Kolb-Archive.digest.vol-bo

July 22, 1999 - August 13, 1999



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From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: Clevis Pins for Mark III and Firestar II
Date: Jul 22, 1999
Hi Johann: Go to the bottom of this message, and click on Archive Search Engine. When it comes up, scroll down the archive list, and click Kolb. For Output Method, click 2 Frame, Index. In Search String, type in " Struts". Scroll down to # 93 Aug 98 John Hauck. Open each message in the string down to # 99. There's more related messages from # 130 to # 146. Hope this helps. Big Lar. ----- Original Message ----- From: Johann G. Johannsson <johann.g(at)centrum.is> Sent: Wednesday, July 21, 1999 2:10 PM Subject: Kolb-List: Clevis Pins for Mark III and Firestar II > > Dear List members. > > I need some help on the Clevis Pins used on the Mark III and the > Firestar II. > I can not go and measure the pins on my plane, (am at work) but will > need to order some spare pins. > Does anyone have the correct size for the Clevis Pins needed for the > Kolb planes? > Someone on the list mentioned about a spacer for the lower wing strut. > The pins have enlarged the holes on the cage, and I would like to solve > the problem. > I can not find the solution on the archive list. > Hope you can help, > > Best regards, > Johann G. > Iceland. > > ________________________________________________________________________________
From: "Beauford Tuton" <beaufordw(at)worldnet.att.net>
Subject: Re: Painting cage
Date: Jul 22, 1999
Frank and Winnie: Shot my cage with the Stits two-part epoxy, using a paasche airbrush to cut overspray and waste... The airbrush was a tad slow, but really made the primer go a long way... took about two hours to shoot the cage. Came out pretty slick... good coverage and gloss. You can get a good airbrush like the Paasche H series from Harbour Freight for less than $50. After about two months, roughed the primer with #600 wet or dry paper and shot over it with automotive acrylic enamel with polyurethane crosslinker added...(hardener)... Be really carefully shooting the enamel with the hardener added... it really adds super gloss and hardness, but conventional spray masks are worthless for it... you need an external source air supply... I use an old aqua-lung... that hardened acrylic is superior, but will absolutely kill you if you breathe it... Did the same on the tail boom, using a standard size gun... great gloss and it is hard as a rock. As to what not to spray... had a helluva time getting the tailboom to slide into the painted ring on the cage... Debated whether to sand off all the epoxy inside the ring... instead, ended up chilling the tube with a bag of ice and slightly heating the ring... went right in.... same for the drag strut attach fittings... I worried about sanding off all the epoxy anti-corrosion protection, just to make it go together... decided the ice and heat trick was a better bet and it worked for me ... Good luck... Bill Tuton The Aluminum Butcher of Brandon, FL Flailing away at FF #076 -----Original Message----- From: Frank & Winnie Hodson <fwhodson(at)bigfoot.com> Date: Thursday, July 22, 1999 12:37 AM Subject: RE: Kolb-List: Painting cage > > >> I'm getting ready to paint the fuselage and the small parts >> associated with >> it. I have read of parts that are hard to fit when they are painted. Any >> recommendation of which areas to mask off. >> >> > ________________________________________________________________________________
From: rick106(at)juno.com
Date: Jul 22, 1999
Subject: Re: Kolb crash in Minnesota, again.
Bruce and ALL I hope all goes ok if I may and I hope that you all don't think that this is tacky on my crash of my Mk.3 on father's day IF I did not have my helment on I would not be here today their were tube marks all over the helment. once again I hope and pray that BRUCE will be ok Rick Libersat writes: > >Thanks to all of all who expressed concern. Bruce's plane did go down >yesterday (7/21) afternoon; he will be OK; FAA and TSB are >investigating but >the report I received from Bruce late last night indicated some >problem with >the tail; "it felt loose and I couldn't control it at all so I tried >to stay >over water and avoid a very crowded swimming beach". Will try and >keepall of >you posted on outcome of investigation and Bruce's physical status. >Took >them 30-45 minutes to extricate him from the plane. >Please respond to this address with any questions. >Thanks again for your concern and good thoughts. >Helen Fletcher >----- Original Message ----- >From: <gerken(at)us.ibm.com> >To: >Sent: Thursday, July 22, 1999 7:11 AM >Subject: Kolb-List: Kolb crash in Minnesota, again. > > >> >> See: >> http://www.channel4000.com/news/stories/news-990721-150015.html >> >> Supposedly it is a Kolb Mkiii (according to last nights television >news). >Does >> anyone know who the pilot was? My friend saw the news report and >told me >that >> the pilot ended up with a pc of aluminum tube stuck thru his neck. >Hopefully the >> guy(s) is recovering OK. >> I am not sure of whether the plane had floats or not. I heard he >had >just >> taken off from across the lake and had 100' altitude when it fell >off one >side >> and hit the water in a spiral. >> >> > > > > > > > ________________________________________________________________________________
From: "Rob Reynolds" <rfreynol(at)mindspring.com>
Subject: Re: FAA Sales
Date: Jul 22, 1999
Yes, the FAA does have and 'official' bill of sale form. It's main use when individuals buy/sell a plane. I can't remember the OMB Form Number, but when I was at the local FSDO yesterday, they had a stack of them sitting there. -Rob ----- Original Message ----- From: <RLCPTL(at)aol.com> Sent: Thursday, July 22, 1999 12:58 PM Subject: Kolb-List: FAA Sales > > Big Lar wrote - - - Whazzat ?? What FAA approved form ?? Anyone else heard > of this ?? All I've got is the original receipt they sent when they received > my check. Isn't that enough ?? Big Lar. > > The bill of sale or receipt that came with my kit satisfied the FAA when I > submitted my registration application papers. I don't know of any special > FAA approved form for a "sales slip." > Ron Christensen > MKIII1/2 > > ________________________________________________________________________________
From: "Bruce Fletcher" <bwf(at)emailmn.com>
Subject: Re: Kolb crash in Minnesota, again.
Date: Jul 22, 1999
Thanks so much for your good thoughts, Bruce will be OK, they discovered some fractured vertebrae in his lower back so we're waiting to see about surgery. Learned that the problem (confirmed by the FAA investigator) was the rudder. Will try and keep you posted. ----- Original Message ----- From: <rick106(at)juno.com> Sent: Thursday, July 22, 1999 8:02 PM Subject: Re: Kolb-List: Kolb crash in Minnesota, again. > > Bruce and ALL > I hope all goes ok if I may and I hope that you all don't think that > this is tacky on my crash of my Mk.3 on father's day IF I did not have my > helment on I would not be here today their were tube marks all over the > helment. once again I hope and pray that BRUCE will be ok > > Rick Libersat > > writes: > > > >Thanks to all of all who expressed concern. Bruce's plane did go down > >yesterday (7/21) afternoon; he will be OK; FAA and TSB are > >investigating but > >the report I received from Bruce late last night indicated some > >problem with > >the tail; "it felt loose and I couldn't control it at all so I tried > >to stay > >over water and avoid a very crowded swimming beach". Will try and > >keepall of > >you posted on outcome of investigation and Bruce's physical status. > >Took > >them 30-45 minutes to extricate him from the plane. > >Please respond to this address with any questions. > >Thanks again for your concern and good thoughts. > >Helen Fletcher > >----- Original Message ----- > >From: <gerken(at)us.ibm.com> > >To: > >Sent: Thursday, July 22, 1999 7:11 AM > >Subject: Kolb-List: Kolb crash in Minnesota, again. > > > > > >> > >> See: > >> http://www.channel4000.com/news/stories/news-990721-150015.html > >> > >> Supposedly it is a Kolb Mkiii (according to last nights television > >news). > >Does > >> anyone know who the pilot was? My friend saw the news report and > >told me > >that > >> the pilot ended up with a pc of aluminum tube stuck thru his neck. > >Hopefully the > >> guy(s) is recovering OK. > >> I am not sure of whether the plane had floats or not. I heard he > >had > >just > >> taken off from across the lake and had 100' altitude when it fell > >off one > >side > >> and hit the water in a spiral. > >> > >> > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "Bruce Fletcher" <bwf(at)emailmn.com>
Subject: Re: Kolb crash in Minnesota, again.
