Zenith-Archive.digest.vol-gg

November 26, 2006 - December 08, 2006



      someone could do demos for building spars or bending ribs and such. I think
      we have a very nice place to hold one here in San Antonio, but I have too
      many issues to be able to sponsor it. Maybe someone else could do the main
      sponsoring and I could help.  The local EAA chapter has a club house
      w/kitchen, and smoker/bbq grill. There's place for camping or stay at the
      local hotels.
      
      Randy Stout
      San Antonio TX
      www.geocities.com/r5t0ut21
      n282rs at earthlink.net 
      
      -----Original Message-----
From: owner-zenith-list-server(at)matronics.com
[mailto:owner-zenith-list-server(at)matronics.com] On Behalf Of Mack Kreizenbeck Sent: Saturday, November 25, 2006 12:59 PM
Subject: Re: Coast to coast and back in my 601XL
--> Juan, I like your idea about getting together and flying somewhere as a group. I hope to have my flying machine finished this spring! Anyone else out there got any suggestions? The poh-oh-unemployed farm boy from Idaho 601 XL QBK --------------------------------- ________________________________________________________________________________
Date: Nov 26, 2006
From: Brandon Tucker <btucke73(at)yahoo.com>
Subject: RE: PROP CHOICES
Robin, My information is several months old, but I will give you what I know. I met Paul at EAA chapter 1 fly-in in southern California. At that time, they were working on getting props built for the Vans series of aircraft. They were going for the bigger numbers in the RV's. Paul has one installed in his Lancair, which he flew to the event, and one installed in the Reno racer based in Fallbrook, Ca. At the time, there were no solid plans for building props in the 100 hp range, only the desire to do so in the future. If John Moyle is still monitoring the list, he will have more accurate information. John, who is the US Woodcomp dealer, partnered with Paul for the prop production. If you receive Contact magazine, I am confident that they will be all over the progress of the prop, as John is also the associate editor, or some other important sounding title. He is also a 601 XL builder... VR/ Brandon Tucker --------------------------------- ________________________________________________________________________________
From: "Jonathan Starke" <jonathan(at)entry.co.za>
Subject: Re: Sensitive Elevator
Date: Nov 24, 2006
Hi Dan, The oscilations I am talking about are induced by me, when correcting in heavy turbulence, as the slightest movement on the stick forwards or backwards causes a pitch change. I.e. deflecting the ailerons to lidt a dropped wing in turbulance is very dificult to not move the stick in the pitch direction as well. Then Weight and Balance is bang on the manual, a I would not fly it otherwise. (Done with three digital scales, by my AMO) Jonathan > >Jonathan, >Occilations are an indication of the CG getting too far aft >causing instability in the pitch axis? Had you checked the >weight and ballance? >Dan ________________________________________________________________________________
Date: Nov 27, 2006
From: Matt Dralle <dralle(at)matronics.com>
Subject: List of Contributors Coming Soon - Make Sure You're Listed!
Dear Listers, The List of Contributors (LOC) is just around the corner! On December 1st I post a list of everyone that so generously made a Contribution to support the Lists. Its my way of publicly thanking everyone that took a minute to show their appreciation for the Lists. As a number of people have pointed out in their Contribution comments, the List seems at least as valuable of a building/flying/recreating tool as a typical your magazine subscription! And how interactive is a magazine, after all? :-) Won't you take minute and assure that your name is on the upcoming LOC? Tell others that you appreciate the Lists. Making a Contribution to support the Lists is fast and easy using your Visa, MasterCard, or Paypal account: http://www.matronics.com/contribution Or, by droping a personal check in the mail to: Matronics / Matt Dralle PO Box 347 Livermore CA 94551-0347 USA (Please include your email address on the check!) I would like to thank everyone that has so generously made a Contribution thus far during this year's List Fund Raiser! Remember that its YOUR support that keeps these Lists running and improving! Don't forget to include a little comment about how the Lists have helped you! Thank you! Matt Dralle Matronics Email List Administrator ________________________________________________________________________________
From: Trevor Page <webmaster(at)upac.ca>
Subject: Re: Torquing GSC Propeller Bolts
Date: Nov 27, 2006
John, I have a similar arrangement of a prop extension on my 601HD but I'm using a 68" Warp Drive prop. My extension is a simpler arrangement of a heavy walled 6061 tube with match drilled holes that use long prop bolts to directly bolts the whole thing to the prop flange. The main concern on mine is not stripping the threads on either the bolts or the prop flange cause neither are cheap to replace! Rotax recommends a max of 94 ft/Lbs on the prop flange according to my manual. My bolts extend enough past the prop flange to have washers and nuts on the back to keep things from backing out. Trev Page C-IDUS 601HD R912 On Nov 26, 2006, at 12:37 PM, John M. Goodings wrote: > > > Our CH601HD Zodiac with a Rotax 912S 100 HP engine has a 68-inch, 3- > blade > GSC wooden prop. In our installation, there is a prop flange > extension. > The prop is held on by 6 1/4-inch bolts (3 through the aluminum blade > roots), and by 6 5/16-inch bolts onto the flange extension. GSC > Systems > says use 100 inch pounds of torque for the 1/4 inch bolts, and 140 > for the > 5/16; these values are critical. Normally, with a washer under > both the > head and the nut, one holds the bolt head stationary, and torques the > nylon lock nut; these nyloks are the preferred nuts recommended by > GSC. > Because of the design of the prop flange extension, it is not > possible to > get the torque wrench onto the nuts. Thus, one holds the nut > stationary, > and torques the bolt head. THIS IS NOT THE SAME THING. My son Peter > (co-builder of our aircraft, and a professional mechanical > engineer) knows > from practical experience that putting the torque wrench on the > bolt head > can undertorque the nut by possibly 20-30%, or even more. It > stands to > reason: the bolt shaft (or grip) inevitably experiences some > friction in > passing through the parts being bolted together on the way to the nut. > There is a little part called a "crow's foot" to overcome this > difficulty, > which goes over the nut, extends radially outward for about an > inch, and > has a square hole for attachment of the torque wrench. It happened > that I > had always torqued the prop bolts on our aircraft. In setting out to > retorque the bolts yesterday because the weather is now turning cold, > Peter realized right away that there was a problem. I had never > used a > crow's foot (I did not know of their existence!). I'm guessing > that many > others using this Rotax/GSC prop installation were also unaware of > this > problem. What have others done about this? Were they aware of the > problem? > > John Goodings, C-FGPJ, CH601HD with R912S, Toronto/Ottawa/Waterloo > > ________________________________________________________________________________
Subject: Is Comcast Blocking the Digest Again??
From: "lwhitlow" <ldwhitlow(at)comcast.net>
Date: Nov 27, 2006
Hey Matt Me thinks the demons at Comcast are blocking the list again. I get the homebuilt list daily but I haven't got the Zenith List since the 24'th Larry Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77274#77274 ________________________________________________________________________________
From: "Carl Bertrand" <cgbrt(at)mondenet.com>
Subject: 701 slats again
Date: Nov 27, 2006
From: "Carl Bertrand" <cgbrt(at)mondenet.com> To: Subject: Re: Zenith-List: 701 no slats again Hi Joe Have followed this thread with interest. I've experimented with the 701's wing design but not with vgs. I opted for air pressure operated slats and a thinner airfoil. For more info on the results see my presentation at: eaa245.dhs.org/ I never considered flying the 701 without slat but I'm not surprised that it could be a hand full. My take is that the Cof G and the centre of pressure would move back, the Cp more so causing a nose heavy pitch moment at all speeds and angles of attack. I would expect all stall speeds to increase with the clean wing and top speed to probably remain the same or decrease because of the blunt leading edge. Adding vgs should delay the stall but should also increase drag? Very interested in the results anyone gets if you try the no slat configuration. Carl 701/912/amphibs ________________________________________________________________________________
From: Bryan Martin <bryanmmartin(at)comcast.net>
Subject: Re: Fuel Pump Placement and Fuel Line Question
Date: Nov 27, 2006
A 70 micron filter is just a fine mesh screen like those found in gascolators and the screens in automotive fuel tanks. The stuff blocked by these screens winds up in the sediment bowl or fuel tank sump where it can be drained during pre-flight. My fuel pumps are just downstream of the gascolator at the low point of the system. I certainly wouldn't put anything finer ahead of the pump. The idea is to minimize any flow restrictions on the inlet side of the pump to avoid reducing the pressure to the point where the fuel might vaporize in the line. On Nov 26, 2006, at 10:07 PM, lwhitlow wrote: > > > Bryan > > the Facet install sheet specifies a 70 micon filter on the inlet > side of the pump > > Has anyone else put a filter on the inlet side of the Facet pump?? > > >> >> >> Bryan wrote >> >> I wouldn't put a filter on the suction side of the fuel pump. It >> isn't necessary and it increases the risk of a fuel stoppage. All you >> should have on the suction side of the pump is the screen in the >> tank. The screen keeps the bigger stuff out of the fuel pump and >> filter will keep the small stuff from clogging the carbureter jets. >> The filter should go in the line just before the carburetor. Even on >> cars the filter is on the pressure side of the pump. > > -- Bryan Martin N61BM, CH 601 XL, RAM Subaru, Stratus redrive. ________________________________________________________________________________
From: "Robert N. Eli" <robert.eli(at)adelphia.net>
Subject: Re: 701 slats again
Date: Nov 27, 2006
Carl, I talked to Chris Heintz at Air Venture several years ago about the 701 airfoil, and the aerodynamic design of the slats. The airfoil is an old standard airfoil (it is a NACA 640-18) with just a slot added. In other words, if you simply remove the slot and leave the fixed slat in its design postion to define the nose of the airfoil, then you have standard NACA 640-18 airfoil. If one wants to remove the slat from the airfoil design, the original airfoil can be recovered by simply covering the slots with sheet metal that matches the airfoil contour. Bob Eli ----- Original Message ----- From: "Carl Bertrand" <cgbrt(at)mondenet.com> Sent: Monday, November 27, 2006 8:18 AM Subject: Fw: Zenith-List: 701 slats again > > > From: "Carl Bertrand" <cgbrt(at)mondenet.com> > To: > > Subject: Re: Zenith-List: 701 no slats again > > Hi Joe > Have followed this thread with interest. > I've experimented with the 701's wing design but not with vgs. I opted for > air pressure operated slats and a thinner airfoil. > For more info on the results see my presentation at: eaa245.dhs.org/ > I never considered flying the 701 without slat but I'm not surprised that > it could be a hand full. My take is that the Cof G and the centre of > pressure would move back, the Cp more so causing a nose heavy pitch moment > at all speeds and angles of attack. I would expect all stall speeds to > increase with the clean wing and top speed to probably remain the same or > decrease because of the blunt leading edge. > Adding vgs should delay the stall but should also increase drag? > Very interested in the results anyone gets if you try the no slat > configuration. > > Carl 701/912/amphibs > > > ________________________________________________________________________________
Subject: What size Druzs Fasteners?
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Nov 27, 2006
Anybody know or have easy access to what size Druzs fasteners Zenith ships with the wing locker kit? I need to order the retaining washers that DON'T come with the kit and can't make it to the airport for a couple of days. -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77309#77309 ________________________________________________________________________________
From: "Dave Ruddiman" <pacificpainting(at)comcast.net>
Subject: Re: Is Comcast Blocking the Digest Again??
Date: Nov 27, 2006
I've got Comcast and haven't had any problems receiving since a while back. ----- Original Message ----- From: "lwhitlow" <ldwhitlow(at)comcast.net> Sent: Monday, November 27, 2006 4:23 AM Subject: Zenith-List: Is Comcast Blocking the Digest Again?? > > Hey Matt > > Me thinks the demons at Comcast are blocking the list again. > > I get the homebuilt list daily but I haven't got the Zenith List since the > 24'th > > Larry > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=77274#77274 > > > ________________________________________________________________________________
Date: Nov 27, 2006
From: TYA2 <tya2@4-fly.net>
Subject: Re: What size Dzus Fasteners?
Dear Gig, I own a CH2000 which used Zenair part number AJW5-30 Winged Dzus Pin which are charged out at $3.49 Canadian each, and I just ordered Zenair part number SR 5 SS Dzus Pin Snap Rings at $0.20 each from Zenair Canada. These fasteners were used in the top to bottom cowling joint, and the cowling to airframe. Aircraft Spruce probably sell them too. Reg CH2000 in -30F Northern Alberta > >Anybody know or have easy access to what size Dzus fasteners Zenith ships >with the wing locker kit? I need to order the retaining washers that DON'T >come with the kit and can't make it to the airport for a couple of days. > >-------- >W.R. "Gig" Giacona >601XL Under Construction >See my progress at www.peoamerica.net/N601WR > > >Read this topic online here: > >http://forums.matronics.com/viewtopic.php?p=77309#77309 > > ________________________________________________________________________________
From: "Robin Bellach" <601zv(at)ritternet.com>
Subject: What size Druzs Fasteners?
Date: Nov 27, 2006
AJ5-30 ----- Original Message ----- From: "Gig Giacona" <wr.giacona(at)cox.net> Sent: Monday, November 27, 2006 8:47 AM Subject: Zenith-List: What size Druzs Fasteners? > > Anybody know or have easy access to what size Druzs fasteners Zenith ships > with the wing locker kit? I need to order the retaining washers that DON'T > come with the kit and can't make it to the airport for a couple of days. > ________________________________________________________________________________
Date: Nov 27, 2006
From: TYA2 <tya2@4-fly.net>
Subject: CH2000 Winter Front
Zenair Canada has a winter front baffle for CH2000 /alarus CH640 aircraft that will help keep the oil temperature higher. Cost was $48.00 Canadian from the factory. If it ever warms up here I will get around to installing it. I also ordered new fuel lines because mine are date expired and I need to renew them for the import inspection. Any one out there have a supplier for wing covers for the CH2000? Reg in Edmonton CH2000 SN 20-0010 ________________________________________________________________________________
Date: Nov 27, 2006
From: TYA2 <tya2@4-fly.net>
Subject: Bruce's Custom Cover & CH2000
Dear Listmates, When I enquired about the availability of a Canopy Cover for the CH2000, many of you sent negative reviews of Bruce's Covers. I want to report that the Custom Cover I recently received and which was recommended by the factory in Midland arrived in good condition. This cover perfectly fits my CH2000, has spots for the door handles, and the hand holds, and is constructed of high quality materials. I went with Bruce's because of previous good experiences 12 years ago with a Bruces Cover on an American AA-5 I previously owned. I realize sometimes a business name remains but the company has changed and so has the workmanship. I must say I find that the CH2000 cover is a high quality item. I also ordered engine intake plugs and they also high quality. If you have an Alarus or CH2000, Bruce's Cover will do the job, someone obviously did a very good job of pattern making. Now to find an engine blanket and wing covers... Reg in Edmonton Alberta N8202Z 1995 CH2000 ________________________________________________________________________________
Date: Nov 27, 2006
From: "Paul Tipton" <PTIPTON(at)swmail.sw.org>
Subject: Re: Coast to coast and back in my 601XLCoast to coast and
back in my 601XL Great idea. I went to the Texas Fly-in in Hondo and was the only 701 there. Paul Tipton 321PT ________________________________________________________________________________
Date: Nov 27, 2006
From: ALAN BEYER <agbeyer(at)sbcglobal.net>
Subject: Re: What size Druzs Fasteners?
Giacona,=0A=0AI don't know off hand. Just food for thought. I made my hol es for the screws a little larger so it is easyer to line them up when you close the door. All I did was use an "O" ring over the end of the screw an d it works good. They have been in place for over two years.=0A=0AAL from Oshkosh=0A=0A=0A----- Original Message ----=0AFrom: Gig Giacona <wr.giacona (at)cox.net>=0ATo: zenith-list(at)matronics.com=0ASent: Monday, November 27, 2006 8:47:48 AM=0ASubject: Zenith-List: What size Druzs Fasteners?=0A=0A=0A--> Zenith-List message posted by: "Gig Giacona" =0A=0AAnyb ody know or have easy access to what size Druzs fasteners Zenith ships with the wing locker kit? I need to order the retaining washers that DON'T come with the kit and can't make it to the airport for a couple of days.=0A=0A- -------=0AW.R. "Gig" Giacona=0A601XL Under Construction=0ASee my progress at www.peoamerica.net/N601WR=0A=0A=0A=0A=0ARead this topic online here:=0A=0Ahttp://forums.matronics.com/viewtopic.php?p=77309#77309=0A=0A ====== ________________________________________________________________________________
Subject: Re: What size Druzs Fasteners?
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Nov 27, 2006
Good idea. Unfortunatly I already ordered the retainers from AS. Thanks though. agbeyer(at)sbcglobal.net wrote: > Giacona, > > I don't know off hand. Just food for thought. I made my holes for the screws a little larger so it is easyer to line them up when you close the door. All I did was use an "O" ring over the end of the screw and it works good. They have been in place for over two years. > > AL from Oshkosh > > > --- -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77398#77398 ________________________________________________________________________________
Date: Nov 27, 2006
From: Andre Abreu <andre_abreu_2000(at)yahoo.com>
Subject: Zodiac 601XL Performance Again (sorry)
Sorry to bring this up once again... but why does the Zenith website claim this performance figure?=0A=0AI think this figure below is for the Rotax. =0A=0A75% CRUISE @ 8,000 ft. (TAS*)155 mph=0A=0A=0Ahttp://www.zenithair.co m/zodiac/xl/performance.html=0A=0A=0AI would love this to be true... =0Abut like my mother tried to beat in my head ... if it's too good to be true... =0Ahow does that go?=0A=0AKind Regards,=0AAndy Abreu ________________________________________________________________________________
Subject: Re: What size Druzs Fasteners?
From: "DaveG601XL" <david.m.gallagher(at)ge.com>
Date: Nov 27, 2006
I used what I think were 5/16" e-clips from Home Depot. They fit the groove. Dave G Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77420#77420 ________________________________________________________________________________
Subject: C-85 in 601XL???
From: "DaveG601XL" <david.m.gallagher(at)ge.com>
Date: Nov 27, 2006
I am early in my 601XL build and am still considering engine choices. I have the opportunity to use a C-85 engine. It was meant for another project that will probably never get completed due to the builders age. It is a close family member, so if I asked for it, I could probably get it for free. Has anybody put a C-85 in an XL or ever considered it? I am concerned with how much of a deficit I would see in speed, max weight and useful load vs. the published and actuals people are seeing with the Rotax and Jabiru engines. Thanks for any advice or opinions, Dave G Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77422#77422 ________________________________________________________________________________
Date: Nov 27, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: 701 slats again
All that is true however you will have moved the leading edge of the wing back 4 inches, thus needing to redo your moment and ARM. Or the CG will be off. Juan -----Original Message----- >From: "Robert N. Eli" <robert.eli(at)adelphia.net> >Sent: Nov 27, 2006 8:52 AM >To: zenith-list(at)matronics.com >Subject: Re: Zenith-List: 701 slats again > > >Carl, > >I talked to Chris Heintz at Air Venture several years ago about the 701 >airfoil, and the aerodynamic design of the slats. The airfoil is an old >standard airfoil (it is a NACA 640-18) with just a slot added. In other >words, if you simply remove the slot and leave the fixed slat in its design >postion to define the nose of the airfoil, then you have standard NACA >640-18 airfoil. If one wants to remove the slat from the airfoil design, the >original airfoil can be recovered by simply covering the slots with sheet >metal that matches the airfoil contour. > >Bob Eli > >----- Original Message ----- >From: "Carl Bertrand" <cgbrt(at)mondenet.com> >To: >Sent: Monday, November 27, 2006 8:18 AM >Subject: Fw: Zenith-List: 701 slats again > > >> >> >> >> >> >> >> From: "Carl Bertrand" <cgbrt(at)mondenet.com> >> To: >> >> Subject: Re: Zenith-List: 701 no slats again >> >> Hi Joe >> Have followed this thread with interest. >> I've experimented with the 701's wing design but not with vgs. I opted for >> air pressure operated slats and a thinner airfoil. >> For more info on the results see my presentation at: eaa245.dhs.org/ >> I never considered flying the 701 without slat but I'm not surprised that >> it could be a hand full. My take is that the Cof G and the centre of >> pressure would move back, the Cp more so causing a nose heavy pitch moment >> at all speeds and angles of attack. I would expect all stall speeds to >> increase with the clean wing and top speed to probably remain the same or >> decrease because of the blunt leading edge. >> Adding vgs should delay the stall but should also increase drag? >> Very interested in the results anyone gets if you try the no slat >> configuration. >> >> Carl 701/912/amphibs >> >> >> >> >> >> >> >> >> > > ________________________________________________________________________________
Date: Nov 27, 2006
From: Steven Janicki <mmesa005(at)yahoo.com>
Subject: 601XL - Engine out / Glide Experience
Hello All,=0A =0AI am planning to build a 601XL in the near future and have been reading the recent threads about the unfortunate loss of a 601XL and pilot.=0A =0AI don't know what happened and don't want to speculate about w hat happened, etc. I would like to know if anyone has experience with simul ated engine out landings and would share those experiences with the group? I would also appreciate any experiences with how the 601XL glides during si mulated engine out practice and any comparisons to other aircraft, i.e. Ces sna 172, etc. =0A =0AThanks in advance,=0A =0ASteven=0A=0A ________________________________________________________________________________
Subject: Re: Zodiac 601XL Performance Again (sorry)
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Nov 27, 2006
You do realize that is True Airspeed? http://www.paragonair.com/public/aircraft/calc_TAS.html aabreu wrote: > Sorry to bring this up once again... but why does the Zenith website claim this performance figure? > > I think this figure below is for the Rotax. > > 75% CRUISE @ 8,000 ft. (TAS*) > 155 mph > > > http://www.zenithair.com/zodiac/xl/performance.html (http://www.zenithair.com/zodiac/xl/performance.html) > > > I would love this to be true... > but like my mother tried to beat in my head ... if it's too good to be true... > how does that go? > > Kind Regards, > Andy Abreu -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77434#77434 ________________________________________________________________________________
Date: Nov 27, 2006
From: Brandon Tucker <btucke73(at)yahoo.com>
Subject: RE: C-85 in 601XL???
Dave, I have a good friend that is almost complete with his 601HDS with Cont O-200. He is too old to fly it, but has been very slowly plugging along on the aircraft for over 12 years. I think he was one of the very first kit buyers. He is now too old to even work on it, and has friends do the work. His wife asked me to finish the project, which I hope to do, but I am too busy getting mine back in the air. He has a mold in the shop for a custom cowling to house the engine. I am not sure if he bought or built his engine mount. I also know that he has a Warp Drive to put on it, and put the battery behind the seats. If you e-mail me off-list with specific questions about the installation, I can call and ask. R/ Brandon --------------------------------- ________________________________________________________________________________
From: "Josh Olson" <mrbizi(at)yahoo.com>
Subject: 601XL - Engine out / Glide Experience
Date: Nov 27, 2006
Steven: I would like to know as well. I am also considering building the Zodiac but I would like to know glide speed and glide ratio information as well. If anyone responds, please cc me as well. Thanks, Josh Olson Email: mrbizi(at)yahoo.com _____ From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com] On Behalf Of Steven Janicki Sent: Monday, November 27, 2006 5:54 PM Subject: Zenith-List: 601XL - Engine out / Glide Experience Hello All, I am planning to build a 601XL in the near future and have been reading the recent threads about the unfortunate loss of a 601XL and pilot. I don't know what happened and don't want to speculate about what happened, etc. I would like to know if anyone has experience with simulated engine out landings and would share those experiences with the group? I would also appreciate any experiences with how the 601XL glides during simulated engine out practice and any comparisons to other aircraft, i.e. Cessna 172, etc. Thanks in advance, Steven ________________________________________________________________________________
From: "Josh Olson" <mrbizi(at)yahoo.com>
Subject: Zodiac 601XL Performance Again (sorry)
Date: Nov 27, 2006
Andre: FYI. This figure is based on the Jabiru 3300 install I believe. Josh Olson Email: mrbizi(at)yahoo.com _____ From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com] On Behalf Of Andre Abreu Sent: Monday, November 27, 2006 4:39 PM Subject: Zenith-List: Zodiac 601XL Performance Again (sorry) Sorry to bring this up once again... but why does the Zenith website claim this performance figure? I think this figure below is for the Rotax. 75% CRUISE @ 8,000 ft. (TAS*) 155 mph http://www.zenithair.com/zodiac/xl/performance.html I would love this to be true... but like my mother tried to beat in my head ... if it's too good to be true... how does that go? Kind Regards, Andy Abreu ________________________________________________________________________________
Date: Nov 28, 2006
From: Matt Dralle <dralle(at)matronics.com>
Subject: Who is "Matt Dralle" & What Are "The Lists"? [Please Read]
Dear Listers, Who is Matt Dralle and what exactly are these Lists? Well, I've been working in the information technology industry for over 20 years primarily in computer networking design and implementation. I have also done extensive work in web development and CGI design during this period. I started the Matronics Email Lists back in 1990 with about 30 fellow RV builders from around the world. Since that time, I have added 63 other kinds of aircraft related Lists to the line up and numerous other List related services such as the Forums, Wiki, Archives and Search Engine just to name a few. For flexibility and reliability, I have chosen to run all of my own servers here locally. Other List-related systems include a 1 Gigabit, fully switched network infrastructure, a commercial-grade Netscreen firewall, a Barracuda spam filter, a local T1 Internet router, and a commercial-grade business T1 Internet connection with full static addressing. The computer servers found here include a brand new, quad-processor Xeon Linux server for List web services, a dual-processor Xeon Linux system dedicated to the email processing List functions, and another P4 Linux system serving as a remote storage disk farm for the archives, databases, and for an on-line hard drive-based backup system with 3.2 Terra Bytes of storage, soon to be upgraded to over 6 Terra Bytes! This entire system is protected by three large, commercial-grade uninterrupted power supply (UPS) systems that assure the Lists are available even during a local power outage! Speaking of power, imagine how much electricity it takes to run all of these systems. One month this Summer, I had a staggering $1368 bill for electricity alone! I recently upgraded all of the computer racking infrastructure including new power feeds and dedicated air conditioning for the room that serves as the Computer Center for the Matronics Email Lists. This year I added another rack to house the new MONSTER quad-processor web system that didn't quite fit into the first rack! Here's a composite photo of the List Computer Center before the addition of the second rack: http://www.matronics.com/MattDralle-ListComputerCenter.jpg As you can see, I take running these Lists very seriously and I am dedicated to providing an always-on, 24x7x365 experience for each and every Lister. But building and running this system isn't cheap. As I've stated before, I don't support any of these systems with commercial advertising on the Lists. It is supported 100% through List member Contributions! That means you... and you... and YOU! To that end, I hold a List Fund Raiser each November and ask that members make a small Contribution to support the continued operation and upgrade of this ever-expanding system. Its solely YOUR Contributions that keeps it running! Please make a Contribution today to support these Lists! http://www.matronics.com/contribution Or, by dropping a personal check in the mail to: Matronics / Matt Dralle PO Box 347 Livermore CA 94551-0347 USA (Please include your email address on the check!) Thank you! Matt Dralle Matronics Email List Administrator ________________________________________________________________________________
Subject: Re: 701 slats again
From: "secatur" <appraise1(at)bigpond.com>
Date: Nov 28, 2006
More interesting reading The vast reduction in drag allows all these aircraft to fly considerably faster for the same power, climb better, glide better, and with the benefit of Vortex Generators, lift-off and touch-down just as short as with slats, but with more control. In summary for my Savannah: Fast cruise @ 5200 rpm has gone from 79 kt to 85 kt. = + 6 kts Top speed has gone from 94 kts to 103 kts! = + 9 kts. Fuel burn @ 75 kts has gone from 17 L/hr to 13 L/hr. = 23.5% less! Best climb rate @ 55 kts is 100 fpm higher. Best glide @ 40-45 kts is 100 fpm better. Stalls (idle power, no flap): With slats no real stall, just a stable high-descent mush @ less than 30 kts. Without slats, no VGs* a distinct stall and roll to the left @ 34 kts. Without slats and with VGs no stall, just a stable mush @ less than 30 kts. *VGs = Vortex Generators, more about them elsewhere. L/hr x 0.26 = US Gal/hr. Kts x 1.15 = mph. This testing was done in a Savannah aircraft, a kitplane from I.C.P. in Italy, www.icp.it/avio.htm or http://www.skykits.com/ . Its pretty much a clone of a Zenair CH701, same wing profile but a longer wing, and a different tail section. Powered by a 100hp 912ULS, 4-blade Brolga prop pitched for climb (16 blocks), carrying pilot (73kg) and 30 litres fuel. ore interesting reading from www.stolspeed.com Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77566#77566 ________________________________________________________________________________
Date: Nov 28, 2006
From: Monty Graves <mgraves(at)usmo.com>
Subject: Re: RE: PROP CHOICES
Don't forget about Culver props. www.culverprops.com ________________________________________________________________________________
From: "Clive Richards" <s.c.richards(at)homecall.co.uk>
Subject: Crack in 601HD firewall stiffner 6F8-2
Date: Nov 28, 2006
Hi list we have found a crack in the firewall stiffner near the port engine mount and have had to replace the stiffner We beleave this may be because we are using a Continental 0-200 & a header tank so are on a fairley forward C of G. Have any of you with this combination had any problems ? We have difficulty in Just lowering the nose on landing, it tends to want to drop when you remove the power. It is possably caused because to much we trimmed off the stiffner to fit the original faulty engine mount. We found this when changing the nose wheel bungey which was fraid at the bottom tube and started to shed rubber. We have done a lot of tuch & goes try to perfect our landings Clive Richards GCBDG 52 Hrs Estimated 250 T&G / Landings ________________________________________________________________________________
Date: Nov 28, 2006
Subject: 701 slats again
From: rhartwig11(at)juno.com
This discussion contains a lot of speculation on what would happen if you removed the slats or covered the slot between slats and wings, etc. Some of it is not very well thought out as to what happens to the CG range. I would suggest trying to learn from those who have removed the slats and are flying their 701's in that configuration (and I suppose the experience with modified Savannahs should also be considered.) I would hope that anyone making this modification would use the data from those who have been successful and would then proceed with extreme caution. I understand that the CG range on the 701 is approximately 30-39 % of the airfoil measured from the front of the slat--I have not checked that out myself. Unslatted wings are usually approximately 20 to 28% (Forgive me if these numbers are off of few % + or -.) What is the CG range of the 701 airfoil if you measure from the leading edge of the wing instead of the slat? Is a slat aerodynamically part of the airfoil when calculating CG range? I don't know, but you can bet I am going to find out. Also keep in mind the effect of removing the weight of the slats even though they are light and have a small moment arm. Think it out. Research it. Learn from others who've "dunit." Proceed with caution. Rich Hartwig, 701 kit Waunakee, WI rhartwig11(at)juno.com ________________________________________________________________________________
From: "Jim Hoak" <planejim(at)bellsouth.net>
Date: Nov 28, 2006
Subject: Re: Crack in 601HD firewall stiffner 6F8-2
Clive, If I remember correctly, Art Mitchell had this problem with early 601HDs used for training. ( Lots of landings). I think he was using Rotax engines though. The fix was a "L" stiffner riveted on to each end of 6F8-2 along the diaginal edges. I heard of this and added the stiffners before ever flying my HD. (1996) I now have 745 landings and 536 hours. Even with the Rotax 912UL I find that I need to keep much UP elevator just at touch-down to keep the nose wheel from dropping down fairly hard. I have found that the slower you get the airplane just before the mains touch, the less tendency to bang the nose down. In other words, slow it down on landing. I keep reminding myself and now make very consistant and SOFT landings. Jim Hoak 912UL - 536 hrs - 745 landings ----- Original Message ----- From: Clive Richards To: zenith-list(at)matronics.com Sent: Tuesday, November 28, 2006 6:26 AM Subject: [Norton AntiSpam] Zenith-List: Crack in 601HD firewall stiffner 6F8-2 Hi list we have found a crack in the firewall stiffner near the port engine mount and have had to replace the stiffner We beleave this may be because we are using a Continental 0-200 & a header tank so are on a fairley forward C of G. Have any of you with this combination had any problems ? We have difficulty in Just lowering the nose on landing, it tends to want to drop when you remove the power. It is possably caused because to much we trimmed off the stiffner to fit the original faulty engine mount. We found this when changing the nose wheel bungey which was fraid at the bottom tube and started to shed rubber. We have done a lot of tuch & goes try to perfect our landings Clive Richards GCBDG 52 Hrs Estimated 250 T&G / Landings ________________________________________________________________________________
From: "Robert N. Eli" <robert.eli(at)adelphia.net>
Subject: Re: 701 slats again
Date: Nov 28, 2006
Rich, I completely agree with your recommendations. Just removing the 701 slat, with no modifications, produces a "snub-nosed" airfoil, that is unlike any standard airfoil, and would seem to create all sorts of potentially dangerous issues. If the slot is covered, and the original NACA airfoil is recovered, then there will be CG range issues that should be carefully researched before risking the change. I think the information to answer the latter questions are out there somewhere. I know that extensive research has been conducted in the past comparing airfoils with and without slats. Bob Eli N701K ----- Original Message ----- From: <rhartwig11(at)juno.com> Sent: Tuesday, November 28, 2006 7:56 AM Subject: Zenith-List: 701 slats again > > This discussion contains a lot of speculation on what would happen if you > removed the slats or covered the slot between slats and wings, etc. Some > of it is not very well thought out as to what happens to the CG range. I > would suggest trying to learn from those who have removed the slats and > are flying their 701's in that configuration (and I suppose the > experience with modified Savannahs should also be considered.) I would > hope that anyone making this modification would use the data from those > who have been successful and would then proceed with extreme caution. I > understand that the CG range on the 701 is approximately 30-39 % of the > airfoil measured from the front of the slat--I have not checked that out > myself. Unslatted wings are usually approximately 20 to 28% (Forgive me > if these numbers are off of few % + or -.) What is the CG range of the > 701 airfoil if you measure from the leading edge of the wing instead of > the slat? Is a slat aerodynamically part of the airfoil when calculating > CG range? I don't know, but you can bet I am going to find out. Also > keep in mind the effect of removing the weight of the slats even though > they are light and have a small moment arm. Think it out. Research it. > Learn from others who've "dunit." Proceed with caution. > Rich Hartwig, 701 kit > Waunakee, WI > rhartwig11(at)juno.com > > > ________________________________________________________________________________
Date: Nov 28, 2006
From: john butterfield <jdbutterfield(at)yahoo.com>
Subject: getting bumped on the digest
Hi list for the past several months, i have been getting bumped off the digest about once or twice a week. when it happens now, i usually find it in my bulk mail folder. i move it and it works for awhile then gets bumped. not much effort to move according to the value of the list. next time it happens to you, check your bulk mail folder john butterfield 601XL, corvair torrance, ca ________________________________________________________________________________
Subject: Re: Crack in 601HD firewall stiffner 6F8-2
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Nov 28, 2006
Any way we can get a photo of the crack? I'd like to make sure I know exactly where it is developing. [quote="s.c.richards(at)homecall."]Hi list we have found a crack in the firewall stiffner near the port engine mount and have had to replace the stiffner We beleave this may be because we are using a Continental 0-200 & a header tank so are on a fairley forward C of G. Have any of you with this combination had any problems ? We have difficulty in Just lowering the nose on landing, it tends to want to drop when you remove the power. It is possably caused because to much we trimmed off the stiffner to fit the original faulty engine mount. We found this when changing the nose wheel bungey which was fraid at the bottom tube and started to shed rubber. We have done a lot of tuch & goes try to perfect our landings Clive Richards GCBDG 52 Hrs Estimated 250 T&G / Landings > [b] -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77620#77620 ________________________________________________________________________________
From: Phil Maxson <pmaxpmax(at)HOTMAIL.COM>
Subject: 601XL - Engine out / Glide Experience
Date: Nov 28, 2006
Here is some very practical information about how I make landings. So far I've got about 120 hours on my plane, and I don't know how many landings. I would say maybe 80 - 100. When I fly a standard landing pattern (i.e. same as a Cessna 152/172) I use about 75% power on the downwind leg. I leave that amount of power in unti l I get to the corner, that is, until I turn base. At that point I'm still 1000 feet AGL, and I pull the power back to almost idle. I glide in from there with minor changes to power. If I'm low, I add power, if I'm high I use more flaps, or even add a side slip. So to answer your original question, the glide performance isn't as good as a 172, but it's not that different. Best glide speed is about 85 mph in m y plane.Phil Maxson601XL/CorvairNorthwest New Jersey Date: Mon, 27 Nov 2006 15:53:59 -0800From: mmesa005(at)yahoo.comSubject: Zenit h-List: 601XL - Engine out / Glide ExperienceTo: zenith-list-digest@matroni cs.com Hello All, I am planning to build a 601XL in the near future and have been reading the recent threads about the unfortunate loss of a 601XL and pilot. I don't know what happened and don't want to speculate about what happened, etc. I would like to know if anyone has experience with simulated engine o ut landings and would share those experiences with the group? I would also appreciate any experiences with how the 601XL glides during simulated engin e out practice and any comparisons to other aircraft, i.e. Cessna 172, etc. Thanks in advance, Steven _________________________________________________________________ ________________________________________________________________________________
From: "Craig Payne" <craig(at)craigandjean.com>
Subject: 601XL - Engine out / Glide Experience
Date: Nov 28, 2006
Phil - how do you set the flaps during the various phases of landing? -- Craig ________________________________________________________________________________
Date: Nov 28, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: 701 slats again
you will not gain as mouch speed if you do not elliminate the negative lift foil horizontal stab. That is what the savana did. hence the higher speed. -----Original Message----- >From: secatur <appraise1(at)bigpond.com> >Sent: Nov 28, 2006 4:18 AM >To: zenith-list(at)matronics.com >Subject: Zenith-List: Re: 701 slats again > > >More interesting reading > > >The vast reduction in drag allows all these aircraft to fly considerably faster for the same power, climb better, glide better, and with the benefit of Vortex Generators, lift-off and touch-down just as short as with slats, but with more control. > >In summary for my Savannah: > >Fast cruise @ 5200 rpm has gone from 79 kt to 85 kt. = + 6 kts >Top speed has gone from 94 kts to 103 kts! = + 9 kts. >Fuel burn @ 75 kts has gone from 17 L/hr to 13 L/hr. = 23.5% less! >Best climb rate @ 55 kts is 100 fpm higher. >Best glide @ 40-45 kts is 100 fpm better. > >Stalls (idle power, no flap): >With slats no real stall, just a stable high-descent mush @ less than 30 kts. >Without slats, no VGs* a distinct stall and roll to the left @ 34 kts. >Without slats and with VGs no stall, just a stable mush @ less than 30 kts. > >*VGs = Vortex Generators, more about them elsewhere. >L/hr x 0.26 = US Gal/hr. >Kts x 1.15 = mph. > >This testing was done in a Savannah aircraft, a kitplane from I.C.P. in Italy, www.icp.it/avio.htm or http://www.skykits.com/ . Its pretty much a clone of a Zenair CH701, same wing profile but a longer wing, and a different tail section. Powered by a 100hp 912ULS, 4-blade Brolga prop pitched for climb (16 blocks), carrying pilot (73kg) and 30 litres fuel. >ore interesting reading from www.stolspeed.com > > >Read this topic online here: > >http://forums.matronics.com/viewtopic.php?p=77566#77566 > > ________________________________________________________________________________
From: NYTerminat(at)aol.com
Date: Nov 28, 2006
Subject: Re: Enough!!!
By all means leave the gate open!!!! 63 degrees today, sunny and smooth flying. Upstate New York N701ZX CH701/912S In a message dated 11/28/2006 5:45:59 P.M. Eastern Standard Time, zsmith3rd(at)earthlink.net writes: --> Zenith-List message posted by: Zed Smith Will you guys in the northern latitudes just cut it out?? North Texas has enjoyed mild temps in the mid 70's for two or three months.....now we are told that somebody north of Oklahoma has left a gate open. It is 73 F as I type this plea for sanity.....close those gates, fellows! The prediction is for 25 F Friday morning, and the "S-word" has been mentioned. We may have to resort to wearing sleeves as we pull rivets and use the dreaded Green ScotchBrite pads. Have mercy...... Regards to all who are snowbound, Zed do not archive!!! ________________________________________________________________________________
From: "Gary Boothe" <gboothe(at)calply.com>
Subject: Enough!!!
Date: Nov 28, 2006
Yeah, global warming..oops, sorry, no polytiks.I withdraw my comment.. _____ From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com] On Behalf Of John Marzulli Sent: Tuesday, November 28, 2006 3:39 PM Subject: Re: Zenith-List: Enough!!! What ever they did in OK, it hit us here in Seattle. We haven't seen temperatures this low in years! We got more snow in the last two days then in the previous three years combined! On 11/28/06, Zed Smith wrote: Will you guys in the northern latitudes just cut it out?? North Texas has enjoyed mild temps in the mid 70's for two or three months.....now we are told that somebody north of Oklahoma has left a gate open. It is 73 F as I type this plea for sanity.....close those gates, fellows! The prediction is for 25 F Friday morning, and the "S-word" has been mentioned. We may have to resort to wearing sleeves as we pull rivets and use the dreaded Green ScotchBrite pads. -- John Marzulli http://701Builder.blogspot.com/ "Flying a plane is no different than riding a bicycle... it's just a lot harder to put baseball cards in the spokes. ________________________________________________________________________________
Date: Nov 28, 2006
From: Dennis Wieck <dwieck(at)bellsouth.net>
Subject: Re: 701 slats again
He said remove the SLOT not the SLAT > Carl, > > I talked to Chris Heintz at Air Venture several years ago about the 701 > airfoil, and the aerodynamic design of the slats. The airfoil is an old > standard airfoil (it is a NACA 640-18) with just a slot added. In other > words, if you simply remove the slot and leave the fixed slat in its design > postion to define the nose of the airfoil, then you have standard NACA > 640-18 airfoil. If one wants to remove the slat from the airfoil design, the > original airfoil can be recovered by simply covering the slots with sheet > metal that matches the airfoil contour. > > Bob Eli ________________________________________________________________________________
From: Trevor Page <webmaster(at)upac.ca>
Subject: CZAW cowl question
Date: Nov 28, 2006
________________________________________________________________________________
From: "Jim Fosse" <jfosse1(at)shawneelink.net>
Subject: 701 Slats Again
Date: Nov 28, 2006
For an interesting and informative commentary on 701 and Savannah slats, or the lack thereof, go to: www.stolspeed.com. Jim Fosse ________________________________________________________________________________
From: "John Bolding" <jnbolding1(at)teleshare.net>
Subject: Re: Enough!!!
Date: Nov 28, 2006
Hey Ron, I know where Rotan is , I was BORN there, not much in the area then except cotton fields,dust,rattlesnakes and oil wells. LOW&SLOW John ----- Original Message ----- From: ron wehba To: zenith-list(at)matronics.com Sent: Tuesday, November 28, 2006 9:31 PM Subject: Re: Zenith-List: Enough!!! hi zed, ron here in rotan, north west of abilene, we are gittin' out a da way of it , going to canton for the next few days. wind might not even be blowing there,, stay warm ----- Original Message ----- From: "Zed Smith" <zsmith3rd(at)earthlink.net> To: Sent: Tuesday, November 28, 2006 4:21 PM Subject: Zenith-List: Enough!!! ________________________________________________________________________________
Subject: Re: 701 slats again
From: "secatur" <appraise1(at)bigpond.com>
Date: Nov 28, 2006
READ previous post, or go to www.stolspeed.com Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77746#77746 ________________________________________________________________________________
From: "Hans" <harina(at)bigpond.net.au>
Subject: RE: 701 slats again
Date: Nov 29, 2006
I've been flying my 701 for 475 hrs total,175 hrs without slats, so I think maybe I should comment on this thread. I was the first 701 flyer in Australia to remove the slats ,after seeing the results that the savannahs got. See www.stolspeed.com. I must say that I like it much better without the slats and will never change back!! Since then two other 701's at our airfield have removed their slats,and I have flown their aircraft-same result. To answer some of those specific dire predictions: >my take is that the C of G and the centre of pressure would move back,the Cp more so causing a nose heavy pitch moment at all speeds and angles of attack< Not so in real life..... before I took the slats off I did a test flight and set the trim to neutral cruise. About one hour later I did another test flight with the slats off, same conditions,same load. no change at all in cruise trim! Take-off,climb,decent,and landing,all felt balanced and correct... >I would expect all stall speeds to increase with the clean wing< With the clean wing,yes of course the stall speed increased and became more abrupt,but with the VG's it came back very much like with slats,and angle of attack much the same as with slats. >and top speed to probably remain the same or decrease because of the blunt leading edge< Not so- top speed and cruise speed definitely increased without the slats and fuel consumption really decreased for the same cruise speed.15%.The blunt leading edge doesn't seem to effect the speed in this speed range.You would think so,but the Savannah with that same blunt profile as the 701 goes pretty much the same speed as the new "finer" leading edge that the Savannah put on their new "VG" model . >adding VG"s should delay the stall but should also increase drag?< No they do not increase drag-see the Updates page in www.stolspeed.com. >if one wants to remove the slats from the airfoil design, the original airfoil can be recovered by simply covering the slots with sheet metal that matches the airfoil contour Be careful about that one! See the slats vs. VG's page, C of G section, in www.stolspeed.com. When original built with slats, 95 litre wing tanks,and 912 S,my loaded Cof G calculated at 477 mm aft of the slat leading edge,1433 mm cord = 33% m.a.c This number would seem quite far aft by conventional practice,but it sure didn't fly as if it had a aft C of G .removing the slats moved the leading edge aft 160 mm , so the same C of G position was now located 317 mm from the new leading edge, with the cord now 1270 mm = 25% m.a.c. , which is right in the range recommended for any conventional wing. I recently did a new weight and balance on very good scales- without slats =26%m.a.c, loaded up for travel- full fuel ( wing tanks),20 kg baggage , 40 litres of fuel in pax seat - 503 kg ( 1107 lbs).It flies just perfect like this. Well I have tried no slats and I wouldn't go back, no way! And it's not as if I am easily influenced by other people's claims- I'm a sceptical, independent-minded Dutchman,ex-Royal Dutch Air Force. I fly my plane hard,and practice STOL landings all the time,so I have a really good feel for it at all speeds. Always doing glide approach and idle power landings-That is the real test of a well balanced aircraft. Hans van Santen ________________________________________________________________________________
From: "Dave Ruddiman" <pacificpainting(at)comcast.net>
Subject: 801 Tire Clearance
Date: Nov 29, 2006
801 People, I haven't started my fuselage yet so I don't know the answer to this question. What is the clearance between the wheels and the gear legs? Both the mains and the nose. I assume 8.50 tires will fit, but I am curious if anything larger will. If anyone knows, I would appreciate knowing too. Dave in Salem - snow melted, getting cold ________________________________________________________________________________
Date: Nov 29, 2006
From: Matt Dralle <dralle(at)matronics.com>
Subject: Just A Few Days Left; Trailing Last Year...
Dear Listers, There are just a few more days left of this year's List Fund Raiser! Response has been very good, but we are behind last year in the number of people that have made a Contribution and as a percentage of the total number of subscribers. Please remember that there isn't any sort of commercial advertising on the Lists and the *only* means of keeping these Lists running is through your Contributions during this Fund Raiser. Please make a Contribution today! http://www.matronics.com/contribution Thank you! Matt Dralle Matronics Email List Administrator ________________________________________________________________________________
Subject: Re: Enough!!!
From: "secatur" <appraise1(at)bigpond.com>
Date: Nov 29, 2006
Hey...what about us poor slobs in Australia...some of us ain't seen rain for 5 YEARS! I think we'd all jump at the chance to get a couple feet of snow and a bit of relief fro 38 degrees! lol Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77814#77814 ________________________________________________________________________________
Subject: Re: Who is "Matt Dralle" & What Are "The Lists"? [Please
Read]
From: "secatur" <appraise1(at)bigpond.com>
Date: Nov 29, 2006
Hey Matt, not to put too fine a point on it , (and I'm sure it's totally great) but when soliciting donations it is customary to include annual financials. Yes? Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77815#77815 ________________________________________________________________________________
From: Trevor Page <webmaster(at)upac.ca>
Subject: CZAW cowl question again
Date: Nov 29, 2006
(Looks like my first post got stripped) Just wondering if anyone on the list has any input on something: I'm just completed the conversion of my 601HD to the CZAW cowl and rad placement. It was very easy and it's a very nice kit. I reckon I got an extra 5Mph out of the plane because of the cleaner profile (I've flown it for 1 hour so far) However, I still seem to have higher oil temps. I have an 80HP 912 and I sprung for the larger oil cooler which I've installed as directed in front of the muffler can. Now, the oil cooler inlet duct in the cowl is rather small: I see a 3/4" opening at the end of the NACA duct. Has anyone with a recent R912 install on an HD or XL with the same oil cooler placement have the same issue with a small opening? There seems to be a real lack of pictures of the install to compare mine against so maybe someone can chime in? My oil temps reach 260F which seems a bit higher than most but I do know that my older engine has an oil temp probe located on the bottom front oil outlet fitting rather than the newer location at the oil pump housing. I reckon my temps are going to be higher since the oil temps are read after the oil has gone through the engine just before going into the tank. How much higher? I have no idea but does 30F seems reasonable? More? Right now I'm waiting to hear back from anyone before I go and do something drastic like make the opening bigger cutting the roof of the NACA duct forward or make up some kind of ducting work to come closer the oil cooler and seal it up somehow. Thanks in advance! Trev Page C-IDUS 601HD R912 I've included a picture of the cowl so you can see what I'm talking about on the forum ________________________________________________________________________________
From: "Doug Moellering" <dfmoeller(at)austin.rr.com>
Subject: Making a Vixen File Tool
Date: Nov 29, 2006
OK, here's an easy one for those who have made hand held (wooden handle) deburring tools out of half-length vixen files, as depicted in the video on scratchbuilding released by HomebuiltHelp.com. How on earth would one drill screw holes through the hardened tool steel of the file????? I've broken more than a few bits, and yet to scratch the surface! I'm guessing that heat must be applied to the file to undo the tempering, but doesn't that ruin the file? Anybody that has been there; done that, would be more than welcome to give me a tip or two. Doug ________________________________________________________________________________
Date: Nov 29, 2006
From: "Carlos Sa" <carlossa52(at)gmail.com>
Subject: Re: Making a Vixen File Tool
Doug, if you are thinking of deburring holes, consider fine sand paper. I have used it with very good results. Carlos CH601-HD, plans On 29/11/06, Doug Moellering wrote: > > dfmoeller(at)austin.rr.com> > > OK, here's an easy one for those who have made hand held (wooden handle) > deburring tools out of half-length vixen files, as depicted in the video > on > scratchbuilding released by HomebuiltHelp.com. > > How on earth would one drill screw holes through the hardened tool steel > of > the file????? I've broken more than a few bits, and yet to scratch the > surface! I'm guessing that heat must be applied to the file to undo the > tempering, but doesn't that ruin the file? > > Anybody that has been there; done that, would be more than welcome to give > me a tip or two. > > Doug > > ________________________________________________________________________________
From: "R.P." <zodie(at)adelphia.net>
Subject: Re: Making a Vixen File Tool
Date: Nov 29, 2006
----- Original Message ----- From: "Doug Moellering" <dfmoeller(at)austin.rr.com> Sent: Wednesday, November 29, 2006 5:22 AM Subject: Zenith-List: Making a Vixen File Tool > > > OK, here's an easy one for those who have made hand held (wooden handle) > deburring tools out of half-length vixen files, as depicted in the video > on scratchbuilding released by HomebuiltHelp.com. > > How on earth would one drill screw holes through the hardened tool steel > of the file????? I've broken more than a few bits, and yet to scratch the > surface! I'm guessing that heat must be applied to the file to undo the > tempering, but doesn't that ruin the file? > > Anybody that has been there; done that, would be more than welcome to give > me a tip or two. > > Doug The vixen file deburring tools that I have used were epoxied to the wooden block. Don't screw it, glue it. Rick Pitcher ________________________________________________________________________________
Subject: Re: Making a Vixen File Tool
Date: Nov 29, 2006
From: "John Hines" <John.Hines(at)craftontull.com>
At the bank and stuff. John R. Hines IT Manager Crafton, Tull & Associates, Inc. 901 N. 47th Street, Suite 200 Rogers, AR 72756 Office: 479-878-2449 Mobile: 479-366-4783 Fax: 479-631-6224 John.Hines(at)craftontull.com www.craftontull.com Crafton, Tull & Associates, Inc. exists to anticipate and understand the needs of our clients and provide them with successful solutions. -----Original Message----- From: owner-zenith-list-server(at)matronics.com Sent: Wed Nov 29 07:22:48 2006 Subject: Zenith-List: Making a Vixen File Tool OK, here's an easy one for those who have made hand held (wooden handle) deburring tools out of half-length vixen files, as depicted in the video on scratchbuilding released by HomebuiltHelp.com. How on earth would one drill screw holes through the hardened tool steel of the file????? I've broken more than a few bits, and yet to scratch the surface! I'm guessing that heat must be applied to the file to undo the tempering, but doesn't that ruin the file? Anybody that has been there; done that, would be more than welcome to give me a tip or two. Doug This email and any files transmitted with it are confidential and intended solely for the use of the individual or entity to whom they are addressed. If you have received this email in error please notify the system manager. This message contains confidential information and is intended only for the individual named. If you are not the named addressee you should not disseminate, distribute or copy this e-mail. Please notify the sender immediately by e-mail if you have received this e-mail by mistake and delete this e-mail from your system. If you are not the intended recipient you are notified that disclosing, copying, distributing or taking any action in reliance on the contents of this information is strictly prohibited. Re: Zenith-List: Making a Vixen File Tool

