Richmond, VA ________________________________________________________________________________
From: "Steven J. Devine" <steve(at)tzogon.com>
Subject: Re: splice plates: machine shop
Date: Feb 16, 2001
> > I have an excellent relationship with a local/online machine shop... I am talking > to them now about the possibility of them making up new plates for anyone > who is interested. Will post further details when they become available. Sounds like everyone is all set or close to it, given the hole transfer tool discussion and such... but at least one person was asking about a machine shop willing to transfer the holes, so here it is: Custom Metal Products 78 Stone Place Melrose, MA 02176 (781) 438-5300 http://www.cmproducts.com Excellent facilities, sprectacular workmanship on the parts I've seen there and the work they've done for me. Steve Steven J. Devine, President, Consultant, TZOGON Enterprises Incorporated President, EAA Chapter 136 (LWM/Merrimac Valley) steve@tzogon.com HAM Tech lic: N1YZJ http://www.tzogon.com http://www.tzogon.com/~steve/glass_cockpit http://www.tzogon.com/~steve/stolch801 ________________________________________________________________________________
From: Sjl219(at)aol.com
Date: Feb 16, 2001
Subject: Re: "Z" ' s around bottom fuse access 701
>>>>>>>> I am just about ready to rivet traverse members to my lower rear fuselage skin. Plans sheet no. 7.F.6 shows 2 pieces of "z" located on the sides of the bottom skin access opening, example is at plan coordinates (185,177). I cannot find a measurement specifiying how far outboard these z's should be positioned. They don't seem to interact with other parts so I could just pick a distance and it looks like it would probably work, but if others who have been this way before have an opinion on where they should be located, I would appreciate the benefit of their experience. Randy, they certainly do interact with other parts. Look at the plans again, and also the exploded diagram, and you'll see there really are 3 Zs. Two along the sides of the access hole and one at the rear. To the front is the bearing. Thus, you are constructing a reinforcement box around the access hole. When you cut the Zs to specified length, you'll have answered your question about placement. Take some precautions and plan ahead for what you are going to do about the access hole. ZAC just says rivet it shut and drill it out when you need to get in there. Instead, I chose to leave extra skin between the hole and the Zs to act as a flange of sorts. Then I installed a doubler on this flange and tinnerman plates. So my access door is secured with a bunch of T6XB screws. By the way, the plans don't clearly show that the Zs are attached to each other. I used scrap to link mine for added rigidity. Stan ________________________________________________________________________________
Date: Feb 16, 2001
From: Gerald Applefeld <jerryvmd(at)blazenet.net>
Subject: Re: splice plates
I'm a scratch builder of 601HD and I received my info on plates in the mail at least two weeks ago. I have nothing but good comments to say about customer sevice from ZAC. My biggest complaint overall was that there were several pages missing from my original drawing/plans package that I didn't know were missing until I was ready for that part of the plane. eg. 6E5 drawing of throttle bellcrank and drawing on installation of the brake cylinders on the rudder pedals. I bought my plans in 1994 at Oshkosh. Thought maybe these were updates and I fell through the cracks in getting them, but when I called Missouri they said they should have been in the original package. However they quickly provided the drawings at no charge. Just my two cents. John Tarabocchia wrote: > > Barry Mayne wrote: > > > > > Just a quick question to all on the list, > > What is the situation if you are not on the internet or subscribe to the > > newsletter, has ZAC going to notify all builders about the splice plates or > > are they relying on the grapevine to let everyone know. I am obviously on > > the list and use the internet but what if I wasn't ? ZAC haven't sent me > > anything about it and I only found out by information passed on to me by a > > builder who exchanges information with me on engines. I know of three > > builders down here in Australia who are not on the internet or use the > > newsletter and I have no contact info on them so I don't know if they are > > aware of the problem. > > > > Interesting to hear how many of you guys have actually been contacted by > > ZAC. > > > > Barry Mayne HDS Jabiru 3300 > > > > Interesting point. I'm a scratch builder and I definitely haven't receive a > notice. Come to think of it, I don't think that the factory could give a dam > about us plans buyers. Funny though' when I called to purchase supplies such > as rivets and small items, they don't mind talking to me then. I also love the > looks I get at the tent at Sun-N-Fun when I say Hello to Nick Heintz and > introduce myself as a scratch builder. I would have thought I had tree heads > or something. Are there any other scratch builders that get that feeling? > > Just my observation...... > > Hey Barry.....You like that Jabiru. What this dawn 0-200 is going to cost me > now, I could have bought the 3300 and the firewall forward kit. Oh--Well, You > live and you learn.... > > John W. Tarabocchia > > 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html > Airframe 100% Complete... > Installing Wire and Engine... > ________________________________________________________________________________
From: "Randy L. Thwing" <n4546v(at)mindspring.com>
Subject: Re: "Z" ' s around bottom fuse access 701
Date: Feb 16, 2001
Thanks for the response, please notice I always give coordinates on the plans page for the parts I am inquiring about, for example for one of these z's, I mentioned plans page 7.F.6 coordinates (185,177). These are measurements on the plans sheets measures in mm, the first number is measured from the right border across, the second number is measured from the the top border down, like a road map. It allows one to precisely locate the parts one is refering to, or talking bout. I think your positioning the z's about 560 wide is just about right. Regards, Randy > > I take it you are refering to the 2 longitudinal member thats go on either > side of the access door. The access door is approximately 500mm wide. You > really only have to put the Z's wide enough for teh door. I put my z spacing > at 560mm wide AT THE RIVETLINES, so that I have an inch or so either side of > the rivetlines. I'm going to be putting the door on with rivnuts so that it > can be easily removed if a problem comes up. Teh purpose of the z's is > simply to transfer the load that is carried in the skin to the transverse > member to the frame in such a way that the access hole and panel doesn't > take any excess load that could fail the skin. BAD BAD THING in a semi > monocoque structure. > > Hope this helps, > > > > 701 Listers: > I am just about ready to rivet traverse members to my lower rear > fuselage skin. Plans sheet no. 7.F.6 shows 2 pieces of "z" located on the > sides of the bottom skin access opening, example is at plan coordinates > (185,177). I cannot find a measurement specifiying how far outboard these > z's should be positioned. They don't seem to interact with other parts so I > could just pick a distance and it looks like it would probably work, but if > others who have been this way before have an opinion on where they should be > located, I would appreciate the benefit of their experience. > Regards, > Randy L. Thwing, 701 plans, 60 hp Franklin, 50.0001 complete ________________________________________________________________________________
From: "Eric Ingraham" <iflyul(at)hotmail.com>
Subject: Re: 701 Dedalius Wings
Date: Feb 16, 2001
Hey Doug.....I considered using their wing and cost wise it appears to be comparable.....If you check the builders on the net section of the Z site, there's a guy by the name of Al Hartman who has a 701 with that wing and a Rotax 912......He loves it.....I spoke to Sebastion H and he said Dedalius was supposed to provide them with a wing to test fo strength and to date they haven't done it.... Sebastion doesn't think it's built strong enough.......good luck and fly safe.......Eric >From: Douglas Corarito <dougc(at)infoequipt.com> >Reply-To: zenith-list(at)matronics.com >To: zenith-list(at)matronics.com >Subject: Zenith-List: 701 Dedalius Wings >Date: Fri, 16 Feb 2001 07:42:10 -0500 > > >Has anyone considered the Dedalius wings for their 701? > >I'm wondering why you did/didn't decide to go with the wings. > >Does anyone know anybody that's flying with this system? > >I'm interested in knowing performance numbers. > >-- > > >Doug > > >INFOequipt,Inc. >dougc(at)infoequipt.com >http://www.infoequipt.com > > ________________________________________________________________________________