Date: Jul 22, 1999
All I can say, Ralph, is that the FAA confirmed Bruce's feelings that it was the rudder that caused the problem. Obviously a much closer inspection will help us all learn more but that will take some time. Bruce has a few fractured vertebrae in his lower back and will be laid up for a while. I've been assured that the release of the plane from the Police impound lot will occur very soon and we will have the plane towed to our Medicine Lake property. Will try to keep you posted, please keep both of us in your good thoughts. Helen Fletcher ----- Original Message ----- From: Ralph H Burlingame <ul15rhb(at)juno.com> Sent: Thursday, July 22, 1999 7:11 PM Subject: Re: Kolb-List: Kolb crash in Minnesota, again. > > Hi All, > > Commenting on Bruce's Kolb Mark III that crashed yesterday out on > Medicine Lake in Plymouth MN, this was a modified Kolb with extended all > aluminum Titan wings, Rotax 912 80hp engine, IVO Magnum ground-adjustable > prop, Lotus monofloat with outrigger, retractable electric driven > gearlegs, and was built by the late Jim Lee. I flew with Bruce this past > Saturday as he met me at the private field I set up and launch from. One > of the things I first noticed was the loose tail-bracing. The bottom > cables were slack and I recommended that we replace the bottom wing nut > with a ny-lock one right away. I gave him a new one and watched him > replace it. There was still a lot of slack and I made some other > recommendations. We took off and flew to Winsted, about 20 miles away and > cruised 60 mph together. After our stay, we both took off and flew the > remaining distance back to the field while he continued on home. I gassed > up and flew over Medicine Lake to see if he made it back ok. I confirmed > that he did and flew the rest of the evening. It was last evening while > watching the local news that I saw the plane in the water while rescuer's > hauled him out on a stretcher. > > I hope Bruce is doing well and am anxious to find out the details of this > crash. > > Ralph Burlingame > Original FireStar, 447 powered > > > writes: > > > >Thanks to all of all who expressed concern. Bruce's plane did go down > >yesterday (7/21) afternoon; he will be OK; FAA and TSB are > >investigating but > >the report I received from Bruce late last night indicated some > >problem with > >the tail; "it felt loose and I couldn't control it at all so I tried > >to stay > >over water and avoid a very crowded swimming beach". Will try and > >keepall of > >you posted on outcome of investigation and Bruce's physical status. > >Took > >them 30-45 minutes to extricate him from the plane. > >Please respond to this address with any questions. > >Thanks again for your concern and good thoughts. > >Helen Fletcher > >----- Original Message ----- > >From: <gerken(at)us.ibm.com> > >To: > >Sent: Thursday, July 22, 1999 7:11 AM > >Subject: Kolb-List: Kolb crash in Minnesota, again. > > > > > >> > >> See: > >> http://www.channel4000.com/news/stories/news-990721-150015.html > >> > >> Supposedly it is a Kolb Mkiii (according to last nights television > >news). > >Does > >> anyone know who the pilot was? My friend saw the news report and > >told me > >that > >> the pilot ended up with a pc of aluminum tube stuck thru his neck. > >Hopefully the > >> guy(s) is recovering OK. > >> I am not sure of whether the plane had floats or not. I heard he > >had > >just > >> taken off from across the lake and had 100' altitude when it fell > >off one > >side > >> and hit the water in a spiral. > >> > >> > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: WVarnes(at)aol.com
Date: Jul 22, 1999
Subject: Re: Clevis Pins for Mark III and Firestar II
<< The enlargement is in the lower lift strut. When I drilled the holes for the clevis pins, they were a tight fit. I did use the 1/4 " drill >> johann, If you only need a few thousandths larger diameter pin to take up the slack, order some 'Close Tolerance Bolts' from one of the aviation suppliers. These bolts have a ground finish and are usually just a tad tighter fitting than a regular bolt or pin.Cut the bolts to the same length as the original pins, grind a radius on the cut end to make it easier to install and then drill a hole for the safety pin. Bill Varnes Audubon NJ USA Original FireStar 377 ________________________________________________________________________________
From: "Lindy" <lindy(at)snowhill.com>
"Tom Ferguson" , "Ted Cowan" , "Scott Sharon Wilcox" , "Sam Cox" , "Rutledge Fuller" , "Paul Spadin" , "Michael Highsmith" , "Kolb Builders" , "John Hauck" , "Greg Moloney" , "Fly Ultralights" , "Dave Thomas" , "Danny Day" , "Buddy Carilse" , "Bob Moorehead" , "ASC2"
Subject: Fw: 178 Seconds to Live
Date: Jul 22, 1999
----- Original Message ----- From: Ben Cole <bencole(at)mindspring.com> Sent: Thursday, July 22, 1999 9:17 PM Subject: FW: 178 Seconds to Live > >Return-Path: > >From: Roger Bitton <sptflt19(at)idt.net> > >Reply-To: "sptflt19(at)idt.net" > >To: "'bencole(at)mindspring.com'" > >Subject: FW: 178 Seconds to Live > >Date: Thu, 22 Jul 1999 07:10:46 -0700 > >Organization: Sport Flight Aviation > >Encoding: 81 TEXT > > > > > > > >-----Original Message----- > >From: John Talbert [SMTP:talbert(at)stonemedia.com] > >Sent: Wednesday, July 21, 1999 5:41 PM > >To: Alfred Langer; Bill Anderson; Brian Talbert; Christine Dow; Dan > >Paumier; Fred; Howard Pearce; Irene Langer; John; John Redwine; Tom > >Whitaker > >Subject: 178 Seconds to Live > > > >Here's a little insight into what might possibly have happened to John > >Kennedy Jr. > > > > > > > >178 Seconds to Live > > > > How long can a pilot who has little or no instrument training > >expect to > >live after he flies into bad weather and loses visual contact? > >Researchers at the University of Illinois did some tests and came up > >with some very interesting data. Twenty student "guinea pigs" flew into > >simulated instrument weather, and all went into graveyard spirals or > >roller coasters [attribute to the U of I flight training > >program??]. The outcome differed in only one respect - the time required > >till control was lost. The interval ranged from 480 seconds to 20 > >seconds. The average time was 178 seconds -- two seconds short of three > >minutes. > > > > Here's the fatal scenario. . . . . . . > >The sky is overcast and the visibility is poor. That reported five mile > >visibility looks more like two, and you can't judge the height of the > >overcast. > >Your altimeter tells you that you are at 1500 feet but your map tells > >you that there's local terrain as high as 1200 feet. There might be a > >tower nearby because you're not sure how far off course you are. But > >you've flown into worse weather than this, > >so press on. > > You find yourself unconsciously easing back just a bit on the > >controls to clear those towers. With no warning, you're in the soup. You > >peer so > >hard into the milky white mist that your eyes hurt. You fight the > >feeling in your stomach. You try to swallow, only to find your mouth > >dry. Now you realize you should have waited for better weather. The > >appointment was important, but not all that important. > >Somewhere a voice is saying, "You've had it -- it's all over!" > >You now have 178 seconds to live. > > Your aircraft feels on even keel but your compass turns slowly. You > >push a little rudder and add a little pressure on the controls to stop > >the > >turn but this feels unnatural and you return the controls to their > >original position. This feels better but now your compass is turning a > >little faster and your > >airspeed is increasing slightly. You scan your instruments for help but > >what you see looks somewhat unfamiliar. You're sure that this is just a > >bad spot. You'll break out in a few minutes. > >(But you don't have a few minutes left. . .) > > You now have 100 seconds to live. > >You glance at your altimeter and you are shocked to see it unwinding. > >You're already down to 1200 feet. Instinctively, you pull back on the > >controls but the altimeter still unwinds. The engine is into the red and > >the airspeed, nearly so. > > You have 45 seconds to live. > >Now you're sweating and shaking. There must be something wrong with the > >controls; pulling back only moves the airspeed indicator further into > >the red. You can hear the wind tearing at the aircraft. You are about to > >meet your Maker; you have 10 seconds to live. > > Suddenly you see the ground. The trees rush up at you. You can see > >the > >horizon if you turn your head far enough but it's at a weird angle -- > >you're almost inverted. You open your mouth to scream but. . . . . .. > >.you just ran out of seconds. > > > >Think about it before you press on into marginal weather > > > >-- > >Bob Cox robertcox(at)copper.net > >Pickerington Ohio ICQ # 23392522 > >Challenger II > >Home Page > > > > > > > > ________________________________________________________________________________