At the bank and stuff.





John R. Hines
IT Manager
John.Hines(at)craftontull.com

Office: 479-878-2449
Mobile: 479-366-4783
Fax: 479-631-6224
www.craftontull.com
901 N. 47th Street, Suite 200 ·Rogers, AR 72756
http://www.craftontull.com/images/emailsignature_block1.gif" border=0>
Crafton, Tull & Associates, Inc. exists to anticipate and understand the needs of our clients and provide them with successful solutions.
----- Original Message-----
From: owner-zenith-list-server(at)matronics.com <owner-zenith-list-server(at)matronics.com>
Sent: Wed Nov 29 07:22:48 2006
Subject: Zenith-List: Making a Vixen File Tool

--> Zenith-List message posted by: "Doug Moellering" <dfmoeller(at)austin.rr.com>

OK, here's an easy one for those who have made hand held (wooden handle)
deburring tools out of half-length vixen files, as depicted in the video on
scratchbuilding released by HomebuiltHelp.com.

How on earth would one drill screw holes through the hardened tool steel of
the file?????  I've broken more than a few bits, and yet to scratch the
surface!  I'm guessing that heat must be applied to the file to undo the
tempering, but doesn't that ruin the file?

Anybody that has been there; done that, would be more than welcome to give
me a tip or two.

Doug


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This email and any files transmitted with it are confidential and intended solely for the use of the individual or entity to whom they are addressed. If you have received this email in error please notify the system manager. This message contains confidential information and is intended only for the individual named. If you are not the named addressee you should not disseminate, distribute or copy this e-mail. Please notify the sender immediately by e-mail if you have received this e-mail by mistake and delete this e-mail from your system. If you are not the intended recipient you are notified that disclosing, copying, distributing or taking any action in reliance on the contents of this information is strictly prohibited.

      
      
      
________________________________________________________________________________
Subject: Re: Making a Vixen File Tool
Date: Nov 29, 2006
From: "John Hines" <John.Hines(at)craftontull.com>
Oops! Sorry guys, I responded to the wrong email. Sorry. John R. Hines IT Manager Crafton, Tull & Associates, Inc. 901 N. 47th Street, Suite 200 Rogers, AR 72756 Office: 479-878-2449 Mobile: 479-366-4783 Fax: 479-631-6224 John.Hines(at)craftontull.com www.craftontull.com Crafton, Tull & Associates, Inc. exists to anticipate and understand the needs of our clients and provide them with successful solutions. -----Original Message----- From: owner-zenith-list-server(at)matronics.com Sent: Wed Nov 29 08:21:22 2006 Subject: Re: Zenith-List: Making a Vixen File Tool At the bank and stuff. John R. Hines IT Manager John.Hines(at)craftontull.com Office: 479-878-2449 Mobile: 479-366-4783 Fax: 479-631-6224 www.craftontull.com <http://www.craftontull.com/> 901 N. 47th Street, Suite 200 =C2=B7Rogers, AR 72756 <http://www.craftontull.com/> Crafton, Tull & Associates, Inc. exists to anticipate and understand the needs of our clients and provide them with successful solutions. -----Original Message----- From: owner-zenith-list-server(at)matronics.com Sent: Wed Nov 29 07:22:48 2006 Subject: Zenith-List: Making a Vixen File Tool OK, here's an easy one for those who have made hand held (wooden handle) deburring tools out of half-length vixen files, as depicted in the video on scratchbuilding released by HomebuiltHelp.com. How on earth would one drill screw holes through the hardened tool steel of the file????? I've broken more than a few bits, and yet to scratch the surface! I'm guessing that heat must be applied to the file to undo the tempering, but doesn't that ruin the file? Anybody that has been there; done that, would be more than welcome to give me a tip or two. Doug This Month -- Get Some AWESOME FREE Gifts!) on www.buildersbooks.com HREF="http://www.matronics.com/contribution">http://www.matronics.com/c ontribution bsp; -Matt Dralle, List Admin. Zenith-List Email Forum - HREF="http://www.matronics.com/Navigator?Zenith-List">http://www.matron ics.com/Navigator?Zenith-List This email and any files transmitted with it are confidential and intended solely for the use of the individual or entity to whom they are addressed. If you have received this email in error please notify the system manager. This message contains confidential information and is intended only for the individual named. If you are not the named addressee you should not disseminate, distribute or copy this e-mail. Please notify the sender immediately by e-mail if you have received this e-mail by mistake and delete this e-mail from your system. If you are not the intended recipient you are notified that disclosing, copying, distributing or taking any action in reliance on the contents of this information is strictly prohibited. This email and any files transmitted with it are confidential and intended solely for the use of the individual or entity to whom they are addressed. If you have received this email in error please notify the system manager. This message contains confidential information and is intended only for the individual named. If you are not the named addressee you should not disseminate, distribute or copy this e-mail. Please notify the sender immediately by e-mail if you have received this e-mail by mistake and delete this e-mail from your system. If you are not the intended recipient you are notified that disclosing, copying, distributing or taking any action in reliance on the contents of this information is strictly prohibited. Re: Zenith-List: Making a Vixen File Tool

Oops!  Sorry guys, I responded to the wrong email.  Sorry.





John R. Hines
IT Manager
John.Hines(at)craftontull.com

Office: 479-878-2449
Mobile: 479-366-4783
Fax: 479-631-6224
www.craftontull.com
901 N. 47th Street, Suite 200 ·Rogers, AR 72756
http://www.craftontull.com/images/emailsignature_block1.gif" border=0>
Crafton, Tull & Associates, Inc. exists to anticipate and understand the needs of our clients and provide them with successful solutions.
----- Original Message-----
From: owner-zenith-list-server(at)matronics.com <owner-zenith-list-server(at)matronics.com>
Sent: Wed Nov 29 08:21:22 2006
Subject: Re: Zenith-List: Making a Vixen File Tool

At the bank and stuff.






John R. Hines  
IT Manager     
John.Hines(at)craftontull.com     
       

Office: 479-878-2449
Mobile: 479-366-4783
Fax: 479-631-6224      
       
www.craftontull.com <http://www.craftontull.com/>      
901 N. 47th Street, Suite 200 ·Rogers, AR 72756
 <http://www.craftontull.com/>& nbsp;
Crafton, Tull & Associates, Inc. exists to anticipate and understand the needs of our clients and provide them with successful solutions.      
-----Original Message-----
From: owner-zenith-list-server(at)matronics.com <owner-zenith-list-server(at)matronics.com>
Sent: Wed Nov 29 07:22:48 2006
Subject: Zenith-List: Making a Vixen File Tool

--> Zenith-List message posted by: "Doug Moellering" <dfmoeller(at)austin.rr.com>

OK, here's an easy one for those who have made hand held (wooden handle)
deburring tools out of half-length vixen files, as depicted in the video on
scratchbuilding released by HomebuiltHelp.com.

How on earth would one drill screw holes through the hardened tool steel of
the file?????  I've broken more than a few bits, and yet to scratch the
surface!  I'm guessing that heat must be applied to the file to undo the
tempering, but doesn't that ruin the file?

Anybody that has been there; done that, would be more than welcome to give
me a tip or two.

Doug


===========
This Month --
Get Some AWESOME FREE Gifts!)
on
www.buildersbooks.com
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===========
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HREF="http://www.matron ics.com/Navigator?Zenith-List">http://www.matron ics.com/Navigator?Zenith-List
===========







This email and any files transmitted with it are confidential and intended solely for the use of the individual or entity to whom they are addressed. If you have received this email in error please notify the system manager. This message contains confidential information and is intended only for the individual named. If you are not the named addressee you should not disseminate, distribute or copy this e-mail. Please notify the sender immediately by e-mail if you have received this e-mail by mistake and delete this e-mail from your system. If you are not the intended recipient you are notified that disclosing, copying, distributing or taking any action in reliance on the contents of this information is strictly prohibited.


===========
This Month --
Get Some AWESOME FREE Gifts!)
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This email and any files transmitted with it are confidential and intended solely for the use of the individual or entity to whom they are addressed. If you have received this email in error please notify the system manager. This message contains confidential information and is intended only for the individual named. If you are not the named addressee you should not disseminate, distribute or copy this e-mail. Please notify the sender immediately by e-mail if you have received this e-mail by mistake and delete this e-mail from your system. If you are not the intended recipient you are notified that disclosing, copying, distributing or taking any action in reliance on the contents of this information is strictly prohibited.

      
      