Date: Feb 16, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
Subject: Splice plates
I can't for the life of me find any info on the Zenith web site about the notice. I thought someone had noted it could be found on the web site. Does any one have a URL to link me to it? -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: "Randy L. Thwing" <n4546v(at)mindspring.com>
Subject: Re: "Z" ' s around bottom fuse access 701
Date: Feb 16, 2001
----- Original Message ----- From: <Sjl219(at)aol.com> Sent: Friday, February 16, 2001 5:48 AM Subject: Re: Zenith-List: "Z" ' s around bottom fuse access 701 > > I am just about ready to rivet traverse members to my lower rear > fuselage skin. Plans sheet no. 7.F.6 shows 2 pieces of "z" located on the > sides of the bottom skin access opening, example is at plan coordinates > (185,177). I cannot find a measurement specifiying how far outboard these > z's should be positioned. They don't seem to interact with other parts so I > could just pick a distance and it looks like it would probably work, but if > others who have been this way before have an opinion on where they should be > located, I would appreciate the benefit of their experience. > > > Randy, they certainly do interact with other parts. Look at the plans again, > and also the exploded diagram, and you'll see there really are 3 Zs. Two > along the sides of the access hole and one at the rear. To the front is the > bearing. Thus, you are constructing a reinforcement box around the access > hole. When you cut the Zs to specified length, you'll have answered your > question about placement. Take some precautions and plan ahead for what you > are going to do about the access hole. ZAC just says rivet it shut and drill > it out when you need to get in there. Instead, I chose to leave extra skin > between the hole and the Zs to act as a flange of sorts. Then I installed a > doubler on this flange and tinnerman plates. So my access door is secured > with a bunch of T6XB screws. By the way, the plans don't clearly show that > the Zs are attached to each other. I used scrap to link mine for added > rigidity. > Stan Stan: Thanks for the response, I fully appreciate that the side Z's interact with other parts by the fact their aft ends overlap and are attached to the rear Z, and their forward ends overlap and are attached to 7.F.6.1. But as far as their outboard location near or away from the access opening, the only other part that touches them is the short L that is placed on the bottom skin after the Z's and 7.F.5.4 are located. I meant no other parts rely on the outboard placement of the side Z's. As far as "the plans don't clearly show that the Zs are attached to each other", I'm one of the biggest critics of uncorrected plans mistakes and lack of revisions when problems are known, but in this case, I believe the plans clearly show the side Z's overlaping and being attached to the rear Z (aft) and 7.F.6.1 (forward) on sheet 7.F.2 at the lower right hand corner, and on 7.F.6 in the second diagram from the top, the top view of the bottom skin. Again, there is just no spec. telling you how far "outboard" to position the side Z's. I normally would provide coordinates when refering to plans location, but my full size plans are at home and I'm at the plant now where I only have reduced size copies to refer to. The above is offered in the interest of accuracy. Thanks for the help, Randy L. Thwing, 701 plans, 50.0002% ________________________________________________________________________________
From: "Randy L. Thwing" <n4546v(at)mindspring.com>
Subject: Re: 701 Dedalius Wings
Date: Feb 16, 2001
701 Listers: I recently weighed one of my completed ZA wings, less fuel tank, slats, and tip: 23 lbs., say 55 lb. for the pair finished. My understanding is the Dedalius wing, for which plans are not offered, is only available in a kit for about $6000.00. This wing probably has less than $200.00 in material contained in it, so from STRICTLY a plans builders perspective, I just couldn't justify it. I believe Al Hartman lives in Blue Diamond, NV which is near Las Vegas. Last month, our EAA chapter went on a flyin breakfast to Stovepipe Wells, in Northern Death Valley, about 100 miles from LV. I flew my 48 Bonanza to attend, (38 airplanes & 60 plus people showed up) and when we walked from the restaurant back to the strip, Al's 701 was parked there. As we arrived before him, and departed before him, I didn't get a chance to speak to him, but I know he flies regularly. I also believe he purchased the ship complete (possibly from Flypass?) and didn't build it. Regards, Randy L. Thwing, 701 plans Sent: Friday, February 16, 2001 4:33 PM Subject: Re: Zenith-List: 701 Dedalius Wings > > Hey Doug.....I considered using their wing and cost wise it appears to be > comparable.....If you check the builders on the net section of the Z site, > there's a guy by the name of Al Hartman who has a 701 with that wing and a > Rotax 912......He loves it.....I spoke to Sebastion H and he said Dedalius > was supposed to provide them with a wing to test fo strength and to date > they haven't done it.... Sebastion doesn't think it's built strong > enough.......good luck and fly safe.......Eric ________________________________________________________________________________
Date: Feb 16, 2001
From: Mark Wood <mawood(at)zoo.uvm.edu>
Subject: Re: splice plates
>Zenith Aircraft and Flypass both know that I am a >plans builder... worse than that, I purchased those >plans second hand and the first service that Zenith >Aircraft gave me was to transfer the ownership of >those plans in their record. >========================================================== If you are a plans builder, why are you worried about the size of the splice plates that ZAC has supplied with the kits??? ________________________________________________________________________________
Date: Feb 16, 2001
From: Keith Maloney <kmaloney(at)lsil.com>
Subject: Splice Plate
Opinion: It appears to me that this was a manufacturing error because the plates were cut too narrow or the holes drilled in the wrong place. The recall is for edge distance from the inboard/outboard edges of the plates and edge of the holes and the edge distance of the larger holes (3/8) and the top of the plates. It does not address the edge distance of the smaller holes (5/16) and the top of the plates. From reading everyone's remarks it seems to me that people are using this recall to re-dimention the the small holes, no where in this document does it say the plans are wrong. Thus the most inboard of the small upper hole will not have 10mm edge distance as shown in the recall. The planes call for 12.5mm from center of hole to edge of plate, that's 8.5mm for dimension "d" at best. Further more it gives a theoretical value that is even smaller. If one were to build, without modification, to the plans there is no way the dimensions could be held for that hole as required for the larger holes. My point is this, if you are replacing your splice plates because of the upper most inboard hole I think you are misinterpreting the recall. As far as Zenith and scratch builders go. As a scratch builder I've asked several questions by e-mail and received prompted responses in all cases. The one time I called in C. Heintz got on the phone himself and took considerable time talking with me. Keith Maloney ________________________________________________________________________________
From: "Robert Loer" <rloer(at)mighty.net>
Subject: Re: 701 Dedalius Wings
Date: Feb 16, 2001
The Dedalius wings are a copy (authorized or not I do not know but the guy did have a Pegazair) of the Pegazair 100 STOL. I had one partially built before being consumed by a fire. The slats are automatically deployed using gravity and air pressure. Performance specs on this page are pretty accurate according to those on the Pegazair news list that are flying them. http://www.ultralightnews.com/plansbuyerguide/pegazair100stol.htm Robert Loer ----- Original Message ----- From: Douglas Corarito <dougc(at)infoequipt.com> Sent: Friday, February 16, 2001 4:42 AM Subject: Zenith-List: 701 Dedalius Wings > > Has anyone considered the Dedalius wings for their 701? > > I'm wondering why you did/didn't decide to go with the wings. > > Does anyone know anybody that's flying with this system? > > I'm interested in knowing performance numbers. > > -- > > > Doug > > > INFOequipt,Inc. > dougc(at)infoequipt.com > http://www.infoequipt.com > > ________________________________________________________________________________
Date: Feb 16, 2001
From: Douglas Corarito <dougc(at)infoequipt.com>
Subject: Re: 701 Dedalius Wings