From: "Clarence R. Perry Jr." <perryr(at)123.net>
Subject: For Sale: Crashed Kolb Ultrastar
Date: Jul 22, 1999
For Sale: 1984 Kolb Ultrastar 100 Hours TTE/A Flew great until aborted take-off/crash in June 1999. Serious fuselage/landing gear damage (Cromoly steel) Some holes in wing covering from prop turning into toothpicks. Cuyuna UL/II Engine still runs great. I have all original build plans and revisions plus original builders notes/sales receipts. Comes with fully enclosed trailer. Helmet. Great project for someone who knows how to weld and has the time. Asking $2000.00 for all or trade for PPG. Located in Michigan. For Crash pics, see: http://mula.perrydice.com/ultrasta.htm For what it look like before/and trailer, see: http://mula.perrydice.com/robsnew.htm Thanks for your time, Rob Perry rob.perry(at)perrydice.com ________________________________________________________________________________
Date: Jul 22, 1999
From: "Eastman's Online Genealogy Newsletter" <newsletter(at)rootscomputing.com>
Subject: Re: FAA Sales
>Yes, the FAA does have and 'official' bill of sale form. It's main use when >individuals buy/sell a plane. I can't remember the OMB Form Number, but >when I was at the local FSDO yesterday, they had a stack of them sitting >there. AC Form 8050-2 which is called "Aircraft Bill of Sale." The instructions on the form state: "The Federal Aviation Act of 1958 requires the registration of each United States civil aircraft as a prerequisite to its operation. The applicant for registration must submit evidence of ownership that meets the requirements prescribed in Part 47 of the Federal Aviation Regulations. "This form identifies the aircraft being purchased, and provides space for purchaser and seller identification and signature. This is intended only to be a suggested bill of sale form which meets the recording requirements of the Federal Aviation Act, and......" If I interpret that correctly, the FAA suggests that you use this form but that is not a requirement. The top copy goes to the FAA, along with $5.00 as a filing fee. The second copy is kept by the purchaser. ________________________________________________________________________________
Date: Jul 22, 1999
From: Dennis & Diane Kirby <kirbyd(at)flash.net>
Subject: Full Enclosure
Dear Fellow Kolbers - Here's a question for you Mark-3 owners with the Full Enclosure: What is supposed to cover the area immediately aft of the door side bows? My full enclosure kit came with door frames and lexan to cover them, and the sewn vinyl enclosure for the rear top half of the fuselage cage, but no reference to that area just aft of the doors. I'm thinking of installing cut-to-fit sixteenth-inch lexan sheets. That would be an easy addition. But I still wonder if that was the original intent for the "full enclosure." What have you been-there-built-that Mark-3 owners done in this area? A related question: if I do install tall, triangularish lexan panels there, what would happen if I flew with the doors removed? Seems to me you'd have a pair of big scoops sticking out the sides, causing boatloads of drag. This sort of follows Peter Volum's earlier concerns on wanting to see pictures of the full enclosure - any input would help me too. Thanks - Dennis Kirby Mark-3 in Cedar Crest, New Mexico s/n 300, 80% finished ________________________________________________________________________________
Date: Jul 23, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Full Enclosure
I don't have my vinyl enclosure any more, but yours should have come with two curved 1/2" tubes. These tubes will fit just inside the rear edge of your door Lexan when the doors are closed. (one on each side) The vinyl enclosure fit over the tubes, and ran back to the edge of the fuselage, where it was attached with velcro. The upper back part of the rear enclosure, the back part of it wraps around the vertical tubes that run from the side of the cage up to the front spar carrythrough. Velcro tabs attach the lower edge to the cross bar that runs just above and behind the seats. I can't remember what the top was attached to. The aluminum 1/2" tubes (side bows) were attached to that little threaded nut plate that you install on the fuselage gusset near the lower rear corner of the doors, and a gusset that was formed and bolted to the windshield support tube. If you use lexan rigid side windows, you can still use the same side bow, to attach the lexan to, just not the vinyl rear enclosure. You cannot fly with the side bows in place and the doors off, either with the rigid rear windows, or the vinyl rear enclosure, the wind will wreck it. I have located all three sheets from kolb showing how the side bows, & rear lexan was to be fabricated and installed. If Mustek EVER sends me a power adapter for my scanner, I will send you a .jpg copy of the pages. Richard Pike MKIII N420P (42OldPoops) > >Dear Fellow Kolbers - >Here's a question for you Mark-3 owners with the Full Enclosure: What >is supposed to cover the area immediately aft of the door side bows? My >full enclosure kit came with door frames and lexan to cover them, and >the sewn vinyl enclosure for the rear top half of the fuselage cage, but >no reference to that area just aft of the doors. I'm thinking of >installing cut-to-fit sixteenth-inch lexan sheets. That would be an >easy addition. But I still wonder if that was the original intent for >the "full enclosure." What have you been-there-built-that Mark-3 owners >done in this area? A related question: if I do install tall, >triangularish lexan panels there, what would happen if I flew with the >doors removed? Seems to me you'd have a pair of big scoops sticking out >the sides, causing boatloads of drag. This sort of follows Peter >Volum's earlier concerns on wanting to see pictures of the full >enclosure - any input would help me too. Thanks - >Dennis Kirby >Mark-3 in Cedar Crest, New Mexico >s/n 300, 80% finished ________________________________________________________________________________
From: "Beauford Tuton" <beaufordw(at)worldnet.att.net>
Subject: Re: Painting cage
Date: Jul 23, 1999
Frank and Winnie: I left out one little detail about putting the acrylic enamel on over the epoxy.... You probably knew this already, but wait to apply the acrylic until AFTER you have covered the cage, and only use the acrylic for cosmetic appearances on the exposed parts which will not be exposed to the MEK-based Stits poly products.... The MEK will, of course, do a job on the acrylic enamel... Bill Tuton -----Original Message----- From: Frank & Winnie Hodson <fwhodson(at)bigfoot.com> Date: Thursday, July 22, 1999 12:37 AM Subject: RE: Kolb-List: Painting cage > > >> I'm getting ready to paint the fuselage and the small parts >> associated with >> it. I have read of parts that are hard to fit when they are painted. Any >> recommendation of which areas to mask off. >> > >Dear Will: > >A good rule of thumb for surfaces that if painted may cause trouble is if >these parts need to be sleeved into another part. Aileron control horns, >horizontal stabilizer attachment horns, the inside surfaces of the tail boom >receiving rings etc. > >I used a STITS (POLYFIBER) two part epoxy primer with good luck. I was able >to remove unwanted/excess coverage over the next several weeks with the >associated epoxy reducer and polyfiber reducer. > >Good Luck: FRANK HODSON, Oxford ME > > ________________________________________________________________________________