      
________________________________________________________________________________
Subject: Re: Making a Vixen File Tool
From: "Chris Lewis" <christopherlewis(at)earthlink.net>
Date: Nov 29, 2006
No drilling required! Skip the drilling and just bond the file to the wooden handle with some JB Weld-type epoxy (make sure the file is clean!). Drill a couple of shallow holes up into your wooden handle to help prevent shearing of the top side of the joint. Don't forget to chmfer the edges to prevent digging in if you get off level. Enjoy. Chris in Seattle -------- 701 Scratch Builder Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77835#77835 ________________________________________________________________________________
From: "Joe Kerr" <kerrjf(at)charter.net>
Subject: Zenith 601XL Plans for sale
Date: Nov 29, 2006
Unused 601XL plans are now for sale on Ebay, Item # 250055386707. ________________________________________________________________________________
From: JAPhillipsGA(at)aol.com
Date: Nov 29, 2006
Subject: Buying a Partial Built Kit
Dear Thread Friends, I'm looking to buy a kit that the original owner has finished most of the tail and part of a wing. A couple questions arise. What documentation for sale to satisfy the FAA for certification is required? When I bought my XL kit directly from ZAC I received a sales certificate that I had to include a copy of to the FAA for certification. Who out there has bought a started kit and successfully got it through FAA ? Second question is what amount of work can be accomplished by the first builder that will still allow me to be granted a repairman's certificate when I get her flying? That is the "tall pole" in the tent because I would not own a plane I can't work on. Hope to hear soon from some of you smart fellows. Best regards, Bill of Georgia N505WP 601XL-3300 96 hours ________________________________________________________________________________
From: "Zodie Rocket" <zodierocket(at)hsfx.ca>
Subject: Making a Vixen File Tool
Date: Nov 29, 2006
Doug, please go with the Epoxy method. Bonding the Vixen file is a lot better then the screw method. Don't forget to knock off the edges. Mark Townsend Can-Zac Aviation Ltd. president@can-zacaviation.com www.can-zacaviation.com -----Original Message----- From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com] On Behalf Of Doug Moellering Sent: Wednesday, November 29, 2006 8:23 AM Subject: Zenith-List: Making a Vixen File Tool OK, here's an easy one for those who have made hand held (wooden handle) deburring tools out of half-length vixen files, as depicted in the video on scratchbuilding released by HomebuiltHelp.com. How on earth would one drill screw holes through the hardened tool steel of the file????? I've broken more than a few bits, and yet to scratch the surface! I'm guessing that heat must be applied to the file to undo the tempering, but doesn't that ruin the file? Anybody that has been there; done that, would be more than welcome to give me a tip or two. Doug -- 11/29/2006 -- 11/29/2006 ________________________________________________________________________________
Date: Nov 29, 2006
From: "Michael Valentine" <mgvalentine(at)gmail.com>
Subject: Re: Making a Vixen File Tool
Sorry to ask the obvious, but how does one cut the file in the first place??? Michael in NH ________________________________________________________________________________
Subject: Re: Making a Vixen File Tool
From: "Chris Lewis" <christopherlewis(at)earthlink.net>
Date: Nov 29, 2006
Cutting Vixen File You could just use a cut-off wheel to score both sides part-way through and then place the file in a vise and whack it with a deadblow hammer. It should snap right off. Grind to suit your curved end shapes and then chamfer the sharp edges to prevent gouging Chris in Seattle -------- 701 Scratch Builder Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77914#77914 ________________________________________________________________________________
Date: Nov 29, 2006
From: ALAN BEYER <agbeyer(at)sbcglobal.net>
Subject: Re: Buying a Partial Built Kit
A friend of mine just finished and is now flying a Zodiac HD. He got the k it from a guy that had the wings and tail stuff already done. He had no tr ouble with the FAA. I am not sure what steps he took to register the plane . The best guy to talk to is Joe Norris of the EAA. He is in Aviation Ser vices and is a DAR. He did the inspection on my HDS. As far as working on your plane the FAA told me that a trained monkey, or your wife can work on the plane, but you need the Repairmans Cert. to inspect it.=0A=0AAl from O shkosh=0AHDS-3300 (N645AB)=0A275 Hrs.=0A=0A=0A=0A----- Original Message --- -=0AFrom: "JAPhillipsGA(at)aol.com" <JAPhillipsGA(at)aol.com>=0ATo: zenith-list@m atronics.com=0ASent: Wednesday, November 29, 2006 1:54:07 PM=0ASubject: Zen ith-List: Buying a Partial Built Kit=0A=0ADear Thread Friends, I'm looking to buy a kit that the original owner has finished most of the tail and part of a wing. A couple questions arise. What documentation for sale to satisf y the FAA for certification is required? When I bought my XL kit directly f rom ZAC I received a sales certificate that I had to include a copy of to t he FAA for certification. Who out there has bought a started kit and succes sfully got it through FAA ? Second question is what amount of work can be accomplished by the first builder that will still allow me to be granted a repairman's certificate when I get her flying? That is the "tall pole" in t he tent because I would not own a plane I can't work on. Hope to hear soon from some of you smart fellows. Best regards, Bill of Georgia=0AN505WP=0A60 =========== ________________________________________________________________________________
Subject: Cortec thickness and Loose Rivets over time...?
From: "PatrickW" <pwhoyt(at)yahoo.com>
Date: Nov 29, 2006
Thread Friends, I'm planning on applying Cortec to the mating surfaces before riveting my stabilizer together. Are there any concerns with the cortec "wearing down" over a long time and resulting in loose rivets...? Maybe after a few years of exposure to heat/moisture/vibration? Being that it's also water soluble, will moisture erode it? Thanks, - PatrickW Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77922#77922 ________________________________________________________________________________
Subject: Re: CZAW cowl question again
From: "zodieman" <webmaster(at)upac.ca>
Date: Nov 29, 2006
Here's the picture of the CZAW cowl I mentioned. Notice the oil cooler inlet on the bottom. The opening at the back is only 3/4". Since it's on an upwards angle when installed, cutting the "roof" of the inlet will make for a wider opening to allow more air in. I've also attached another picture of a red 601 with the same cowl and the lower inlet seems to be missing much of the so-called "roof". You can clearly see the oil cooler in there. Any thoughts? Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77923#77923 Attachments: http://forums.matronics.com//files/red601_676.jpg http://forums.matronics.com//files/czawcowl_205.jpg ________________________________________________________________________________
Date: Nov 29, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: Cortec thickness and Loose Rivets over time...?
if riveted correctly, the surfaces should be solid for the life of the plane, why the Cortec might I ask? Juan -----Original Message----- >From: PatrickW <pwhoyt(at)yahoo.com> >Sent: Nov 29, 2006 5:20 PM >To: zenith-list(at)matronics.com >Subject: Zenith-List: Cortec thickness and Loose Rivets over time...? > > >Thread Friends, > >I'm planning on applying Cortec to the mating surfaces before riveting my stabilizer together. > >Are there any concerns with the cortec "wearing down" over a long time and resulting in loose rivets...? > >Maybe after a few years of exposure to heat/moisture/vibration? Being that it's also water soluble, will moisture erode it? > >Thanks, > >- PatrickW > > >Read this topic online here: > >http://forums.matronics.com/viewtopic.php?p=77922#77922 > > ________________________________________________________________________________
Date: Nov 29, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: Buying a Partial Built Kit
I just am in process of registeting the plane on the famous -01 FAA paper. if amateur status, equals 40 hr fly off but repairman's certificate for annuals is literally automatic. Option two is LSA status which equals a 25 hour fly off, but would need to take 16hour repairman's license. You friend probably did what a lot of people have done, sign that it was 51% amateur built. Juan -----Original Message----- >From: ALAN BEYER <agbeyer(at)sbcglobal.net> >Sent: Nov 29, 2006 5:05 PM >To: zenith-list(at)matronics.com >Subject: Re: Zenith-List: Buying a Partial Built Kit > >A friend of mine just finished and is now flying a Zodiac HD. He got the kit from a guy that had the wings and tail stuff already done. He had no trouble with the FAA. I am not sure what steps he took to register the plane. The best guy to talk to is Joe Norris of the EAA. He is in Aviation Services and is a DAR. He did the inspection on my HDS. As far as working on your plane the FAA told me that a trained monkey, or your wife can work on the plane, but you need the Repairmans Cert. to inspect it. > >Al from Oshkosh >HDS-3300 (N645AB) >275 Hrs. > > >----- Original Message ---- >From: "JAPhillipsGA(at)aol.com" <JAPhillipsGA(at)aol.com> >To: zenith-list(at)matronics.com >Sent: Wednesday, November 29, 2006 1:54:07 PM >Subject: Zenith-List: Buying a Partial Built Kit > >Dear Thread Friends, I'm looking to buy a kit that the original owner has finished most of the tail and part of a wing. A couple questions arise. What documentation for sale to satisfy the FAA for certification is required? When I bought my XL kit directly from ZAC I received a sales certificate that I had to include a copy of to the FAA for certification. Who out there has bought a started kit and successfully got it through FAA ? Second question is what amount of work can be accomplished by the first builder that will still allow me to be granted a repairman's certificate when I get her flying? That is the "tall pole" in the tent because I would not own a plane I can't work on. Hope to hear soon from some of you smart fellows. Best regards, Bill of Georgia >N505WP >60=========== ________________________________________________________________________________
Subject: Re: Cortec thickness and Loose Rivets over time...?
From: "Ron Lendon" <rlendon(at)comcast.net>
Date: Nov 29, 2006
Don't put it on to thick. I can see through my primer. -------- Ron Lendon, Clinton Township, MI Corvair Zodiac XL, ScrapBuilder ;-) http://www.mykitlog.com/rlendon Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77939#77939 ________________________________________________________________________________
Date: Nov 29, 2006
From: Paul Mulwitz <p.mulwitz(at)worldnet.att.net>
Subject: Re: Buying a Partial Built Kit
Hi Juan, I think you could be mistaken on the 25 hour phase I test period for LSA airplanes. We had one fellow get only 5 hours for a Kitfox last year. The inspector (not DAR) felt the engine and propeller were established (not certified, though) partners and decided a 5 hour test period was appropriate. On the Experimental-AB choice the minimum is 25 hours and 40 is required if the power plant is considered a new combination or design. I believe the down side of Experimental - LSA is the requirement for the 2 day course for authority to sign off annual condition inspections. Best regards, Paul XL fuselage At 02:51 PM 11/29/2006, you wrote: >I just am in process of registeting the plane on the famous -01 FAA >paper. if amateur status, equals 40 hr fly off but >repairman's certificate for annuals is literally automatic. Option >two is LSA status which equals a 25 hour fly off, but would need to >take 16hour repairman's license. You friend probably did what a lot >of people have done, sign that it was 51% amateur built. > >Juan - ________________________________________________________________________________
From: "george may" <gfmjr_20(at)HOTMAIL.COM>
Subject: Buying a Partial Built Kit
Date: Nov 29, 2006
"documentation for sale to satisfy the FAA for certification is required" Bill-- I bought my kit from an individual. You will need the FAA Bill of Sale to be filled out by you and signed by the seller. In addition you will need to call Zenith and have them send you a Bill of sale showing the sale to the original purchaser. The government is looking for a complete chain of ownership. The last question is tougher----it depends. Typically it depends on how good you are at convincing the FAA inspector or DAR that you assembled 51% of the kit. Remember you don't really have to have assembled 51% of all of the kit parts , only items that are listed as part of the 51% effort. For example you would not have to have assembled all of the ribs, just enough to understand how to do it etc. Keep a good log and photos of your efforts I've built 2 planes under these conditions and never had any issue with the FAA. Hope that helps George May 601XL 912s 13 hours _________________________________________________________________ View Athletes Collections with Live Search http://sportmaps.live.com/index.html?source=hmemailtaglinenov06&FORM=MGAC01 ________________________________________________________________________________
Date: Nov 29, 2006
From: <zman601xl(at)verizon.net>
Subject: Re: Just A Few Days Left; Trailing Last Year...
From: Matt Dralle <dralle(at)matronics.com> Date: 2006/11/29 Wed AM 02:36:56 CST Subject: Zenith-List: Just A Few Days Left; Trailing Last Year... Dear Listers, There are just a few more days left of this year's List Fund Raiser! Response has been very good, but we are behind last year in the number of people that have made a Contribution and as a percentage of the total number of subscribers. Please remember that there isn't any sort of commercial advertising on the Lists and the *only* means of keeping these Lists running is through your Contributions during this Fund Raiser. Please make a Contribution today! http://www.matronics.com/contribution Thank you! Matt Dralle Matronics Email List Administrator Matt, I'm a little late this year,but I should have a check in the mail by Friday. Regards,Bob Haring ________________________________________________________________________________
Date: Nov 29, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: Buying a Partial Built Kit
just quoting what EAA specialists at EAA told me. 25hours LSA or 40 Amateur. Juan -----Original Message----- >From: Paul Mulwitz <p.mulwitz(at)worldnet.att.net> >Sent: Nov 29, 2006 6:36 PM >To: zenith-list(at)matronics.com >Subject: Re: Zenith-List: Buying a Partial Built Kit > > >Hi Juan, > >I think you could be mistaken on the 25 hour phase I test period for >LSA airplanes. We had one fellow get only 5 hours for a Kitfox last >year. The inspector (not DAR) felt the engine and propeller were >established (not certified, though) partners and decided a 5 hour >test period was appropriate. > >On the Experimental-AB choice the minimum is 25 hours and 40 is >required if the power plant is considered a new combination or design. > >I believe the down side of Experimental - LSA is the requirement for >the 2 day course for authority to sign off annual condition inspections. > >Best regards, > >Paul >XL fuselage > > >At 02:51 PM 11/29/2006, you wrote: > >>I just am in process of registeting the plane on the famous -01 FAA >>paper. if amateur status, equals 40 hr fly off but >>repairman's certificate for annuals is literally automatic. Option >>two is LSA status which equals a 25 hour fly off, but would need to >>take 16hour repairman's license. You friend probably did what a lot >>of people have done, sign that it was 51% amateur built. >> >>Juan > >- > > ________________________________________________________________________________
From: Gpjann(at)aol.com
Date: Nov 29, 2006
Subject: Crackes in Firewall stiffeners...
The XL has beefed-up the 601 firewall. It may give you some ideas on how to strengthen that area. GPJ ________________________________________________________________________________
From: "Dave Austin" <daveaustin2(at)can.rogers.com>
Subject: Re: Crackes in Firewall stiffeners...
Date: Nov 29, 2006
My upper firewall stiffener cracked and twisted a bit after 50 odd hours. Probably one landing where the nose wheel caught on something. I stop-drilled the crack and put angle stiffeners on the 45 degree ends underneath and 25 thou material on top to extend the load farther in. No further problems up to 585 hours. Dave Austin 601HDS - 912, Spitfire Mk VIII ________________________________________________________________________________
Subject: Re: Buying a Partial Built Kit
From: "DaveG601XL" <david.m.gallagher(at)ge.com>
Date: Nov 29, 2006
When I bought my wing kit partially assembled by somebody else, he had the forethought to give me his ZAC bill of sale. See if you can get the same. DaveG Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77977#77977 ________________________________________________________________________________
Subject: Re: Cortec thickness and Loose Rivets over time...?
From: "DaveG601XL" <david.m.gallagher(at)ge.com>
Date: Nov 29, 2006
Juan, I, like Patrick, am using Cortec initially because ZAC recommended it. Now I love it because of it's lack of fumes when applying it. But if you put it on too thick or slap it on roughly so it bubbles, there is some thickness to it that I was also concerned about. I have scraped some off in places and re-applied due to it being too thick. DaveG Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77978#77978 ________________________________________________________________________________
Subject: Re: 601XL - Engine out / Glide Experience
From: "Ron Lendon" <rlendon(at)comcast.net>
Date: Nov 29, 2006
Another thing you can practice is landings during takeoff. What I mean here is practice your soft field take offs always. it helps you get the feel of the plane just before lift / stall. This will become habit if you do them all the time. -------- Ron Lendon, Clinton Township, MI Corvair Zodiac XL, ScrapBuilder ;-) http://www.mykitlog.com/rlendon Read this topic online here: http://forums.matronics.com/viewtopic.php?p=77995#77995 ________________________________________________________________________________
Date: Nov 29, 2006
From: Brandon Tucker <btucke73(at)yahoo.com>
Subject: Re: Buying a Partial Built Kit
Bill, George is correct. You need an FAA bill of sale from every owner in the chain; One from ZAC, and one from every previous owner. However, if you already bought a kit from ZAC, you can register the aircraft using the kit serial number and bill of sale provided by ZAC. Where individual parts come from are of little concern. This truly is just a paperwork drill - not for the weak hearted or time constrained... Also, I noticed that someone has plans for sale on the list. When these plans change hands, make life easier for the purchaser, and fill out an FAA bill of sale for the plans. With those plans come a serial number for an aircraft. Regardless if any parts were sold, a bill of sale will be required to register the aircraft. R/ Brandon --------------------------------- ________________________________________________________________________________
Date: Nov 29, 2006
From: Brandon Tucker <btucke73(at)yahoo.com>
Subject: N601XT flies... for real this time...
Gents, Finally got the aircraft flight ready again this morning and took her up. 601 HDS / Conventional gear with aluminum spring Corvair bored .060 over - standard WW conversion Calsbad, Ca. SKC / 60 miles vis / 65 deg Climb out was less than expected at about 800 FPM at 3000 rpm. The engine sputters just a little bit at full throttle, so this is the performance cracked just a bit from full. I have to tune in the aerocarb a little bit this week. I am still indicating high oil temps, so a new sender is on order. Indicated temps are not jiving with laser temp finder on the ground. It required full right aileron trim to go hands off. More flight stuff to follow in the next few days... Some things to mention. DO NOT waste your money on Azusa brakes. They couldn't slow a piss ant's motorbike. I bought a hydraulic disc upgrade from GPSAC, and after a little bit of fab work to install, they work much better. I still saved a few bucks from the Matco setup, but it was not worth the heartache. Also, for the tailwheel folks, I would bypass the tailwheel from the plans altogether. I installed the Matco full swiveling taiwheel this week, and love it. It is a very good deal at under $150, and installation is a piece of cake. Someday I'll get somebody to take some pictures of the plane in flight and forward them to the list... R/ Brandon --------------------------------- ________________________________________________________________________________
Date: Nov 29, 2006
From: xl <xl(at)prosody.org>
Subject: Re: Buying a Partial Built Kit
The form that you will use to verify that you did > 51% of the work is: FAA FORM 8000-38, FABRICATION/ASSEMBLY OPERATION CHECKLIST Go to www.faa.gov and search for 8000-38. Even though I built from '51% kit' my DAR made me fill out the form to 'verify' that I did >50% of the work. Joe E N633Z @ BFI CH601XL, 408 hours Jabiru 3300, Sensenich 49x64 wood prop On Wed, 29 Nov 2006 JAPhillipsGA(at)aol.com wrote: > ....snip > started kit and successfully got it through FAA ? Second question is what amount > of work can be accomplished by the first builder that will still allow me to > be granted a repairman's certificate when I get her flying? That is the "tall > ....snip > N505WP > 601XL-3300 > 96 hours ________________________________________________________________________________
Date: Nov 30, 2006
From: Matt Dralle <dralle(at)matronics.com>
Subject: Last "Official" Day Of The List Fund Raiser!
Dear Listers, Well, its November 30th and that means three things... 1) Today I am now officially 43 years old... (arg...) 2) It marks that last "official" day of the List Fund Raiser! 3) Its the last day I will be bugging everyone for a whole year! :-) If you use the Lists and enjoy the content and the no-advertising, no-spam, and no-censorship way in which they're run, please make a Contribution today to support their continued operation and upkeep. Your $20 or $30 goes a long way to further the List operation and keep the bills paid. I will be posting the List of Contributors next week, so make sure your name is on it! :-) Thank you to everyone that has made a Contribution so far this year! It is greatly appreciated. List Contributions: http://www.matronics.com/contribution Best regards, Matt Dralle Matronics Email List Administrator ________________________________________________________________________________
Subject: Alternator Recommendations
From: "Wingrider" <rwhitt3(at)HOTMAIL.COM>
Date: Nov 30, 2006
Hi, I am new to the Matronics newsgroups although I have been reading the post for a while this is my first time writing in. I'm building a Zenith 601HDS and will probably go with William Wynne's Corvair conversion. I'm trying to figure my electrical loads before installing the landing lights and closing up the wings and don't believe the typical JD garden tractor alternator is sufficient for my application; I expect a full load amp draw of between 35 and 40 amps. Maybe I'm way off base and maybe I shouldn't use a pair of 100 watt off road lights for landing lights. I'd like your recommendations for a small lightweight automotive alternator. From what Ive read it sounds like I should stick with the three wire alternators and shy away from the one wire versions but are there recommendations for specific alternators? There seems to be differing opinions on the whether the load dump issue is a real concern or not. I understand Bob Nuckolls is working on a product to nullify the concern with using internally regulated alternators. Is there any news on this product at this time? Attached is my initial swag at my electrical loads. -------- Rich Whittington Tullahoma, TN Zenith 601HDS Under Construction Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78119#78119 Attachments: http://forums.matronics.com//files/ch601hds_electrical_loads_analysis1_852.xls ________________________________________________________________________________
Date: Nov 30, 2006
From: "John M. Goodings" <goodings(at)yorku.ca>
Subject: Re: Zenith-List Digest: CZAW Cowl Question Again
Initially, in our CH601HD with R912S, the oil and coolant temperatures were too high. Two fixes took care of the problem. The first was to increase the airflow EXIT area by cutting out quite a bit of fibreglass. An increased intake area won't do much if the exit area is too restricted. The exit area must be much bigger than the intake area. [However, this fix can be uncertain if the lower back exit area of the cowl has a down-turning lip on it. This lip, if present, creates a low-pressure area beneath the cowl to SUCK the hot air out. My point is, if this lip is present on your cowl (it wasn't on mine, but I've seen it on a CZAW-built 601XL), I wouldn't mess with the exit area.] The second fix was to make sure the intake duct was a close fit around the radiator so that the air has to go through the rad, and cannot escape around the edges. We added fibrglass strips to improve the close fit. We did NOT increase any intake areas. John Goodings, C-FGPJ, CH601HD with R912S, Toronto/Ottawa/Waterloo. ________________________________________________________________________________
Subject: Re: Cortec thickness and Loose Rivets over time...?
From: "PatrickW" <pwhoyt(at)yahoo.com>
Date: Nov 30, 2006
amyvega2005(at)earthlink. wrote: > why the Cortec might I ask? When I went to the Rudder Workshop it's what Zenith used. Prior to the start of the workshop they painted everyone's aluminum rudder pieces with Cortec. So I figured I'd go with what they did and use it. I just didn't know if I should put it on quite as thick. I think there is an additional benefit to Cortec - it's sticky, and after the parts are riveted together it will be like "rivets plus glue". Would add more shear strength I would think. But would also harder to slide parts around, like fitting a piano hinge between two skin sheets for example. - PatrickW Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78157#78157 ________________________________________________________________________________
Date: Nov 30, 2006
From: Brandon Tucker <btucke73(at)yahoo.com>
Subject: RE: Alternator Recommendations
I bought a 45 amp internally regulated alternator to install in my HDS Corvair, and sold it after figuring out that there is no way to make it fit under the nosebowl. If you are going with the WW Corvair conversion, the small dynamo is the only thing that will fit. Your only other option is to mount the alt in the back of the motor, which will require a little more work than just buying parts from William and bolting them on. Not too much work, but more... IMHO, load shedding, and possibly going with smaller lights, and LEDs when possible would be easier than engineering your own alternator setup. You can purchase the overvoltage protection unit from Bob. I have it installed in my aircraft. After having a regulator fail in a Citabria, and frying the battery, I like the idea of having built in overvoltage protection. He now also has a low voltage indication BAMM unit now, but I know nothing about it other than what it says on the website. R/ Brandon --------------------------------- ________________________________________________________________________________
Date: Nov 30, 2006
From: Mike Moore <soarmoore2(at)yahoo.com>
Subject: Re: N601XT flies... for real this time...
Brandon, Congrats on getting airborne! Noticed your tailwheel upgrade comments and wondered if you would share some info on the Matco installation. I'm just starting on a 601XL taildragger and would prefer a swiveling tailwheel versus the stock fixed wheel. I'd like to know what was involved in the installation versus the fixed wheel, if it would be a significant rework project if installed at a later date, and where I can find additional info. Appreciate any response you send. M2 Brandon Tucker wrote: Gents, Finally got the aircraft flight ready again this morning and took her up. 601 HDS / Conventional gear with aluminum spring Corvair bored .060 over - standard WW conversion Calsbad, Ca. SKC / 60 miles vis / 65 deg Climb out was less than expected at about 800 FPM at 3000 rpm. The engine sputters just a little bit at full throttle, so this is the performance cracked just a bit from full. I have to tune in the aerocarb a little bit this week. I am still indicating high oil temps, so a new sender is on order. Indicated temps are not jiving with laser temp finder on the ground. It required full right aileron trim to go hands off. More flight stuff to follow in the next few days... Some things to mention. DO NOT waste your money on Azusa brakes. They couldn't slow a piss ant's motorbike. I bought a hydraulic disc upgrade from GPSAC, and after a little bit of fab work to install, they work much better. I still saved a few bucks from the Matco setup, but it was not worth the heartache. Also, for the tailwheel folks, I would bypass the tailwheel from the plans altogether. I installed the Matco full swiveling taiwheel this week, and love it. It is a very good deal at under $150, and installation is a piece of cake. Someday I'll get somebody to take some pictures of the plane in flight and forward them to the list... R/ Brandon --------------------------------- ________________________________________________________________________________
Subject: Re: N601XT flies... for real this time...
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Nov 30, 2006
Congrats on your first flight. What prop and pitch do you have? [quote="btucke73(at)yahoo.com"]Gents, Finally got the aircraft flight ready again this morning and took her up. 601 HDS / Conventional gear with aluminum spring Corvair bored .060 over - standard WW conversion Calsbad, Ca. SKC / 60 miles vis / 65 deg Climb out was less than expected at about 800 FPM at 3000 rpm. The engine sputters just a little bit at full throttle, so this is the performance cracked just a bit from full. I have to tune in the aerocarb a little bit this week. I am still indicating high oil temps, so a new sender is on order. Indicated temps are not jiving with laser temp finder on the ground. It required full right aileron trim to go hands off. More flight stuff to follow in the next few days... Some things to mention. DO NOT waste your money on Azusa brakes. They couldn't slow a piss ant's motorbike. I bought a hydraulic disc upgrade from GPSAC, and after a little bit of fab work to install, they work much better. I still saved a few bucks from the Matco setup, but it was not worth the heartache. Also, for the tailwheel folks, I would bypass the tailwheel from the plans altogether. I installed the Matco full swiveling taiwheel this week, and love it. It is a very good deal at under $150, and installation is a piece of cake. Someday I'll get somebody to take some pictures of the plane in flight and forward them to the list... R/ Brandon > [b] -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78178#78178 ________________________________________________________________________________
Date: Nov 30, 2006
From: Keystone Engineering LLC <keystone(at)gci.net>
Subject: 8.50x6.00 on 801
Dave I have 8.50x6.00 tires on my 801. I had problems with flat tires until I modified the rim to accommodate a normal 8.50x6.00 tube. There are not 8.50 tubes that I could find with the 90 degree stem. The manufacture of the rim had a site that showed how and where to drill the hole. I did it 3 years ago so the site may no longer exist. If you need some pics let me know. There is about 1/4" of clearance between the tire and the gear legs. I'm not sure you could go much wider without re-engineering the wheel and brake attachment. Bill Wilcox N801BW Valdez, Alaska 375 hrs From: "Dave Ruddiman" <pacificpainting(at)comcast.net> Subject: Zenith-List: 801 Tire Clearance 801 People, I haven't started my fuselage yet so I don't know the answer to this question. What is the clearance between the wheels and the gear legs? Both the mains and the nose. I assume 8.50 tires will fit, but I am curious if anything larger will. If anyone knows, I would appreciate knowing too. ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: RE: Alternator Recommendations
Date: Nov 30, 2006
A rule of thumb is if you have a load meter then install loads only up to the capacity of the charging system. Without the load meter only install to 80%. I guess the reverse is true... without a meter and 30A of continuous use ( everything on after starting) the generator/alternator should be capable of producing 36A. Noel -----Original Message----- From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com] On Behalf Of Brandon Tucker Sent: Thursday, November 30, 2006 12:00 PM Subject: Zenith-List: RE: Alternator Recommendations I bought a 45 amp internally regulated alternator to install in my HDS Corvair, and sold it after figuring out that there is no way to make it fit under the nosebowl. If you are going with the WW Corvair conversion, the small dynamo is the only thing that will fit. Your only other option is to mount the alt in the back of the motor, which will require a little more work than just buying parts from William and bolting them on. Not too much work, but more... IMHO, load shedding, and possibly going with smaller lights, and LEDs when possible would be easier than engineering your own alternator setup. You can purchase the overvoltage protection unit from Bob. I have it installed in my aircraft. After having a regulator fail in a Citabria, and frying the battery, I like the idea of having built in overvoltage protection. He now also has a low voltage indication BAMM unit now, but I know nothing about it other than what it says on the website. R/ Brandon ________________________________________________________________________________
Date: Nov 30, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: Cortec thickness and Loose Rivets over time...?
I would put it sparingly. Weight is one issue, going on thick has nominal return. -----Original Message----- >From: PatrickW <pwhoyt(at)yahoo.com> >Sent: Nov 30, 2006 10:25 AM >To: zenith-list(at)matronics.com >Subject: Zenith-List: Re: Cortec thickness and Loose Rivets over time...? > > >amyvega2005(at)earthlink. wrote: >> why the Cortec might I ask? > > >When I went to the Rudder Workshop it's what Zenith used. Prior to the start of the workshop they painted everyone's aluminum rudder pieces with Cortec. > >So I figured I'd go with what they did and use it. I just didn't know if I should put it on quite as thick. > >I think there is an additional benefit to Cortec - it's sticky, and after the parts are riveted together it will be like "rivets plus glue". > >Would add more shear strength I would think. But would also harder to slide parts around, like fitting a piano hinge between two skin sheets for example. > >- PatrickW > > >Read this topic online here: > >http://forums.matronics.com/viewtopic.php?p=78157#78157 > > ________________________________________________________________________________
Subject: Re: CZAW cowl question again
From: "zodieman" <webmaster(at)upac.ca>
Date: Nov 30, 2006
Finally, some pictures of my installed cowl for anyone who wants to have a look and comment: Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78242#78242 Attachments: http://forums.matronics.com//files/imgp0884_168.jpg http://forums.matronics.com//files/imgp0883_368.jpg http://forums.matronics.com//files/imgp0882_957.jpg http://forums.matronics.com//files/imgp0868_716.jpg http://forums.matronics.com//files/imgp0866_184.jpg http://forums.matronics.com//files/imgp0865_155.jpg ________________________________________________________________________________
Date: Nov 30, 2006
From: Jaybannist(at)cs.com
Subject: Enough Already!
Calf-rope!! (anyone know what that means?) Here in Dallas, it is now 51 degrees cooler than it was at this time yesterday! At 29 degrees, (no heat in the airplane work area) I can't even squeeze a rivet puller. I know that makes me a wimp, but, hey, we Southerners just aren't used to "yankee" weather. Enough already, I'm ready for Winter to be over! Jay in Dallas ________________________________________________________________________________
Date: Nov 30, 2006
From: Peter Chapman <pchapman(at)ionsys.com>
Subject: Re: CZAW cowl question again
Trevor Page / zodieman wrote: >>I'm just completed the conversion of my 601HD to the CZAW cowl and >>rad placement. It was very easy and it's a very nice kit. I Just to confirm, what was the configuration before the change? Was it the old under-fuselage rad placement? I'm curious about the use of a more sophisticated cowl like this, although who knows what supply there might be in the future, given the end of CZAW's production for Zenair. Peter Chapman Toronto, ON 601 HDS / 912 / C-GZDC (Original style cowl, rads moved into sides of cowl as Flypass used to do) ________________________________________________________________________________
From: "David Mikesell" <skyguynca(at)skyguynca.com>
Subject: Re: Enough Already!
Date: Nov 30, 2006
Yeah Jay, I know where your saying. I was born and raised in the DFW area, joined the army to get away to better places...well I spent 12 years in Germany, not only did I hate the cold before.....now I despise it with a passion!! David Mikesell 23597 N. Hwy 99 Acampo, CA 95220 skyguynca(at)skyguynca.com www.skyguynca.com ----- Original Message ----- From: <Jaybannist(at)cs.com> Sent: Thursday, November 30, 2006 1:41 PM Subject: Zenith-List: Enough Already! > > Calf-rope!! (anyone know what that means?) Here in Dallas, it is now 51 > degrees cooler than it was at this time yesterday! At 29 degrees, (no > heat in the airplane work area) I can't even squeeze a rivet puller. I > know that makes me a wimp, but, hey, we Southerners just aren't used to > "yankee" weather. Enough already, I'm ready for Winter to be over! > > Jay in Dallas > > > ________________________________________________________________________________
From: "Dave G." <d.goddard(at)ns.sympatico.ca>
Subject: Re: Enough Already!
Date: Nov 30, 2006
I really don't blame you for complaining. Bad enough life has stuck you in Texas, having a slight chill or any other discomfort is far too much to heap on top of such a grave misfortune. Don't worry, you're bound to be back to your normal misery soon enough. ----- Original Message ----- From: <Jaybannist(at)cs.com> Sent: Thursday, November 30, 2006 5:41 PM Subject: Zenith-List: Enough Already! > > Calf-rope!! (anyone know what that means?) Here in Dallas, it is now 51 > degrees cooler than it was at this time ________________________________________________________________________________
Subject: Re: CZAW cowl question again
From: "zodieman" <webmaster(at)upac.ca>
Date: Nov 30, 2006
I spoke to CZAW about the availability and so far they're still more than happy to supply kits and parts for 601s considering the firewall-forward system of their SportCruiser is identical to the 601 system they developed. On another note, I took some detailed measurements of my oil cooler and placement and wouldn't you know it.. they are all perfect according to this article I found: http://www.ch601.org/resources/cooling_systems2.htm Looks like maybe the folks in the Czech republic we're doing their homework! Even though the placement, inlet size and distances are right I still have to make up a plenum of sort to funnel the air into the oil cooler but It's worth a try. I reckon I can whip that up in a few hours of glass work Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78275#78275 ________________________________________________________________________________
From: "Dave Ruddiman" <pacificpainting(at)comcast.net>
Subject: No email.
Date: Nov 30, 2006
Is it just me not receiving mail from the list, or is it Comcast blocking again? Dave in Salem ________________________________________________________________________________
Date: Nov 30, 2006
From: "Dave Thompson" <dave.thompson(at)verizon.net>
Subject: Re: 601XL - Engine out / Glide Experience
My primary flight instructor before I got my license in the 70's was a crusty, crabby old ex-Marine flight instructor (I know, once a Marine, always a Marine). It seemed that we spent more time on Emergency procedures than basic flight. He had me learn very steep slips, simulated electrical failures and engine off procedures. One time we flew out to a California desert dry lake and he pulled back the throttle several miles away. This was while I was plotting a new course. He had me follow through and actually land on the lake bed. When I attempted to take off again from a full stop, he pulled back the throttle again at about 500 feet. He then told me that the scratch on the lake bed ahead was a "bunch of bushes" that I had to avoid on landing again. We performed several "forced landings" and "aborted take-offs" that day. On the way back to EMT (El Monte, CA) he pulled back the throttle again over a rural part of town. He gave me power again at about 200 feet over a deserted road. We had three more similar days before I had my final check ride. At the time, I was very irritated with him. Several years later, the two-cycle engine seized in my B1RD ultralight and I had to make a forced landing on a highway center meridian. When the engine quit, I calmly remembered my training and experience and flew the ultralight all the way down to a perfect landing. I was pleasantly surprised at how calm I was during that emergency. There is no better way to prepare yourself for an emergency than practice. Dave Thompson dave.thompson(at)verizon.net Westminster, CA 601XL rudder workshop, Corvair engine in parts and no money for a kit. ________________________________________________________________________________
Date: Nov 30, 2006
From: Brandon Tucker <btucke73(at)yahoo.com>
Subject: Re: Matco Tailwheel install: was Re: N601XT flies... for real
this time... Mike, The installation was much simpler than the tailwheel from the plans, with the exception of having to weld a little. First, buy leaf spring #4 from here: http://aircraftspruce.com/catalog/lgpages/leafsprings.php I had to weld about a 5" extention to it to get it to reach the forward spring mount bolt. I kept most of the spring cool with a wet rag while welding at the end. The part of the spring that "springs" did not lose any heat treating. I'll try to get a picture of it and send it to you. I bought the solid Matco tailwheel from here: http://aircraftspruce.com/catalog/lgpages/matco_tw.php After flying it today, I think the inflatable wheel would be better. You really feel the rough asphalt with the solid wheel. You then buy the spring kit here: http://aircraftspruce.com/catalog/lgpages/comp_springs.php Installation was less than 2 hours including welding an extension to the spring. It was a very easy upgrade. -Much easier than scratch building the tailwheel the first time... R/ Brandon --------------------------------- ________________________________________________________________________________
Date: Nov 30, 2006
From: Brandon Tucker <btucke73(at)yahoo.com>
Subject: Re: N601XT flies... for real this time...
Gig, I have the Warp Drive set at 8 deg at the tip. It yielded about 3000 on takeoff today. I tried attaching pics, but Matronics denied... I will try to get some pictures and video up on a website tonight for all to view. R/ Brandon --------------------------------- ________________________________________________________________________________
From: "Craig Payne" <craig(at)craigandjean.com>
Subject: No email.
Date: Nov 30, 2006
If you ever have any doubts just go to the web interface to the list and see if there are messages there that you haven't seen. -- Craig ________________________________________________________________________________
From: "Dave Ruddiman" <pacificpainting(at)comcast.net>
Subject: Re: No email.
Date: Nov 30, 2006
Thanks Craig. I didn't know I could do that. Dave ----- Original Message ----- From: Craig Payne To: zenith-list(at)matronics.com Sent: Thursday, November 30, 2006 9:44 PM Subject: RE: Zenith-List: No email. If you ever have any doubts just go to the web interface to the list and see if there are messages there that you haven't seen. -- Craig ________________________________________________________________________________
Subject: Re: Alternator Recommendations
From: "Wingrider" <rwhitt3(at)HOTMAIL.COM>
Date: Dec 01, 2006
Thanks for the advice, it will be a while till I'm at the engine stage but I was trying to figure out what I could use for landing lights before I closed up the wings. The advice on the AeroElectric group is the Suzuki Sameri alternator which looks like a good option to me. -------- Rich Whittington Tullahoma, TN Zenith 601HDS Under Construction Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78368#78368 ________________________________________________________________________________
From: Trevor Page <webmaster(at)upac.ca>
Subject: Re: CZAW cowl question again
Date: Dec 01, 2006
Peter, I had the same arrangement you have not (inside the cowl with outside scoops a la Flypass). Never worked right for me. This new system is much nicer and cleaner looking and I got a few more Mph out of the deal... Trev Page C-IDUS 601HD R912 On Nov 30, 2006, at 4:53 PM, Peter Chapman wrote: > > Trevor Page / zodieman wrote: > >>> I'm just completed the conversion of my 601HD to the CZAW cowl >>> and rad placement. It was very easy and it's a very nice kit. I > > Just to confirm, what was the configuration before the change? > Was it the old under-fuselage rad placement? > > I'm curious about the use of a more sophisticated cowl like this, > although who knows what supply there might be in the future, given > the end of CZAW's production for Zenair. > > > Peter Chapman > Toronto, ON 601 HDS / 912 / C-GZDC > (Original style cowl, rads moved into sides of cowl as Flypass used > to do) > > ________________________________________________________________________________
Subject: Re: N601XT flies... for real this time...
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Dec 01, 2006
FWIW I'm pretty sure WW has his at 9 degrees. [quote="btucke73(at)yahoo.com"]Gig, I have the Warp Drive set at 8 deg at the tip. It yielded about 3000 on takeoff today. I tried attaching pics, but Matronics denied... I will try to get some pictures and video up on a website tonight for all to view. R/ Brandon > [b] -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78407#78407 ________________________________________________________________________________
Subject: Re: Alternator Recommendations
From: "eedetail" <eedetail(at)qwest.net>
Date: Dec 01, 2006
The pair of 100w landing lights will be overkill in my opinion. If money is no object go with a pair of HID lights. Xenondepot.com has a pair for $469 plus shipping. Rated at 35w each, they draw less than 5 amps each. One is as bright or brighter than a 100w bulb. No matter how much light a landing light puts out, it only shows you what you are about to hit, nothing else. TimE Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78420#78420 ________________________________________________________________________________
From: "Robin Bellach" <601zv(at)ritternet.com>
Subject: Re: Alternator Recommendations
Date: Dec 01, 2006
The 35-watt automotive type lights I got from Harbor Freight for less than $10 per pair seem to put out as much light as a 100-watt 4509 when I compared them. Robin in AR N601ZV ----- Original Message ----- From: "eedetail" <eedetail(at)qwest.net> Sent: Friday, December 01, 2006 10:46 AM Subject: Zenith-List: Re: Alternator Recommendations > > The pair of 100w landing lights will be overkill in my opinion. > If money is no object go with a pair of HID lights. Xenondepot.com has > a pair for $469 plus shipping. Rated at 35w each, they draw less than 5 > amps each. One is as bright or brighter than a 100w bulb. No matter how > much light a landing light puts out, it only shows you what you are about > to hit, nothing else. > TimE > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=78420#78420 > > > ________________________________________________________________________________
Date: Dec 01, 2006
From: Mike Moore <soarmoore2(at)yahoo.com>
Subject: Re: Matco Tailwheel install: was Re: N601XT flies... for
real this time... Brandon, Thanks for the response/info. Will file for the present till I get working on the fuselage and decide when I get closer to that point. Meanwhile, I'll watch for any comments you publish concerning how your installation works out in actual use. Regards, M2 Brandon Tucker wrote: Mike, The installation was much simpler than the tailwheel from the plans, with the exception of having to weld a little. First, buy leaf spring #4 from here: http://aircraftspruce.com/catalog/lgpages/leafsprings.php I had to weld about a 5" extention to it to get it to reach the forward spring mount bolt. I kept most of the spring cool with a wet rag while welding at the end. The part of the spring that "springs" did not lose any heat treating. I'll try to get a picture of it and send it to you. I bought the solid Matco tailwheel from here: http://aircraftspruce.com/catalog/lgpages/matco_tw.php After flying it today, I think the inflatable wheel would be better. You really feel the rough asphalt with the solid wheel. You then buy the spring kit here: http://aircraftspruce.com/catalog/lgpages/comp_springs.php Installation was less than 2 hours including welding an extension to the spring. It was a very easy upgrade. -Much easier than scratch building the tailwheel the first time... R/ Brandon --------------------------------- ________________________________________________________________________________