Robert, Thanks for the link. I saw cruise (75% ?) listed at 105 mph. OK, those of you flying a 701+912, what are you seeing at "cruise"? I'm not planning on building a 701 to go fast. However, I'm assuming that one would go to a variable geometery wing with hopes of seeing a significant increase in speed while still maintaining slow flight STOL characteristics. I need to know if this set of wings is worth it. BTW - I tried to email Al Hartman (from the ZAC list) and it bounced. Anybody have his email? > >The Dedalius wings are a copy (authorized or not I do not know but the guy >did have a Pegazair) of the Pegazair 100 STOL. I had one partially built >before being consumed by a fire. The slats are automatically deployed using >gravity and air pressure. Performance specs on this page are pretty accurate >according to those on the Pegazair news list that are flying them. > >http://www.ultralightnews.com/plansbuyerguide/pegazair100stol.htm > >Robert Loer >----- Original Message ----- >From: Douglas Corarito <dougc(at)infoequipt.com> >To: >Sent: Friday, February 16, 2001 4:42 AM >Subject: Zenith-List: 701 Dedalius Wings > > >> >> Has anyone considered the Dedalius wings for their 701? >> >> I'm wondering why you did/didn't decide to go with the wings. >> >> Does anyone know anybody that's flying with this system? >> >> I'm interested in knowing performance numbers. >> >> -- >> >> >> Doug >> >> >> INFOequipt,Inc. >> dougc(at)infoequipt.com >> http://www.infoequipt.com >> >> > > -- Doug INFOequipt,Inc. dougc(at)infoequipt.com http://www.infoequipt.com ________________________________________________________________________________
From: "Robert Loer" <rloer(at)mighty.net>
Subject: Re: 701 Dedalius Wings
Date: Feb 16, 2001
By the way.... Here is the page for the Pegazair. http://www.tapanee.com/index.html Robert Loer ----- Original Message ----- From: Douglas Corarito <dougc(at)infoequipt.com> Sent: Friday, February 16, 2001 11:09 AM Subject: Zenith-List: Re: 701 Dedalius Wings > > Robert, Thanks for the link. > > I saw cruise (75% ?) listed at 105 mph. > > OK, those of you flying a 701+912, what are you seeing at "cruise"? > > I'm not planning on building a 701 to go fast. However, I'm assuming > that one would go to a variable geometery wing with hopes of seeing a > significant increase in speed while still maintaining slow flight > STOL characteristics. > > I need to know if this set of wings is worth it. > > > BTW - I tried to email Al Hartman (from the ZAC list) and it bounced. > Anybody have his email? > > > > > >The Dedalius wings are a copy (authorized or not I do not know but the guy > >did have a Pegazair) of the Pegazair 100 STOL. I had one partially built > >before being consumed by a fire. The slats are automatically deployed using > >gravity and air pressure. Performance specs on this page are pretty accurate > >according to those on the Pegazair news list that are flying them. > > > >http://www.ultralightnews.com/plansbuyerguide/pegazair100stol.htm > > > >Robert Loer > >----- Original Message ----- > >From: Douglas Corarito <dougc(at)infoequipt.com> > >To: > >Sent: Friday, February 16, 2001 4:42 AM > >Subject: Zenith-List: 701 Dedalius Wings > > > > > >> > >> Has anyone considered the Dedalius wings for their 701? > >> > >> I'm wondering why you did/didn't decide to go with the wings. > >> > >> Does anyone know anybody that's flying with this system? > >> > >> I'm interested in knowing performance numbers. > >> > >> -- > >> > >> > >> Doug > >> > >> > >> INFOequipt,Inc. > >> dougc(at)infoequipt.com > >> http://www.infoequipt.com > >> > >> > > > > > > -- > > > Doug > > > INFOequipt,Inc. > dougc(at)infoequipt.com > http://www.infoequipt.com > > ________________________________________________________________________________
From: "The Meiste's" <meiste(at)essex1.com>
Subject: Nico Swaging
Date: Feb 16, 2001
List, I have a nico swaging tool (screw down style) that has instructions that state: 1st swag should be at the thimble (loop) end. 2nd swag should be in the middle of nico 3rd swag is made at the cut off end of nico. From what I have read in the archives on the subject, everyone is swaging the middle first, then the thimble (loop) end second, and last the cut end. Just curious if there is any spec out there stating for a fact which procedure is actually correct? Thanks! Kelly Meiste ________________________________________________________________________________
Date: Feb 16, 2001
From: Carlos Sa <wings1(at)videotron.ca>
Subject: Re: Light-Conducting Fibers
Hi, George I had a swimming pool installed last summer, and lighting is provided by a central source and conducted by 3/4" (I guess) fiber optics cable to different spots on the swimming pool wall. You could disassemble the cable and use a few strands; they are about 1-2 mm in diameter. I do not know what the cost is, but this certainly isn't high grade material. Try your local swimming pool store... Carlos > > Hello, Zenith builders: > > Does anyone know of a source of inexpensive light-conducting glass or > acrylic fibers? I'm looking for 20 to 25 inch lengths to conduct light for > illumination, not for optical data transmission, so the optical quality > needn't be too high. Also, I need a source of information telling me how to > work with such fibers. Any help will be much appreciated. > > The intended application is non-electric fuel gauging. > ________________________________________________________________________________
From: "Darryl West" <rdwest(at)cadvision.com>
Subject: Re: Splice plates
Date: Feb 16, 2001
http://www.zenithair.com/bldr/bldr.htm Darryl ......... ----- Original Message ----- From: "John Tarabocchia" <zodiac.builder(at)verizon.net> Sent: Friday, February 16, 2001 10:00 AM Subject: Zenith-List: Splice plates > > I can't for the life of me find any info on the Zenith web site about > the notice. I thought someone had noted it could be found on the web > site. Does any one have a URL to link me to it? > > -- > > John W. Tarabocchia > > 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html > > Airframe 100% Complete... > Installing Wire and Engine... > > ________________________________________________________________________________
Date: Feb 16, 2001
Subject: Re: Nico Swaging
From: Jim <jashford(at)hawaii.rr.com>
Kelly, As you make the three different swages the ????(whatcha ma call it)lengthens. Swaging the center first "fixes" the location. I found that gripping the cable end as close to the end as possible with vise grips, pulling the cable tight around the thimble and then doing the center swage, followed by the thimble end and then the opposite end, resulted in a tight fit around the thimble and the swage lenghtening sufficiently(after removal of vise grips) to almost cover the cut end of the cable. Where possible, use a vise to hold the thimble. Jim Ashford > From: "The Meiste's" <meiste(at)essex1.com> > Reply-To: zenith-list(at)matronics.com > Date: Fri, 16 Feb 2001 17:12:00 -0600 > To: "Zenith List" > Subject: Zenith-List: Nico Swaging > > > List, > I have a nico swaging tool (screw down style) that has instructions that > state: > 1st swag should be at the thimble (loop) end. > 2nd swag should be in the middle of nico > 3rd swag is made at the cut off end of nico. > > From what I have read in the archives on the subject, everyone is swaging > the middle first, then the thimble (loop) end second, and last the cut end. > > Just curious if there is any spec out there stating for a fact which > procedure is actually correct? > > Thanks! > > Kelly Meiste > > > > > > ________________________________________________________________________________
Date: Feb 16, 2001
From: Phil Raker <phadr2(at)yahoo.com>
Subject: Re: splice plates
My first notice was by letter from ZAC, then about three days later on this list. Phil Raker: HDS/Stratus in NW MN (almost as remote as Oz?) --- fhulen wrote: > > > > Barry, > > My first notice about the splice plates was a > letter received in the mail. > > Yours is probably on a boat somewhere betwen Oz > and Hawaii. > > Cliff > > ++ Seems to be hit-and-miss. I heard about a letter > received by a local > builder in my area about 2 weeks ago, but I have > never received one. > Fred > > > > through > > http://www.matronics.com/archives > http://www.matronics.com/emaillists > > Matronics! > > > > > Get personalized email addresses from Yahoo! Mail - only $35 a year! http://personal.mail.yahoo.com/ ________________________________________________________________________________
From: "Larry McFarland" <larrymc(at)qconline.com>
Subject: Reduction Drive from Ireland
Date: Feb 16, 2001
Good evening builders, I've recently acquired a Subaru EA-81 that has been fitted with an adapter for a Rotax Redrive. I didn't take the drive unit because it wasn't the right ratio. However, there is a Redrive on the web called the RZ2 for Rotax from www.av8r.co.uk in ireland that has a capacity for 120 hp and a centrifugal clutch that allows engagement at 1800 to 2100 rpm. It seems priced right and comes in several ratios. Anyone have any experience with this unit? I'm very interested Also, the EA-81 has hydraulic lifters. Does anyone have problems with that? Appreciative of all input and thanks, Larry C. McFarland larrymc(at)qconline.com At a year and 6 months, 601HDS tail feathers, center section complete and wings are nearly done & I'm welding leading edge tanks after the Pitot and strobe wiring are complete. ________________________________________________________________________________