From: "Chris Sudlow" <suds77(at)earthlink.net>
Subject: nose cone install
Date: Jul 23, 1999
Group, I'm installing/fitting the nose cone on the Mark III. Is it better to bolt, or rivet, the cone and the nose skid to the cage? Thanks for any suggestions. chris ________________________________________________________________________________
Date: Jul 23, 1999
From: Ron Hoyt <Ronald.R.Hoyt@gd-is.com>
Subject: Re: nose cone install
Riveting is easier. However, I wanted to get inside the area for break maintenance rather than stand on my head so I bolted it on. I also extended the instrument panel forward 6" making the peddle area harder to access. > > >Group, > >I'm installing/fitting the nose cone on the Mark III. Is it better to bolt, >or rivet, the cone and the nose skid to the cage? > >Thanks for any suggestions. > >chris > > ________________________________________________________________________________
From: dama(at)mindspring.com
Subject: Wing Rigging
Date: Jul 23, 1999
I am about to rig the wings on my FSII and have a couple of questions. First how important is the electronic level? It seems to me that setting the boom to a negative 4 degree angle is a preliminary thing and the final adjustment is lining up the wing tabs to the cage tabs. Therefore the precision of the electronic level is not needed. Secondly, with the cage leveled, is the tail supposed to be that high off the ground. It seems that the thing would be flying very nose low. Any other advice for this part of the project is very welcomed. Sincereley, Kip Laurie FS-705 Atlanta -----Original Message----- From: Ralph H Burlingame <ul15rhb(at)juno.com> Date: Wednesday, July 21, 1999 7:58 PM Subject: Kolb-List: 178 seconds > > >178 Seconds to Live > >How long can a pilot who has little or no instrument training expect to >live after he flies into bad weather and loses visual contact? > >Researchers at the University of Illinois did some tests and came up >with some very interesting data. Twenty student "guinea pigs" flew into >simulated instrument weather, and all went into graveyard spirals or >roller coasters [attribute to the U of I flight training program??]. The >outcome differed in only one respect - the time required till control was >lost. The interval ranged from 480 seconds to 20 seconds. The average >time was 178 seconds -- two seconds short of three minutes. > >Here's the fatal scenario. . . . . . . >The sky is overcast and the visibility is poor. That reported five mile >visibility looks more like two, and you can't judge the height of the >overcast. Your altimeter tells you that you are at 1500 feet but your map >tells >you that there's local terrain as high as 1200 feet. There might be a >tower nearby because you're not sure how far off course you are. But >you've flown into worse weather than this, so press on. >You find yourself unconsciously easing back just a bit on the >controls to clear those towers. With no warning, you're in the soup. >You peer so hard into the milky white mist that your eyes hurt. You fight > >the feeling in your stomach. You try to swallow, only to find your mouth >dry. Now you realize you should have waited for better weather. The >appointment was important, but not all that important. >Somewhere a voice is saying, "You've had it -- it's all over!" >You now have 178 seconds to live. >Your aircraft feels on even keel but your compass turns slowly. You >push a little rudder and add a little pressure on the controls to stop >the turn but this feels unnatural and you return the controls to their >original position. This feels better but now your compass is turning a >little faster and your airspeed is increasing slightly. >You scan your instruments for help but what you see looks somewhat >unfamiliar. You're sure that this is just a bad spot. You'll break out in >a few minutes. > >(But you don't have a few minutes left. . .) > >You now have 100 seconds to live. >You glance at your altimeter and you are shocked to see it unwinding. >You're already down to 1200 feet. Instinctively, you pull back on the >controls but the altimeter still unwinds. The engine is into the red and >the airspeed, nearly so. You have 45 seconds to live. >Now you're sweating and shaking. There must be something wrong with the >controls; pulling back only moves the airspeed indicator further into >the red. You can hear the wind tearing at the aircraft. You are about to >meet your Maker; you have 10 seconds to live. Suddenly you see the >ground. The trees rush up at you. You can see the horizon if you turn >your head far enough but it's at a weird angle -- > >you're almost inverted. You open your mouth to scream but. . . . . .. >you just ran our of seconds. > >Think about it before you press on into marginal weather > >Lucian Bartosik > > ________________________________________________________________________________
Date: Jul 23, 1999
From: Terry Swartz <tswartz(at)desupernet.net>
Subject: Re: Full Enclosure
I used 1/16 Lexan for the side and rear enclosure and it works out very well. One piece for the back and two more pieces, one on each side. I will take some pictures and e-mail them to you as soon as I get to the airport. Terry Dennis & Diane Kirby wrote: > > Dear Fellow Kolbers - > Here's a question for you Mark-3 owners with the Full Enclosure: What > is supposed to cover the area immediately aft of the door side bows? My > full enclosure kit came with door frames and lexan to cover them, and > the sewn vinyl enclosure for the rear top half of the fuselage cage, but > no reference to that area just aft of the doors. I'm thinking of > installing cut-to-fit sixteenth-inch lexan sheets. That would be an > easy addition. But I still wonder if that was the original intent for > the "full enclosure." What have you been-there-built-that Mark-3 owners > done in this area? A related question: if I do install tall, > triangularish lexan panels there, what would happen if I flew with the > doors removed? Seems to me you'd have a pair of big scoops sticking out > the sides, causing boatloads of drag. This sort of follows Peter > Volum's earlier concerns on wanting to see pictures of the full > enclosure - any input would help me too. Thanks - > Dennis Kirby > Mark-3 in Cedar Crest, New Mexico > s/n 300, 80% finished > ________________________________________________________________________________
From: "Frank & Winnie Hodson" <fwhodson(at)bigfoot.com>
Subject: Wing Rigging
Date: Jul 23, 1999
> > I am about to rig the wings on my FSII and have a couple of > questions. First > how important is the electronic level? Secondly, with the cage leveled, > is the tail > supposed to be that high off the ground. It seems that the thing would be > flying very nose low. Any other advice for this part of the > project is very > welcomed. > Sincereley, > Kip Laurie FS-705 > Atlanta IMHO the precision level is very desirable (read necessary) for several stages of the project: -The leveling of the saw horses/table to build the wings. -The rigging of the wings to the cage. -For calculating the weight and balance. As for the tail being so high during the rigging process: Yes it does need to be that high to be able to level the wings. This attitude does not reflect the final flying angle, as the wings will have to have a positive angle of incidence to the flight path to develop the required lift, especially in slow flight, and the fuselage will be more level. Good Luck: Frank Hodson, Oxford ME (FS II N6399J) ________________________________________________________________________________
Date: Jul 23, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Wing Rigging