Date: Dec 01, 2006
From: MrBizi <mrbizi(at)yahoo.com>
Subject: fuel selector, flap control
Does anyone know if a fuel selector with left/both/right/off would work (i.e. like a C172) in the Zodiac? Trying to make the LSA Zodiac XL to train my brother and having a "both" selector would help so he can focus more on the other aspects of flying than worrying about which tank it is on..... Also, does anyone now if it is possible (and where to get it) to put a Cessna notched indent type Flap Selector on a Zodiac? Again, for ease of use when learning it helps to be able to put a 1st notch of flaps and then focus your eyes outside instead of flipping a switch.... watching the indicator... waiting for 10 degrees.... then letting go of the switch to stop the flap movement..... then looking outside... Thanks for any advice anyone might have! thanks, Josh Olson ________________________________________________________________________________
From: "Craig Payne" <craig(at)craigandjean.com>
Subject: fuel selector, flap control
Date: Dec 01, 2006
I recall a discussion about "both" being bad in low-wing aircraft. Something perhaps about cross-flow between the tanks or problems when one tank is empty. In general I think you only see "both" on high-wing aircraft. A real Internet expert will now jump in, tell me I'm full of baloney and that he flew for 10,000 hours with a both setting on his SR-71, etc. As to the flap stuff take a look at this: http://www.aircraftextras.com/FPS-Plus.htm And a less-expensive solution - a linear actuator ($70) and a controller ($50) that remembers preset positions: http://www.surpluscenter.com/item.asp?UID 06120112260557 <http://www.surpluscenter.com/item.asp?UID 06120112260557&item=5-1577-2&ca tname> &item=5-1577-2&catname http://www.surpluscenter.com/item.asp?UID 06120112260557 <http://www.surpluscenter.com/item.asp?UID 06120112260557&catname=&item=5- 1577-C> &catname=&item=5-1577-C -- Craig ________________________________________________________________________________
From: "Samm Munn" <heliav8r(at)swbell.net>
Subject: Re: Enough Already!
Date: Dec 01, 2006
Mark Twain once said, "The coldest winter I ever spent was a summer in San Francisco." ----- Original Message ----- From: John Marzulli To: zenith-list(at)matronics.com Sent: Friday, December 01, 2006 11:25 AM Subject: Re: Zenith-List: Enough Already! I live in Seattle, lived north of Dallas, lived in Maryland, and been to Alaska in the dead of winter... but to this day the coldest place I've ever been is San Francisco. Something about the cold there just chills you right through your bones. ________________________________________________________________________________
Date: Dec 01, 2006
From: Jack Russell <clojan(at)sbcglobal.net>
Subject: Re: fuel selector, flap control
Boy did we have a discussion on this one when I was doing my fuel system. I went with the both and yes there are some production low wings with both. One of the problems that arise is that when on both and you are low in the tanks you could suck air instead of fuel from the lower wing in a turn. I use a placard that says not to use both with less than 1//3 tanks. The other problem is that with both if you do run out in one tank which way do you turn the valve, left or right. It takes a few seconds to start again and if you are close to the ground you may not have those seconds. If you are on Left you know you need right. I tend to switch the tank depending on the landing pattern to use the tank that is the highest in turns. Jack Jack Russell -Clovis CA 601 XL Jabiru 3300 Progress update at: http://www.geocities.com/clojan@sbcglobal.net/zodiacbarn.html ________________________________________________________________________________
Date: Dec 01, 2006
From: Big Gee <taffy0687(at)yahoo.com>
Subject: Re: fuel selector, flap control
????????????????????????????????????????????????=0A???????????????????????? ????????????????????????=0A???????????????????????????????????????????????? =0A????????????????????????????????????????????????=0A????????????????????? ???????????????????????????=0A????????????????????????????????????????????? ???=0A=0AFritz=0A=0A=0A----- Original Message ----=0AFrom: MrBizi <mrbizi@y ahoo.com>=0ATo: zenith-list(at)matronics.com=0ASent: Friday, December 1, 2006 1:03:58 PM=0ASubject: Zenith-List: fuel selector, flap control=0A=0A=0ADoes anyone know if a fuel selector with left/both/right/off would work (i.e. l ike a C172) in the Zodiac? Trying to make the LSA Zodiac XL to train my b rother and having a "both" selector would help so he can focus more on the other aspects of flying than worrying about which tank it is on.....=0A =0A =0AAlso, does anyone now if it is possible (and where to get it) to put a Cessna notched indent type Flap Selector on a Zodiac? Again, for ease of use when learning it helps to be able to put a 1st notch of flaps and then focus your eyes outside instead of flipping a switch.... watching the indic ator... waiting for 10 degrees.... then letting go of the switch to stop th e flap movement..... then looking outside...=0A =0AThanks for any advice an =======================0A=0A=0A =0A_______________________________________________________________________ _____________=0AWant to start your own business?=0ALearn how on Yahoo! Smal l Business.=0Ahttp://smallbusiness.yahoo.com/r-index ________________________________________________________________________________
Date: Dec 01, 2006
From: MrBizi <mrbizi(at)yahoo.com>
Subject: fuel selector, flap control
Thanks for your help! Aircraftextras is a great site! Thanks for sharing Craig Payne wrote: I recall a discussion about "both" being bad in low-wing aircraft. Something perhaps about cross-flow between the tanks or problems when one tank is empty. In general I think you only see "both" on high-wing aircraft. A real Internet expert will now jump in, tell me I'm full of baloney and that he flew for 10,000 hours with a both setting on his SR-71, etc. As to the flap stuff take a look at this: http://www.aircraftextras.com/FPS-Plus.htm And a less-expensive solution - a linear actuator ($70) and a controller ($50) that remembers preset positions: http://www.surpluscenter.com/item.asp?UID 06120112260557&item=5-1577-2&catname http://www.surpluscenter.com/item.asp?UID 06120112260557&catname=&item=5-1577-C -- Craig ________________________________________________________________________________
Subject: Re: Alternator Recommendations
From: "eedetail" <eedetail(at)qwest.net>
Date: Dec 01, 2006
Well, yes you are both correct. As voltage drops, current increases in order to maintain the same power. My less than 5 amp is based upon actual measurements last nite, using only battery power, and an analog ammeter. I found in actual practice that my 35w landing light will sometimes draw up to 5 amps and trip the breaker. TimE Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78464#78464 ________________________________________________________________________________
Subject: Re: fuel selector, flap control
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Dec 01, 2006
mrbizi(at)yahoo.com wrote: > Does anyone know if a fuel selector with left/both/right/off would work (i.e. like a C172) in the Zodiac? Trying to make the LSA Zodiac XL to train my brother and having a "both" selector would help so he can focus more on the other aspects of flying than worrying about which tank it is on..... > I think the added concern over what to do when the engine stops because he is sucking air out of an empty fuel tank out weighs worrying about which tank he is needs to have selected. If you want to reduce that concern during the first hours of training then just manage the fuel for him until he has advanced further in learning to fly. -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78465#78465 ________________________________________________________________________________
Date: Dec 01, 2006
From: MrBizi <mrbizi(at)yahoo.com>
Subject: Re: fuel selector, flap control
Jack: http://www.geocities.com/clojan@sbcglobal.net/zodiacbarn.html Great website! Please let me know where you found the fuel selector that has 'both' I think I might do the same as you. I can manage the fuel when it gets down around 1/3 tank... but for a new pilot like my brother... i'd prefer to have full tanks ALWAYS for him and have a 'both' setting.... Thanks, Josh Jack Russell wrote: Boy did we have a discussion on this one when I was doing my fuel system. I went with the both and yes there are some production low wings with both. One of the problems that arise is that when on both and you are low in the tanks you could suck air instead of fuel from the lower wing in a turn. I use a placard that says not to use both with less than 1//3 tanks. The other problem is that with both if you do run out in one tank which way do you turn the valve, left or right. It takes a few seconds to start again and if you are close to the ground you may not have those seconds. If you are on Left you know you need right. I tend to switch the tank depending on the landing pattern to use the tank that is the highest in turns. Jack Jack Russell -Clovis CA 601 XL Jabiru 3300 Progress update at: http://www.geocities.com/clojan@sbcglobal.net/zodiacbarn.html ________________________________________________________________________________
Subject: Re: fuel selector, flap control
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Dec 01, 2006
Josh, How is training your brother in an aircraft with a dangerous fuel system design in any way a good idea? There are DARs out there that wouldn't even signoff on an airplane with that fuel system. Tens of thousands of pilots have had primary training in aircraft that don't have a "Both" position on the fuel selector. Are you a CFI or a CFI-LS? -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78472#78472 ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Re: Alternator Recommendations
Date: Dec 01, 2006
If the engine is not running you will only get about 11 - 11.5V from your battery that will cause an increase in current draw. With the engine running the buss should have around 13.8 - 14.4V th8us reducing the current needed. Circuit breakers protect from over current not wattage. Noel > -----Original Message----- > From: owner-zenith-list-server(at)matronics.com > [mailto:owner-zenith-list-server(at)matronics.com] On Behalf Of eedetail > Sent: Friday, December 01, 2006 4:02 PM > To: zenith-list(at)matronics.com > Subject: Zenith-List: Re: Alternator Recommendations > > > > Well, yes you are both correct. > As voltage drops, current increases in order to maintain the > same power. > My less than 5 amp is based upon actual measurements last > nite, using only battery power, and an analog ammeter. > I found in actual practice that my 35w landing light will > sometimes draw up to 5 amps and trip the breaker. > TimE > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=78464#78464 > > > > > > > > > > > ________________________________________________________________________________
From: "Clive Richards" <s.c.richards(at)homecall.co.uk>
Subject: Re: Crack in 601HD firewall stiffner 6F8-2
Date: Dec 01, 2006
Gig Photos attached as requested showing position of crack & cracked end with stiffener removed. The piece which broke off is not to hand. We have replaced stiffener but left end wider over engine mount and taken strengthening angle above across full width of fire wall. Clive ----- Original Message ----- From: "Gig Giacona" <wr.giacona(at)cox.net> Sent: Tuesday, November 28, 2006 4:40 PM Subject: Zenith-List: Re: Crack in 601HD firewall stiffner 6F8-2 > > Any way we can get a photo of the crack? I'd like to make sure I know > exactly where it is developing. > > [quote="s.c.richards(at)homecall."]Hi list we have found a crack in the > firewall stiffner near the port engine mount and have had to replace the > stiffner > We beleave this may be because we are using a Continental 0-200 & a > header tank so are on a fairley forward C of G. > We have > difficulty in Just lowering the nose on landing, it tends to want to drop > when you remove the power. It is possably caused because to much we > trimmed off the stiffner to fit the original faulty engine mount. > > > Clive Richards > > GCBDG 52 Hrs Estimated 250 T&G / Landings > >> [b] > > > -------- > W.R. "Gig" Giacona > 601XL Under Construction > See my progress at www.peoamerica.net/N601WR > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=77620#77620 > > > ________________________________________________________________________________
Subject: Re: Crack in 601HD firewall stiffner 6F8-2
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Dec 01, 2006
Thanks for the photos. The earlier poster was right the XL has beefed that area up some But it will go on my list of places to watch anyway. -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78509#78509 ________________________________________________________________________________
From: "Dave Austin" <daveaustin2(at)can.rogers.com>
Subject: Re: Alternator Recommendations
Date: Dec 01, 2006
Re this current vs. voltage vs. resistance stuff.. If the load is resistive, and the voltage drops, the current will DECREASE. If the load is a motor, and the voltage drops, the current will usually be higher as the motor will not reach full rpm. Learned that 55 years ago.. Dave Austin 601HDS - 912, Spitfire Mk VIII ________________________________________________________________________________
Date: Dec 01, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: fuel selector, flap control
on the flap etting, you can put a cessna type swith, just go to AIrcraft spruce. OPtion two is to just count 1 one thousand etc, for flap setting. 2 seconds on the 601 xl factory set up is 20 degrees. ABout as simple as youi can get. -----Original Message----- >From: Big Gee <taffy0687(at)yahoo.com> >Sent: Dec 1, 2006 2:06 PM >To: zenith-list(at)matronics.com >Subject: Re: Zenith-List: fuel selector, flap control > >???????????????????????????????????????????????? >???????????????????????????????????????????????? >???????????????????????????????????????????????? >???????????????????????????????????????????????? >???????????????????????????????????????????????? >???????????????????????????????????????????????? > >Fritz > > >----- Original Message ---- >From: MrBizi <mrbizi(at)yahoo.com> >To: zenith-list(at)matronics.com >Sent: Friday, December 1, 2006 1:03:58 PM >Subject: Zenith-List: fuel selector, flap control > > >Does anyone know if a fuel selector with left/both/right/off would work (i.e. like a C172) in the Zodiac? Trying to make the LSA Zodiac XL to train my brother and having a "both" selector would help so he can focus more on the other aspects of flying than worrying about which tank it is on..... > > >Also, does anyone now if it is possible (and where to get it) to put a Cessna notched indent type Flap Selector on a Zodiac? Again, for ease of use when learning it helps to be able to put a 1st notch of flaps and then focus your eyes outside instead of flipping a switch.... watching the indicator... waiting for 10 degrees.... then letting go of the switch to stop the flap movement..... then looking outside... > >Thanks for any advice an===================== > > > >Want to start your own business? >http://smallbusiness.yahoo.com/r-index ________________________________________________________________________________
Date: Dec 01, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: fuel selector, flap control
some of the production Tomahawks have a (Both) setting. in normal level flight with full tanks or with 1/2 tanks, not a problem. I can see maybe a problem with air suction however that would be a problem on any plane including cessnas. It all boils down to prefeence. Juan -----Original Message----- >From: Jack Russell <clojan(at)sbcglobal.net> >Sent: Dec 1, 2006 2:03 PM >To: zenith-list(at)matronics.com >Subject: Re: Zenith-List: fuel selector, flap control > >Boy did we have a discussion on this one when I was doing my fuel system. I went with the both and yes there are some production low wings with both. One of the problems that arise is that when on both and you are low in the tanks you could suck air instead of fuel from the lower wing in a turn. I use a placard that says not to use both with less than 1//3 tanks. The other problem is that with both if you do run out in one tank which way do you turn the valve, left or right. It takes a few seconds to start again and if you are close to the ground you may not have those seconds. If you are on Left you know you need right. I tend to switch the tank depending on the landing pattern to use the tank that is the highest in turns. Jack > > >Jack Russell -Clovis CA >601 XL Jabiru 3300 > Progress update at: >http://www.geocities.com/clojan@sbcglobal.net/zodiacbarn.html > > ________________________________________________________________________________
Date: Dec 01, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: fuel selector, flap control
Ho by the way my SR 71 has an autosellector. fuel system since I am too busy burning a hole in the sky. :). Juan -----Original Message----- >From: Craig Payne <craig(at)craigandjean.com> >Sent: Dec 1, 2006 1:32 PM >To: zenith-list(at)matronics.com >Subject: RE: Zenith-List: fuel selector, flap control > >I recall a discussion about "both" being bad in low-wing aircraft. Something >perhaps about cross-flow between the tanks or problems when one tank is >empty. In general I think you only see "both" on high-wing aircraft. A real >Internet expert will now jump in, tell me I'm full of baloney and that he >flew for 10,000 hours with a both setting on his SR-71, etc. > >As to the flap stuff take a look at this: > >http://www.aircraftextras.com/FPS-Plus.htm > >And a less-expensive solution - a linear actuator ($70) and a controller >($50) that remembers preset positions: >http://www.surpluscenter.com/item.asp?UID 06120112260557 ><http://www.surpluscenter.com/item.asp?UID 06120112260557&item=5-1577-2&ca >tname> &item=5-1577-2&catname >http://www.surpluscenter.com/item.asp?UID 06120112260557 ><http://www.surpluscenter.com/item.asp?UID 06120112260557&catname=&item=5- >1577-C> &catname=&item=5-1577-C > >-- Craig ________________________________________________________________________________
Date: Dec 01, 2006
From: Brandon Tucker <btucke73(at)yahoo.com>
Subject: Re: Warp Drive pitch: was Re: N601XT flies... for real this
time... Gig, I was initially told 9.5 deg from someone on the list. I then checked the archives and read 8.5. I set it at 8 and am getting 2800 - 2900 rpm on takeoff. I should be getting more. I know it is a carburetor issue. I will be tuning it this weekend. It still sputters a bit at full throttle, so I run it cracked from full. As soon as I get the carb right, I will reset the pitch. R/ Brandon --------------------------------- ________________________________________________________________________________
Subject: Re: CZAW cowl question again
From: "zodieman" <webmaster(at)upac.ca>
Date: Dec 01, 2006
Here are some pictures of the oil cooler plenum. Basically it's an extension to the air inlet on the bottom of the cowl. I'll be doing the final fitting and sealer trimming tomorrow at the air strip. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78572#78572 Attachments: http://forums.matronics.com//files/imgp0901_203.jpg http://forums.matronics.com//files/imgp0900_100.jpg http://forums.matronics.com//files/imgp0897_211.jpg http://forums.matronics.com//files/imgp0896_112.jpg ________________________________________________________________________________
Date: Dec 01, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: Warp Drive pitch: was Re: N601XT flies... for real
this time... To all, do you guys and gals on the list want to get together January 13th at the Sebring Sport pilot show? Should be a fun event. Can we get a little fly in going. Its an excuse to come to sunny FLA,maybe play a light golf? Juan -----Original Message----- >From: Brandon Tucker <btucke73(at)yahoo.com> >Sent: Dec 1, 2006 9:04 PM >To: zenith-list(at)matronics.com >Subject: Zenith-List: Warp Drive pitch: was Re: N601XT flies... for real this time... > >Gig, > > I was initially told 9.5 deg from someone on the list. I then checked the archives and read 8.5. I set it at 8 and am getting 2800 - 2900 rpm on takeoff. I should be getting more. I know it is a carburetor issue. I will be tuning it this weekend. It still sputters a bit at full throttle, so I run it cracked from full. As soon as I get the carb right, I will reset the pitch. > > R/ > > Brandon > > > > > >--------------------------------- ________________________________________________________________________________
From: "Dave Johnson" <david_a_g_johnson(at)btinternet.com>
Subject: Re: Alternator Recommendations
Date: Dec 02, 2006
maybe I'm missing a crucial point, but if the voltage drops, then so does the current - Ohm's Law Dave Johnson ----- Original Message ----- From: "Noel Loveys" <noelloveys(at)yahoo.ca> Sent: Friday, December 01, 2006 9:13 PM Subject: RE: Zenith-List: Re: Alternator Recommendations > > If the engine is not running you will only get about 11 - 11.5V from your > battery that will cause an increase in current draw. With the engine > running the buss should have around 13.8 - 14.4V th8us reducing the > current > needed. > > Circuit breakers protect from over current not wattage. > > Noel > > >> -----Original Message----- >> From: owner-zenith-list-server(at)matronics.com >> [mailto:owner-zenith-list-server(at)matronics.com] On Behalf Of eedetail >> Sent: Friday, December 01, 2006 4:02 PM >> To: zenith-list(at)matronics.com >> Subject: Zenith-List: Re: Alternator Recommendations >> >> >> >> Well, yes you are both correct. >> As voltage drops, current increases in order to maintain the >> same power. >> My less than 5 amp is based upon actual measurements last >> nite, using only battery power, and an analog ammeter. >> I found in actual practice that my 35w landing light will >> sometimes draw up to 5 amps and trip the breaker. >> TimE >> >> >> >> >> Read this topic online here: >> >> http://forums.matronics.com/viewtopic.php?p=78464#78464 > ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Re: Alternator Recommendations
Date: Dec 02, 2006
Only if the resistance is constant. Noel > -----Original Message----- > From: owner-zenith-list-server(at)matronics.com > [mailto:owner-zenith-list-server(at)matronics.com] On Behalf Of > Dave Johnson > Sent: Saturday, December 02, 2006 8:09 AM > To: zenith-list(at)matronics.com > Subject: Re: Zenith-List: Re: Alternator Recommendations > > > > > maybe I'm missing a crucial point, but if the voltage drops, > then so does > the current - Ohm's Law > > Dave Johnson > > ----- Original Message ----- > From: "Noel Loveys" <noelloveys(at)yahoo.ca> > To: > Sent: Friday, December 01, 2006 9:13 PM > Subject: RE: Zenith-List: Re: Alternator Recommendations > > > > > > > If the engine is not running you will only get about 11 - > 11.5V from your > > battery that will cause an increase in current draw. With > the engine > > running the buss should have around 13.8 - 14.4V th8us reducing the > > current > > needed. > > > > Circuit breakers protect from over current not wattage. > > > > Noel > > > > > > > >> -----Original Message----- > >> From: owner-zenith-list-server(at)matronics.com > >> [mailto:owner-zenith-list-server(at)matronics.com] On Behalf > Of eedetail > >> Sent: Friday, December 01, 2006 4:02 PM > >> To: zenith-list(at)matronics.com > >> Subject: Zenith-List: Re: Alternator Recommendations > >> > >> > >> > >> Well, yes you are both correct. > >> As voltage drops, current increases in order to maintain the > >> same power. > >> My less than 5 amp is based upon actual measurements last > >> nite, using only battery power, and an analog ammeter. > >> I found in actual practice that my 35w landing light will > >> sometimes draw up to 5 amps and trip the breaker. > >> TimE > >> > >> > >> > >> > >> Read this topic online here: > >> > >> http://forums.matronics.com/viewtopic.php?p=78464#78464 > > > > > > > > > ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Re: Warp Drive pitch: was Re: N601XT flies... for real this
time...
Date: Dec 02, 2006
If it sputters a bit at full throttle you may have a problem with the timing ( you said you would be at that this weekend) or it could be something as mundane as too low an octane rating in your fuel.... Try some high octane stuff to be sure. My Miata absolutely hates the cheapo stuff and pings all over the place.... If I buy my high octane gas at one of those non-dedicated pumps that last gas pumped was low octane it will let me know... low octane fuel in the gas hose is almost a gallon and the car only takes ten gal from empty. Now I have to look for a gas station with a dedicated pump for high octane. God only knows and he's not telling how it will react to the Eth degraded fuel when and if it ever get here. Noel -----Original Message----- From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com] On Behalf Of Brandon Tucker Sent: Friday, December 01, 2006 10:35 PM Subject: Zenith-List: Warp Drive pitch: was Re: N601XT flies... for real this time... Gig, I was initially told 9.5 deg from someone on the list. I then checked the archives and read 8.5. I set it at 8 and am getting 2800 - 2900 rpm on takeoff. I should be getting more. I know it is a carburetor issue. I will be tuning it this weekend. It still sputters a bit at full throttle, so I run it cracked from full. As soon as I get the carb right, I will reset the pitch. R/ Brandon ________________________________________________________________________________
From: "Bill Naumuk" <naumuk(at)alltel.net>
Subject: Re: 601XL - Engine out / Glide Experience
Date: Dec 02, 2006
Dave- Scratch build. Ask around the list- sooner or later, you wind up scratch building something anyway, so don't use lack of funds as an excuse. You're not the first! For a couple hundred bucks worth of sheet stock, you can build your stab. At least you're making progress! I remember an article in SP where Bingelis responded to people who complained about not having a shop. At one time, he was stationed in Japan, and the only "Shop" he had was a closet. Managed to fabricate the wing ribs and other small parts for an Emaraude and eventually finished it. Like Red Green says- "We're all in there pulling for you." Incidentally, I agree with your assessment of flight instructors. In my opinion, if you don't come out of a biennial with your shirt sticking to your back, you didn't get your money's worth. Bill Naumuk HDS Fuselage Townville, Pa ----- Original Message ----- From: Dave Thompson To: zenith-list(at)matronics.com Sent: Thursday, November 30, 2006 10:34 PM Subject: Re: Zenith-List: 601XL - Engine out / Glide Experience My primary flight instructor before I got my license in the 70's was a crusty, crabby old ex-Marine flight instructor (I know, once a Marine, always a Marine). It seemed that we spent more time on Emergency procedures than basic flight. He had me learn very steep slips, simulated electrical failures and engine off procedures. One time we flew out to a California desert dry lake and he pulled back the throttle several miles away. This was while I was plotting a new course. He had me follow through and actually land on the lake bed. When I attempted to take off again from a full stop, he pulled back the throttle again at about 500 feet. He then told me that the scratch on the lake bed ahead was a "bunch of bushes" that I had to avoid on landing again. We performed several "forced landings" and "aborted take-offs" that day. On the way back to EMT (El Monte, CA) he pulled back the throttle again over a rural part of town. He gave me power again at about 200 feet over a deserted road. We had three more similar days before I had my final check ride. At the time, I was very irritated with him. Several years later, the two-cycle engine seized in my B1RD ultralight and I had to make a forced landing on a highway center meridian. When the engine quit, I calmly remembered my training and experience and flew the ultralight all the way down to a perfect landing. I was pleasantly surprised at how calm I was during that emergency. There is no better way to prepare yourself for an emergency than practice. Dave Thompson dave.thompson(at)verizon.net Westminster, CA 601XL rudder workshop, Corvair engine in parts and no money for a kit. ________________________________________________________________________________
Subject: Re: fuel selector, flap control
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Dec 02, 2006
Ok, but the OP was trying to make things easier by having the BOTH setting. Having to change fuel management style during the flight isn't any easier. amyvega2005(at)earthlink. wrote: > all, > > Zenith's news letter #122 dated Jan 2001 has an interesting report from a gent in Switzerland on the fuel tank selector subject He states" Both position is used until 1/2 tank. to assure pilot switches to one tank, blinking light warns of half tank status. Below 25 liters a panel light warns of low tank. > > > -- -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78656#78656 ________________________________________________________________________________
From: "Josh Olson" <mrbizi(at)yahoo.com>
Subject: Re: fuel selector, flap control
Date: Dec 02, 2006
Thanks for everyone's input on this. I've learned a great deal. I had no idea that the kit had a preferred fuel selector or the flap control. I have learned a great deal about the differences between the typical C172 which I'm used to and a low wing plane which I would be learning to fly myself. I now understand the point of fuel management with left/right and the issues that are posed from a 'both' indicator on a low wing that doesn't have an air channel between both tanks, etc. I also appreciate the simple 1 thousand 1, 1 thousand 2, etc. for the flaps. I did not know that the flap control in the Zodiac XL Kit worked like that and now that I do it helps make something that I thought was more complex, seem just as easy. Thank you all for your patience with me and your input so that I could learn. Thanks, Josh Olson Email: mrbizi(at)yahoo.com -----Original Message----- From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com] On Behalf Of Gig Giacona Sent: Saturday, December 02, 2006 12:21 PM Subject: Zenith-List: Re: fuel selector, flap control Ok, but the OP was trying to make things easier by having the BOTH setting. Having to change fuel management style during the flight isn't any easier. amyvega2005(at)earthlink. wrote: > all, > > Zenith's news letter #122 dated Jan 2001 has an interesting report from a gent in Switzerland on the fuel tank selector subject He states" Both position is used until 1/2 tank. to assure pilot switches to one tank, blinking light warns of half tank status. Below 25 liters a panel light warns of low tank. > > > -- -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78656#78656 ________________________________________________________________________________
Subject: Re: fuel selector, flap control
From: "Martin Pohl" <mpohl(at)pohltec.ch>
Date: Dec 02, 2006
For the flap control, look at this: You can order it through: Rgds Martin Zodiac XL CZAW QBK -------- Martin Pohl Zodiac XL QBK 8645 Jona, Switzerland www.pohltec.ch/ZodiacXL Read this topic online here: http://forums.matronics.com/viewtopic.php?p=78714#78714 ________________________________________________________________________________
Date: Dec 02, 2006
From: Brett Hanley <bretttdc(at)yahoo.com>
Subject: fuel selector
I once had a car that would cover four hundred miles without refueling. Tha t's about six hours on a interstate highway. I did drive it that far witho ut refueling once. But as an everyday action four hours is a long time to sit in a luxury car. Four hours in a light plane is an ordeal. How big is your bladder? Does anyone on this list ever or regularly fly their XL or 7 01 more than four hours on any leg? If so how often.=0A =0AA standard XL c arries at least twenty gallons. For some reason I am thinking it may be tw enty three gallons. I really do not remember. I do not think that any of the popular engine choices burn more than about four gallons an hour. Usin g that data we should get at least five hours of cruise as a general rule. Of course it would be fool hearted to not to allow for a reserve. So lets say we have four hours to cruise and can land with a more than generous res erve. Unless we have been in a two hour bank neither tank should "suck air " either.=0A =0ASo why not just plumb all the tanks together. Put one shu t off valve in the cockpit. This way we can save some time,weight and mone y. Then plan your flight so that you land with at least thirty minute's of fuel. If that's not enough add a couple leading edge tanks and plumb th em in with the rest as well. It just sounds simpler. In my not so humble op inion this simplistic approach would breed far more safety than any possibl e valve arrangement.=0A =0AI would love to hear some realistic feed back to this simplistic approach. I am not an expert on fuel management but I thi nk I am going to do this on mine.=0A =0ABrett Hanley=0ANW HOUSTON TEXAS=0A =0APS If anyone is interested I am looking for a hanger mate on a small pri vate airstrip near the intersection of Jones Road and FM1960. Home builders welcome. If interested please contact me off list.=0A =0A713-589-9988=0A =0A=0A =0A_________________________________________________________________ ___________________=0ANeed a quick answer? Get one in minutes from people w ho know.=0AAsk your question on www.Answers.yahoo.com ________________________________________________________________________________
Date: Dec 02, 2006
From: Gary Gower <ggower_99(at)yahoo.com>
Subject: Re: 601XL - Engine out / Glide Experience
Bill Naumuk wrote: st1\:* { BEHAVIOR: url(#default#ieooui) } Dave- Scratch build. Ask around the list- sooner or later, you wind up scratch building something anyway, so don't use lack of funds as an excuse. You're not the first! For a couple hundred bucks worth of sheet stock, you can build your stab. At least you're making progress! I remember an article in SP where Bingelis responded to people who complained about not having a shop. At one time, he was stationed in Japan, and the only "Shop" he had was a closet. Managed to fabricate the wing ribs and other small parts for an Emaraude and eventually finished it. Like Red Green says- "We're all in there pulling for you." Incidentally, I agree with your assessment of flight instructors. In my opinion, if you don't come out of a biennial with your shirt sticking to your back, you didn't get your money's worth. Bill Naumuk HDS Fuselage Townville, Pa ----- Original Message ----- From: Dave Thompson To: zenith-list(at)matronics.com Sent: Thursday, November 30, 2006 10:34 PM Subject: Re: Zenith-List: 601XL - Engine out / Glide Experience My primary flight instructor before I got my license in the 70s was a crusty, crabby old ex-Marine flight instructor (I know, once a Marine, always a Marine). It seemed that we spent more time on Emergency procedures than basic flight. He had me learn very steep slips, simulated electrical failures and engine off procedures. One time we flew out to a California desert dry lake and he pulled back the throttle several miles away. This was while I was plotting a new course. He had me follow through and actually land on the lake bed. When I attempted to take off again from a full stop, he pulled back the throttle again at about 500 feet. He then told me that the scratch on the lake bed ahead was a bunch of bushes that I had to avoid on landing again. We performed several forced landings and aborted take-offs that day. On the way back to EMT (El Monte, CA) he pulled back the throttle again over a rural part of town. He gave me power again at about 200 feet over a deserted road. We had three more similar days before I had my final check ride. At the time, I was very irritated with him. Several years later, the two-cycle engine seized in my B1RD ultralight and I had to make a forced landing on a highway center meridian. When the engine quit, I calmly remembered my training and experience and flew the ultralight all the way down to a perfect landing. I was pleasantly surprised at how calm I was during that emergency. There is no better way to prepare yourself for an emergency than practice. Dave Thompson dave.thompson(at)verizon.net Westminster, CA 601XL rudder workshop, Corvair engine in parts and no money for a kit. href="http://www.aeroelectric.com">www.aeroelectric.com href="http://www.buildersbooks.com">www.buildersbooks.com href="http://www.kitlog.com">www.kitlog.com href="http://www.homebuilthelp.com">www.homebuilthelp.com href="http://www.matronics.com/contribution">http://www.matronics.com/chref="http://www.matronics.com/Navigator?Zenith-List">http://www.matron --------------------------------- ________________________________________________________________________________
From: "Gary Boothe" <gboothe(at)calply.com>
Subject: 601XL - Engine out / Glide Experience
Date: Dec 03, 2006
Dave, Ditto....Bill talked me into scratch building after I had purchased tail and wing kits. I am saving thousands of $$ just on the Center Section! The best part though, there is ENORMOUS satisfaction from making every part! Good luck with your project, Gary Boothe Cool, CA 601 HDSTD, WW Conversion 90% done, Tail done, wings done, working on c-section Bill Naumuk wrote: Dave- Scratch build. Ask around the list- sooner or later, you wind up scratch building something anyway, so don't use lack of funds as an excuse. You're not the first! For a couple hundred bucks worth of sheet stock, you can build your stab. At least you're making progress!..... Bill Naumuk HDS Fuselage Townville, Pa Dave Thompson dave.thompson(at)verizon.net Westminster, CA 601XL rudder workshop, Corvair engine in parts and no money for a ________________________________________________________________________________
From: "Bill Naumuk" <naumuk(at)alltel.net>
Subject: Fw: Too picky?
Date: Dec 03, 2006
> Carlos- > I found that premade flannel bonnets work much better than anything > else with my rotary polisher and the rough grits. Now I'm down to the > final S compound and flannel tucked in under the elastic of a wool bonnet > and there are certain spots that defy a final shine. The flannel loads up > in no time, too. I scrap bonnets/swatches when they load up- Ma won't hear > of putting them in HER washing machine! Contamination? After the C stage, > I wiped the surface down with alcohol and paper towels to remove the > excess. > I'm starting to wonder if my problem is temperature related. My shop is > heated with a ventless propane garage heater, but I'm reluctant to leave > it burning when I'm not working. Maybe the aluminum is still cold-soaked > even though the ambient temperature is comfortable. > Have you noticed anything temperature related? I'll admit that with > hunting season, getting ready for winter, and routine maintenance around > the house I haven't been able to get my 13hrs a week in on the project but > I've been polishing the C section since October! > Bill Naumuk > HDS Fuselage > Townville, Pa > ----- Original Message ----- > From: "Carlos Sa" <carlosfsa(at)yahoo.com> > To: "Bill Naumuk" > Sent: Saturday, December 02, 2006 10:38 PM > Subject: Re: Too picky? > > >> Hello, Bill >> >> >> I think I went through that myself, but it was due to my specific working >> conditions and method: >> When I was using aluminum polishing compounds, the compound used on the >> first pass left behind >> deposits of very fine material (much like sand), and when I used the >> compound for finishing, >> since I was working on a flat, horizontal surface, I picked up those >> deposits, and nasty swirls >> ensued. >> >> In another occasion (using the famous Mother's paste), I was using cheap >> paper towels, and those >> were messing my finish. I learned my lesson, and now only use "expensive" >> paper towels. >> >> So, in your case, I would look for (a) contamination or >> (b)imperfections/roughness on the buffer >> material itself (terry cloth bonnets? wool? felt?). You may need to >> experimet with different >> buffer on a test piece... >> >> Of course, there is the remote chance that you are pickier than I am... >> ;-) >> >> Seriously, I hope this gives you some idea where to look for a fix. >> >> Cheers >> >> Carlos >> >> --- Bill Naumuk wrote: >> >>> Carlos- >>> I can't seem to get the finish I want. I'm directly under >>> fluorescent lights and I wonder >>> if I'm not overdoing it. I'm to the point where I'll be polishing right >>> through the skin if I'm >>> not careful, and still can't get rid of the scratches. >>> Thoughts? >>> Bill Naumuk >>> HDS Fuselage >>> Townville, Pa >> >> >> __________________________________________________ >> http://mail.yahoo.com >> > ________________________________________________________________________________
Date: Dec 03, 2006
From: john butterfield <jdbutterfield(at)yahoo.com>
Subject: stick switches and fuel selector valve
hi list i am trying to decide what switches are really useful on the stick. i am going to use a radio transmit switch and perhaps an elevator trim. are they hard to wire, ect helpful hints are requested also, after looking at my fuel selector valve, it comes with loose screws and there is a reference to greasing the o-ring inside. i tried to pull the nozzle pieces out, but they are in very tight and i don't want to force them if no grease is necessary. the valve is the one supplied with the kit as for our English friend, remember the level of acrimony is inversely related to the level of intelligence of the poster. john butterfield 601XL, corvair torrance, ca ________________________________________________________________________________
From: "Craig Payne" <craig(at)craigandjean.com>
Subject: stick switches and fuel selector valve
Date: Dec 03, 2006
Some have an "Ident" button for their transponder on the stick. I assume they fly in controlled airspace a lot. -- Craig ________________________________________________________________________________
Date: Dec 03, 2006
From: LarryMcFarland <larry(at)macsmachine.com>
Subject: Re: stick switches and fuel selector valve
Hi John, There's a tendency to put switches at the fingertips, but I'd resist more than the transmit switch for the control stick. Trim is a once or twice issue during flight and would place second to transmit activities. The prospect of chasing a broken wire in the control stick after the airworthiness is also a much larger problem if an when it happens. The idea of mixing wires to multifunction switches in the stick are best left to the computer joystick where you can set at a table to fix the errant connection. Being upside down in a 601 isn't a pretty picture. Recommendation is to keep it simple and put your trim switches on the panel near the throttle and the remaining switches in an order that can be memorized easily. I used colored shrink tubing to differentiate pumps from aux battery, the EIS and so forth. The o-ring is fuel proof, was probably greased before assembly and likely will not leak the first 10 years. Being in an aircraft probably suggested long term maintenance. I'd not try to get to it unless it becomes a problem or at least call the manufacturer for tech support. Best regards, Larry McFarland at www.macsmachine.com john butterfield wrote: > > hi list > i am trying to decide what switches are really useful > on the stick. i am going to use a radio transmit > switch and perhaps an elevator trim. are they hard to > wire, ect helpful hints are requested > > also, after looking at my fuel selector valve, it > comes with loose screws and there is a reference to > greasing the o-ring inside. i tried to pull the > nozzle pieces out, but they are in very tight and i > don't want to force them if no grease is necessary. > the valve is the one supplied with the kit > > as for our English friend, remember the level of > acrimony is inversely related to the level of > intelligence of the poster. > > john butterfield > 601XL, corvair > torrance, ca > > ________________________________________________________________________________
From: "Dave Ruddiman" <pacificpainting(at)comcast.net>
Subject: 801 Cargo Pod
Date: Dec 03, 2006
Hello Fellow 801 Builders, (you other guys too) Is the cargo pod I've seen pictures of a custom made installation or are there plans somewhere. I'm not sure if I would need one but there is probably mounting reinforcements that need to be installed in case I decided to. Dave in Salem ________________________________________________________________________________
From: "Edward Moody II" <dredmoody(at)cox.net>
Subject: Re: stick switches and fuel selector valve
Date: Dec 03, 2006
I've had a five button Ray Allen grip on the front stick in an ultralight for 3.5 years without any trouble. I will use a seven buttom version on my left stick and a one button grip on the right stick in my 601XL. The PTT at the 'trigger" position is not one that is easily accidentally activated unless you tend to be a bit clutzy. The elevator and aileron trim button are easy to access and completely intutitve to use. During the progress of a flight I change the trim as the fuel burn changes the CG and as speed changes as well. I expect the same to be true in the 601XL. In addition, I expect to use aileron trim to counter fuel use from the wing tanks. Since the Zodiac is a lot faster and more comfy than the UL, I expect to fly farther and longer on X-C flights. Because of that, I will have the transceiver frequency toggle function and the x-ponder Ident function wired to buttons on the left stick too. These grips are not terribly difficult to wire, they don't screw up in my experience, and the convenience is something I want to have. If you have room on the panel for trim switches and don't mind reaching there for those functions, keep your stick grip simple..... you can even put your ptt buttom there. If you like convenience, get the button-infested type of grip. I like the convenience. Ed Moody II Rayne, LA 601XL/Jabiru/baggage area ----- Original Message ----- From: john butterfield To: Zenith-List Digest Server Sent: Sunday, December 03, 2006 11:28 AM Subject: Zenith-List: stick switches and fuel selector valve hi list i am trying to decide what switches are really useful on the stick. i am going to use a radio transmit switch and perhaps an elevator trim. are they hard to wire, ect helpful hints are requested also, after looking at my fuel selector valve, it comes with loose screws and there is a reference to greasing the o-ring inside. i tried to pull the nozzle pieces out, but they are in very tight and i don't want to force them if no grease is necessary. the valve is the one supplied with the kit as for our English friend, remember the level of acrimony is inversely related to the level of intelligence of the poster. john butterfield 601XL, corvair torrance, ca ________________________________________________________________________________
From: JAPhillipsGA(at)aol.com
Date: Dec 03, 2006
Subject: Re: stick switches and fuel selector valve
I also have the Allen 5 button handle grip on the CIP (left) side with only a PTT button on the right side grip. Dual sticks. The wires are all very fine size and need a protective sleve especialy at the bottom of the sticks. The only recomendation I can make is that I wish I had installed a connector at the bottom of each stick to make removing the sticks easier. Anytime you have to do anything behind the pannel or down at the brakes the stick has to come out to gain access. I did not install a connector when I built and it has been an issue getting "down under." I really like having the four trim buttons on the stick because I don't have to look away from flying or changes my hands to tune the flight. Best regards, Bill of Georgia 601xl - 3300 100 hours ________________________________________________________________________________
From: RURUNY(at)aol.com
Date: Dec 03, 2006
Subject: Re: stick switches and fuel selector valve
I have a PTT Elevator trim up trim down Radio Memory select on right Freq flip from stby to active on left The radio buttons on stick can be changed to an aileron trim easily if I add it later. The right part of the Y stick just gets a PTT. Brian 701 ________________________________________________________________________________
Date: Dec 03, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: stick switches and fuel selector valve