From: "David Tellet" <telletdl(at)erols.com>
Subject: 601 Stabilizer Skin Rivets
Date: Feb 16, 2001
I know this has been discussed a little before (in the archives), but I still not sure about it. The plans call for A4 pitch 40 for the stabilizer skin to the spars, but this means that on the top skin to the aft spar an A4 will go through the skin, the elevator hinge, the spar, and the spar doubler. This seems to be too much material for the A4. It also means that the doublers will be attached to the spar web with A5's and the spar flange with A4's - doesn't seem right to me. I have a fax question in to Zenith, but I was hoping for a quicker answer. Can anybody clarify this for me? Is there a maximum thickness of joining materials for the A4 and A5? Thanks a lot. David Tellet, 601HD, working on tail feathers. ________________________________________________________________________________
From: PWalsh8045(at)aol.com
Date: Feb 16, 2001
Subject: Re: splice plates
I received a letter from ZAC about the plates......abnd received the plates 2 days after faxing the order form....Good company!!!! ________________________________________________________________________________
From: PWalsh8045(at)aol.com
Date: Feb 16, 2001
Subject: Re: splice plates
naaa...scratch builders would have met specs from the plans.....kits were recalled from factory error....IMHO... ________________________________________________________________________________
From: "Bill Morelli" <billvt(at)together.net>
Subject: Re: Nico Swaging
Date: Feb 16, 2001
Kelly, The Tony Begelis books and my tech advisor and DAR say that the correct way to swage is 1 - center, 2 - thimble, 3 - cut off end Bill >1st swag should be at the thimble (loop) end. >2nd swag should be in the middle of nico >3rd swag is made at the cut off end of nico. ________________________________________________________________________________
From: "Steve Dixon" <dix39(at)home.com>
Subject: Re: Nico Swaging
Date: Feb 16, 2001
I looked in AC 43.13-1A, Acceptable Methods, Techniques, and Practices, which shows the sequence being center first, thimble end, then opposite end, just as Jim said. This must be the correct way. Now, would someone please tell me how to access the plans changes (updates ?) for the 701? Also, is anyone on the list using a VW with a GP type redrive on one of these? Thanks. Steve Dixon ----- Original Message ----- From: "Jim" <jashford(at)hawaii.rr.com> Sent: Friday, February 16, 2001 5:27 PM Subject: Re: Zenith-List: Nico Swaging > > Kelly, > > As you make the three different swages the ????(whatcha ma call > it)lengthens. Swaging the center first "fixes" the location. I found that > gripping the cable end as close to the end as possible with vise grips, > pulling the cable tight around the thimble and then doing the center swage, > followed by the thimble end and then the opposite end, resulted in a tight > fit around the thimble and the swage lenghtening sufficiently(after removal > of vise grips) to almost cover the cut end of the cable. Where possible, use > a vise to hold the thimble. > > Jim Ashford > > > From: "The Meiste's" <meiste(at)essex1.com> > > Reply-To: zenith-list(at)matronics.com > > Date: Fri, 16 Feb 2001 17:12:00 -0600 > > To: "Zenith List" > > Subject: Zenith-List: Nico Swaging > > > > > > List, > > I have a nico swaging tool (screw down style) that has instructions that > > state: > > 1st swag should be at the thimble (loop) end. > > 2nd swag should be in the middle of nico > > 3rd swag is made at the cut off end of nico. > > > > From what I have read in the archives on the subject, everyone is swaging > > the middle first, then the thimble (loop) end second, and last the cut end. > > > > Just curious if there is any spec out there stating for a fact which > > procedure is actually correct? > > > > Thanks! > > > > Kelly Meiste > > > > > > > > > > > > > > ________________________________________________________________________________
Date: Feb 17, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Priming without fear
One of the difficult thing during this project has been familly relation while I was priming the parts. My wife really gets pissed off by the smell of Zinc Chromate (or Oxide). Once, I primed at night and the smell woke her up... I thought she would leave me... Well, all to say that I found a simple solution. So stupid I am ashame that I did not do that before. Yesterday, I purchased a fan that I inserted against my garage window. It pushes the air (and heat) out. Now, instead of pushing primer vapors through the house, I pull air from it and there is no smell in the house. I even got an approval from my wife to prime at night!!! I am so happy with this that the fan is my picture of the day for today. ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Get personalized email addresses from Yahoo! Mail - only $35 a year! http://personal.mail.yahoo.com/ ________________________________________________________________________________
Date: Feb 17, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: 601 Stabilizer Skin Rivets
The grip range for the A4 rivet (Avex 1691-412, equiv to Zenair's 1604-412) is .093" to .250". Frankly, we all attached less than .093" of material with our rivets and at .250", the A4 rivet does not work. I tried to attach two pieces of 1/8" with it and the rivet is too short (this may be because we re-shape the rivet head?). Regarding the stab application, there is 0.016 + 0.016 + 0.040 + 0.040 + 0.025 = 0.137" of material. This is well within specifications. In doubt, you can always try it. For the A5 rivet, the specified grip range is 0.125" to 0.312" (for 1691-514 equiv to Zenair's 1604-514) Michel PS: When I say "equiv to Zenair's", I mean the the dimensions are supposed to be the same. C. Heintz mandates that we use the UK rivets (part no 1604). Source: Advell Cherry Textron Breakstem Fastening catalog, page 14 (Avex Fastening Systems) --- David Tellet wrote: > > > I know this has been discussed a little before (in > the archives), but I > still not sure about it. The plans call for A4 > pitch 40 for the stabilizer > skin to the spars, but this means that on the top > skin to the aft spar an A4 > will go through the skin, the elevator hinge, the > spar, and the spar > doubler. This seems to be too much material for the > A4. It also means that > the doublers will be attached to the spar web with > A5's and the spar flange > with A4's - doesn't seem right to me. > > I have a fax question in to Zenith, but I was hoping > for a quicker answer. > Can anybody clarify this for me? Is there a maximum > thickness of joining > materials for the A4 and A5? > > Thanks a lot. ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Get personalized email addresses from Yahoo! Mail - only $35 a year! http://personal.mail.yahoo.com/ ________________________________________________________________________________
From: "The Meiste's" <meiste(at)essex1.com>
Subject: Re: Nico Swaging
Date: Feb 17, 2001
Thanks to all that replied with advice, looks like not much debate here. Only wish the tool manufacturers could get it right. This week at work I'll be doing a lot of destructive testing on nico's with 1/16 to 1/4" cable, I'll be swaging with all kinds of tools (everything from hammer's and vises, to screw downs and the bolt cutter styles). I'll also intentionally make some poor swages, & swages not made as recommended by all you that replied. Hopefully by the end of the week I'll have some test data I can share with anyone who is interested. Just seems like this should be done as when scanning the achieves it seems this is the one thing that brings down our planes most often (usually with fatal results). Thanks again to all the replies, and if anyone has a particular type of test you would like me to try on a nico let me know & I'll do my best to simulate it. Kelly Meiste 601 HD a year from flying yet. > List, > I have a nico swaging tool (screw down style) that has instructions that > state: > 1st swag should be at the thimble (loop) end. > 2nd swag should be in the middle of nico > 3rd swag is made at the cut off end of nico. > > From what I have read in the archives on the subject, everyone is swaging > the middle first, then the thimble (loop) end second, and last the cut end. > ________________________________________________________________________________
Date: Feb 17, 2001
From: John Tarabocchia <zodiac.builder(at)verizon.net>
Subject: Chatting