Don't think about nose low or tail high, that's irrelevant. Think about wing angle of attack. When the thing is trimmed out right, you will be flying with the wing at a slight positive angle of attack, 4 or 5 degrees at normal cruise. The stabilizer will be one or two degrees front down, the wing will be 4 or 5 degrees front up. You could care less what angle the tail boom is at. And the lower the nose cone, the better you can see out. Enjoy. Richard Pike MKIII N420P (42Oldpoops) > >I am about to rig the wings on my FSII and have a couple of questions. First >how important is the electronic level? It seems to me that setting the boom >to a negative 4 degree angle is a preliminary thing and the final adjustment >is lining up the wing tabs to the cage tabs. Therefore the precision of the >electronic level is not needed. Secondly, with the cage leveled, is the tail >supposed to be that high off the ground. It seems that the thing would be >flying very nose low. Any other advice for this part of the project is very >welcomed. >Sincereley, >Kip Laurie FS-705 >Atlanta ________________________________________________________________________________
Date: Jul 23, 1999
From: "Douglas G. Murray" <dgmurray(at)telusplanet.net>
Subject: Re: Wing Rigging
> I am about to rig the wings on my FSII and have a couple of questions. First > how important is the electronic level? It seems to me that setting the boom > to a negative 4 degree angle is a preliminary thing and the final adjustment > is lining up the wing tabs to the cage tabs. Therefore the precision of the > electronic level is not needed. Secondly, with the cage leveled, is the tail > supposed to be that high off the ground. It seems that the thing would be > flying very nose low. Any other advice for this part of the project is very > welcomed. > Sincereley, > Kip Laurie FS-705 > Atlanta Yup - the nose is real low and it will be there in flight so that you can have an incredible view. You don't really need an electronic level but if there is one available it will speed up the process. The most important thing is to triple check ALL the measurements BEFORE drilling those alignment holes. Make sure the wings have the same incidence. You might be off in degrees in relation to the longitudinal plane but be sure that BOTH wings are at the same angle of incidence. Start with a 1/8" bit and work up to a size just smaller than the finished size needed. Then use a UNIBIT drill to 'ream' the final hole size. A twist drill bit doesn't leave a perfectly round hole for the clevis pin to sit in and reamers can be costly. Doug Murray FireStar 1 Flying since 1990 Southern Alberta ________________________________________________________________________________
From: "Frank & Winnie Hodson" <fwhodson(at)bigfoot.com>
Subject: Is anybody home????
Date: Jul 23, 1999
> Hello Frank > You can call me for tech questions I will try to help you as much > as I can. > For tech questions call me @ 717-362-1057 > > John Yates > Chief Operating Officer > 606-862-9692 610-948-4136 717-362-1057 > www.tnkolbaircraft.com > tnkolbaircraft@sun-spot.com > www.kolbaircraft.com > johny(at)epix.net FYI KOLBERS: I was able to reach John today at 717-362-1057. He was very helpful and empathetic to my situation. The phone numbers to TNK are still connected to an answering machine, including the additional number specifically set aside for the parts department. The message clearly states that normal hours are until 5 PM (even though my calls have all been around 4 PM). The part that I needed was ordered through John who FAX'D it through to the company...time will tell! Also of interest Esther Kolb called to say that she will be making a personal trip shortly and will obtain the necessary signatures for the AC form # 8050-2. She thinks I should have it in hand in about two weeks. FRANK HODSON: OXFORD ME P.S. Anybody have any comments on the area code disparity for the company numbers? ________________________________________________________________________________
Date: Jul 23, 1999
From: "Douglas G. Murray" <dgmurray(at)telusplanet.net>
Subject: Re: nose cone install
> > > Group, > > I'm installing/fitting the nose cone on the Mark III. Is it better to bolt, > or rivet, the cone and the nose skid to the cage? > > Thanks for any suggestions. > > chris > Chis - I pop riveted my nose cone on. To get to the back of the IP I ended up cutting out the fiberglass dash panel and making an aluminum IP supported on four Cessna IP Lord shock mounts. I haven't had a problem in 8 years and if I need to get behind the panel I just undo four nuts and the panel lays down onto the floor. Doug Murray FireStar 1 Flying since 1990 Southern Alberta ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: nose cone install
Date: Jul 23, 1999
I don't know how often it may be a factor, but I wanted to be able to remove the nose cone fairly easily, in case I need to work on something, or fix some damage, or whataever. So, instead of using rivets, I ordered a bunch of the AN366F-832 anchor nuts, on page 90 of the '98-'99 A/C Spruce catalog. Used round headed screws with large washers on the outside, to avoid cracking the fiberglass. Might be overkill, I guess, but I've had it on and off a couple of times already, and it comes off, and goes back on easily and solidly in just a few minutes. Lining them up to the screw holes and getting ready to rivet them was a bitch. Also, they're meant for solid rivets, and I had to - carefully - open the holes up to 1/8" for the pop-rivets. The anchor nuts have ny-loc inserts, so they shouldn't (??) come loose under vibration. Big Lar. ----- Original Message ----- From: Douglas G. Murray <dgmurray(at)telusplanet.net> Sent: Friday, July 23, 1999 7:58 PM Subject: Re: Kolb-List: nose cone install > > > > > > > > Group, > > > > I'm installing/fitting the nose cone on the Mark III. Is it better to bolt, > > or rivet, the cone and the nose skid to the cage? > > > > Thanks for any suggestions. > > > > chris > > > > Chis - I pop riveted my nose cone on. To get to the back of the IP I ended up > cutting out the fiberglass dash panel and making an aluminum IP supported on > four Cessna IP Lord shock mounts. I haven't had a problem in 8 years and if I > need to get behind the panel I just undo four nuts and the panel lays down onto > the floor. > > Doug Murray FireStar 1 Flying since 1990 > Southern Alberta > > ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Welding
Date: Jul 23, 1999
Well folks, I bragged about the powder coating shop, and I bragged about the machine shop. Doesn't look like I can brag too much about my choice of welders. This guy came down here last weekend with a truck load of equipment, and welded up the door frames, and matching - sills ??, I guess you'd call them ?? Anyway, the solid part the door closes against. He didn't do too bad on the doors, and he admitted he was more used to heavy steel plate. Ran a couple of practise beads on some scrap tubing, and away he went. Frames were fine, and lower edge of the sills are fine, the upper side of the center is fine, BUT --- now we get to the underside of the center, where the hinges and center support rod for the gull wings meet the upper frame loop. Started grinding it smooth this afternoon, before the gnats (no-see-ums) drove me back in the house. That one section looks like a semi-terminal case of pin-hole, and not-so-pin-hole cancer. This isn't a structural area, but it is cosmetic, and I want it better than that. I have in mind to center punch the worst of them, to dimple them, then get my oxy-acetylene torch and fill braze it fairly smooth. Then polish it out, and paint. Any thoughts or suggestions ?? I don't think bondo or such would hold in such a limited area - about 4" of " chromoly tubing. Today I went and got the air compressor and sand blaster (bead blaster) from work, and plan on using it tomorrow to prep for painting. Someone mentioned a concern for work hardening the parts - as in bead blasting a crankshaft to toughen it. That may be, but I believe it would take a lot more than I'll be giving this. Then too, as I say, it's a non-structural area. Any thoughts on That ?? Before I paint, I'll take some pics, if anyone's interested. Tomorrow, I'll be going to the dragster builders shop, and we'll have at the engine mount, and the fuel injection throttle body. The plan is to graft a Ford Tempo throttle body onto a VW type 3 fuel inj. intake. Should be interesting. Gives about 3 times the intake area. This brute should Breathe ! ! ! I'll keep you-all posted. Go-Gittum Lar. ________________________________________________________________________________
Date: Jul 24, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re: Water landings.