PTT and trim if desired. Pain with all the wiring, I am just doing PTT on stick and trim buttons by the throttle. Juan -----Original Message----- >From: john butterfield <jdbutterfield(at)yahoo.com> >Sent: Dec 3, 2006 12:28 PM >To: Zenith-List Digest Server >Subject: Zenith-List: stick switches and fuel selector valve > > >hi list >i am trying to decide what switches are really useful >on the stick. i am going to use a radio transmit >switch and perhaps an elevator trim. are they hard to >wire, ect helpful hints are requested > >also, after looking at my fuel selector valve, it >comes with loose screws and there is a reference to >greasing the o-ring inside. i tried to pull the >nozzle pieces out, but they are in very tight and i >don't want to force them if no grease is necessary. >the valve is the one supplied with the kit > >as for our English friend, remember the level of >acrimony is inversely related to the level of >intelligence of the poster. > >john butterfield >601XL, corvair >torrance, ca > > > > > ________________________________________________________________________________
Date: Dec 03, 2006
From: Tim & Diane Shankland <tshank(at)core.com>
Subject: Re: Fw: Too picky?
Bill, I don't think you have a temperature problem I did my wings in the unheated attic of my garage in February. They were on the floor and I worked around them with pads on my knees. It was below freezing during part of that time. Tim Shankland Bill Naumuk wrote: > > >> Carlos- >> I found that premade flannel bonnets work much better than >> anything else with my rotary polisher and the rough grits. Now I'm >> down to the final S compound and flannel tucked in under the elastic >> of a wool bonnet and there are certain spots that defy a final shine. >> The flannel loads up in no time, too. I scrap bonnets/swatches when >> they load up- Ma won't hear of putting them in HER washing machine! >> Contamination? After the C stage, I wiped the surface down with >> alcohol and paper towels to remove the excess. >> I'm starting to wonder if my problem is temperature related. My >> shop is heated with a ventless propane garage heater, but I'm >> reluctant to leave it burning when I'm not working. Maybe the >> aluminum is still cold-soaked even though the ambient temperature is >> comfortable. >> Have you noticed anything temperature related? I'll admit that >> with hunting season, getting ready for winter, and routine >> maintenance around the house I haven't been able to get my 13hrs a >> week in on the project but I've been polishing the C section since >> October! >> Bill Naumuk >> HDS Fuselage >> Townville, Pa >> ----- Original Message ----- From: "Carlos Sa" <carlosfsa(at)yahoo.com> >> To: "Bill Naumuk" >> Sent: Saturday, December 02, 2006 10:38 PM >> Subject: Re: Too picky? >> >> >>> Hello, Bill >>> >>> >>> I think I went through that myself, but it was due to my specific >>> working conditions and method: >>> When I was using aluminum polishing compounds, the compound used on >>> the first pass left behind >>> deposits of very fine material (much like sand), and when I used the >>> compound for finishing, >>> since I was working on a flat, horizontal surface, I picked up those >>> deposits, and nasty swirls >>> ensued. >>> >>> In another occasion (using the famous Mother's paste), I was using >>> cheap paper towels, and those >>> were messing my finish. I learned my lesson, and now only use >>> "expensive" paper towels. >>> >>> So, in your case, I would look for (a) contamination or >>> (b)imperfections/roughness on the buffer >>> material itself (terry cloth bonnets? wool? felt?). You may need to >>> experimet with different >>> buffer on a test piece... >>> >>> Of course, there is the remote chance that you are pickier than I >>> am... ;-) >>> >>> Seriously, I hope this gives you some idea where to look for a fix. >>> >>> Cheers >>> >>> Carlos >>> >>> --- Bill Naumuk wrote: >>> >>>> Carlos- >>>> I can't seem to get the finish I want. I'm directly under >>>> fluorescent lights and I wonder >>>> if I'm not overdoing it. I'm to the point where I'll be polishing >>>> right through the skin if I'm >>>> not careful, and still can't get rid of the scratches. >>>> Thoughts? >>>> Bill Naumuk >>>> HDS Fuselage >>>> Townville, Pa >>> >>> >>> >>> __________________________________________________ >>> http://mail.yahoo.com >>> >> > > ________________________________________________________________________________
Date: Dec 03, 2006
From: Brandon Tucker <btucke73(at)yahoo.com>
Subject: RE: N601XT flight photos
If only the plane was as fast as it looks! The guys around here tease me about the flames, but hell, my 4 year old is impressed... I put a couple of hours on the plane today after tinkering with the carburetor and swapping out the temperature sender. The oil temp never broke 200 on climb out, and was between 180 and 190 the whole flight. CHT's were actually a little cool at cruise, until I leaned out the carburetor a bit. I have to adjust it for tomorrow's flight. It is flying very well so far. I'll get some better performance numbers after I wear-in the engine. R/ Brandon --------------------------------- ________________________________________________________________________________
From: Tebenkof(at)aol.com
Date: Dec 04, 2006
Subject: 701 POH
Any kind soul out there who can steer me to an appropriate model for the POH for my 701? The building work is just about done. I just woke up the fact that the paper work is not. Jim Greenough 701 / 99.5321% complete in Portland OR ________________________________________________________________________________
Date: Dec 04, 2006
From: "laurens ackerman" <lackerma(at)gmail.com>
Subject: Grand Rapids Horizon I
Does anyone in this list have any experience with the Grand Rapids Horizon I EFIS and EIS? -- Laurens Ackerman lackerma(at)gmail.com ________________________________________________________________________________
From: "DAVID MILLER" <tigermiller1595(at)msn.com>
Subject: Rotec radial engine?
Date: Dec 04, 2006
Has anybody looked at using one of those 110 hp Rotec radials on a 60 1 XL? Anyone got any knowledge or experience with them or the company ? =0AThanks=0ADave Miller =0A(scratch build 601 XL) ________________________________________________________________________________
From: Afterfxllc(at)aol.com
Date: Dec 04, 2006
Subject: Re: stick switches and fuel selector valve
The supplied fuel selector was shipped without the screws in the right and left line inlets to allow you to rotate them if necessary, If you don't have to rotate them just put the screws back in and hook it up, I had to pull mine out and rotate them so the fittings would be tight and pointed in the right direction. the are hard to pull out and mine had plenty of grease in them already. The reason they rotate is so you don't have to over tighten the fitting and cause damage or crack the housing. Hope this helps. Jeff ________________________________________________________________________________
From: "LRM" <lrm(at)skyhawg.com>
Subject: Re: 701 POH
Date: Dec 04, 2006
Ok, I'm having a brain fart. What's a POH? I may want one or I may already have one. Larry, www.skyhawg.com ----- Original Message ----- From: Tebenkof(at)aol.com To: zenith-list(at)matronics.com Sent: Sunday, December 03, 2006 11:48 PM Subject: Zenith-List: 701 POH Any kind soul out there who can steer me to an appropriate model for the POH for my 701? The building work is just about done. I just woke up the fact that the paper work is not. Jim Greenough 701 / 99.5321% complete in Portland OR ------------------------------------------------------------------------- ----- 11/28/2006 ________________________________________________________________________________
From: "Neitzel" <n963wb(at)frontiernet.net>
Subject: Re: Rotec radial engine?
Date: Dec 04, 2006
Greetings, Seriously considered the Rotec radial for my 701, would really have looked and sounded neat. Talked with representatives while at Oshkosh and they were very informative and had nothing but good comments for their product. At the time there were not a lot of these engines out so not much of a track record. I eventually rejected the radial in favor of the 2200 Jabiru because that installation is 100 pounds lighter. After a long summer of other projects I am finally able to get back to pulling rivets. Need to finish the flaperons and slats then can start final assembly. Dick Neitzel Sayner, WI 701 Jabiru N962WB ________________________________________________________________________________
From: "John Bolding" <jnbolding1(at)teleshare.net>
Subject: Re: 701 POH
Date: Dec 04, 2006
Man , I'm glad I never had any of those !! (yeah, right) Pilot Operating Handbook. LOW&SLOW John Ok, I'm having a brain fart. What's a POH? I may want one or I may already have one. Larry, www.skyhawg.com ----- ________________________________________________________________________________
Subject: Re: 701 POH
From: "Chris Lewis" <christopherlewis(at)earthlink.net>
Date: Dec 04, 2006
There's a 701 Flight Manual "Sample" on the Zenith builder's page for the 701. It's from CZAW and should be a great place to start. Chris in Seattle -------- 701 Scratch Builder Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79033#79033 ________________________________________________________________________________
From: Bryan Martin <bryanmmartin(at)comcast.net>
Subject: Re: 701 POH
Date: Dec 04, 2006
Pilot's Operating Handbook (They used to be called owner's manuals) On Dec 4, 2006, at 10:02 AM, LRM wrote: > Ok, I'm having a brain fart. What's a POH? I may want one or I > may already have one. > > Larry, www.skyhawg.com ________________________________________________________________________________
Subject: Re: 701 POH
Date: Dec 04, 2006
From: nyterminat(at)aol.com
Larry, You are required to have one. Pilot Operating Handbok Bob Spudis -----Original Message----- From: lrm(at)skyhawg.com Sent: Mon, 4 Dec 2006 10:02 AM Subject: Re: Zenith-List: 701 POH Ok, I'm having a brain fart. What's a POH? I may want one or I may already have one. Larry, www.skyhawg.com ----- Original Message ----- From: Tebenkof(at)aol.com Sent: Sunday, December 03, 2006 11:48 PM Subject: Zenith-List: 701 POH Any kind soul out there who can steer me to an appropriate model for the POH for my 701? The building work is just about done. I just woke up the fact that the paper work is not. Jim Greenough 701 / 99.5321% complete in Portland OR href="http://www.aeroelectric.com">www.aeroelectric.com href="http://www.buildersbooks.com">www.buildersbooks.com href="http://www.kitlog.com">www.kitlog.com href="http://www.homebuilthelp.com">www.homebuilthelp.com href="http://www.matronics.com/contribution">http://www.matronics.com/chref="http://www.matronics.com/Navigator?Zenith-List">http://www.matron Date: 11/28/2006 ________________________________________________________________________ ________________________________________________________________________________
From: "Craig Payne" <craig(at)craigandjean.com>
Subject: Forward Skin Access
Date: Dec 04, 2006
Why not post the file to the file archive section of this list? -- Craig ________________________________________________________________________________
Date: Dec 04, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: 701 POH
Dudes, if you go on line or get a DVD disk from zenith, they have a copy of the Chech rotax powered POH. you can use that as a template then inject usefull tidbits of info in your own to customize it. Example" here in florida I put in the POH Pretake off check list "prior to entering active runway, make certain no Alligators in eccess of ten feet in length are on runway", once that is checked I then go to "confirm Coyotes are off the taxiway prior to taxiing to active". True Story to both. Juan -----Original Message----- >From: nyterminat(at)aol.com >Sent: Dec 4, 2006 11:16 AM >To: zenith-list(at)matronics.com >Subject: Re: Zenith-List: 701 POH > >Larry, > >You are required to have one. Pilot Operating Handbok > >Bob Spudis > > >-----Original Message----- >From: lrm(at)skyhawg.com >To: zenith-list(at)matronics.com >Sent: Mon, 4 Dec 2006 10:02 AM >Subject: Re: Zenith-List: 701 POH > > >Ok, I'm having a brain fart. What's a POH? I may want one or I may already have one. > >Larry, www.skyhawg.com >----- Original Message ----- >From: Tebenkof(at)aol.com >To: zenith-list(at)matronics.com >Sent: Sunday, December 03, 2006 11:48 PM >Subject: Zenith-List: 701 POH > > >Any kind soul out there who can steer me to an appropriate model for the POH for my 701? The building work is just about done. I just woke up the fact that the paper work is not. > >Jim Greenough >701 / 99.5321% complete >in Portland OR > > >href="http://www.aeroelectric.com">www.aeroelectric.com >href="http://www.buildersbooks.com">www.buildersbooks.com >href="http://www.kitlog.com">www.kitlog.com >href="http://www.homebuilthelp.com">www.homebuilthelp.com >href="http://www.matronics.com/contribution">http://www.matronics.com/chref="http://www.matronics.com/Navigator?Zenith-List">http://www.matron > > >Date: 11/28/2006 > > >________________________________________________________________________ ________________________________________________________________________________
From: "Al Young" <armyret(at)mchsi.com>
Subject: Re: 701 POH
Date: Dec 04, 2006
Jim- The POH is basically the same as the Information Manual you find in any 172. Contains General info on the aircraft; Normal Op proceedures; Performance; Weight and Bal; System descriptions; handling service & Maintenance; Emerg proceedures etc etc. I bought a great manual from ACFT Spruce a few years ago, but cannot find it in their catalog now. It was Published by Brown Aircraft Supplies of Burbank, CA. It was designed for experimental aircraft, and all you had to do is fill in the blanks basically. I also put my builders log in it and flight test log. If you can find a source for this manual it's more than worth the money. Al Young N601AY ----- Original Message ----- From: Tebenkof(at)aol.com To: zenith-list(at)matronics.com Sent: Sunday, December 03, 2006 11:48 PM Subject: Zenith-List: 701 POH Any kind soul out there who can steer me to an appropriate model for the POH for my 701? The building work is just about done. I just woke up the fact that the paper work is not. Jim Greenough 701 / 99.5321% complete in Portland OR ________________________________________________________________________________
Subject: Re: Rotec radial engine?
From: "Eddie G." <silentlight(at)verizon.net>
Date: Dec 04, 2006
You mean like this? http://www.rotecradialengines.com/customers/MickDye.htm Two other things to keep in mind when chosing Rotec vs an engine like Jabiru: it uses reduction gear and I think it only has a 1000 hour TBO. Eddie Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79095#79095 ________________________________________________________________________________
Date: Dec 04, 2006
From: Jaybannist(at)cs.com
Subject: Forward Skin Access
Craig, Done. According to Dralle, it might not be available for a while. If you want to see it earlier, just let me know. Jay "Craig Payne" wrote: > >Why not post the file to the file archive section of this list? > >-- Craig > > ________________________________________________________________________________
From: "DAVID MILLER" <tigermiller1595(at)msn.com>
Subject: Rotec radial engine?
Date: Dec 04, 2006
Has anybody looked at using one of those 110 hp Rotec radials on a 60 1 XL? Anyone got any knowledge or experience with them or the company ? =0AThanks=0ADave Miller =0A(scratch build 601 XL) ________________________________________________________________________________
Date: Dec 04, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: Rotec radial engine?
Eddie, Niether the rotec nor the Jabiru have GEar reduction, The TBO on the jabiru is 1000 on the top end only. Rotec is a great engine though. Juan -----Original Message----- >From: "Eddie G." <silentlight(at)verizon.net> >Sent: Dec 4, 2006 2:03 PM >To: zenith-list(at)matronics.com >Subject: Zenith-List: Re: Rotec radial engine? > > >You mean like this? >http://www.rotecradialengines.com/customers/MickDye.htm > >Two other things to keep in mind when chosing Rotec vs an engine like Jabiru: it uses reduction gear and I think it only has a 1000 hour TBO. > >Eddie > > >Read this topic online here: > >http://forums.matronics.com/viewtopic.php?p=79095#79095 > > ________________________________________________________________________________
Subject: Re: Rotec radial engine?
From: "Eddie G." <silentlight(at)verizon.net>
Date: Dec 04, 2006
See 1st and 5th bullet from the top. Rotec has a 3:2 Planetary Speed Reduction Unit. http://www.rotecradialengines.com/specs.htm Eddie amyvega2005(at)earthlink. wrote: > Eddie, > Niether the rotec nor the Jabiru have GEar reduction, The TBO on the jabiru is 1000 on the top end only. Rotec is a great engine though. > > Juan > > -- Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79114#79114 ________________________________________________________________________________
From: "Craig Payne" <craig(at)craigandjean.com>
Subject: Re: Rotec radial engine?
Date: Dec 04, 2006
>> Niether the rotec nor the Jabiru have GEar reduction... Oh? http://www.rotecradialengines.com/engdev.htm "It was apparent that the R2800 despite its good direct drive characteristics could benefit from a small amount of propeller speed reduction as is the case with most small capacity engines. Rotec Engineering spent the next period designing and manufacturing their new planetary PSRU which was carefully designed to fit neatly into front nose with minimal disruption to the out side dimensions. They called on the help of well known Australian aero-engineer Bill Whitney to do some calculations regarding the new design. "Bill is simply the best, we are in debt to him, few have his knowledge about all facets of aviation dynamics, he has been very generous in his willingness to help our new company get ahead particularly regarding technical issues". The (PRSU) as mentioned earlier is in planetary configuration, at a reduction ratio of 3:2 so engine revs are relatively low when compared to the high revving ratios other manufactures employ." They are literally trying to wring the last drop of HP from their small capacity engines". Ratios approaching 4:1 are not uncommon amongst some manufactures. The first tests on the new geared R2800 proved to be nothing short of a revelation; the propeller diameter went from the direct drive 68" to 76" with more pitch than before. The PSRU had allowed the R2800 to realise more potential as the engine had 'unloaded', the propeller range had increased dramatically allowing for more user flexibility." -- Craig ________________________________________________________________________________
From: "Craig Payne" <craig(at)craigandjean.com>
Subject: Forward Skin Access
Date: Dec 04, 2006
A number of builders have made almost all of the forward skin removable. For one example take a look at the pictures on Larry's site under "Canopy": www.macsmachine.com -- Craig ________________________________________________________________________________
From: "Craig Payne" <craig(at)craigandjean.com>
Subject: Forward Skin Access
Date: Dec 04, 2006
>> I am also thinking of cutting and trimming the "head chopping" sun leadge on the panel... I'm planning on replacing the whole control panel lip with silicon baffle material. The front skin will stop flush with the control panel. -- Craig ________________________________________________________________________________
Subject: Re: Rotec radial engine?
From: "Eddie G." <silentlight(at)verizon.net>
Date: Dec 04, 2006
I just received my "The 912 Competition" video. It shows how Rotec is put together. Nice workmanship. Looks like almost everything is CNC'ed at their shop. But the planetary gears looks a bit too thin, unless that's a norm in aviation for that size engine. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79127#79127 ________________________________________________________________________________
Date: Dec 04, 2006
From: <dredmoody(at)cox.net>
Subject: Re: Forward Skin Access
To make the aft edge of the forward skin more user friendly you can buy an appropriate length of clear poly tubing at a local hardware store, split it lengthwise, inject it with clear silicon sealer and slip it onto the edge. Cheap, lightweight, easy, and stays put once set. Ed ---- Juan Vega wrote: > > > Jay, > > that looks pertty cool. I like it. I was thinking on putting the entire piece on nutplates so the whole thing would come off. Am I missing something that would not make that possible? I think yours maybe better idea becasue you don't have to remove the canopy. I am also thinking of cutting and trimming the "head chopping" sun leadge on the panel, and replacing it with a leather one like on Cessnas. I found a place that can custom make one for cheap price. ANy thoughts? > > Juan ________________________________________________________________________________
From: "Josh Olson" <mrbizi(at)yahoo.com>
Subject:
Date: Dec 04, 2006
Folks... Does anyone know where I can get a list of what is included in the 2006 CH601XL QBK? (It has to be the 2006 version since the earlier QBKs had less stuff completed from what I can tell.) I want to know exactly what is in the kit and then I want to know exactly what else I'd need to buy/build to get a fully functioning plane. It doesn't seem like I can find that anywhere. I'm looking to build a XL just like the demo one they have on the Zenith website... with these particulars... Jabiru 3300, Dual Dynon displays D100 EFIS, D120 EMS, Trutrack ADI Autopilot w/ Alt hold, Garmin GPSMAP 496, SL30 Nav/Com, GTX330 Transponder, PS Engineering Intercom, BRS Parachute... these items I can find and source... The issue I'm having is getting a detailed list of what comes in the 2006 Quick Build Kit.... I need to know what comes with it (i.e. does upholstery? Its not in the standard kit but the picture of the QBK on the website shows upholstery... what else do I need to get a plane finished and up flying?) Also, does anyone know if the 51% rule would allow me to get a Quick Build Kit and still have a local A&P install my Jabiru 3300 and have a local paint shop paint the plane and still have it qualify for the 51% rule? Thanks, Josh Olson Email: mrbizi(at)yahoo.com ________________________________________________________________________________
Subject: Re: Camera question
From: "Eddie G." <silentlight(at)verizon.net>
Date: Dec 04, 2006
Asking a point and shoot camera to capture 10 megapixels with a small 1/2.5" to 1/1.8" CCD might be too much right now. Most of them do better in the 8 megapixle or less range. Megapixles is not as determining factor for the end photo as are the size of CCD and the type of processor. DSLRs normally have a larger CCD. The one in my EOS 5D is the same size as a 35mm film frame. Depends on how much you want to spend, as far as image quality goes Canon S80, A740 and Fuji E900 would be on the top of my list. See reviews on steves-digicams.com (read his conclusions on each camera). You need to decide for yourself what size, what zoom range (I prefer 28mm in the wide angle because I photograph landscapes), what functions, what kind of memory, what kind of file format, etc. etc. And don't be fooled by things like "Leica" or "Zeiss" written on lenses of Japanese cameras. Most of those lenses are made in Japan, not Germany. As far as point and shoot cameras go Canon, Nikon, Fuji and Olympus are generally good lens manufacturers. Eddie Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79145#79145 ________________________________________________________________________________
From: "Carl Bertrand" <cgbrt(at)mondenet.com>
Subject: Re: 701 POH
Date: Dec 04, 2006
ZAC did provide a POH at one time when you sent in a picture of yopur completed a/c. Given them a try. Carl. 701 ________________________________________________________________________________
Subject: Fuel Tank Ends
From: "Ron Lendon" <rlendon(at)comcast.net>
Date: Dec 04, 2006
Scratch Builders, I am making the end caps for the fuel tanks and wanted to ask others about forming the corners. Should I shrink the metal and have a corner all around? Or, just form the flanges and leave the corners out and fill with weld? I made some parts with 5mm constant flange, but had to anneal the corners to get the 6061 T6 material to flow. The parts look OK just didn't know about fatigue in the corners. What do you think? Pictures attached at the forum -------- Ron Lendon, Clinton Township, MI Corvair Zodiac XL, ScrapBuilder ;-) http://www.mykitlog.com/rlendon Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79162#79162 Attachments: http://forums.matronics.com//files/tank_end1_152.jpeg http://forums.matronics.com//files/tank_end_631.jpeg ________________________________________________________________________________
Date: Dec 04, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: Rotec radial engine?
shit................ I owe you a beer. Do you drink Dos XX? Juan -----Original Message----- >From: Craig Payne <craig(at)craigandjean.com> >Sent: Dec 4, 2006 3:25 PM >To: zenith-list(at)matronics.com >Subject: RE: Zenith-List: Re: Rotec radial engine? > > >>> Niether the rotec nor the Jabiru have GEar reduction... > >Oh? > >http://www.rotecradialengines.com/engdev.htm > >"It was apparent that the R2800 despite its good direct drive >characteristics could benefit from a small amount of propeller speed >reduction as is the case with most small capacity engines. Rotec Engineering >spent the next period designing and manufacturing their new planetary PSRU >which was carefully designed to fit neatly into front nose with minimal >disruption to the out side dimensions. They called on the help of well known >Australian aero-engineer Bill Whitney to do some calculations regarding the >new design. "Bill is simply the best, we are in debt to him, few have his >knowledge about all facets of aviation dynamics, he has been very generous >in his willingness to help our new company get ahead particularly regarding >technical issues". > >The (PRSU) as mentioned earlier is in planetary configuration, at a >reduction ratio of 3:2 so engine revs are relatively low when compared to >the high revving ratios other manufactures employ." They are literally >trying to wring the last drop of HP from their small capacity engines". >Ratios approaching 4:1 are not uncommon amongst some manufactures. > >The first tests on the new geared R2800 proved to be nothing short of a >revelation; the propeller diameter went from the direct drive 68" to 76" >with more pitch than before. The PSRU had allowed the R2800 to realise more >potential as the engine had 'unloaded', the propeller range had increased >dramatically allowing for more user flexibility." > >-- Craig > > ________________________________________________________________________________
Date: Dec 04, 2006
From: LarryMcFarland <larry(at)macsmachine.com>
Subject: Re: Forward Skin Access
Juan, You needn't use nut plates for such a panel. J-nuts that work with 6-32 screws can be used with considerable confidence. They are much cheaper and don't let go. I've got them on my removable forward top skin and I've had the top off probably a dozen times in two years and 85 hours of flying my 601. On the leading edge overhanging the panel, I bent a piece of 1/2-inch aluminum tube and used a Dremel cutter to cut a slit on the edge and used 4 bent tabs to secure it with the same screws that hold the forward top skin. It's a much easier job, as you use almost 90 screws, but very secure and the screws blend into the rivet heads. http://www.macsmachine.com/images/largeassembly2/full/uclips.gif http://www.macsmachine.com/images/cowling/full/firstcowlfitting.gif http://www.macsmachine.com/images/completion/full/601ezclosefrtrt.gif Larry McFarland - 601HDS at www.macsmachine.com Juan Vega wrote: > > > Jay, > > that looks pertty cool. I like it. I was thinking on putting the entire piece on nutplates so the whole thing would come off. Am I missing something that would not make that possible? I think yours maybe better idea becasue you don't have to remove the canopy. I am also thinking of cutting and trimming the "head chopping" sun leadge on the panel, and replacing it with a leather one like on Cessnas. I found a place that can custom make one for cheap price. ANy thoughts? > > Juan > ________________________________________________________________________________
Date: Dec 04, 2006
From: LarryMcFarland <larry(at)macsmachine.com>
Subject: Re: Fuel Tank Ends
Ron, A nice shape to work with, but I'd reverse the ends placing the flanges under the main skins as you've done so that the heat you put into welding is better distributed between the cap flange and the edge of the main skins. 6061-T6 is not the best material for a tank as applies to a welded construct. 5052-H32 is ideal as it's yield to work hardening is better for holding its shape. You're corners will fill easily the way you've got them, but if reversed, a little easier. You can put more material into the weld if you've got 1/8-inch of drum hanging outside the main skin edge and the edge won't burn away so readily as the edge weld of a typical flange- weld would. Practice a lot before you ruin the first set of tanks by making sample welds to proof your skills or that of the guy you entrust to the job. I welded the tanks with clecos and then removed the clecos one by one and welded them shut. If you want to make the job of welding much easier, make the ends out of .040 if you haven't already as less than that is difficult to control heat- distortion and get consistent welds. Best of luck, Larry McFarland - 601HDS at www.macsmachine.com Ron Lendon wrote: > > Scratch Builders, > > I am making the end caps for the fuel tanks and wanted to ask others about forming the corners. Should I shrink the metal and have a corner all around? Or, just form the flanges and leave the corners out and fill with weld? > > I made some parts with 5mm constant flange, but had to anneal the corners to get the 6061 T6 material to flow. The parts look OK just didn't know about fatigue in the corners. > > What do you think? > > Pictures attached at the forum > > -------- > Ron Lendon, Clinton Township, MI > Corvair Zodiac XL, ScrapBuilder ;-) > http://www.mykitlog.com/rlendon > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=79162#79162 > > > Attachments: > > http://forums.matronics.com//files/tank_end1_152.jpeg > http://forums.matronics.com//files/tank_end_631.jpeg > ________________________________________________________________________________
Date: Dec 04, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: Forward Skin Access
great website by the way, you need to send me the plans for that kick ass recumbant Bike! Do you have close up pics of the portion of the turtle deck you riveted, the very end pieces adjacent to the canopy screw. I like your idea. Juan -----Original Message----- >From: LarryMcFarland <larry(at)macsmachine.com> >Sent: Dec 4, 2006 8:09 PM >To: zenith-list(at)matronics.com >Subject: Re: Zenith-List: Forward Skin Access > > >Juan, >You needn't use nut plates for such a panel. J-nuts that work with 6-32 >screws can be used with considerable confidence. They are much cheaper >and don't let go. I've got them on my removable forward top skin and >I've had the top off probably a dozen times in two years and 85 hours of >flying my 601. On the leading edge overhanging the panel, I bent a >piece of 1/2-inch aluminum tube and used a Dremel cutter to cut a slit >on the edge and used 4 bent tabs to secure it with the same screws that >hold the forward top skin. >It's a much easier job, as you use almost 90 screws, but very secure and >the screws blend into the rivet heads. > >http://www.macsmachine.com/images/largeassembly2/full/uclips.gif >http://www.macsmachine.com/images/cowling/full/firstcowlfitting.gif >http://www.macsmachine.com/images/completion/full/601ezclosefrtrt.gif > >Larry McFarland - 601HDS at www.macsmachine.com > >Juan Vega wrote: >> >> >> Jay, >> >> that looks pertty cool. I like it. I was thinking on putting the entire piece on nutplates so the whole thing would come off. Am I missing something that would not make that possible? I think yours maybe better idea becasue you don't have to remove the canopy. I am also thinking of cutting and trimming the "head chopping" sun leadge on the panel, and replacing it with a leather one like on Cessnas. I found a place that can custom make one for cheap price. ANy thoughts? >> >> Juan >> > > ________________________________________________________________________________
From: Tebenkof(at)aol.com
Date: Dec 04, 2006
Subject: Re: 701 POH
Thanks for all the help with the POH. POO ON HOOD was enlighteningl, and the other ideas even better. Jim ________________________________________________________________________________
Date: Dec 04, 2006
From: Tim & Diane Shankland <tshank(at)core.com>
Subject: New information
Some time back there were several threads on a couple of topics, one was whether the prop would windmill with he engine off and another on how well the 601 glided with a stopped prop. I now find myself in a more knowledgeable position on these topics. Last Saturday I was returning from an uneventful test flight on my 601HD. I have 25 hours on it and I had flown a three airport round robin of about 1 1/2 hours. I had just announced that I was entering downwind on my home airport and there was that smell you never want to smell, smoke in the airplane. I had the heater near full on, it was in the 30's (F) at altitude and had a good air flow I quickly also open the pilot side vent. My Stratus Suburu is set up with two batteries and all switches are two position center off rockers so I can load either BUS A or BUS B. The ignition switch with the primary ignition and fuel pump was on BUS A the secondary ignition was on BUS B. The secondary fuel pump was still off since I hadn't gotten into the pattern yet. When the smoke started I tried turning off BUS B, the engine faltered, I turned it back on the it picked up again only to stop a few seconds later. The good thing was that the smoke had started to dissipate and it was real quiet in the airplane I tried the ignition key to restart but the started wouldn't work. Since by this time I was about 900 feet above the ground and with the runway off to the left of the airplane I quit working with the engine and decided to land the airplane. I Called to all traffic that I was executing a dead stick approach , fortunately there was no one in the pattern. I must say that I did one of my better landing and coasted off at the intersection on on to the taxi way. Since apparently no one at the airport was listening to the radio no one came out so I just grabbed my wounded bird by the prop and walked to back to the terminal. Now for my observations, first NOTHING will get your attention like smoke second there is something surreal when the prop stops turning and your still in the air Additional observations I was doing between 80 and 90 mph when the engine quit, the prop stopped and did not windmill, maybe it will at higher speed but I wasn't going to give away any altitude to find out. The 601 HD glided better this the engine stopped then it does with a low RPM, it really landed very nicely and I may experiment with more very low RPM landings. As for what happened, I opened up the top of the panel tonight and it was one of those how could that ever happen things. A plug that I use connect to two switches in my canopy for an alarm panel got its open back side positioned to touch on unused terminal on the ignition switch that was obviously hot. That caused a ground through that wire. I hadn't put a circuit breaker in the primary ignition circuit because of a concern I had for false tripping, I am going to add one because having the engine stop with no smoke is preferable to stopping with smoke. I am also going to add a emergency starter circuit, I already have a separate ignition and fuel pump circuit but since engine wind milling is not assured I want to be able to do all engine functions independent of the primary ignition circuit. The short only burned for a few seconds then a small wire in that circuit burned open. this cut all power to the primary ignition and fuel circuit, since the secondary ignition was on the engine continued but without the secondary fuel pump it soon quit. Without a starter available it was not possible to restart the engine. Anyway when I got home my wife asked how everything went, and I told her I had some excitement, she never likes it when I say that. Tim Shankland ________________________________________________________________________________
Date: Dec 04, 2006
From: LarryMcFarland <larry(at)macsmachine.com>
Subject: Re: Forward Skin Access
Juan, I built the bike with my daughter when I was teaching her to gas weld this summer. It's a freehand design from three bikes. The piece you speak of is well photographed in the canopy pages. The j-nuts were purchased from McMaster-Carr and I'll get the numbers for you tomorrow morning. These j-nuts cost about $10.00 per package of 50. Larry Juan Vega wrote: > > great website by the way, you need to send me the plans for that kick ass recumbant Bike! > Do you have close up pics of the portion of the turtle deck you riveted, the very end pieces adjacent to the canopy screw. I like your idea. > > Juan > -----Original Message----- > >> From: LarryMcFarland <larry(at)macsmachine.com> >> Sent: Dec 4, 2006 8:09 PM >> To: zenith-list(at)matronics.com >> Subject: Re: Zenith-List: Forward Skin Access >> >> >> >> Juan, >> You needn't use nut plates for such a panel. J-nuts that work with 6-32 >> screws can be used with considerable confidence. They are much cheaper >> and don't let go. I've got them on my removable forward top skin and >> I've had the top off probably a dozen times in two years and 85 hours of >> flying my 601. On the leading edge overhanging the panel, I bent a >> piece of 1/2-inch aluminum tube and used a Dremel cutter to cut a slit >> on the edge and used 4 bent tabs to secure it with the same screws that >> hold the forward top skin. >> It's a much easier job, as you use almost 90 screws, but very secure and >> the screws blend into the rivet heads. >> >> http://www.macsmachine.com/images/largeassembly2/full/uclips.gif >> http://www.macsmachine.com/images/cowling/full/firstcowlfitting.gif >> http://www.macsmachine.com/images/completion/full/601ezclosefrtrt.gif >> >> Larry McFarland - 601HDS at www.macsmachine.com >> >> Juan Vega wrote: >> >>> >>> >>> Jay, >>> >>> that looks pertty cool. I like it. I was thinking on putting the entire piece on nutplates so the whole thing would come off. Am I missing something that would not make that possible? I think yours maybe better idea becasue you don't have to remove the canopy. I am also thinking of cutting and trimming the "head chopping" sun leadge on the panel, and replacing it with a leather one like on Cessnas. I found a place that can custom make one for cheap price. ANy thoughts? >>> >>> Juan >>> >>> >> >> >> >> >> ________________________________________________________________________________
From: "john H" <professor71(at)HOTMAIL.COM>
Subject: 912 Oil Leak
Date: Dec 04, 2006
Hi List I have a very small oil leak on a 912 (200hrs) which is aggravating the heck out of me. After flying I have a little oil showing up around the fuel pump, around the gear box and blowing back on the battery box on the firewall. I just can't seem to find the leak. Oil pressure is fine. Any ideas anyone?? Thanks John _________________________________________________________________ Stay up-to-date with your friends through the Windows Live Spaces friends list. ________________________________________________________________________________
Date: Dec 05, 2006
From: Peter Chapman <pchapman(at)ionsys.com>
Subject: 801 inflight breakup in 2003
Just from what I've read here on the list (and archives), the accident is still a little mysterious and perhaps a bit of a sore spot in that there's little evidence available to support different theories. On the one hand there's still suspicion about the elevator extension, on the other hand it may just be the pilot playing around and overstressing the aircraft. The NTSB documents are pretty sparse. (# LAX03FA102) They don't go into any detail at all, and there was no interest even in describing any probable breakup sequence. It is also difficult to interpret the NTSB's description of damage to various parts, as to which direction the wing and tail parts failed. The elevator extension is mentioned but not commented on. The Factual Report quotes an FAA publication, stating "Amateur builders are free to develop their own designs or build from existing designs. We do not approve these designs and it would be impractical to develop design standards for the wide variety of design configurations, created by designers, kit manufacturers, and amateur builders." So in the end they are seem to be saying, "looking at the structural failure in detail is not our problem". The NTSB report didn't state that the pilot was "heavily impaired by narcotics", but said that chemical traces were consistent with smoking at least one joint within 12 hours. They were trying to be somewhat precise, since for the passenger, they said the same but within 2 hours. So unless there's other evidence, I wouldn't call the pilot "heavily" impaired, although one can still make inferences about his attitude towards the flight if one wishes. Back when the accident happened, it sounded like Ben Haas was hoping to examine the wreckage or otherwise get further info from the investigators, but I guess no further info could be obtained? Presumably Zenair had nothing more to add? Maybe the importance of all this is less now for 801 owners, given that there's a newer design extended horizontal tail (stab & elevator) that presumably is beefed up over both the original short span tail and the Flypass elevator extansion? I don't have any particular angle on all this; I was just curious about the implications of a couple recent posts mentioning the accident. Peter Chapman Toronto, ON ________________________________________________________________________________
From: "Dave Ruddiman" <pacificpainting(at)comcast.net>
Subject: 801 Elevator Extension
Date: Dec 04, 2006
I don't want to get anything started, but what's this about an elevator extension? I've heard here and there that 801's run out of elevator on landing. I don't know if it's true or not since mine's not done yet. I got my tail this year. Are the newest tails different than the previous ones. Would someone fill me in please? Dave in Salem ________________________________________________________________________________
From: "Tom Faulkner" <tomtafcor(at)triton.net>
Subject: 801 Elevator Extension
Date: Dec 05, 2006
Dave: Zenith added about 6" on each end of the 801 stabilizer about May 2004. I decided to go that route even though I had my stab already done. I made the first one as a test for Zenith. I never flew with the shorter stab, so have no comparison. Zenith also up graded their demo to the new size. The reason given for the change was that most builders were using larger engines with more weight. Tom Faulkner N801TP ________________________________________________________________________________
From: Trevor Page <webmaster(at)upac.ca>
Subject: Re: 912 Oil Leak
Date: Dec 05, 2006
Perhaps a bad seal on the PTO? Have you checked the gasket on the fuel pump housing? The fuel pump is driven by the gearbox so maybe you have a leak there.. Trev Page C-IDUS 601HD R912 On Dec 4, 2006, at 11:55 PM, john H wrote: > > Hi List > I have a very small oil leak on a 912 (200hrs) which is aggravating > the heck out of me. After flying I have a little oil showing up > around the fuel pump, around the gear box and blowing back on the > battery box on the firewall. I just can't seem to find the leak. > Oil pressure is fine. Any ideas anyone?? > Thanks > John > > _________________________________________________________________ > Stay up-to-date with your friends through the Windows Live Spaces > friends list. > > ________________________________________________________________________________
Date: Dec 05, 2006
From: William Dominguez <bill_dom(at)yahoo.com>
Subject: Question for gas welders.
What type of filler rods should be used to gas weld 6061-T6? I need to start practicing my welds so I have the skills developed by the time I have to make my tanks sometime next year. William Dominguez Zodiac 601XL Plans Miami Florida --------------------------------- ________________________________________________________________________________
From: "Carl Bertrand" <cgbrt(at)mondenet.com>
Subject: Re: 912 Oil Leak
Date: Dec 05, 2006
Hi John, Had a simmilar problem and traced it to the fuel pump gasket/spacer. A dab of hi temp sealer solved the problem. Carl 701 912 with 450 hrs. ________________________________________________________________________________
From: "Dave Ruddiman" <pacificpainting(at)comcast.net>
Subject: Re: 801 Elevator Extension
Date: Dec 05, 2006
Hi Tom, Thanks for the information. I was getting one part mixed up with the other. I was thinking that the elevator itself was extended back. Like the nose to the trailing edge, where the trim tab goes, was made longer. Is running out of elevator on landing a "real" issue. Seems like if it is, it would hamper any really short landings. What's your experience? Dave ----- Original Message ----- From: Tom Faulkner To: zenith-list(at)matronics.com Sent: Tuesday, December 05, 2006 5:30 AM Subject: RE: Zenith-List: 801 Elevator Extension Dave: Zenith added about 6" on each end of the 801 stabilizer about May 2004. I decided to go that route even though I had my stab already done. I made the first one as a test for Zenith. I never flew with the shorter stab, so have no comparison. Zenith also up graded their demo to the new size. The reason given for the change was that most builders were using larger engines with more weight. Tom Faulkner N801TP ________________________________________________________________________________
From: "n801bh(at)netzero.com" <n801bh(at)netzero.com>
Date: Dec 05, 2006
Subject: Re: 801 inflight breakup in 2003
Within a week of the accident I called the LA division of the Faa that w as doing the investigation, Spoke with the lead guy and he went strictly by the protocal and didn't speculate on the crash. I told him I was a c urrent builder and was asking some questions for about a dozen other bui lders. He did say and I quote " if you are building one of thses planes I would be VERY concerned". My next question to him was, can I look over the wreckage either by myself or with you present, he said they were a bout to conclude their inspection of the wreckage and that I would need to contact the next of kin for permission. The 17 year old daughter was not in a frame of mind to even talk to so I called the airplane wrecking yard that the debris was in. He told me that if I pay the, at that time , current charges of retrieval and storage which was then 1845.00$ I cou ld come look at it and then to call the insurance company to try to buy the stuff. They never called back.... and I never drove to California to look. Several of us 801 builders almost daily chatted on Yahoo messenger so we set up a group chat and brainstormed for several hours on what we knew. I did call the TV reporter who flew ovewr the site and filmed the wreck age for the evening news, he was a 5000+ pilot and knew what he was talk ing about. Our concensis of the senerio was this, the plane was probabl;y doing aer obatics, most probably a loop, as all the 801 builders know the elevator is fastened on by a single pivot bolt in the middle and two little pins on each end. Those pins are captured by those this aluminum triangle pi eces riveted on to the end of the Horizontal stabilizer. The loading of the elevator sheared off the the tip extensions, that sent the the eleva tor and probably the horizontal stabilizer into the rudder, shearing it off, the plane then instantly went nose down, then failed both wings in the negative G axis and the fuselage then lawn darted another two+ miles till it hit the farm field. It was hard for us to believe how a plane t hat flies at maybe 100mph could scatter itself over that wide of an area but the 14,000 agl that Mark mentioned explains that. What apparently happened when ZAC introduced the 'NEW" larger horizontal stab was to use a longer spar to carry the load, not just add on tip ex tensions. signs and it would be impractical to develop design standards for the wide variety of design configurations, created by designers, kit manufacturers, and amateur builders." So in the end they are seem to be saying, "looking at the structural failure in detail is not our problem". The NTSB report didn't state that the pilot was "heavily impaired by narcotics", but said that chemical traces were consistent with smoking at least one joint within 12 hours. They were trying to be somewhat precise, since for the passenger, they said the same but within 2 hours. So unless there's other evidence, I wouldn't call the pilot "heavily" impaired, although one can still make inferences about his attitude towards the flight if one wishes. Back when the accident happened, it sounded like Ben Haas was hoping to examine the wreckage or otherwise get further info from the investigators, but I guess no further info could be obtained? Presumably Zenair had nothing more to add? Maybe the importance of all this is less now for 801 owners, given that there's a newer design extended horizontal tail (stab & elevator) that presumably is beefed up over both the original short span tail and the Flypass elevator extansion? I don't have any particular angle on all this; I was just curious about the implications of a couple recent posts mentioning the accident. Peter Chapman Toronto, ON ======================== =========== ======================== =========== ======================== ===========