I notice that a lot of listers are on AOL. Has anyone ever thought of meeting in a chat room, Perhaps on a monthly meeting basis. Would be kool to chat with a bunch of others real time. Also people who are on AOL could download Instant Messenger (FREE) from http://www.aol.com and chat with other AOL members...... I've also wonders if it would be neat to have association of Zodiac Builder. I notice that a lot of other planes has groups. There seems to be enough of us builders. Just some thoughts......I know I think to much -- John W. Tarabocchia 601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html Airframe 100% Complete... Installing Wire and Engine... ________________________________________________________________________________
From: AWilson62(at)aol.com
Date: Feb 17, 2001
Subject: Re: "Z" ' s around bottom fuse access 701
Hey guys, My 701 also has rivnuts all the way around. that is alot of work putting them in and alot of work removing to inspect. I slowly got to the point where I only use 5 screws. one on each side and 3 across the top. It works fine and is secure. If i were to do it all over again I would make the door, two doors that overlap. Kinda like bomb bay doors. They would be held with a couple of spring clips. this is easy access so you can preflight inside everyother flight and the door would not hit the ground when you open it. I have been flying 34 hours now with just the 5 screws without any problem. Alan ________________________________________________________________________________
Date: Feb 17, 2001
From: Jim and Lucy <jpollard(at)mnsi.net>
Subject: Re: Chatting
>ve also wonders if it would be neat to have association of Zodiac >Builder. I notice that a lot of other planes has groups. There seems >to be enough of us builders. > >Just some thoughts......I know I think to much A chat room is allready set up at http://clubs.yahoo.com/clubs/zenithkitaircraft I do not check it very often but I have never seen anyone in it. Jim Pollard ch601hds waiting for spar plates to fix my 9.5mm edge distances. ________________________________________________________________________________
Date: Feb 17, 2001
From: Gary Liming <gary(at)liming.org>
Subject: Re: Priming without fear
At 08:14 2001.02.17., you wrote: > >One of the difficult thing during this project has >been familly relation while I was priming the parts. >My wife really gets pissed off by the smell of Zinc >Chromate (or Oxide). Zinc Chromate doesn't really have an odor. It is the toluene vehicle that is the pungent smell. Maybe this sounds picky, but the zinc chromate is known to cause cancer and birth defects, and you can't smell it after the vehicle evaporates. Ever since reading about this stuff, I have tried to look into what is the best way around it. My notes so far are on my website http://www.liming.org/ch801 under the "research" and "corrosion" links. It has a summary of the EAA video on corrosion in case you are interested - bottom line - save your money and just read the summary. I have never been at ease with this stuff. I have been doing some investigation about it with few definitive answers. So far, I have used the water based primer that ZAC had at their workshop (good stuff in that it didn't smell, but they don't sell it.) I got some Zinc Oxide spray (offered by Tempo who does the ZC and who says it is as good as ZC protection wise, but without the health hazard. Others express doubt about this, but I have yet to see anything other than just an opinion. If anyone has some facts about ZC or the oxide or how it compares to self etch epoxy primers, I would love to know. Gary Liming 801 with cabin fever, waiting for warmer weather to start the wings. ________________________________________________________________________________
Date: Feb 17, 2001
From: Gary Liming <gary(at)liming.org>
Subject: Re: 701 Dedalius Wings
At 06:42 2001.02.16., you wrote: > >Has anyone considered the Dedalius wings for their 701? I know they don't offer it, but would something like that improve the speed of the 801? The Va and Vne is set by other criteria about the structure, so would a wing replacement help? Gary Liming 801 ________________________________________________________________________________
From: "tom tiedman" <ttiedman(at)hotmail.com>
Subject: Re:splice plates,scratch-build ZAC support.
Date: Feb 17, 2001
Hi List, I received notice from ZAC here in Minnesota via U.S. mail, regarding splice plates, that was postmarked Jan. 29th, before I even saw it on the ZAC website. I bought my hand-drawn plans in 1993 (6-3089), and I'm scratchbuilding, also. I have found over the years that ZAC has been extremely helpful and speedy, whether I'm asking for advice, or buying a part... at least they have been for me, a customer from early last decade, and for that I'm grateful. So it has been my experience anyway that ZAC does indeed care about their scratchbuilders as much as their kitbuilders, both in passing along critical info. as well as in their after-purchase support. I still have my splice plate information letter. I won't be needing it, and would be happy to mail it along to anyone who hasn't received it yet or anyone you know without a computer... first come, first served. Just send me your street address to ttiedman(at)hotmail.com, and I'll mail it right out to you! Tom >From: John Tarabocchia <zodiac.builder(at)verizon.net> >Reply-To: zenith-list(at)matronics.com >To: zenith-list(at)matronics.com >Subject: Re: Zenith-List: splice plates >Date: Thu, 15 Feb 2001 22:50:57 -0500 > > > >Barry Mayne wrote: > > > > > Just a quick question to all on the list, > > What is the situation if you are not on the internet or subscribe to the > > newsletter, has ZAC going to notify all builders about the splice plates >or > > are they relying on the grapevine to let everyone know. I am obviously >on > > the list and use the internet but what if I wasn't ? ZAC haven't sent me > > anything about it and I only found out by information passed on to me by >a > > builder who exchanges information with me on engines. I know of three > > builders down here in Australia who are not on the internet or use the > > newsletter and I have no contact info on them so I don't know if they >are > > aware of the problem. > > > > Interesting to hear how many of you guys have actually been contacted by > > ZAC. > > > > Barry Mayne HDS Jabiru 3300 > > > >Interesting point. I'm a scratch builder and I definitely haven't receive >a >notice. Come to think of it, I don't think that the factory could give a >dam >about us plans buyers. Funny though' when I called to purchase supplies >such >as rivets and small items, they don't mind talking to me then. I also love >the >looks I get at the tent at Sun-N-Fun when I say Hello to Nick Heintz and >introduce myself as a scratch builder. I would have thought I had tree >heads >or something. Are there any other scratch builders that get that feeling? > >Just my observation...... > >Hey Barry.....You like that Jabiru. What this dawn 0-200 is going to cost >me >now, I could have bought the 3300 and the firewall forward kit. Oh--Well, >You >live and you learn.... > > >John W. Tarabocchia > >601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html >Airframe 100% Complete... >Installing Wire and Engine... > > ________________________________________________________________________________
From: "The Meiste's" <meiste(at)essex1.com>
Subject: Throttle Rods
Date: Feb 17, 2001
Need help from the "been there, done that" group. I'm trying to install the left & right throttle rods on my 601. For you guy's that have done this, what's the secret to installing these onto the throttle bellcrank. It's easy to assemble either the left or right separately, but installing both rods to the bellcrank is imposable as I see it. The slots in the firewall, and the vertical end rods do not allow enough left & right movement of the bellcrank to engage one rod & then the other. Sorry this may be confusing to many, but the guys that have done this should know what I'm talking about. Also for those of you who have not bent the throttle rod ends (that fit into the vert rods on the bellcrank) be careful, they will crack if bent to sharply. Kelly Meiste 601 HD Tri-Gear ________________________________________________________________________________
From: "Daniel Pelletier" <pelletie1(at)hotmail.com>
Subject: Re: Throttle Rods
Date: Feb 18, 2001