Any of you guys interested in knowing how to make a "water landing" in a Firestar without floats and without getting killed "as per the late Mr. Kennedy-the good die young and all of that" - not an expert, but have made one, and I hope the last one. Have pictures - and can tell you how it feels. At least what "not" to do. I guess the best advice is not to do it at all, but most of the time the water is better than the treesif you have a choice, I got some tree pictures too if you want to see them. ________________________________________________________________________________
Date: Jul 24, 1999
From: Terry Swartz <tswartz(at)desupernet.net>
Subject: Re: Is anybody home????
Frank 717 area code is South Central PA, Lancaster, Harrisburg area where I live. Terry Frank & Winnie Hodson wrote: > > > Hello Frank > > You can call me for tech questions I will try to help you as much > > as I can. > > For tech questions call me @ 717-362-1057 > > > > John Yates > > Chief Operating Officer > > 606-862-9692 610-948-4136 717-362-1057 > > www.tnkolbaircraft.com > > tnkolbaircraft@sun-spot.com > > www.kolbaircraft.com > > johny(at)epix.net > > FYI KOLBERS: > > I was able to reach John today at 717-362-1057. He was very helpful and > empathetic to my situation. > The phone numbers to TNK are still connected to an answering machine, > including the additional number specifically set aside for the parts > department. The message clearly states that normal hours are until 5 PM > (even though my calls have all been around 4 PM). > The part that I needed was ordered through John who FAX'D it through to the > company...time will tell! > Also of interest Esther Kolb called to say that she will be making a > personal trip shortly and will obtain the necessary signatures for the AC > form # 8050-2. She thinks I should have it in hand in about two weeks. > > FRANK HODSON: OXFORD ME > > P.S. Anybody have any comments on the area code disparity for the company > numbers? > ________________________________________________________________________________
From: "Brian Hale" <AccessToData(at)email.msn.com>
Subject: Re: Is anybody home????
Date: Jul 24, 1999
> I was able to reach John today at 717-362-1057. He was very helpful and > empathetic to my situation I called TNK at 606 862 9622 and got right thru to the receptionist. She confirmed that my order was ready. Nice southern accent too. Brian Hale Sacramento, CA. ________________________________________________________________________________
From: DBindl(at)cs.com
Date: Jul 24, 1999
Subject: Re: Water landings.
In a message dated 7/24/99 1:27:06 AM Central Daylight Time, possums(at)mindspring.com writes: << Have pictures - and can tell you how it feels. >> I for one would be very interested! Daniel ________________________________________________________________________________
From: WillU(at)aol.com
Date: Jul 24, 1999
Subject: Re: Wing Rigging
In a message dated 7/24/99 10:24:06 AM Mountain Daylight Time, dama(at)mindspring.com writes: > Secondly, with the cage leveled, is the tail > supposed to be that high off the ground. It seems that the thing would be > flying very nose low. Any other advice for this part of the project is very > welcomed. Here is a picture of a FireStar II flying so you can get an idea of how high the tail is in flight. It's not a very good picture because I scanned it from a print out Tim gave me. http://members.aol.com/WillU/tl20.jpg Regards Will Uribe El Paso, TX Building a FireStar II http://members.aol.com/WillU/index.html ________________________________________________________________________________
From: "Adam Violett" <aviolett(at)worldinter.net>
Subject: Re: Water landings.
Date: Jul 24, 1999
Absolutely interested! Please, do tell about both. Adam Original Firestar, Kansas City area > Any of you guys interested in knowing how to make a "water landing" in a > Firestar without floats and without getting killed I got some tree pictures too if you want to see them. ________________________________________________________________________________
Date: Jul 24, 1999
From: Tom Barton <barton(at)ameslab.gov>
Subject: Mark II tailwheel gear needed
Since I'm really desparate I'll try again. I am the not-so-proud, new owner of a restored Kolb Mark II (with R582 and FL amphib floats) which I have never flown since the tailwheel assembly was totally destroyed by improperly securing it for transit from Mississippi to Iowa in a UHaul truck. Thus by telephone we ordered from Kolb a steerable tailwheel to be delivered by FedEx (an extra $22). I don't know what the heck I was sent, nor do any of the A&P's and homebuilders at our airport, but it most certainly is not a steerable tailwheel for a Kolb Mark II. It for all the world just looks like a bunch of thin-walled tubes randomly welded together as if for a practice piece in a high school welding class (that at least was the best guess by a local A&P with extensive experience in UL's). Thus, I would appreciate learning where I can purchase quickly a steerable tailwheel that would work on my Kolb Mark II (not III). Nothing I can find in catalogs would seem to work since the Mark II uses a 3/4" Al tailrod and everything else seems to attach to a flat plate. I have no idea what the other Kolb models use since this is the first Kolb I've ever seen as no one else has one around here. Our summers don't last long up here and I really want to fly this bird before putting it up for the winter. Thanks, Tom (Tom Barton, 815 Onyx Circle, Ames, IA 50010, 515-294-2770) P.S. I plan to return that thing that Kolb sent yesterday, but I still want to know what the heck it is. I'd include some pictures but someone vandalized my digital camera. It's not been a good summer! P.P.S. Please do not suggest the use of a grocery cart wheel as it is not the wheel but the system of attachment that I need. ________________________________________________________________________________
From: WillU(at)aol.com
Date: Jul 24, 1999
Subject: Re: Mark II tailwheel gear needed
Hi Tom A search of the Kolb list archives turned this up http://members.aol.com/n8754k/page/ssdc537.jpg This is the 4 inch diameter "homebuilders special" special tailwheel from Aircraft Spruce. P/N L-693 is made for a 5/8" round spring, so it has to be bored out to 3/4" for the SlingShot tail rod. I'm not sure if that's the same size as other Kolbs. Watch you wallet and CG because this wheel is $223, and it weighs 2 lbs more than the original wheel. The beauty of it is that it's full swivel and makes the plane a dream to move around on the ground. Also, it's far wider than the original wheel, so it doesn't disc the runway as you go :-) Good Luck Will Uribe El Paso, TX Building a FireStar II Will's FireStar II In a message dated 7/24/99 4:22:08 PM Mountain Daylight Time, Tom Barton writes: > Thus, I would appreciate learning where I can purchase quickly a steerable > tailwheel that would work on my Kolb Mark II (not III). Nothing I can find > in catalogs would seem to work since the Mark II uses a 3/4" Al tailrod and > everything else seems to attach to a flat plate. ________________________________________________________________________________
From: HShack(at)aol.com
Date: Jul 24, 1999
Subject: Re: Water landings.