Within a week of the accident I called the LA division of the F aa that was doing the investigation, Spoke with the lead guy and he went strictly by the protocal and didn't speculate on the crash. I told him I was a current builder and was asking some questions for about a dozen other builders. He did say and I quote " if you are building one of thse s planes I would be VERY concerned". My next question to him was, can I look over the wreckage either by myself or with  you present, he sa id they were about to conclude their inspection of the wreckage and that I would need to contact the next of kin for permission. The 17 year old daughter was not in a frame of mind to even talk to so I called the air plane wrecking yard that the debris was in. He told me that if I pay the , at that time, current charges of retrieval and storage which was then 1845.00$ I could come look at it and then to call the insurance company to try to buy the stuff. They never called back.... and I never drove to California to look.

Several of us 801 builders almost daily chatted on Yahoo messenger so we set up a group chat and brainstormed for several hours on what we kn ew. I did call the TV reporter who flew ovewr the site and filmed the wr eckage for the evening news, he was a 5000+ pilot and knew what he was t alking about.

Our concensis of the senerio was this, the plane was probabl;y doing aerobatics, most probably a loop, as all the 801 builders know the eleva tor is fastened on by a single pivot bolt in the middle and two little p ins on each end. Those pins are captured by those this aluminum triangle pieces riveted on to the end of the Horizontal stabilizer. The loading of the elevator sheared off the the tip extensions, that sent the the el evator and probably the horizontal stabilizer into the rudder, shearing it off, the plane then instantly went nose down, then failed both wings in the negative G axis and the fuselage then lawn darted another two+ mi les till it hit the farm field. It was hard for us to believe how a plan e that flies at maybe 100mph could scatter itself over that wide of an a rea but the 14,000  agl that Mark mentioned explains that.

What apparently happened when ZAC introduced the 'NEW" larger horizon tal stab was to use a longer spar to carry the load, not just add on tip extensions.


























signs and it&n bsp;would be impractical to develop 
design& nbsp;standards for the wide variety of des ign configurations, 
created by designers, k it manufacturers, and amateur builders."   So 
in the end they are seem to&nb sp;be saying, "looking at the structural < BR>failure in detail is not our problem".< BR>
The NTSB report didn't state that t he pilot was "heavily impaired by 
narc otics", but said that chemical traces were  consistent with 
smoking at least one& nbsp;joint within 12 hours. They were tryi ng to be 
somewhat precise, since for&n bsp;the passenger, they said the same but& nbsp;
within 2 hours. So unless there's  ;other evidence, I wouldn't call the 
p ilot "heavily" impaired, although one can  still make inferences 
about his attitude&nb sp;towards the flight if one wishes.

Bac k when the accident happened, it sounded&n bsp;like Ben Haas was hoping 
to examin e the wreckage or otherwise get further&nb sp;info from the 
investigators, but I  guess no further info could be obtained?&n bsp;
Presumably Zenair had nothing more to&n bsp;add?

Maybe the importance of all thi s is less now for 801 owners, given&n bsp;
that there's a newer design extended&nb sp;horizontal tail (stab & 
elevator) th at presumably is beefed up over both  the original short 
span tail and the&n bsp;Flypass elevator extansion?

I don't have& nbsp;any particular angle on all this; I&n bsp;was just curious 
about the implications  of a couple recent posts mentioning  the accident.


Peter Chapman
Toronto, ON&nbs ========================        -- Please Support&nb p;        (And Get Som ;November is the Annual List Fund Raiser.&  link below to find out more about




      
      