Hi Kelly, I deal with the same problem. My throttle installation is as follow. I buy at Canadian Tire two throttle friction lock T-handle who normally operate a cable. I cut the cables and a part of the gain and make filets 1/4-28 and fit an aluminium 1\4 rod with a jonction at the T-handle. At the other end, I make filet 1\4-28 and fit a fork clevis with 3\16 hole. I make a hole in the top of the bellcrank and fix the fork clevis to the rod with castlenuts and cutterpin. I did the samething on the other side. With fillets, you have adjustments for the both operation. My sole problem is to find a swivel jonction 1\4-28 when I want to lock my throttle. Hope it will serve you. Regards Daniel 601 HDS >I'm trying to install the left & right throttle rods on my 601. For you >guy's that have done this, what's the secret to installing these onto the >throttle bellcrank. >It's easy to assemble either the left or right separately, but installing >both rods to the bellcrank is imposable as I see it. >The slots in the firewall, and the vertical end rods do not allow enough >left & right movement of the bellcrank to engage one rod & then the other. >Sorry this may be confusing to many, but the guys that have done this >should >know what I'm talking about. >Also for those of you who have not bent the throttle rod ends (that fit >into >the vert rods on the bellcrank) be careful, they will crack if bent to >sharply. > >Kelly Meiste >601 HD Tri-Gear > > ________________________________________________________________________________
From: "Gary & Cindy" <cingar(at)mtco.com>
Subject: Re: Throttle Rods
Date: Feb 18, 2001
Kelly, I just finished the throttle install a couple weeks ago. The first thing is that the dimension for the bend on the rods looks like it says 70mm on prints, but that can't be right. If you look at the handle end, the dim. is 50mm and visually the bent part is about 50% of that, so I bent mine 25mm and that worked fine. As far as sliding the bell crank back and forth to get both rods installed, I installed the throttle bearings so that they are a total of 40mm wider than the dimension of the outside of the vertical end rods. That allows the bellcrank to slide about 15 mm in either direction, and caused me to have to flex the throttle rod a small amount to get it into the vertical end rod. Two washers and a cotter pin on each end of the bellcrank stops any lateral movement when complete. The last thing I can think to tell you, is that I found no dimension for the holes in the firewall, so I cut mine 12mm wide and approx 30 mm in length because the rod does move up and down some in its travel and that will allow a small amount of lateral movement of the rods also. I have a foam type sound and heat barrier on the inside of the firewall that just has a slot in it to provide a bit of a seal for all things passing thru the firewall. Hope this helps...I understand the frustration when there is a lack of detail in the prints. Gary -----Original Message----- From: The Meiste's <meiste(at)essex1.com> Date: Saturday, February 17, 2001 4:23 PM Subject: Zenith-List: Throttle Rods > >Need help from the "been there, done that" group. >I'm trying to install the left & right throttle rods on my 601. For you >guy's that have done this, what's the secret to installing these onto the >throttle bellcrank. >It's easy to assemble either the left or right separately, but installing >both rods to the bellcrank is imposable as I see it. >The slots in the firewall, and the vertical end rods do not allow enough >left & right movement of the bellcrank to engage one rod & then the other. >Sorry this may be confusing to many, but the guys that have done this should >know what I'm talking about. >Also for those of you who have not bent the throttle rod ends (that fit into >the vert rods on the bellcrank) be careful, they will crack if bent to >sharply. > >Kelly Meiste >601 HD Tri-Gear > > ________________________________________________________________________________
From: "Gary & Cindy" <cingar(at)mtco.com>
Subject: Re: Throttle Rods
Date: Feb 18, 2001
Kelly, I thought of one more related item that everyone should probably check. After the throttle bellcrank was installed and because again there was no dimension on the prints, it looked like the top stop plate on the gear tube might hit the throttle bellcrank as it passed by, so I took a little off the stop plate. This happened because there was no dimension for the throttle bearing hole, so I moved it forward from center, thinking that would allow more travel in the vertical end rods of the throttle bellcrank. Gary -----Original Message----- From: The Meiste's <meiste(at)essex1.com> Date: Saturday, February 17, 2001 4:23 PM Subject: Zenith-List: Throttle Rods > >Need help from the "been there, done that" group. >I'm trying to install the left & right throttle rods on my 601. For you >guy's that have done this, what's the secret to installing these onto the >throttle bellcrank. >It's easy to assemble either the left or right separately, but installing >both rods to the bellcrank is imposable as I see it. >The slots in the firewall, and the vertical end rods do not allow enough >left & right movement of the bellcrank to engage one rod & then the other. >Sorry this may be confusing to many, but the guys that have done this should >know what I'm talking about. >Also for those of you who have not bent the throttle rod ends (that fit into >the vert rods on the bellcrank) be careful, they will crack if bent to >sharply. > >Kelly Meiste >601 HD Tri-Gear > > ________________________________________________________________________________
Date: Feb 18, 2001
From: Michel Therrien <mtherr(at)yahoo.com>
Subject: Re: 601 Stabilizer Skin Rivets
Oups! I made a mistake with part nos. The US Countersunk rivets are the 1682 not 1691 (which are the lo profile dome rivets). The UK version of the US 1682 is 1604. I use the UK ones. Sorry! Michel --- Michel Therrien wrote: > > > The grip range for the A4 rivet (Avex 1691-412, > equiv > to Zenair's 1604-412) is .093" to .250". Frankly, > we > all attached less than .093" of material with our > rivets and at .250", the A4 rivet does not work. I > tried to attach two pieces of 1/8" with it and the > rivet is too short (this may be because we re-shape > the rivet head?). > > Regarding the stab application, there is 0.016 + > 0.016 > + 0.040 + 0.040 + 0.025 = 0.137" of material. This > is > well within specifications. > > In doubt, you can always try it. > > For the A5 rivet, the specified grip range is 0.125" > to 0.312" (for 1691-514 equiv to Zenair's 1604-514) > > Michel > PS: When I say "equiv to Zenair's", I mean the the > dimensions are supposed to be the same. C. Heintz > mandates that we use the UK rivets (part no 1604). > > Source: Advell Cherry Textron Breakstem Fastening > catalog, page 14 (Avex Fastening Systems) > > > --- David Tellet wrote: > > > > > > I know this has been discussed a little before (in > > the archives), but I > > still not sure about it. The plans call for A4 > > pitch 40 for the stabilizer > > skin to the spars, but this means that on the top > > skin to the aft spar an A4 > > will go through the skin, the elevator hinge, the > > spar, and the spar > > doubler. This seems to be too much material for > the > > A4. It also means that > > the doublers will be attached to the spar web with > > A5's and the spar flange > > with A4's - doesn't seem right to me. > > > > I have a fax question in to Zenith, but I was > hoping > > for a quicker answer. > > Can anybody clarify this for me? Is there a > maximum > > thickness of joining > > materials for the A4 and A5? > > > > Thanks a lot. > > > ===== > ---------------------------- > Michel Therrien CH601-HD > http://pages.infinit.net/mthobby > http://www.pcperfect.com/mthobby/ch601 > > Get personalized email addresses from Yahoo! Mail - > only $35 > a year! http://personal.mail.yahoo.com/ > > > > through > > http://www.matronics.com/archives > http://www.matronics.com/emaillists > > Matronics! > > > > > ===== ---------------------------- Michel Therrien CH601-HD http://pages.infinit.net/mthobby http://www.pcperfect.com/mthobby/ch601 Get personalized email addresses from Yahoo! Mail - only $35 a year! http://personal.mail.yahoo.com/ ________________________________________________________________________________
From: "Michael Brook" <walruss(at)optushome.com.au>
Subject: 701 main gear
Date: Feb 19, 2001
I have a question for the 701 builders. I'm at the point of installing the main gear on my stols. You have to cut out a couple of notches for the bolts in the gear brackets. How did you go about this. There aren't any dimensions on the distance between the notches. I had a brief look at it and my brackets are about 1090 apart. The thing that concerns me is that each of the notches would have to be right at the end of the flat top surfaces just before it starts to curve down. This isn't the best place to have a notch froma stress point of view. But I think that is how it will have to be. one other question. The baggage floor joins with the seat back and rests on the trapezoidal pieces rivetted to the side skins. What are the rivet details of the baggage floor on to the trapezoidal pieces? regards, Mike 2 planes. 2 701's 536hrs build time, back up to speed, putting on the gear and the seatbacks. hmmmm.. ________________________________________________________________________________
From: "Chuck Deiterich" <cfd(at)tstar.net>
Subject: Fw: 701 rivets etc.