In a message dated 7/24/99 2:19:17 AM Eastern Daylight Time, possums(at)mindspring.com writes: << Any of you guys interested in knowing how to make a "water landing" in a Firestar without floats and without getting killed "as per the late Mr. Kennedy-the good die young and all of that" >> Please tell us... Howard Shackleford FS I SC ________________________________________________________________________________
From: WGeorge737(at)aol.com
Date: Jul 24, 1999
Subject: Re: Mark II tailwheel gear needed
In a message dated 7/24/99 10:43:28 AM, barton(at)ameslab.gov writes: << Thus, I would appreciate learning where I can purchase quickly a steerable tailwheel that would work on my Kolb Mark II (not III). Nothing I can find in catalogs would seem to work since the Mark II uses a 3/4" Al tailrod and everything else seems to attach to a flat plate. >> Tom: I searched for a more substantial piece to replace the tailwheel on my Mk-3. I located a light weight steerable tailwheel assembly to accept the 3/4 strut. I got it last week but have not installed it yet. I sent some 4130 tubing out to get heat treated and it has not come back yet. It will be used instead of the aluminum rod. The tailwheel is only 4 inches in diameter but is very substantial. The only problem I have found prior to installing it is the that the hole is .745 instead of .750 so I will have to take it to a machine shop and get it enlarged a bit. The manufacturer is Aviation Products Inc. 805-646-6042 Good luck Bill George Mk-3 582 Powerfin ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Busy Day
Date: Jul 24, 1999
Today is finally winding down, and ole Lar is about wore out. This morning, Vamoose came off the porch and into the driveway for the 1st time, and got a much needed bath. Soaked with sweat Lar needed (and got) one too. 104 out there by 9:00 AM. Then out to my friends' shop in Banning. Turns out Gary Fore owns "ForePlay Racing," and races in A Gas Supercharged. He's held ET and Top Speed records for some years now. What a shop the man has. And talk about TOYS ! ! ! Hoooooeee ! ! ! The Plasma cutter made short work of the engine mount material, and the milling machine squared the sides up. Such a deal ! ! ! Then he cut the nose off the VW type 3 F.I. intake, milled it square, and milled a chunk of aluminum to an exact (read that as Precise) fit to the 2.3L Ford throttle body. Then heli-arced that to the front of the cut down intake, so now the Ford throttle body bolts right up to my VW intake. The thing looks like it grew there. Next week the whole intake system will go to the powder coater. I got the final pieces (pushrods) on the engine yesterday, so by next weekend, the engine should be sitting in its' mounts on top of Vamoose. Hell of a deal. Too bad it won't be ready for vacation next month. Sure hope Ben doesn't hold me to that rash statement I made about Golden West in Sept. Guess I'd just have to snivel out. Sorry Ben, I'll be coming from the North, and won't be able to "carry" my plane up there. Actually, I really had planned on trailering it to Merced. Thought that would be worth a few chuckles, and maybe draw some interest, but I just don't think the timing will work out. Vacation ends on Sept.12th, and I'll really be moving by then, heading home after 3 weeks on the road. Worn Out Lar. ________________________________________________________________________________
Date: Jul 25, 1999
From: Jerry Bidle <jbidle(at)airmail.net>
Subject: Re: Source for Full Swivel Tailwheel
One of the past SlingShot builders put one on his plane. If I recall he got his from Aircraft Spruce. I suggest your call them or more likely their source below and save a few bucks. The RV-4 & 6 builders have similar need and tail wheel spring (rod) size may be nearly the same. RV'ers usually they order or swap the tail spring (rod) for a modified unit turned down to slightly smaller than 3/4". Because of there speed (RV's) the mount has to be tight to prevent shimmy. They actually use heat and cold when installing them. I don't think this is a necessary step with Kolb but may explain Bill's statement below. Here's a source that sells full swivel tail wheels: (These are the one the RV'ers are using) Aviation Products Inc. 114 Bryant Ojai, CA 93023 Tel: 805-646-6042. Price was around $180 Ask what they are bored out to - compare that to what you need and if necessary if they can supply a different size if necessary. I understand these folks are pretty good to work with. Post your findings. Good luck, they work real well on RV's. Jerry Bidle > > >In a message dated 7/24/99 10:43:28 AM, barton(at)ameslab.gov writes: > ><< Thus, I would appreciate learning where I can purchase quickly a steerable >tailwheel that would work on my Kolb Mark II (not III). Nothing I can find >in catalogs would seem to work since the Mark II uses a 3/4" Al tailrod and >everything else seems to attach to a flat plate. >> > >Tom: > >I searched for a more substantial piece to replace the tailwheel on my Mk-3. >I located a light weight steerable tailwheel assembly to accept the 3/4 >strut. I got it last week but have not installed it yet. I sent some 4130 >tubing out to get heat treated and it has not come back yet. It will be used >instead of the aluminum rod. The tailwheel is only 4 inches in diameter but >is very substantial. The only problem I have found prior to installing it is >the that the hole is .745 instead of .750 so I will have to take it to a >machine shop and get it enlarged a bit. > >The manufacturer is Aviation Products Inc. 805-646-6042 > >Good luck > >Bill George >Mk-3 582 Powerfin > > ________________________________________________________________________________
Date: Jul 25, 1999
Subject: nose cone attachment
From: Robert L Doebler <bobdoebler(at)juno.com>
I"ve always attached fiberglass cowlings, that I later wanted to remove with aluminum piano hinges. Just like we install our control surfaces. Pull the hinge pin and cowling comes off. Also, piano hinge helps support the fiberglass. works for me Bob Doebler ________________________________________________________________________________
From: BILLBEAM(at)aol.com
Date: Jul 25, 1999
Subject: Re: New Kolb Co.