      
________________________________________________________________________________
Date: Dec 05, 2006
From: N5SL <nfivesl(at)yahoo.com>
Subject: Re: Question for gas welders.
William:=0A=0AHere's my advice on building your own tanks - Make them thic ker and take them to someone to have them TIG-welded. Or buy a TIG welder and do it yourself. =0A=0AI made mine to the plans and every welder I talk ed to wanted them thicker. I finally found a guy who did a great job on th em but advised next time to make them thicker. Gas welding them would be a real trick. I can gas weld steel just fine, but aluminum is really tricky and I've managed to ruin several pieces of aluminum with gas-welding. =0A =0AMost of the advice I received was to make them .050" minimum. I've look ed at other aluminum wing tanks and they are at least .050" thick. =0A=0AF ind a local welder (like a speed shop) and get some advice before buying yo ur aluminum for the tanks. =0A=0AGood luck,=0A=0AScott Laughlin=0AHack wel der=0AOmaha, Nebraska=0A601XL/Corvair=0Awww.cooknwithgas.com=0A=0A----- Ori ginal Message ----=0AFrom: William Dominguez <bill_dom(at)yahoo.com>=0A=0ASubj ect: Zenith-List: Question for gas welders.=0A=0A What type of filler ro ds should be used to gas weld 6061-T6?=0A=0A=0A=0A=0A=0A=0A =0A____________ ________________________________________________________________________=0A Need a quick answer? Get one in minutes from people who know.=0AAsk your qu estion on www.Answers.yahoo.com ________________________________________________________________________________
Date: Dec 05, 2006
From: LarryMcFarland <larry(at)macsmachine.com>
Subject: Re: Question for gas welders.
William, Try a 4043 or a 5356 filler rod for what you're doing. You'll find gas welding is very much like riding a unicycle in the dark and it takes a little more practice as you've got to be very quick in recognizing the puddle. I burned up a 4 x 8 sheet of aluminum learning to weld with the torch and only made one tank. If you have any resources to purchase a TIG welder, I'd highly recommend it. They have become much cheaper to own and operate as well as providing excellent welds on mounts, gear and the like. I'd also recommend you use 5052-H32 aluminum of .040 to .050 thickness in lieu of 6061-T6. It's a much better alloy for a tank and a little less costly material. Larry McFarland - 601HDS with 3 TIG welded tanks at www.macsmachine.com William Dominguez wrote: > What type of filler rods should be used to gas weld 6061-T6? > I need to start practicing my welds so I have the skills developed by > the time I have to make my tanks sometime next year. > > William Dominguez > Zodiac 601XL Plans > Miami Florida > > * > > > * ________________________________________________________________________________
From: "Tom Faulkner" <tomtafcor(at)triton.net>
Subject: 801 stabilizer
Date: Dec 05, 2006
Is running out of elevator on landing a "real" issue. Seems like if it is, it would hamper any really short landings. What's your experience? Dave: I have had no problem with lack of elevator. The trick is the proper use of power at flare and getting the speed down on approach. Tom ________________________________________________________________________________
Subject: Re: New information
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Dec 05, 2006
Good piloting Tim. -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79320#79320 ________________________________________________________________________________
Date: Dec 05, 2006
From: Paul Mulwitz <p.mulwitz(at)worldnet.att.net>
Subject: Re: Question for gas welders.
Hi William, This sounds like a good question for your welding supply house. The really important part of welding aluminum is a combination of a huge flame (because the aluminum conducts heat just as well as electricity) and to keep oxygen from the joint. I have never tried this task, but I suspect you need a heavily reducing mixture of gases. Good luck, Paul XL fuselage At 05:51 AM 12/5/2006, you wrote: >What type of filler rods should be used to gas weld 6061-T6? >I need to start practicing my welds so I have the skills developed >by the time I have to make my tanks sometime next year. > >William Dominguez >Zodiac 601XL Plans >Miami Florida > > --------------------------------------------- ________________________________________________________________________________
Date: Dec 05, 2006
From: Johns optonline account <jfmasell(at)optonline.net>
Subject: Question for gas welders.
I finally decided to rivet my tanks and am doing so now. If you would like to see pics I would be glad to put on list. I am using Pro-Seal and Rivets foe all parts I have done the fittings for two tanks and now I am starting to rivet the body. John Maselli Still building ST801 on Long Island NY East Moriches Spadaro's Intl Airport -----Original Message----- From: owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com]On Behalf Of LarryMcFarland Sent: Tuesday, December 05, 2006 10:35 AM Subject: Re: Zenith-List: Question for gas welders. William, Try a 4043 or a 5356 filler rod for what you're doing. You'll find gas welding is very much like riding a unicycle in the dark and it takes a little more practice as you've got to be very quick in recognizing the puddle. I burned up a 4 x 8 sheet of aluminum learning to weld with the torch and only made one tank. If you have any resources to purchase a TIG welder, I'd highly recommend it. They have become much cheaper to own and operate as well as providing excellent welds on mounts, gear and the like. I'd also recommend you use 5052-H32 aluminum of .040 to .050 thickness in lieu of 6061-T6. It's a much better alloy for a tank and a little less costly material. Larry McFarland - 601HDS with 3 TIG welded tanks at www.macsmachine.com William Dominguez wrote: > What type of filler rods should be used to gas weld 6061-T6? > I need to start practicing my welds so I have the skills developed by > the time I have to make my tanks sometime next year. > > William Dominguez > Zodiac 601XL Plans > Miami Florida > > * > > > * ________________________________________________________________________________
Date: Dec 05, 2006
From: John Collins <oldguyflier(at)yahoo.com>
Subject: 601 Landing Gear Height
Hello, List, In the latest "EAA Sport Pilot", in the cover article on the CH601XL, the reviewer discusses the landing manners. He says that the AMD planes have a taller gear than the plans-built version, allowing better full-stall landings. Does anyone on the list know that this is true, and what the difference is? Does anyone know the dimensions of the Aircraft Spruce composite gear? Who makes their gear? (the guy who answered the phone at AS had no idea) I am exploring landing gear options, as well as the use of vortex generators. They allow a higher angle of attack, which requires a higher deck angle on landing to be of use there, so landing gear hieght is important there, too. Thanks in advance, John Collins --------------------------------- ________________________________________________________________________________
Date: Dec 05, 2006
From: Brandon Tucker <btucke73(at)yahoo.com>
Subject: RE: Question for gas welders.
I TIG welded my LE tanks and my header tank. I made the wing tanks out of 5052 .032, and the header tank out of 6061 .025 (as per plans). If I were to do it all again, I would make them out of at least .040. I did notice that 5052 was slightly easier to weld, but was a full time 6061 welder as a teenager, so it was not a problem. The problem is how thin the material is. Thicker is MUCH easier. I used to weld aluminum soda cans together for fun, but can barely get a nice bead on .025 now. Go thicker - the weight penalty for this size of tank is neglegible. VR/ Brandon Tucker --------------------------------- Any questions? Get answers on any topic at Yahoo! Answers. Try it now. ________________________________________________________________________________
Subject: Re: Fuel Tank Ends
From: "Ron Lendon" <rlendon(at)comcast.net>
Date: Dec 05, 2006
Larry and Wayne, The print shows the edges coming together like the picture below and has a notation "BEAD WELD ALL FLANGE SEAMS". This should make it easier to fuse the materials while adding filler rod and it should also make a really strong joint. I'm not to sure about the methods you are speaking of so I will probally make it like the print. I am still open for suggestions. -------- Ron Lendon, Clinton Township, MI Corvair Zodiac XL, ScrapBuilder ;-) http://www.mykitlog.com/rlendon Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79427#79427 ________________________________________________________________________________
From: JAPhillipsGA(at)AOL.COM
Date: Dec 05, 2006
Subject: Re: New information
Tim, for all us that have not experienced your event yet let me say we are all glad and happy you made it okay ! Best regards and get her back up, Bill of Georgia 601XL-3300 100 hours ________________________________________________________________________________
Date: Dec 05, 2006
From: LarryMcFarland <larry(at)macsmachine.com>
Subject: Wing walk tread strip
Hi guys, I'm looking at a roll of adhesive backed tread strip that has to be cut to three pieces to fit my wing walks and grumbling about how grossly coarse the grit is and wishing there were a better alternative. The black looks correct, but I've concerns about it staying where it is put and the grit coming loose. I should have purchased it this week instead of 3 years ago and now have doubts about its adhesive as well. Does anyone have a tread strip that they're happy with? Something that once on has had no qualms about it being too rough or hard to keep its shape year after year. I'd like to hear from anyone who's applied it and feel they've purchased the right stuff. Larry McFarland - 601HDS at www.macsmachine.com ________________________________________________________________________________
From: "john H" <professor71(at)HOTMAIL.COM>
Subject: Wing walk tread strip
Date: Dec 05, 2006
Hi Larry I used skateboard grip tape. It has held great for 2 years now. I went with clear but should have used black. Clear doesnt stay clear for long. I got the stuff at blackholeboards.com at least I think that was the link. Relatively inexpensive too. Regards John >From: LarryMcFarland <larry(at)macsmachine.com> >Reply-To: zenith-list(at)matronics.com >To: zenith-list(at)matronics.com >Subject: Zenith-List: Wing walk tread strip >Date: Tue, 05 Dec 2006 19:14:44 -0600 > > >Hi guys, >I'm looking at a roll of adhesive backed tread strip that has to be cut to >three pieces >to fit my wing walks and grumbling about how grossly coarse the grit is and >wishing >there were a better alternative. The black looks correct, but I've concerns >about it staying >where it is put and the grit coming loose. I should have purchased it this >week instead of >3 years ago and now have doubts about its adhesive as well. > >Does anyone have a tread strip that they're happy with? Something that >once on has had >no qualms about it being too rough or hard to keep its shape year after >year. I'd like to hear >from anyone who's applied it and feel they've purchased the right stuff. > >Larry McFarland - 601HDS at www.macsmachine.com > > _________________________________________________________________ Get free, personalized commercial-free online radio with MSN Radio powered by Pandora http://radio.msn.com/?icid=T002MSN03A07001 ________________________________________________________________________________
Subject: Re: 601 Landing Gear Height
From: "leinad" <leinad(at)hughes.net>
Date: Dec 05, 2006
John I bought and plan to use the ACS composite gear for my XL, but I have to say that in hind sight, it was probably a mistake. You are right, the gear is not the same dimensions. It's just a tad taller, and MUCH narrower. If I've done my calculations right the XL plans call for a gear that is 18 1/4" tall. The composite gear will is 19 3/4" tall. The plans call for a gear 77 1/2 inches wide, while the composite gear is only 69 1/2" wide if you follow the manufacturers installation instructions (which by the way are scant). In my opinion it is questionable to call this an XL landing gear as it takes a significant design change to install the gear, as it comes in 2 parts which must be bolted to the air frame. Another draw back: It took 7 months to get the parts. The advantage, less weight.. Lots less weight! ACS gets the parts from a Czech company called ComLet. You could go direct to them at www.comlet.cz Take care. Dan Dempsey > Hello, List, > > In the latest "EAA Sport Pilot", in the cover article on the CH601XL, the reviewer discusses the landing manners. He says that the AMD planes have a taller gear than the plans-built version, allowing better full-stall landings. Does anyone on the list know that this is true, and what the difference is? > > Does anyone know the dimensions of the Aircraft Spruce composite gear? Who makes their gear? (the guy who answered the phone at AS had no idea) > > I am exploring landing gear options, as well as the use of vortex generators. They allow a higher angle of attack, which requires a higher deck angle on landing to be of use there, so landing gear hieght is important there, too. > > Thanks in advance, > John Collins -------- Scratch building XL with Corvair Engine Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79471#79471 ________________________________________________________________________________
From: NYTerminat(at)aol.com
Date: Dec 05, 2006
Subject: Re: 601 Landing Gear Height
Dan, I also ordered and received the Comlet 2 pc gear for my 701. I was interested in replacing my aluminum gear to reduce the weight of my 701. I was under the impression that this was a direct replacement gear, NOT. I am not interested in redesigning the undercarriage and contacted ACS of my displeasure that this gear will not fit without major redesign work. They wrote me back saying they were going to contact the manufacturer, but I haven't heard anything yet. This was over one month ago. I guess it is time to write again to find out what is going on. I would have loved to use the gear but not since I have I have already finished building and painting. Bob Spudis N701ZX CH701/912S/87+hrs hoping the snow will hold off for a while In a message dated 12/5/2006 9:13:26 P.M. Eastern Standard Time, leinad(at)hughes.net writes: --> Zenith-List message posted by: "leinad" John I bought and plan to use the ACS composite gear for my XL, but I have to say that in hind sight, it was probably a mistake. You are right, the gear is not the same dimensions. It's just a tad taller, and MUCH narrower. If I've done my calculations right the XL plans call for a gear that is 18 1/4" tall. The composite gear will is 19 3/4" tall. The plans call for a gear 77 1/2 inches wide, while the composite gear is only 69 1/2" wide if you follow the manufacturers installation instructions (which by the way are scant). In my opinion it is questionable to call this an XL landing gear as it takes a significant design change to install the gear, as it comes in 2 parts which must be bolted to the air frame. Another draw back: It took 7 months to get the parts. The advantage, less weight.. Lots less weight! ACS gets the parts from a Czech company called ComLet. You could go direct to them at www.comlet.cz Take care. Dan Dempsey > Hello, List, > > In the latest "EAA Sport Pilot", in the cover article on the CH601XL, the reviewer discusses the landing manners. He says that the AMD planes have a taller gear than the plans-built version, allowing better full-stall landings. Does anyone on the list know that this is true, and what the difference is? > > Does anyone know the dimensions of the Aircraft Spruce composite gear? Who makes their gear? (the guy who answered the phone at AS had no idea) > > I am exploring landing gear options, as well as the use of vortex generators. They allow a higher angle of attack, which requires a higher deck angle on landing to be of use there, so landing gear hieght is important there, too. > > Thanks in advance, > John Collins -------- Scratch building XL with Corvair Engine Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79471#79471 ________________________________________________________________________________
From: Trevor Page <webmaster(at)upac.ca>
Subject: Re: Wing walk tread strip
Date: Dec 05, 2006
Larry, the stuff I put on mine was not the usual paper-backed stuff. While on the hunt to find the usual I ran across some vinyl-based treads trip that's normally used in shower stalls. I put on 2 thin strips on either side and it works perfectly. Also, since it's vinyl it won't deteriorate after washing. I bought it at a local hardware store in the plumbing section. P.S. Mine is grey so it fits in perfectly with my colour scheme. Trev Page C-IDUS 601HD R912 On Dec 5, 2006, at 8:14 PM, LarryMcFarland wrote: > > > Hi guys, > I'm looking at a roll of adhesive backed tread strip that has to be > cut to three pieces > to fit my wing walks and grumbling about how grossly coarse the > grit is and wishing > there were a better alternative. The black looks correct, but I've > concerns about it staying > where it is put and the grit coming loose. I should have purchased > it this week instead of > 3 years ago and now have doubts about its adhesive as well. > > Does anyone have a tread strip that they're happy with? Something > that once on has had > no qualms about it being too rough or hard to keep its shape year > after year. I'd like to hear > from anyone who's applied it and feel they've purchased the right > stuff. > > Larry McFarland - 601HDS at www.macsmachine.com > > ________________________________________________________________________________
From: "Robin Bellach" <601zv(at)ritternet.com>
Subject: 601 Landing Gear Height
Date: Dec 05, 2006
I just checked my Grove gear to compare. It's about 20-3/4" high and 73" wide. It saves about 11 pounds ( 32 instead of 43). ----- Original Message ----- From: "leinad" <leinad(at)hughes.net> Sent: Tuesday, December 05, 2006 8:11 PM Subject: Zenith-List: Re: 601 Landing Gear Height > > John > I bought and plan to use the ACS composite gear for my XL, but I have to > say that in hind sight, it was probably a mistake. > > You are right, the gear is not the same dimensions. It's just a tad > taller, and MUCH narrower. If I've done my calculations right the XL > plans call for a gear that is 18 1/4" tall. The composite gear will is 19 > 3/4" tall. The plans call for a gear 77 1/2 inches wide, while the > composite gear is only 69 1/2" wide if you follow the manufacturers > installation instructions (which by the way are scant). > > In my opinion it is questionable to call this an XL landing gear as it > takes a significant design change to install the gear, as it comes in 2 > parts which must be bolted to the air frame. > > Another draw back: It took 7 months to get the parts. > > The advantage, less weight.. Lots less weight! > > ACS gets the parts from a Czech company called ComLet. You could go > direct to them at www.comlet.cz > > Take care. > Dan Dempsey > > >> Hello, List, >> >> In the latest "EAA Sport Pilot", in the cover article on the CH601XL, the >> reviewer discusses the landing manners. He says that the AMD planes have >> a taller gear than the plans-built version, allowing better full-stall >> landings. Does anyone on the list know that this is true, and what the >> difference is? >> >> Does anyone know the dimensions of the Aircraft Spruce composite gear? >> Who makes their gear? (the guy who answered the phone at AS had no idea) >> >> I am exploring landing gear options, as well as the use of vortex >> generators. They allow a higher angle of attack, which requires a higher >> deck angle on landing to be of use there, so landing gear hieght is >> important there, too. >> >> Thanks in advance, >> John Collins > > > -------- > Scratch building XL with Corvair Engine > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=79471#79471 > > > ________________________________________________________________________________
From: "Craig Payne" <craig(at)craigandjean.com>
Subject: Wing walk tread strip
Date: Dec 05, 2006
Ray Allen Company (of trim servo fame) offers a non-gritty wing walk material. I bought some but have not installed it yet. I can mail you a small sample if you would like. Look at the bottom of www.rayallencompany.com/products/accessories.html. Spruce sells it but I have had no problem ordering direct from RAC and they sell it for less! WWK-1 ... WING WALK MATERIAL Ray Allen wing walks are a low profile, high quality, self-adhesive, non-slip material. The rubbery texture feels much better to the touch (and the knees) than the gritty, sandpaper-like material commonly used for wing walks in the past. One strip of wing walk material measures 26 1/2"(67.3 cm) x 9 1/2"(24.1 cm). This can easily be cut down in size to suit your own application. Installation is simple, just peel off the backing paper and press it down on your wing. $17 This material can also be cut in any length and up to 53" (1.34 m) in width. Call for custom sizes. ________________________________________________________________________________
Date: Dec 06, 2006
From: William Dominguez <bill_dom(at)yahoo.com>
Subject: Fuel tank welding, what about brazing?
First, thanks to al respondent of my previous questions about welding. I bought my gas welding equipment mostly to weld all the 4130 pieces and try if possible to weld the tanks. If I cant weld it I will try alternative methods like riveting and sealing like Vans or brazing with HTS-2000 rods that you can find in this site: http://aluminumrepair.com/ The price of this rod has gone down to $65 for 34 rods (minimum order). In their FAQ they say that it can be also used for aluminum fabrication but the rest of the site always refer to aluminum repair. If their claims are true this product looks very promising for brazing the tank and maybe more, take a look at the video in this page: http://aluminumrepair.com/video_new.asp (you might need to use IE to view it) Ive checked the archives and the only mentions of this product goes back to Jan 2004 by David Barth who questions if this product can be used. Have anyone tried this product? William Dominguez Zodiac 601XL Plans Miami, Florida --------------------------------- ________________________________________________________________________________
From: "Al Young" <armyret(at)mchsi.com>
Subject: Re: Wing walk tread strip
Date: Dec 06, 2006
Larry- I just installed wing walk a week ago. I used Acft Spruce P/N 09-28210. It is self adhesive and is no problem installing. In fact if you trim the corners to slightly round it won't peel up. when I decided to paint the plane, I decided to take up the wing walk before painting and then install new over the paint. It took me and a friend over two hours to get the adhesive off after peeling off the wing walk. I masked off the other wing and painted around it. It really has no grit on it to come off. I think you'll be happy with it. Regards, Al Young N601AY ----- Original Message ----- From: "LarryMcFarland" <larry(at)macsmachine.com> Sent: Tuesday, December 05, 2006 7:14 PM Subject: Zenith-List: Wing walk tread strip > > Hi guys, > I'm looking at a roll of adhesive backed tread strip that has to be cut to > three pieces > to fit my wing walks and grumbling about how grossly coarse the grit is > and wishing > there were a better alternative. The black looks correct, but I've > concerns about it staying > where it is put and the grit coming loose. I should have purchased it > this week instead of > 3 years ago and now have doubts about its adhesive as well. > > Does anyone have a tread strip that they're happy with? Something that > once on has had > no qualms about it being too rough or hard to keep its shape year after > year. I'd like to hear > from anyone who's applied it and feel they've purchased the right stuff. > > Larry McFarland - 601HDS at www.macsmachine.com > > > ________________________________________________________________________________
Date: Dec 06, 2006
From: Juan Vega <amyvega2005(at)earthlink.net>
Subject: Re: Forward Skin Access
thank you for the info looking forward to the numbers. Juan -----Original Message----- >From: LarryMcFarland <larry(at)macsmachine.com> >Sent: Dec 4, 2006 11:08 PM >To: zenith-list(at)matronics.com >Subject: Re: Zenith-List: Forward Skin Access > > >Juan, >I built the bike with my daughter when I was teaching her to gas weld >this summer. It's a freehand design from three bikes. >The piece you speak of is well photographed in the canopy pages. The >j-nuts were purchased from McMaster-Carr and >I'll get the numbers for you tomorrow morning. These j-nuts cost about >$10.00 per package of 50. > >Larry > >Juan Vega wrote: >> >> great website by the way, you need to send me the plans for that kick ass recumbant Bike! >> Do you have close up pics of the portion of the turtle deck you riveted, the very end pieces adjacent to the canopy screw. I like your idea. >> >> Juan >> -----Original Message----- >> >>> From: LarryMcFarland <larry(at)macsmachine.com> >>> Sent: Dec 4, 2006 8:09 PM >>> To: zenith-list(at)matronics.com >>> Subject: Re: Zenith-List: Forward Skin Access >>> >>> >>> >>> Juan, >>> You needn't use nut plates for such a panel. J-nuts that work with 6-32 >>> screws can be used with considerable confidence. They are much cheaper >>> and don't let go. I've got them on my removable forward top skin and >>> I've had the top off probably a dozen times in two years and 85 hours of >>> flying my 601. On the leading edge overhanging the panel, I bent a >>> piece of 1/2-inch aluminum tube and used a Dremel cutter to cut a slit >>> on the edge and used 4 bent tabs to secure it with the same screws that >>> hold the forward top skin. >>> It's a much easier job, as you use almost 90 screws, but very secure and >>> the screws blend into the rivet heads. >>> >>> http://www.macsmachine.com/images/largeassembly2/full/uclips.gif >>> http://www.macsmachine.com/images/cowling/full/firstcowlfitting.gif >>> http://www.macsmachine.com/images/completion/full/601ezclosefrtrt.gif >>> >>> Larry McFarland - 601HDS at www.macsmachine.com >>> >>> Juan Vega wrote: >>> >>>> >>>> >>>> Jay, >>>> >>>> that looks pertty cool. I like it. I was thinking on putting the entire piece on nutplates so the whole thing would come off. Am I missing something that would not make that possible? I think yours maybe better idea becasue you don't have to remove the canopy. I am also thinking of cutting and trimming the "head chopping" sun leadge on the panel, and replacing it with a leather one like on Cessnas. I found a place that can custom make one for cheap price. ANy thoughts? >>>> >>>> Juan >>>> >>>> >>> >>> >>> >>> >>> > > ________________________________________________________________________________
From: Bryan Martin <bryanmmartin(at)comcast.net>
Subject: Re: Wing walk tread strip
Date: Dec 06, 2006
I used the black 3M brand adhesive backed tread tape in 4" width. I've had no trouble with it coming loose in over 100 hours of use. It can be peeled off with a bit of effort but it doesn't come loose on its own. I first applied a couple of strips on the wing walk with a space between them but later I decided to cover the entire wing root out to about a foot from the fuselage. I peeled off the old stuff and put new stuff on. Even after removal the adhesive on the old stuff was still very sticky. In fact I even reused some of the old stuff to fill in around the curve of the fuselage and on the boarding step. It's still holding strong. -- Bryan Martin N61BM, CH 601 XL, RAM Subaru, Stratus redrive. ________________________________________________________________________________
Date: Dec 06, 2006
From: MrBizi <mrbizi(at)yahoo.com>
Subject: CH601 and CH701 safety, accident info requested
Hello. Does anyone know a good site where I can get accident statistics for the CH601 and CH701? I've seen some recent accidents in Zodiac XLs and that really concerns me. However, I'm wondering if the recent accidents are just a coinsidence that 3 happened in November 2006 or is that many accidents to be expected with this experimental class of planes? I'm trying to compare their safety record to that of a production plane like a Cessna. I read Chris Heintz's letter on his design techniques that said his designs should be safer.... but I'm looking for additional proof that they really are safer than the average experimental and to see if they are as safe as a production plane, etc. provided I build it per the plans. Please let me know. Thanks for any advice you might have. Thanks, Josh ________________________________________________________________________________
Date: Dec 06, 2006
From: Keystone Engineering LLC <keystone(at)gci.net>
Subject: 801 Elevator Extension
As someone who has flown the short and long elevators with and without VGs, I feel I may have something to add to the discussion. The plane flys fine with all of the versions. I found I was able to fly slower, stabilized approaches as the elevator became more effective. With the small tail I found the plane sensitive in pitch at very slow speeds which made it difficult to stabilize a very slow approach. I am now able to fly short final at 45 mph. Before I was 50 mph or so. Even with the large tail with VGs I still cannot raise the nose with power. When the nose comes up the 801 will fly. The tail is just not in the prop wash. If the original tail is rated as 100. The original tail with VGs is probably 125. The larger tail is probably 130. The larger tail with VGs is probably 140. Realize this is a subjective rating system and I cannot back it up with data. Well, I take that back. At the Valdez May day fly-in competition with the original tail I was able to take off in 130'. With the bigger tail with VGs I got off in 113.5' I still run out of trim at slow approaches speeds. I'm contemplating adding VG to the top to try to increase the effectiveness of the trim tab. One more word to the wise. Do not fly approaches with full flaps when there is a significant crosswind!!! Keep the flaps up and the 801 handles crosswinds very well. Bill Wilcox N801BW 275 Hrs Valdez, Ak Performing condition inspection Where did all this oily dirt come from??? ________________________________________________________________________________
Subject: Re: CH601 and CH701 safety, accident info requested
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Dec 06, 2006
The problem with aircraft accident statistics at least as far as VFR/GA is the number that is used as a base to compare. The only way to compare is accidents per hours flown and who knows how many hours Cessna 172s were flown last year. I don't and neither does the FAA or NTSB. Any number you see is a simple wild ass guess because nobody has ever asked me officially how many 172 hours I've flown and I've never met anyone who has been asked. Even if there were good numbers on 172 hours flown there aren't enough 601 & 701 hours to statistically valid. Now I'm not saying that accident reports aren't a good thing to look at when choosing an aircraft but you need to look at what the cause of the accidents were. In the case of homebuilts you would probably expect to see a larger number of accidents that happen in the first several hours the plane was flying. Is that because there was a problem with the design or with the particular aircraft or was it because the pilot wasn't current because he had spent the last 5 years building the plane and not flying? I know if I finished my airplane today I would be a hazard to myself and anybody in my flight path because I'm no where close to current. Which is why before the plane is ready I plan to not only get some ours in a 601 but I'm also going to go get some Upset and unsual attidude training. To sum it up when looking at accident reports it isn't the number it is the causes that really mean something. If there is a design flaw the causes will show it sooner or later. [quote="mrbizi(at)yahoo.com"]Hello. Does anyone know a good site where I can get accident statistics for the CH601 and CH701? I've seen some recent accidents in Zodiac XLs and that really concerns me. However, I'm wondering if the recent accidents are just a coinsidence that 3 happened in November 2006 or is that many accidents to be expected with this experimental class of planes? I'm trying to compare their safety record to that of a production plane like a Cessna. I read Chris Heintz's letter on his design techniques that said his designs should be safer.... but I'm looking for additional proof that they really are safer than the average experimental and to see if they are as safe as a production plane, etc. provided I build it per the plans. Please let me know. Thanks for any advice you might have. Thanks, Josh > [b] -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79585#79585 ________________________________________________________________________________
From: "Dave Ruddiman" <pacificpainting(at)comcast.net>
Subject: Re: 801 Elevator Extension
Date: Dec 06, 2006
Bill, What is the "real" indicated stall speed on your plane? Dave ----- Original Message ----- From: Keystone Engineering LLC To: zenith-list(at)matronics.com Sent: Wednesday, December 06, 2006 9:14 AM Subject: Zenith-List: 801 Elevator Extension As someone who has flown the short and long elevators with and without VGs, I feel I may have something to add to the discussion. The plane flys fine with all of the versions. I found I was able to fly slower, stabilized approaches as the elevator became more effective. With the small tail I found the plane sensitive in pitch at very slow speeds which made it difficult to stabilize a very slow approach. I am now able to fly short final at 45 mph. Before I was 50 mph or so. Even with the large tail with VGs I still cannot raise the nose with power. When the nose comes up the 801 will fly. The tail is just not in the prop wash. If the original tail is rated as 100. The original tail with VGs is probably 125. The larger tail is probably 130. The larger tail with VGs is probably 140. Realize this is a subjective rating system and I cannot back it up with data. Well, I take that back. At the Valdez May day fly-in competition with the original tail I was able to take off in 130'. With the bigger tail with VGs I got off in 113.5' I still run out of trim at slow approaches speeds. I'm contemplating adding VG to the top to try to increase the effectiveness of the trim tab. One more word to the wise. Do not fly approaches with full flaps when there is a significant crosswind!!! Keep the flaps up and the 801 handles crosswinds very well. Bill Wilcox N801BW 275 Hrs Valdez, Ak Performing condition inspection Where did all this oily dirt come from??? ________________________________________________________________________________
From: "Harrison-Hutcheson" <samhutcheson(at)kc.rr.com>
Subject: Auxillary fuel pump
Date: Dec 06, 2006
Looking for information concerning need for an auxiliary fuel pump for a CH701 with Rotax 912S engine. Previous flight experience has been basically limited to a low-wing Piper Cherokee 140 which had an auxiliary electric fuel pump that was turned on at several times during a flight - like prior to starting the engine, take-off, landing, and any thing else you did where you really did not want to starve the engine of fuel. I have both main and auxiliary fuel tanks installed so the fuel system will either feed from main tanks (both sides) or auxiliary tanks (both sides) hopefully bypassing the potential problem of making turns with the fuel selector pointing to the lowered wing. If it is desirable (needed?) to have an auxiliary electric fuel pump I would like to solicit information of what pump, sender, and gauge would be appropriate. Thanks in advance, Sam Hutcheson CH701 N6412Z (reserved) ________________________________________________________________________________
Date: Dec 06, 2006
From: Big Gee <taffy0687(at)yahoo.com>
Subject: Re: CH601 and CH701 safety, accident info requested
Hi Josh, I don't know if you mean the published reports by the NTSB or ano ther type of study which someone has done.=0A=0AMy opinion only, Chris H. has designed some very safe aircraft. Unfortunately, there have been some very bad accidents with the 601. Some, "pilot induced", a couple of accid ents are still being investigated.------------ of all the accidents, I am w ondering, (NOT SPECULATING) and waiting for the NTSB report on the one whi ch came apart in flight with a man and his wife on board. (this one raises my eyebrow, thats why I feel very comfortable with the "changes I have mad e on my XL fuel /electrical system.)=0A(not implying anything----- just say ing I made some changes which I the builder/pilot of MY airplane feels more comfortable with)=0A=0AIf you want to see a truely impressive safety recor d, check out the 701 on the NTSB. =0A=0ATo be fair, the "study" should als o show the causes of the accidents. As you mentioned earlier, a lot of ac cidents are caused by fuel mismanagement. =0A=0AFritz XL -- 90/90-- Corv air=0A=0A=0A=0A=0A----- Original Message ----=0AFrom: MrBizi <mrbizi@yahoo. com>=0ATo: zenith-list(at)matronics.com=0ASent: Wednesday, December 6, 2006 11 :37:09 AM=0ASubject: Zenith-List: CH601 and CH701 safety, accident info req uested=0A=0A=0AHello.=0ADoes anyone know a good site where I can get accide nt statistics for the CH601 and CH701? I've seen some recent accidents in Zodiac XLs and that really concerns me. However, I'm wondering if the rece nt accidents are just a coinsidence that 3 happened in November 2006 or is that many accidents to be expected with this experimental class of planes? =0A =0AI'm trying to compare their safety record to that of a production pl ane like a Cessna.=0A =0AI read Chris Heintz's letter on his design techniq ues that said his designs should be safer.... but I'm looking for additiona l proof that they really are safer than the average experimental and to see if they are as safe as a production plane, etc. provided I build it per th e plans.=0A =0APlease let me know. Thanks for any advice you might have. =============0A=0A=0A =0A__________________________ __________________________________________________________=0AAny questions? Get answers on any topic at www.Answers.yahoo.com. Try it now. ________________________________________________________________________________
Date: Dec 06, 2006
From: Dan <dwilde(at)clearwire.net>
Subject: Do instruments need shock mounting?
I quickly looked in the archive and did not see any recent discussion on how to mount the instrument panel. I plan on installing just the basic steam gages on my 701 and will be installing either a Rotax 80 or 100 HP engine. Do these instruments need to be shock isolated? Those of you who are actually flying, what has been your experience. Dan ________________________________________________________________________________
From: JAPhillipsGA(at)aol.com
Date: Dec 06, 2006
Subject: Re: Wing walk tread strip
Al, I lost your address and was waiting for you to post again to answer your question. The distance from the ground to the rear tie down loop is 550 mm. Or at least that it how high mine is. Hope your building is progressing and best regards, Bill of Georgia ________________________________________________________________________________
Date: Dec 06, 2006
From: Brett Hanley <bretttdc(at)yahoo.com>
Subject: gas welding tanks
I just blew off welding the tanks. I bought a quart of proseal from Van"s aircraft for fifty bucks including shipping. Then I riveted the tanks toge ther. I got bigger tanks as a result, did not waist any material and had t hem done in less than a week. I am not that impressed with the result of w elded tanks even when done by experts. This is one area that has been a pr oblem for many kit makers including Zenith from time to time. If you are wo rried about proseal being strong enough I challenge you to try to separate two pieces that where riveted and prosealed together. That will change you r mind. In my opinion the weld is weaker and more prone to fatigue failure . Learning to weld aluminum would be a great way to spend some time. But I think it wise to practice on some thing other than a gasoline tank.=0A =0ABrett=0A=0A=0A =0A______________________________________________________ ______________________________=0AHave a burning question? =0AGo to www.Ans wers.yahoo.com and get answers from real people who know. ________________________________________________________________________________
From: "Phil Maxson" <pmaxpmax(at)HOTMAIL.COM>
Date: Dec 06, 2006
Subject: Do instruments need shock mounting?
I am using a Corvair with a simple steam gauge panel. I used the panel as supplied in the kit, cut the holes with a fly cutter, and mounted it according to plans. Nothing shock mounted. No problems in 120 hours. Phil Maxson 601XL/Corvair Northwest New Jersey -----Original Message----- From: "owner-zenith-list-server(at)matronics.com" on behalf of "Dan" Sent: Thursday, December 07, 2006 12:28 AM To: "zenith-list(at)matronics.com" Subject: Zenith-List: Do instruments need shock mounting? I quickly looked in the archive and did not see any recent discussion on how to mount the instrument panel. I plan on installing just the basic steam gages on my 701 and will be installing either a Rotax 80 or 100 HP engine. Do these instruments need to be shock isolated? Those of you who are actually flying, what has been your experience. Dan ________________________________________________________________________________
From: NYTerminat(at)aol.com
Date: Dec 06, 2006
Subject: Re: Do instruments need shock mounting?
Dan, I installed vibration mounts on my whole panel. Bob Spudis N701ZX CH701/912S In a message dated 12/6/2006 7:30:32 P.M. Eastern Standard Time, dwilde(at)clearwire.net writes: --> Zenith-List message posted by: Dan I quickly looked in the archive and did not see any recent discussion on how to mount the instrument panel. I plan on installing just the basic steam gages on my 701 and will be installing either a Rotax 80 or 100 HP engine. Do these instruments need to be shock isolated? Those of you who are actually flying, what has been your experience. Dan ________________________________________________________________________________
From: NYTerminat(at)aol.com
Date: Dec 06, 2006
Subject: Re: gas welding tanks
Brett, Is there any problem with auto fuel with the proseal? On the RV list some expressed concern that the proseal would deteriorate over time with the auto fuel. Bob Spudis N701ZX In a message dated 12/6/2006 9:14:51 P.M. Eastern Standard Time, bretttdc(at)yahoo.com writes: I just blew off welding the tanks. I bought a quart of proseal from Van"s aircraft for fifty bucks including shipping. Then I riveted the tanks together. I got bigger tanks as a result, did not waist any material and had them done in less than a week. I am not that impressed with the result of welded tanks even when done by experts. This is one area that has been a problem for many kit makers including Zenith from time to time. If you are worried about proseal being strong enough I challenge you to try to separate two pieces that where riveted and prosealed together. That will change your mind. In my opinion the weld is weaker and more prone to fatigue failure. Learning to weld aluminum would be a great way to spend some time. But I think it wise to practice on some thing other than a gasoline tank. Brett ________________________________________________________________________________
Subject: Re: Fuel Tank Ends
From: "Ron Lendon" <rlendon(at)comcast.net>
Date: Dec 06, 2006
Wayne, I will keep the list updated on my experiences. Going to have the welding done by a pro at work, will take pictures and document the process. -------- Ron Lendon, Clinton Township, MI Corvair Zodiac XL, ScrapBuilder ;-) http://www.mykitlog.com/rlendon Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79737#79737 ________________________________________________________________________________
From: "T. Graziano" <tonyplane(at)bellsouth.net>
Subject: Re: Forward Access skin.
Date: Dec 05, 2006
One thing I would highly recommend is making the top forward skin removable. With the skin removed you have really good access to everything in the fwd area, not just wiring and instruments, but also your rudder peddles, brakes, etc. I have removal of the top skin required for my annual conditional inspection, just to check the area and it also makes easy removal of the rudder cable cover I installed over the rudder cables. Like Mr. McFarland, I have removed the top skin at least six times to do some work, inspection. add wiring, etc. I installed my top skin using #6 riv-nuts, loctited before installation. I use 6-32 SS screws to hold the skin on. I know that nut-plates are ideal solution, but I was just too lazy at the time. So far they have worked great with no problems. Mr. McFarlands J-nuts is also a solution. I installed "rubber" tubing on the top skin aft sharp edge. You can slit the tubing and "glue" it to the skin. I bought yellow tubing to match my yellow paint job and it can be seen at http://www.zenithair.com/zodiac/6-photo79.html. NOTE: If you have light paint, you should paint the "glare" shield area of the top skin under the canopy. I originally did not, but it was distracting and have since painted it flat gray. Tubing was procured a the Lowes hardware store (aircraft parts dept of course). also used 1 inch pipe insulation material to cover the aft top skin leading edge at the bow. It is easy on the hand when boarding the airplane. Tony Graziano 601XL/Jab3300 N493TG 179 hrs ------------------------------ Re: Forward Skin Access From: LarryMcFarland (larry(at)macsmachine.com) Date: Mon Dec 04 - 5:10 PM Juan, You needn't use nut plates for such a panel. J-nuts that work with 6-32 screws can be used with considerable confidence. They are much cheaper and don't let go. I've got them on my removable forward top skin and I've had the top off probably a dozen times in two years and 85 hours of flying my 601. On the leading edge overhanging the panel, I bent a piece of 1/2-inch aluminum tube and used a Dremel cutter to cut a slit on the edge and used 4 bent tabs to secure it with the same screws that hold the forward top skin. It's a much easier job, as you use almost 90 screws, but very secure and the screws blend into the rivet heads. ________________________________________________________________________________
From: 4rcsimmons(at)comcast.net (Rich Simmons)
Subject: Re: Jeff Small's comments
Date: Dec 07, 2006
Dear List, Though I comment little I have learned a good bit and have answered some of the questions I toss within myself by reading others comments on issues. Thanks for exposing your concersations to the list. I ahve even asked a couple myself! As for as the non-601XL information, it reminds me of an old saying; All work and no play makes things extrmemy boring. Humor is good for the soul and it's even funnier watching the crusty either squirm or crack a smile. SHOULDIARCHINVEORNOTARCHIVETHAT IS THE QUESTION Ahhh- Don not archive Love the list and they will get a contribution from me. I am just poor at the moment for the holiday cheer. Rich Simmons 601XL Working in the garage and Flying in my head!! Tail Section Done L/H Wing Done R/H Wing 80% Still dreamin about the rest! 2 years left on the schedule -- Thanks, Rich Simmons
Dear List,
 
Though I comment little I have learned a good bit and have answered some of the questions I toss within myself by reading others comments on issues.
 
Thanks for exposing your concersations to the list. I ahve even asked a couple myself!
 
As for as the non-601XL information, it reminds me of an old saying;
 
All work and no play makes things extrmemy boring. Humor is good for the soul and it's even funnier watching the crusty either squirm or crack a smile.
 
SHOULDIARCHINVEORNOTARCHIVETHAT IS THE QUESTION
 
Ahhh- Don not archive
 
Love the list and they will get a contribution from me. I am just poor at the moment for the holiday cheer.
 
Rich Simmons
601XL Working in the garage and Flying in my head!!
Tail Section Done
L/H Wing Done
R/H Wing 80%
Still dreamin about the rest! 2 years left on the schedule
 
--
Thanks,
Rich Simmons

      
      
      
________________________________________________________________________________
From: 4rcsimmons(at)comcast.net (Rich Simmons)
Subject: Re: Auxillary fuel pump
Date: Dec 07, 2006
List, After all of the comments about Aux. fuel pumps and placment, one gentlmen remnminded me that presurizing the gascolator may not tbe the best of ideas. Think out the fuel systems and compare them to Certifified aircraft. Then, live with your decisions. -- Thanks, Rich Simmons
List,
 
After all of the comments about Aux. fuel pumps and placment, one gentlmen remnminded me that presurizing the gascolator may not tbe the best of ideas.
 
Think out the fuel systems and compare them to Certifified aircraft.
Then, live with your decisions.
 