Date: Feb 18, 2001
Michael, Here's some info I sent to Randy Subject: Re: 701 rivets etc. > Randy, > The 701 manual gets too brief when you get to the fuslage, I had to dig > around to get the rivet size and pitch, which I list below, hope it helps. > Use A5 p 40 to attach the uprights, 7.F.5.4, to both the side skins and the > longerons. > Use A4 p 40 to attach bottom channel 7.F.6.1 to floor skin and A5 to attach > bottom channel 7.F.6.1 to longerons. > Use A4 p 40 to attach baggage floor, 7.F.5.7, to tappered channels, 7.F.5.6. > Use A5 p 40 to attach tappered channels, 7.F.5.6, to side skins, I got this > from ZAC via e-mail but differs from the manual update. > Regards, > Chuck > > ----- Original Message ----- > From: Randy L. Thwing > To: Chuck Deiterich > Sent: Monday, February 12, 2001 2:33 PM > Subject: 701 rivets etc. > > > Chuck: > Thanks for the info, Your response was the only one I received with > specifics that truly answered the question, everyone else responded > "generally" and though it's good to hear from everyone, that type of info is > not of much use. I appreciate you're taking the time to be specific. One > small point: Is A5 used to attach Uprights 7.F.5.4 to the longerons, or are > A5's used "forward" of this part? > I have downloaded the 13 pages of plans and manual corrections, they do > contain errors and typos, you have to be very careful. I went through them > and they didn't answer my current inquiries. Thanks again. > Regards, > Randy L. Thwing > > > Randy, > > From: Randy L. Thwing <n4546v(at)mindspring.com> > > Listers: > > I've finally restarted on my 701 project, could anyone advise the > > rivet size and spacing to attach part no. 7.F.6.1 to the rear fuselage > > lower skin? I can't seem to find it in the plans. > use A4 pitch 40 > I also need > > clarification regarding the rivet size used to attach the longerons to > > the rear fuselage skins. My location coordinates refer to a location on > > the plans measured from the printed borders, the first number is across > > from the left border and the second number is down from the top border > > in mm, like a road map. On plans sheet 7.F.6 at location (110, 215) is > > the note: "Longerons Rivets A4 pitch 40 (except splice + rear end). At > > location (220, 215) is the note: "rivets A5 pitch 40 (longerons top + > > bottom) shown within arrows like you switch to A5's for the forward > > portion at some point. Do you use A4 full length on the longerons or is > > there some point up front where you switch to A5? > Use A4 pitch 40 on longerons except use A5 at longeron splices, on longerons > forward of uprights 7.F.5.4, for horisontal tail attach brackets and lower > rudder hinge 7.F.4.2. Bolts on upper rudder hinge. > ZAC has a 701 construction manual update on their web site, but beware there > are some typos. > Chuck D. > ________________________________________________________________________________
Date: Feb 18, 2001
From: Dick Baner <db8(at)mtco.com>
Subject: Re: 701 main gear
You are right about a bad place to narrow the cross section but that is what you have to do. Be sure to keep away from sharp edges for the notch so that the stress point is not sharp at least. On the old flat gear bar this is where it tended to bend on a hard landing. dick baner Michael Brook wrote: > > I have a question for the 701 builders. I'm at the point of installing the > main gear on my stols. You have to cut out a couple of notches for the bolts > in the gear brackets. How did you go about this. There aren't any dimensions > on the distance between the notches. I had a brief look at it and my > brackets are about 1090 apart. The thing that concerns me is that each of > the notches would have to be right at the end of the flat top surfaces just > before it starts to curve down. This isn't the best place to have a notch > froma stress point of view. But I think that is how it will have to be. > > one other question. The baggage floor joins with the seat back and rests on > the trapezoidal pieces rivetted to the side skins. What are the rivet > details of the baggage floor on to the trapezoidal pieces? > > regards, > > Mike 2 planes. 2 701's 536hrs build time, back up to speed, putting on the > gear and the seatbacks. hmmmm.. > ________________________________________________________________________________
From: "HOLCOMBE" <holcombe(at)oregonfast.net>
Subject: Re: 701 main gear
Date: Feb 18, 2001
On the notches in the landing gear be sure to round, smooth, and polish, to reduce the chance of stress concentrations. Richard ----- Original Message ----- From: Michael Brook <walruss(at)optushome.com.au> Sent: Monday, February 19, 2001 1:42 AM Subject: Zenith-List: 701 main gear > > I have a question for the 701 builders. I'm at the point of installing the > main gear on my stols. You have to cut out a couple of notches for the bolts > in the gear brackets. How did you go about this. There aren't any dimensions > on the distance between the notches. I had a brief look at it and my > brackets are about 1090 apart. The thing that concerns me is that each of > the notches would have to be right at the end of the flat top surfaces just > before it starts to curve down. This isn't the best place to have a notch > froma stress point of view. But I think that is how it will have to be. > > one other question. The baggage floor joins with the seat back and rests on > the trapezoidal pieces rivetted to the side skins. What are the rivet > details of the baggage floor on to the trapezoidal pieces? > > > regards, > > Mike 2 planes. 2 701's 536hrs build time, back up to speed, putting on the > gear and the seatbacks. hmmmm.. > > ________________________________________________________________________________
From: "Ralph Llewellyn" <llewellyn(at)tinet.ie>
Subject: Re: Reduction Drive from Ireland
Date: Feb 19, 2001
Larry Do you have any more info on www.av8r.co.uk I'm located in Ireland and would be very interested in following this up. Ralph Llewellyn (701 scratch building ) ________________________________________________________________________________
From: "Larry McFarland" <larrymc(at)qconline.com>
Subject: Re: Reduction Drive from Ireland
Date: Feb 19, 2001
Ralph, Their phone number is 028 7082 37 93 Fax: 028 7082 46 25 The company name is Microflight Ireland, AV8R Engines & they appear to be dealer/representatives for Konig/Zanzottera engines as well. Good luck, Larry Scratch building a 601 HDS, 50% complete since Sept 99. ----- Original Message ----- From: Ralph Llewellyn <llewellyn(at)tinet.ie> Sent: Monday, February 19, 2001 12:04 PM Subject: Re: Zenith-List: Reduction Drive from Ireland > > Larry > > Do you have any more info on www.av8r.co.uk I'm located in Ireland and > would be very interested in following this up. > > Ralph Llewellyn (701 scratch building ) > > > > > > ________________________________________________________________________________
From: "Carl Bertrand" <cgbrt(at)mondenet.com>
Subject: Re: splice plates
Date: Feb 18, 2001