--
Thanks,
Rich Simmons

      
      
      
________________________________________________________________________________
From: "Al Young" <armyret(at)mchsi.com>
Subject: Re: Wing walk tread strip
Date: Dec 07, 2006
Bill- thanks much. I had forgotten that I had asked you. I wanted to compair yours to mine. I've got a problem with my canopy fit that I cannot figure out. also, when I re-installed the wings, suddenly my flaps wouldn't completely retract. I haven't had time to get into either problem very deep as my wife is requiring my full attention. I will get over to the hanger tomorrow and compair. Thanks again Bill. Regards, Al PS- I've attached a pic of the new paint job. ----- Original Message ----- From: JAPhillipsGA(at)aol.com To: zenith-list(at)matronics.com Sent: Wednesday, December 06, 2006 7:23 PM Subject: Re: Zenith-List: Wing walk tread strip Al, I lost your address and was waiting for you to post again to answer your question. The distance from the ground to the rear tie down loop is 550 mm. Or at least that it how high mine is. Hope your building is progressing and best regards, Bill of Georgia ________________________________________________________________________________
Subject: Need engine rpm pickup for Lycoming 360
From: "Jay Herron" <jay(at)agstore.net>
Date: Dec 07, 2006
I am finally ready to start hooking up wires on my 801 with Lycoming O-360a1a. I have a Aveo E-1 and MaxFlight on my panel and need an electronic RPM pickup for the Lycoming. My ultralight (Quicksilver GT400) was very simple to wire up as it had a pulse wire from the electronic ignition already. No electronic ignition on this old Lycoming (Bendix mags). Any suggestions? Jay Herron 801 95% complete Salem, OH Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79836#79836 ________________________________________________________________________________
From: "Dave Austin" <daveaustin2(at)can.rogers.com>
Subject: Re: unbelievable!
Date: Dec 07, 2006
Noel, and others, could we just drop it.. Dave Austin 601HDS - 912 ________________________________________________________________________________
From: "Wade Jones" <waj(at)quik.com>
Subject: Welding fuel tanks
Date: Dec 07, 2006
Hello group ,I am getting ready to weld( I hope) my fuel tanks .My plan is : Use .040 5052-H32 material , 1/16" pure tungsten electrode ,1/16" 5356 filler material ,cleco together ,preheat & stitch weld to control distortion .I lay no claim to fame as an aluminum welder ,however in my earlier live I was a certified pipe welder on several Nuclear power plants .With some practice I may be able to regain some of my lost skills .Can anyone the group offer any suggestions that may help me on this plan . Thanks Wade Jones South Texas ________________________________________________________________________________
Subject: Re: Zenith Plans Built in Kitplane
From: "DaveG601XL" <david.m.gallagher(at)ge.com>
Date: Dec 07, 2006
I don't have the copy in front of me right now but look at the specs for one of the 601's listed there. Looks like 801 specs to me. Little bit of a screw up on the magazines part. Dave G Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79869#79869 ________________________________________________________________________________
Subject: Re: Zenith Plans Built in Kitplane
From: "steveadams" <dr_steve_adams(at)yahoo.com>
Date: Dec 07, 2006
There is also at least 1 serious CH640 scratch builder that I know of. I don't know why it seemed so messed up in the kitplanes listing. http://www.zodiac640.com Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79883#79883 ________________________________________________________________________________
Date: Dec 07, 2006
From: Paul Mulwitz <p.mulwitz(at)worldnet.att.net>
Subject: Re: Welding fuel tanks
Hi Wade, Just a rumor (I don't have the urge to weld tanks myself) that there is a special optical filter you can use while welding aluminum that makes it easier to see the puddle. All I can recommend is you ask you supplier about this. Good luck, Paul XL fuselage >Hello group ,I am getting ready to weld( I hope) my fuel tanks .My >plan is : Use .040 5052-H32 material , 1/16" pure tungsten >electrode ,1/16" 5356 filler material ,cleco together ,preheat & >stitch weld to control distortion .I lay no claim to fame as an >aluminum welder ,however in my earlier live I was a certified pipe >welder on several Nuclear power plants .With some practice I may be >able to regain some of my lost skills .Can anyone the group offer >any suggestions that may help me on this plan . Thanks Wade Jones South Texas > ________________________________________________________________________________
Date: Dec 07, 2006
From: LarryMcFarland <larry(at)macsmachine.com>
Subject: Re: Welding fuel tanks
Wade, You're selection of materials is right on and you might look into an electric lensed helmet if you've not already. I have a bit of history written to a web journal Section 2 starting April 3, for TIG welding my aircrafts tanks. I made almost all the mistakes one could, so there might be more that would be of interest to you. Also the menu entitled "lead edge tanks" and "header tank" have images that show a method, jigs and process for setup welding fittings and testing the tanks, etc. See www.macsmachine.com. If you have specific question on any of this along the way don't hesitate to ask. Larry McFarland - 601HDS Wade Jones wrote: > Hello group ,I am getting ready to weld( I hope) my fuel tanks .My > plan is : Use .040 5052-H32 material , 1/16" pure tungsten electrode > ,1/16" 5356 filler material ,cleco together ,preheat & stitch weld to > control distortion .I lay no claim to fame as an aluminum welder > ,however in my earlier live I was a certified pipe welder on several > Nuclear power plants .With some practice I may be able to regain some > of my lost skills .Can anyone the group offer any suggestions that may > help me on this plan . Thanks Wade Jones South Texas ________________________________________________________________________________
Date: Dec 07, 2006
From: "Bob" <rfg842(at)cox.net>
Subject: Tail wheels
For the tail wheel builders, I finally found the right tail wheel. Pneumatic, ball bearing, 6" for $16.79. Rated at 150 pounds. Multitudes of sizes and material. Check Shepard wheels from Service Caster Corp. http://www.servicecaster.com/?gclid=CPGF-oOtgYkCFRlmWAodzm07AQ Bob, Wichita ________________________________________________________________________________
Date: Dec 07, 2006
From: Big Gee <taffy0687(at)yahoo.com>
Subject: Re: unbelievable! fence
Larry-- I don't have to take anyone cutting down the country I live in. and I don't have to keep quiet about it!!! I didn't bring the subject up !!!! =0AFritz=0A=0A=0A----- Original Message ----=0AFrom: "Elwood140(at)aol.com" =0ATo: zenith-list(at)matronics.com=0ASent: Thursday, Decem ber 7, 2006 2:50:56 PM=0ASubject: Re: Zenith-List: Re: unbelievable! fence =0A=0A=0AFritz, what part of cut the crap do you not understand? Go build =======================0A=0A=0A =0A_______________________________________________________________________ ________________________________________________________________________________
Date: Dec 07, 2006
From: "Dennis Shoup" <zenith601xl(at)gmail.com>
Subject: Re: Zenith Plans Built in Kitplane
The information labeled "Zodiac CH601HD" is for the 801 unless there is a new 601 with 4 seats and a 2200# gross weight. On 12/7/06, DaveG601XL wrote: > > > I don't have the copy in front of me right now but look at the specs for > one of the 601's listed there. Looks like 801 specs to me. Little bit of a > screw up on the magazines part. > > Dave G > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=79869#79869 > > ________________________________________________________________________________
From: "Wade Jones" <waj(at)quik.com>
Subject: Re: Welding fuel tanks
Date: Dec 07, 2006
Thank you ,Paul & Larry for your advise .I already have an electric self darkening lenses in my helmet .I don't think the enhanced vision filter would work on these type helmets ,but I will check with my supplier .And Larry I read about your complete fuel tank building process ,you have a great site . Thanks again Wade ----- Original Message ----- From: "LarryMcFarland" <larry(at)macsmachine.com> Sent: Thursday, December 07, 2006 3:01 PM Subject: Re: Zenith-List: Welding fuel tanks > > > Wade, > You're selection of materials is right on and you might look into an > electric lensed helmet if you've not already. I have a bit of history > written to a web journal Section 2 starting April 3, for TIG welding my > aircrafts tanks. I made almost all the mistakes one could, so there might > be more that would be of interest to you. Also the menu entitled "lead > edge tanks" and "header tank" have images that show a method, jigs and > process for setup welding fittings and testing the tanks, etc. See > www.macsmachine.com. > If you have specific question on any of this along the way don't hesitate > to ask. > > Larry McFarland - 601HDS > > > Wade Jones wrote: >> Hello group ,I am getting ready to weld( I hope) my fuel tanks .My plan >> is : Use .040 5052-H32 material , 1/16" pure tungsten electrode ,1/16" >> 5356 filler material ,cleco together ,preheat & stitch weld to control >> distortion .I lay no claim to fame as an aluminum welder ,however in my >> earlier live I was a certified pipe welder on several Nuclear power >> plants .With some practice I may be able to regain some of my lost skills >> .Can anyone the group offer any suggestions that may help me on this plan >> . Thanks Wade Jones South Texas > > > ________________________________________________________________________________
Date: Dec 07, 2006
From: Christian Tremblay <cj.tremblay(at)videotron.ca>
Subject: Re: Zenith Plans Built in Kitplane
Hi, The model 4 seat at gross weight of 2200 pound is the CH640. This model is derived from the certified model 2 place, IFR CH2000 also named Alarus. Chris _____ De : owner-zenith-list-server(at)matronics.com [mailto:owner-zenith-list-server(at)matronics.com] De la part de Dennis Shoup Envoy=E9 : Thursday, December 07, 2006 5:15 PM =C0 : zenith-list(at)matronics.com Objet : Re: Zenith-List: Re: Zenith Plans Built in Kitplane The information labeled "Zodiac CH601HD" is for the 801 unless there is a new 601 with 4 seats and a 2200# gross weight. On 12/7/06, DaveG601XL wrote: david.m.gallagher(at)ge.com > I don't have the copy in front of me right now but look at the specs for one of the 601's listed there. Looks like 801 specs to me. Little bit of a screw up on the magazines part. Dave G Read this topic online here: http://forums.matronics.com/viewtopic.php?p=79869#79869 ________________________________________________________________________________
Date: Dec 07, 2006
From: john butterfield <jdbutterfield(at)yahoo.com>
Subject: forward skin fastener
larry i would like the part number for the j nuts also. did you use stainless steel screws with them. john butterfield 601XL corvair torrance, ca Any questions? Get answers on any topic at www.Answers.yahoo.com. Try it now. ________________________________________________________________________________
Date: Dec 07, 2006
From: Brandon Tucker <btucke73(at)yahoo.com>
Subject: Re: Welding fuel tanks
Wade, You have the right materials. There is no need to preheat, however. Sometimes when preheating aluminum, you can very slightly contaminate the material, and the weld will not look quite right. It will still work, just not as pretty. With a 1/16" electrode, you can probably go with a step down gas cup. This allows for getting into tighter spots, and better view of what is going on. You will be glad you chose .040. It is much easier... Also, I do not recommend using outside flange joints. They are not as strong. The Tony Bingelis article on welding gas tanks specifically say to use lap joints, and not outside flange. It also points out that you should use pleanty of filler rod... VR/ Brandon 601HDS / Corvair 20 hours on my welded tanks... __________________________________________________ ________________________________________________________________________________
From: NYTerminat(at)aol.com
Date: Dec 07, 2006
Subject: Re: vg's
Joe, Congratulations, I am looking forward to your numbers. Was it hard laying out and installing the VG's? Bob Spudis N701ZX CH701/912S In a message dated 12/7/2006 5:40:34 P.M. Eastern Standard Time, jnjkimbell(at)HOTMAIL.COM writes: I just returned from flying my 701 for the first time since removing the slats and adding VG's/ It was great. A little too windy to check all my numbers, but it does take off and land as short as it did before. Better feel on landing. Stalls seem the same except power off, full flaps give me a little more definite buffet. Still no clean stall power off. Will report actual numbers to the list after completing my tests. Joe from FL Those guys from down under seem to know what they are doing. do not archive ________________________________________________________________________________
Date: Dec 07, 2006
From: "John M. Goodings" <goodings(at)yorku.ca>
Subject: Re: Zenith-List Digest: Do instruments need shock-mounting?
We certainly worried about installing steam gauges without shock-mounting, but no shock-mounting was used in our panel. The instruments include three gyros (an electric turn and bank, and vacuum artificial horizon and directional gyro). We have had no trouble in 100 plus hours of operation with a Rotax 912S engine. But, the engine has a slipper clutch. I think this is necessary in the 100 HP version to reduce vibration during start-up and shut-down. Ours is a tri-gear aircraft. John Goodings, C-FGPJ, CH601HD with R912S, Toronto/Ottawa/Waterloo. ________________________________________________________________________________
From: "Wade Jones" <waj(at)quik.com>
Subject: Re: Welding fuel tanks
Date: Dec 07, 2006
Thanks Aaron And Brandon ,it takes a lot more to gas weld aluminum than to tig weld it .Hey Brandon I e-mailed you awhile back when you first test flew your plane at ocean Side Ca. My daughter has a business just across the field from you ,it is a Budget truck rental on Mission Ave .I have told her to look out her door sometime and see a good looking 601 ,nice paint job . Thanks again Wade Jones ----- Original Message ----- From: Brandon Tucker To: zenith-list(at)matronics.com Sent: Thursday, December 07, 2006 8:28 PM Subject: Zenith-List: Re: Welding fuel tanks Wade, You have the right materials. There is no need to preheat, however. Sometimes when preheating aluminum, you can very slightly contaminate the material, and the weld will not look quite right. It will still work, just not as pretty. With a 1/16" electrode, you can probably go with a step down gas cup. This allows for getting into tighter spots, and better view of what is going on. You will be glad you chose .040. It is much easier... Also, I do not recommend using outside flange joints. They are not as strong. The Tony Bingelis article on welding gas tanks specifically say to use lap joints, and not outside flange. It also points out that you should use pleanty of filler rod... VR/ Brandon 601HDS / ________________________________________________________________________________
From: "Rich" <4rcsimmons(at)comcast.net>
Subject: Re: Do instruments need shock mounting?
Date: Dec 07, 2006
Dear List, The shock mounting for the gauges is new to me but makes sense. Can some one send me a pictorial example of how this is acomplised! Are certified aircraft done this way? I think this is a gooe question so do not ??????? Happy days there mates! ________________________________________________________________________________
From: "Dave Ruddiman" <pacificpainting(at)comcast.net>
Subject: Re: Do instruments need shock mounting?
Date: Dec 07, 2006
I've always heard that you should shock mount your gyros and the rest didn't matter. It seems to make sense, but there are a lot of panels that mount everything solid and don't seem to have any problems. ----- Original Message ----- From: Rich To: zenith-list(at)matronics.com Sent: Thursday, December 07, 2006 8:53 PM Subject: Re: Zenith-List: Do instruments need shock mounting? Dear List, The shock mounting for the gauges is new to me but makes sense. Can some one send me a pictorial example of how this is acomplised! Are certified aircraft done this way? I think this is a gooe question so do not ??????? Happy days there mates! ________________________________________________________________________________
Date: Dec 07, 2006
From: Gary Gower <ggower_99(at)yahoo.com>
Subject: Re: Do instruments need shock mounting?
Hello Dan, I dont think they need any, The 912 instalation (mine is 100 hp) is very quiet and could say vibration free in flight,,, Not counting the 2 seconds before the prop stops at shut down :-) Saludos Gary Gower 701 912S Flying from Chapala, Mexico. I quickly looked in the archive and did not see any recent discussion on how to mount the instrument panel. I plan on installing just the basic steam gages on my 701 and will be installing either a Rotax 80 or 100 HP engine. Do these instruments need to be shock isolated? Those of you who are actually flying, what has been your experience. Dan --------------------------------- Any questions? Get answers on any topic at Yahoo! Answers. Try it now. ________________________________________________________________________________
Date: Dec 08, 2006
From: Matt Dralle <dralle(at)matronics.com>
Subject: Matronics Fund Raiser - 2006 List of Contributors
Dear Listers, I would like to thank everyone that made a Contribution in support of the Lists this year! It was really nice to hear all great comments people had regarding the Lists! As I have said many times before, running these Lists is a labor of love. Your generosity during the List Fund Raiser only underscores the great sentiments people have made regarding the Lists. If you haven't yet made a Contribution in support of this year's Fund Raiser please feel free to do so. The nice List gifts will be available on the site for just a little while longer, so hurry and make your Contribution and get your great gift. Once again, the URL for the Contribution web site is: http://www.matronics.com/contribution I would like to thank Andy Gold of the Builder's Bookstore ( http://www.buildersbooks.com ), Paul Besing of Aeroware Enterprises ( http://www.kitlog.com ), Jon Croke of Homebuilt HELP ( http://www.homebuilthelp.com ) and Bob Nuckolls of AeroElectric ( http://www.aeroelectric.com ) for their extremely generous support during this year's Fund Raiser through the contribution of merchandise. These are great guys that support the aviation industry and I encourage each and every Lister to have a look at their products. Thank you Andy, Paul, Jon and Bob!! Your support is very much appreciated! And finally, below you will find a web link to the 2006 List of Contributors current as of 12/7/06! Have a look at this list of names as these are the people that make all of these List services possible! I can't thank each of you enough for your support and great feedback during this year's Fund Raiser! THANK YOU! http://www.matronics.com/loc/2006.html I will be shipping out all of the gifts in the next few weeks and hope to have everything out by the end of the month. In most cases, gifts will be shipped via US Postal Service. Kitlog Pro serial numbers should go out via email this weekend. Once again, thank you for making this year's List Fund Raiser successful! Best regards, Matt Dralle Matronics Email List Administrator ________________________________________________________________________________
From: NYTerminat(at)aol.com
Date: Dec 08, 2006
Subject: Re: Do instruments need shock mounting?
In a message dated 12/7/2006 11:56:14 P.M. Eastern Standard Time, 4rcsimmons(at)comcast.net writes: Dear List, The shock mounting for the gauges is new to me but makes sense. Can some one send me a pictorial example of how this is acomplised! Are certified aircraft done this way? I think this is a gooe question so do not ??????? Happy days there mates! Aircraft Spruce has different types of mounts, I used the 1" square Lord type. Used the Zenith supplied panel for the backer panel to mount the shoc k mounts, and used a two piece panel over it, one for the gauges and one for my avionics. Cut out the Zenith panel to allow the front panel and instruments to slide into. 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Prices are subject to change without notice. ________________________________________________________________________________
From: "Craig Payne" <craig(at)craigandjean.com>
Subject: Matronics Fund Raiser - 2006 List of Contributors
Date: Dec 08, 2006
Matt, Big thanks for hosting all the lists. If you send me my Home-built Help DVD via US mail please send it to: Craig Payne P.O. Box 982617 Park City, UT 84098 Also, I would still love to host the MGL Stratomaster list on Matronics instead of Yahoo. Their system is fairly unreliable and their support unresponsive. I guess you get what you pay for. -- Craig ________________________________________________________________________________
Date: Dec 08, 2006
From: "Peter Sonders" <sportsflyer(at)comcast.net>
Subject: Re: Welding fuel tanksWelding fuel tanks
________________________________________________________________________________
From: Tebenkof(at)aol.com
Date: Dec 08, 2006
Subject: Re: vg's
Joe, I have been off the list for a time. Is this VGs instead of slats an idea that has been talked about some? Is there some reason to think VGs may be superior? Your numbers are eagerly awaited. I have considered using VGs in additon to the slats on my 701 (not yet flying), but had not considered eliminating the slats. Can you give me more info on this idea? Jim Greenough ________________________________________________________________________________
From: "Bill Steer" <steerr(at)bellsouth.net>
Subject: Re: Do instruments need shock mounting?
Date: Dec 08, 2006
That's true, but the directions that came with my PAI-700 vertical card compass explicitly said the instrument should be shock mounted. I'm attaching a shock-mounted panel in front of the original structural panel. To do that, I've reinforced the structural panel with the usual "L" angle around the top and across the bottom so it ends up wuth a U-shaped channel behind the panel. The top angle can be shaped with a metal stretcher. I also have a vertical reinforcing "L" angle near the center. Then the center of the structural panel is cut out. The new front panel is then attached to this framework with vibration mounts I got from Reid Tool. Some folks have used multiple front panels so they can easily get access to the back of the panel. The removable top skin gives the same or better access, of course. Note that the reinforcing "L" angle costs about an inch of real estate around the edge of the original panel. I don't have any pictures of it, but can take some if anybody is interested. Hope this helps. Bill I've always heard that you should shock mount your gyros and the rest didn't matter. It seems to make sense, but there are a lot of panels that mount everything solid and don't seem to have any problems. The shock mounting for the gauges is new to me but makes sense. Can some one send me a pictorial example of how this is acomplised! ________________________________________________________________________________
From: "Lumkes, John H" <lumkes(at)exchange.purdue.edu>
Subject: Forward Top Skin-601HD
Date: Dec 08, 2006
Hello, With the discussion about accessing the instrument panel, it reminded me of a related question that I could not locate the answer to in the archives. I am still working on a 601HD (finishing firewall assembly) and planning on using the side opening canopy with the latching mechanism modification. I would also like to have the forward top skin removable for access to the instrument panel, but am concerned that with the side opening canopy the top skin is more structurally necessary (no side rails like with the forward hinge) and it might not be a good idea to use rivnuts in place of the rivets. Question 1: Are rivnuts okay in this model and canopy style? Question 2: If not, are there examples of adding an access hatch on the top skin between the tank and instrument panel? Thanks, John ________________________________________________________________________________
From: "Ron Lalonde" <rlalonde(at)HOTMAIL.COM>
Subject: Re: Do instruments need shock mounting?
Date: Dec 08, 2006
For what it is worth, it is a cheap fix. I put the shock mounts on the panel mount of my VP2 and it works great. Will do the same on this 601XL project. Dont really know if it was necessary but I am sure it did not hurt. Better safe than sorry, especially considering the cost of even the basic a/c instruments. Ron Lalonde 601XL Debert, NS Canada >I've always heard that you should shock mount your gyros and the rest >didn't matter. It seems to make sense, but there are a lot of panels that >mount everything solid and don't seem to have any problems. > > > ----- Original Message ----- > From: Rich > To: zenith-list(at)matronics.com > Sent: Thursday, December 07, 2006 8:53 PM > Subject: Re: Zenith-List: Do instruments need shock mounting? > > > Dear List, > > The shock mounting for the gauges is new to me but makes sense. > > > Can some one send me a pictorial example of how this is acomplised! > > > Are certified aircraft done this way? > > > I think this is a gooe question so do not ??????? > > > Happy days there mates! > > _________________________________________________________________ Download now! Visit http://www.telusmobility.com/msnxbox/ to enter and see how cool it is to get Messenger with you on your cell phone. http://www.telusmobility.com/msnxbox/ ________________________________________________________________________________
Date: Dec 08, 2006
From: LarryMcFarland <larry(at)macsmachine.com>
Subject: travel stop and tow bar ring
Hi guys, I've finally put the mill in gear and have been finishing the travel stops and tow bar rings for the 2-inch front gear strut. Several have been mailed to catch up with those that requested them some weeks or months ago. I should have half a dozen extra when the current mailings are complete. If there is anyone else that I've forgotten or needs one, please let me know off line. http://www.macsmachine.com/images/gear/full/travel-stop-and-stear-link.gif http://www.macsmachine.com/images/gear/full/travel-stop-&-ground-handli.gif http://www.macsmachine.com/images/completion/full/601ezclosefrtrt.gif Thanks, Larry McFarland - 601HDS at www.macsmachine.com ________________________________________________________________________________
Subject: Avionics book or videos - any recommendation?
From: "Eddie G." <silentlight(at)verizon.net>
Date: Dec 08, 2006
Greetings, Is there one or two good books or videos that you folks can recommend on VHF antenna basics, selecting and installating antennas on metal-frame aircrafts, avionics, connectors, wiring, etc.? Thanx...Eddie Read this topic online here: http://forums.matronics.com/viewtopic.php?p179#80179 ________________________________________________________________________________
Date: Dec 08, 2006
From: ALAN BEYER <agbeyer(at)sbcglobal.net>
Subject: Re: Forward Top Skin-601HD
John,=0A=0AOn Dec. 4th I sent a post on my inspection covers on my HDS with pics. If you can't find it I can send you the pics.=0A=0AAL from Oshkosh =0A=0A=0A=0A----- Original Message ----=0AFrom: "Lumkes, John H" <lumkes@ex change.purdue.edu>=0ATo: zenith-list(at)matronics.com=0ASent: Friday, December 8, 2006 10:56:36 AM=0ASubject: Zenith-List: Forward Top Skin-601HD=0A=0A =0AHello,=0A =0AWith the discussion about accessing the instrument panel, i t reminded me of a related question that I could not locate the answer to in the archives. I am still working on a 601HD (finishing firewall assembly ) and planning on using the side opening canopy with the latching mechanism modification. I would also like to have the forward top skin removable for access to the instrument panel, but am concerned that with the side openin g canopy the top skin is more structurally necessary (no side rails like wi th the forward hinge) and it might not be a good idea to use rivnuts in pla ce of the rivets.=0AQuestion 1: Are rivnuts okay in this model and canopy s tyle?=0AQuestion 2: If not, are there examples of adding an access hatch on the top skin between the tank and instrument panel?=0A =0AThanks,=0AJohn === ________________________________________________________________________________
Subject: Interesting/Funny Mistake on the Part of the FAA
From: "Gig Giacona" <wr.giacona(at)cox.net>
Date: Dec 08, 2006
I was looking for an address of a 601 builder today and searched the faa database. Check out the engine type on the second group of AMD built 601XLs -------- W.R. "Gig" Giacona 601XL Under Construction See my progress at www.peoamerica.net/N601WR Read this topic online here: http://forums.matronics.com/viewtopic.php?p200#80200 ________________________________________________________________________________
From: VideoFlyer(at)aol.com
Date: Dec 08, 2006
Subject: Re: travel stop and tow bar ring
Great looking plane. I hope to fly mine next spring. The ring for the nose gear is a great idea. How much do you want for one? Let me know. I will send you a check. Thanks Dave Harms Waterloo, Iowa videoflyer(at)aol.com 601XL/Corvair ________________________________________________________________________________
Date: Dec 08, 2006
From: john butterfield <jdbutterfield(at)yahoo.com>
Subject: Nose gear strut 601
hi list, i put the rubber band on the nose wheel strut, and am concerned about the stiffness of the up and down movement. it seems really tight, but that is without an engine on or even the engine mount. should you be able to depress the bungies by pressing down on the firewall? it moves a little, but i would have to exert extream pressure to get it to move a few inches. i assume that on landing, it will work properly, but if it should move fairly easy now, i would rather take it off now and open up the bearings a little. just don't have a feel on how loose it should be thanks in advance john butterfield 601XL corvair torrance, ca Have a burning question? Go to www.Answers.yahoo.com and get answers from real people who know. ________________________________________________________________________________
Date: Dec 08, 2006
From: LarryMcFarland <larry(at)macsmachine.com>
Subject: Re: Forward Top Skin-601HD
John, I've looked at the side opening canopy on a HD and consider the removable forward top skin not to be different from the problems of the forward opening canopy on the XL. The number of fasteners needed for the skin total near 90 and one can use j-nuts rather than rivnuts or plate nuts. The sum total of the fasteners make a rather solid assembly regardless. The difference would be that a piece each side riveted to the longerons would have to be bent to accept the removable skin for side fastening around the perimeter of the access. Better that the firewall and instrument panel be part of the J-nut assembly for access. There are lots of examples of other smaller access panels that can be done, but real access is the challenge. I don't particularly like rivnuts as they eventually spin and make a difficult time of getting a screw out and they are long for the location when a header tank is involved. Larry McFarland - 601HDS at www.macsmachine.com Lumkes, John H wrote: > Hello, > > With the discussion about accessing the instrument panel, it reminded > me of a related question that I could not locate the answer to in the > archives. I am still working on a 601HD (finishing firewall assembly) > and planning on using the side opening canopy with the latching > mechanism modification. I would also like to have the forward top skin > removable for access to the instrument panel, but am concerned that > with the side opening canopy the top skin is more structurally > necessary (no side rails like with the forward hinge) and it might not > be a good idea to use rivnuts in place of the rivets. > Question 1: Are rivnuts okay in this model and canopy style? > Question 2: If not, are there examples of adding an access hatch on > the top skin between the tank and instrument panel? > > Thanks, > John > * > > * ________________________________________________________________________________
From: "John Gilpin" <vgstol(at)bigpond.net.au>
Subject: Slats myth busted!
Date: Dec 09, 2006
Gday, I'm JG, the fella who started all this kafuffle about removing the slats from 701s. It's sure stirred up a debate, just as I knew it would, and I've really enjoyed watching from the side-lines, but now I think it's time to comment. This is understandably a controversial move, since those slats are very much a defining feature of the 701. So I need to explain the history and experience that led to this move - it certainly wasn't just a wild idea on an impulse..... I've been fascinated by the Zenair 701 ever since a magazine article in1988 entitled "Freight Elevator to the Stars!". The 701 in that test report was the prototype, powered by a 50hp Rotax 503! It was a revolutionary aircraft, and I was immediately impressed, and ordered a set of plans. In 1990 I went to Sun'Fun and spent most of the week hanging around the Zenair site and helping to assemble the 701 quick-build kit that was the feature of their display in those days. It was at that display that I met the Columbians who had already tried their 701's without slats and liked them better that way, and had the slats hung up in their hangars. That image has been intriguing me ever since, and lots of book study on aerodynamics and real life observation of different aircraft made it appear truly inevitable. The responsibilities of a young family kept me from building a 701 earlier, but in that time I did fly a single-seat Spectrum Beaver ultralight for 1000 hrs, and modified another Beaver into a twin-engine machine and flew it for 200hrs. Now I finally have the time, and a really good home workshop for aircraft construction, in which we've built two Savannahs from kits, and Hans and I have rebuilt three crashed 701's, two of them with extensive damage, so we know every rivet in these machines! (Each of them had slats at the time of the crashes, but don't anymore...) Hans with his 701 and I with my Savannah each flew about 200hrs in the last year without slats, so we're certainly not 'hangar flyers'. In my case that included a 5000km (3000mile) round trip to Tasmania, with all the variable conditions that you encounter on such a trip, and landings into some challenging small strips. Hans did a 2500km (1500mile) trip to North Queensland and back in very wild and windy conditions, with a passenger and full load. We both fly 'intensively' and are forever trying STOL tactics and landing into tight spots - we do know our aircraft really well! So, that's a summary of the history and experience that I use to guide these experiments with VGs instead of slats. So we're not guessing how the aircraft will fly without slats - we already know the answer to that! I wouldn't have published the results if I wasn't absolutely certain of the facts, checked and double checked. In that article, "The True Story of Leading Edge Slats", at www.stolspeed.com , I tried to demonstrate all the testing and validation that had gone into it. I won't go over all that again now, but if there are questions that I didn't cover in that article then bring them on and we'll look at them. Another bit of interesting evidence that has come to mind is to watch those aircraft with retractable slats. I've seen a video of one manufacturer doing very slow turns, with the slats on the inner wing popping in and out on their own - no apparent change in handling. Also Carl Bertrand's experiments with his retractable slat wing, when one slat stuck - "....very little effect, only light aileron and rudder required....". That just confirms the effect that I would expect from my testing. You sure would think that the rather bluff leading edge of the wing without the slats would be slower in cruise than a 'finer' leading edge. I had thought this as well, and even had already made up new front ribs with the same profile as the wing with slats on, for the new leading edge I thought I was going to need after removing the slats. But when I did the tests with the slats on and the slots covered over, I got a real surprise! Cruise speed was the same as with the bluff leading edge! But the stall was much more abrupt, and the centre of lift had moved forward such that I now had a seriously aft CofG. So now I won't change that leading edge at all. Those unused ribs still gather dust on a top shelf in my workshop - such are the surprises of experimental work......... It's well known that a full-rounded leading edge is good for stall characteristics, and this wing that's left after you remove the slats from a 701 is just perfect in that regard. I've flown it to the limit again and again, and with VGs it's never ever let me down hard! Another surprise was the dramatic effect of the VGs. I had read that they reduced the stall speed a bit and improved low speed handling, but I was amazed at how much difference they made! They allow pretty much the same STOL performance as the slats did, but give much better cruise efficiency, and the landings are easier. Slats are known as a high-lift device, but it should also be noted that they are also a high drag device. The high lift only comes in at the very high angles of attack, but the drag is there at all speeds, and goes from high at cruise to extremely high at stall aoa. The only time I've found a use for all that drag is for power-on spot-landings. Nose way high, hanging on the slats and the prop, 'dragging' the aircraft in below flying speed, with power controlling the descent. Can't see where you're going with the nose so high, but easy to do a spot landing that way - just reduce the power and it'll drop down right now, no floating on. But a real serious down-side of all that drag is getting caught behind the power curve, or getting caught in an increasing stall condition without power. Just imagine all that drag at the highest point of the aircraft, not only slowing you down really quickly but also tending to pull the nose up - makes it increasingly difficult to recover...... A few 701's been bent that way......... At cruise, all that the slats give is d-r-a-g-g-g..... It takes power to overcome that drag. I saved $250 on fuel on a 50hr trip (4 litres/hr less burn @ $1.30/litre) alongside an identical aircraft with slats, so now I've probably already saved $1000 over the 200hrs without slats! There is another benefit of slats (not worth considering), is that in the event of a collision with trees or such hard objects they absorb lots of impact and protect the main structure of the wing...... After repairing those crashed machines we had a pile of mangled slats out behind the workshop, until I sent them away for recycling..... We haven't found any real use either for the good slats we've taken off, except to hang them up in the roof of the hangar - makes a good ornament and conversation starter...... So the slats myth is well and truly 'busted'. To me it's just amazing that someone, including Zenair, hadn't worked this out this long ago...... JG ________________________________________________________________________________
From: "george may" <gfmjr_20(at)HOTMAIL.COM>
Subject: Nose gear strut 601
Date: Dec 08, 2006
John-- It should be very stiff at the point you are at. Once the engine is in place you will notice more elasticity. Keep building--- George May 601XL 912s----19 hours- >From: john butterfield <jdbutterfield(at)yahoo.com> >Reply-To: zenith-list(at)matronics.com >To: Zenith-List Digest Server >Subject: Zenith-List: Nose gear strut 601 >Date: Fri, 8 Dec 2006 12:35:35 -0800 (PST) > > > >hi list, >i put the rubber band on the nose wheel strut, and am >concerned about the stiffness of the up and down >movement. > >it seems really tight, but that is without an engine >on or even the engine mount. > >should you be able to depress the bungies by pressing >down on the firewall? it moves a little, but i would >have to exert extream pressure to get it to move a few >inches. i assume that on landing, it will work >properly, but if it should move fairly easy now, i >would rather take it off now and open up the bearings >a little. just don't have a feel on how loose it >should be > >thanks in advance >john butterfield >601XL corvair >torrance, ca > > >Have a burning question? >Go to www.Answers.yahoo.com and get answers from real people who know. > > _________________________________________________________________ Get the latest Windows Live Messenger 8.1 Beta version.Join now. http://ideas.live.com ________________________________________________________________________________
Date: Dec 08, 2006
From: "Carlos Sa" <carlossa52(at)gmail.com>
Subject: Re: Avionics book or videos - any recommendation?
I suggest a visit to www.aeroelectric.com And, of course, there is the aeroelectric list @ Matronics. Just follow the link to the Matronics Navigator page, in the trailer below... Carlos CH601-HD, plans Montreal, Canada On 08/12/06, Eddie G. wrote: > > > Greetings, > > Is there one or two good books or videos that you folks can recommend on > VHF antenna basics, selecting and installating antennas on metal-frame > aircrafts, avionics, connectors, wiring, etc.? > > Thanx...Eddie > > ________________________________________________________________________________
From: NYTerminat(at)aol.com
Date: Dec 08, 2006
Subject: Re: Avionics book or videos - any recommendation?
Eddy, I got the book from _www.aeroelectric.com_ (http://www.aeroelectric.com) . Well worth the investment. Bob Spudis N701ZX CH701/912S In a message dated 12/8/2006 1:11:34 P.M. Eastern Standard Time, silentlight(at)verizon.net writes: --> Zenith-List message posted by: "Eddie G." Greetings, Is there one or two good books or videos that you folks can recommend on VHF antenna basics, selecting and installating antennas on metal-frame aircrafts, avionics, connectors, wiring, etc.? Thanx...Eddie ________________________________________________________________________________
From: "Neitzel" <n963wb(at)frontiernet.net>
Subject: Big mistake
Date: Dec 08, 2006
Greetings all, Thought I would pass this along so someone else does not make the same mistake that I did. When I finished my wings I needed to get them out of a bulging basement so transported them to my hangar. I had a bunch of foam rubber and thought that would be a good way to keep them apart. Put the first wing on foam then scattered some more foam blocks on top and carefully set the second wing on top. I then covered with a tarp and put some large pieces of cardboard on top of that to avoid hangar rash. When I retrieved the left wing to bring back to my basement work shop to fit flaperon and slat, I discovered that the rubber foam stuck to the wing in several places. Even a trace of corrosion in a couple of places. I have already experimented with polish to make sure these spots will come out and looks like no problem. They were only in the hangar for four months can only imagine what they would have looked like if it had been longer. My hangar is nice and dry but I guess foam rubber sucks moisture from the air. Bottom line I don't recommend rubber foam for long term storage/seperation of parts. Also was wondering if there are any 582 guru's out there. Got a high volt indication on the EIS (17+ volts). Checked tightness of bonding straps and all other related wiring and found none loose. It has 150 hours on it and the battery is only 18 months old. Any thoughts? Any easy way to check the regulator?


November 26, 2006 - December 08, 2006

Zenith-Archive.digest.vol-gg