John, I must say as a scratch builder that I have been treated very fairly by Chris and ZAC. Regards Carl. -----Original Message----- From: John Tarabocchia <zodiac.builder(at)verizon.net> Date: February 15, 2001 10:55 PM Subject: Re: Zenith-List: splice plates > >Barry Mayne wrote: > >> >> Just a quick question to all on the list, >> What is the situation if you are not on the internet or subscribe to the >> newsletter, has ZAC going to notify all builders about the splice plates or >> are they relying on the grapevine to let everyone know. I am obviously on >> the list and use the internet but what if I wasn't ? ZAC haven't sent me >> anything about it and I only found out by information passed on to me by a >> builder who exchanges information with me on engines. I know of three >> builders down here in Australia who are not on the internet or use the >> newsletter and I have no contact info on them so I don't know if they are >> aware of the problem. >> >> Interesting to hear how many of you guys have actually been contacted by >> ZAC. >> >> Barry Mayne HDS Jabiru 3300 >> > >Interesting point. I'm a scratch builder and I definitely haven't receive a >notice. Come to think of it, I don't think that the factory could give a dam >about us plans buyers. Funny though' when I called to purchase supplies such >as rivets and small items, they don't mind talking to me then. I also love the >looks I get at the tent at Sun-N-Fun when I say Hello to Nick Heintz and >introduce myself as a scratch builder. I would have thought I had tree heads >or something. Are there any other scratch builders that get that feeling? > >Just my observation...... > >Hey Barry.....You like that Jabiru. What this dawn 0-200 is going to cost me >now, I could have bought the 3300 and the firewall forward kit. Oh--Well, You >live and you learn.... > > >John W. Tarabocchia > >601hds N6042T Web Site: http://hometown.aol.com/zodiacbuilder/Home.html >Airframe 100% Complete... >Installing Wire and Engine... > > ________________________________________________________________________________
Date: Feb 19, 2001
From: Gary Liming <gary(at)liming.org>
Subject: TSO vs non-TSO
Could someone direct me to a discussion or other source (preferably on the web) about buying TSO vs non-TSO'd instruments, avionics, etc? Are there some things you just don't want to skimp on, or is it usually the case that if a company makes both a TSO and nonTSO versions, then exercising the advantage of making a homebuilt is always the thing to do? I realize this is separate from the question of whether or not a given product or manufacturer is of quality. Have most of you who have completed your aircraft gone nonTSO'd, TSO'd, or a mix? Thanks, Gary Liming 801 ________________________________________________________________________________
Subject: Re: TSO vs non-TSO
From: Glen.Worstell(at)seagate.com
Date: Feb 20, 2001
02/20/2001 07:29:11 AM > Have most of you who have completed your aircraft gone nonTSO'd, TSO'd, or a mix? I have a TSO'd navcom and another that is not. They both work fine. There have been discussions about whether TSO'd stuff is required for IFR or not; my conclusion is that TSO is not required in homebuilts, except for transponders and IFR gps. Your conclusions may vary (murky regs). As there are crappy TSO'd radios (ARC, for example) and some pretty good ones that are not, I'd purchase on reputation and price. Were I to purchase a new navcom I'd get a UPS SL-30. g. 601HD trike, Rotax 912, dual electrical system, IFR, slow but fun ________________________________________________________________________________
From: "David Tanner" <vk3auu(at)sympac.com.au>
Subject: Re: "Z" ' s around bottom fuse access 701
Date: Feb 21, 2001
My bottom door has a piano hinge at the front edge and 2 Dzus fasteners on each other edge. If I were to do it again, I would put the hinge on one side as it touches the ground as it is and I need to put one wheel up on a 4 gallon drum. My battery is also accessible through this door. David Tanner CH701 912UL 165 hours flying ________________________________________________________________________________
Date: Feb 20, 2001
From: Gary Liming <gary(at)liming.org>
Subject: 801 instrument panel template
Not seeing one on the website, I asked ZAC if a measured drawing existed for the 801 instrument panel. Nick said not yet, but was kind enough to make a tracing of an actual panel and send it to me. I made a measured drawing of it with dimensions and put it up at www.liming.org/ch801 You can follow the links to "research" and "801 instrument panel." It is a help in laying out where you want the instruments and avionics to go. Gary Liming 801 ________________________________________________________________________________
From: "Steve Danielson" <steved(at)nc.rr.com>
Subject: Damage tolerances for the 701
Date: Feb 20, 2001
Somewhere (maybe in the plans or assembly guide for the 701) I read a document on allowable damage tolerances after any type of accidents. It talked about the allowable amount of waviness on trailing edges, talked about how to patch over dents, how many rivets etc... I looked quickly through the assembly guide and plans and I didn't spot it. Does anyone know what I am talking about and where to find it? Thanks, Steve Danielson http://home.nc.rr.com/danielson/ ________________________________________________________________________________
From: "Randy L. Thwing" <n4546v(at)mindspring.com>
Subject: those with interest in 701
Date: Feb 20, 2001
Dear 701 Builders and interested friends: I've established a list of my friends with interest in my 701 building project, plus I'm trying to learn how to use my digital camera. I'm sending a picture here and there as I try to document progress. I've added the names of builders and non-builders alike. I'm taking pictures in the lowest resolution to avoid long download times. Comments are always welcome, plus I just like to hear from everyone. If you are interested in receiveing these posts, please email me off list and I will add you to my list. Regards, Randy L. Thwing, 701 plans ________________________________________________________________________________
From: "Robert Isaacs" <bob999(at)worldnet.att.net>
Subject: 601XL
Date: Feb 20, 2001
I sometime feel like maybe I am only one of a few who is working on building a 601XL. Is anyone one else also working on this kit model and if so what kind of problems have you ran into? How far along are you? What kind of engine are being considered? IS THEIR ANYONE OUT THEIR? Bob N601XL ________________________________________________________________________________
From: "Mark Townsend" <mark.townsend(at)xrxgsn.com>
Subject: Re: 601XL
Date: Feb 20, 2001
Hey Bob Were out here, just look for the high forheads from scratching!! Problems ? not yet but it is early for me and I'm still learning. What Kind of Engine? I hav e decided on the CAM125 ,for MANY reasons over the rotax and jab. Mark 601XL scrach building ==============


January 22, 2001 - February 20, 2001

Zenith-Archive.digest.vol-cb