Bob, I too have visited the New Kolb facility and agree with you whole heartily. They spent a fortune just putting in sprinklers for that half mile of sod. I agree that it is great for us Kolbers to have some folks like them take over. Once they get the rough edges smoothed out I believe they will be a Class A company. Did you get to see their new creation for Oshkosh? Heard it climbs like an Otis Elevator. Bruce has always been a creator of the spectacular. This year should be no different. I believe that by winter we will see a bigger and better company. They have the foundation for it. Bill Beams FS438 Wilmore, Ky ________________________________________________________________________________
From: Lrb1476(at)aol.com
Date: Jul 26, 1999
Subject: Heavy Ailerons
Fellow Kolbers, I'm learning how to fly my new Mk lll, and have already bent a gear leg........ordered a new one and am flying with only one week down time. It's hard to get used to the sink rate. If I cut power too much at landing, it comes down pretty fast !!!! My kit is #289, and doesn't have aileron counterbalances like some of the older Mk lll's. My ailerons are quite heavy, and I would like to lighten them up (a little). I remember this discussion in the past, but never came to a clear cut conclusion. Does the factory still make them or were they in the older blue prints? I realize they would have to be added after the fact. Does anyone have an opinion..... It seems like the factory discontinued the counterbalances..... for a reason? ________________________________________________________________________________
Date: Jul 26, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Heavy Ailerons
Don't think the aileron counterbalances will solve the problem. Counterbalances are to prevent aileron flutter, and would not affect the heaviness of the ailerons. I agree that the ailerons are very heavy, especially compared to the very light rudder and elevator. I suspect that the best solution would be spades mounted on the bottom of the ailerons, about in the middle of each one. But that will be a good project for this winter, when I can't fly. Right now it is better to fly a good airplane with heavy ailerons. P.S. Some of the early Rans S-12 Airailes had ailerons that were heavy as sin, and the company came out with a spade kit. Anybody know someone that has/had such a beast, and might have plans, pictures, etc. of those spades? Hate re-inventing the wheel. (Maybe I should just call Rans?) Richard Pike MKIII N420P (42OldPoops) > >Fellow Kolbers, >My kit is #289, and doesn't have aileron counterbalances like some of the >older Mk lll's. My ailerons are quite heavy, and I would like to lighten them >up (a little). I remember this discussion in the past, but never came to a >clear cut conclusion. > >Does the factory still make them or were they in the older blue prints? I >realize they would have to be added after the fact. Does anyone have an >opinion..... It seems like the factory discontinued the counterbalances..... >for a reason? ________________________________________________________________________________
Date: Jul 26, 1999
From: Terry Swartz <tswartz(at)desupernet.net>
Subject: Re: Heavy Ailerons
Richard There is a guy, don't know his name, from NJ. That comes to the Father's Day fly-in here in PA with a Rans S-12 with spades. If I see him or find out who he is I'll take some pictures. As I recall, they were quite complex because the spades hinged depending on the amount of aileron deflection. This same fellow may come to the Labor Day fly-in. I'm also going to Oshkosh and I keep an I out. Terry Richard Pike wrote: > > Don't think the aileron counterbalances will solve the problem. > Counterbalances are to prevent aileron flutter, and would > not affect the heaviness of the ailerons. > I agree that the ailerons are very heavy, especially > compared to the very light rudder and elevator. > I suspect that the best solution would be spades > mounted on the bottom of the ailerons, > about in the middle of each one. > But that will be a good project for this winter, when I can't fly. > Right now it is better to fly a good airplane with heavy ailerons. > > P.S. Some of the early Rans S-12 Airailes had ailerons that > were heavy as sin, and the company came out with a spade kit. > Anybody know someone that has/had such a beast, > and might have plans, pictures, etc. of those spades? > Hate re-inventing the wheel. > (Maybe I should just call Rans?) > Richard Pike > MKIII N420P (42OldPoops) > > > > >Fellow Kolbers, > > >My kit is #289, and doesn't have aileron counterbalances like some of the > >older Mk lll's. My ailerons are quite heavy, and I would like to lighten them > >up (a little). I remember this discussion in the past, but never came to a > >clear cut conclusion. > > > >Does the factory still make them or were they in the older blue prints? I > >realize they would have to be added after the fact. Does anyone have an > >opinion..... It seems like the factory discontinued the counterbalances..... > >for a reason? > ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: Heavy Ailerons
Date: Jul 26, 1999
I have Mk III kit # 274, and received the aileron counterbalance on request, at no charge. If they're not available any more, I could easily measure mine and send them to you. They'd be very simple to build. On the spade question, here's another question. Since the counterbalance already ties into the outer end of the aileron, and points forward, it should almost act as a spade as it is. How about fastening a small tab to the front of it to give more leverage ?? By slowly making the tab larger - in small steps - couldn't you tailor the aileron effort to your own taste ?? Thanks for bringing this up, I would really like an answer from some of the engineer types out there. Big Lar. ----- Original Message ----- From: <Lrb1476(at)aol.com> Sent: Monday, July 26, 1999 11:44 AM Subject: Kolb-List: Heavy Ailerons > > Fellow Kolbers, > > I'm learning how to fly my new Mk lll, and have already bent a gear > leg........ordered a new one and am flying with only one week down time. It's > hard to get used to the sink rate. If I cut power too much at landing, it > comes down pretty fast !!!! > > My kit is #289, and doesn't have aileron counterbalances like some of the > older Mk lll's. My ailerons are quite heavy, and I would like to lighten them > up (a little). I remember this discussion in the past, but never came to a > clear cut conclusion. > > Does the factory still make them or were they in the older blue prints? I > realize they would have to be added after the fact. Does anyone have an > opinion..... It seems like the factory discontinued the counterbalances..... > for a reason? > > ________________________________________________________________________________
Date: Jul 26, 1999
From: Maurice Shettel <mshettel(at)mindspring.com>
Subject: Re: Heavy Ailerons
Has anyone tried servo tabs on their ailerons? Im thinking of going this route sometime this winter. Should work well if done right. Maurice Richard Pike wrote: > > Don't think the aileron counterbalances will solve the problem. > Counterbalances are to prevent aileron flutter, and would > not affect the heaviness of the ailerons. > I agree that the ailerons are very heavy, especially > compared to the very light rudder and elevator. > I suspect that the best solution would be spades > mounted on the bottom of the ailerons, > about in the middle of each one. > But that will be a good project for this winter, when I can't fly. > Right now it is better to fly a good airplane with heavy ailerons. > > P.S. Some of the early Rans S-12 Airailes had ailerons that > were heavy as sin, and the company came out with a spade kit. > Anybody know someone that has/had such a beast, > and might have plans, pictures, etc. of those spades? > Hate re-inventing the wheel. > (Maybe I should just call Rans?) > Richard Pike > MKIII N420P (42OldPoops) > > > > >Fellow Kolbers, > > >My kit is #289, and doesn't have aileron counterbalances like some of the > >older Mk lll's. My ailerons are quite heavy, and I would like to lighten them > >up (a little). I remember this discussion in the past, but never came to a > >clear cut conclusion. > > > >Does the factory still make them or were they in the older blue prints? I > >realize they would have to be added after the fact. Does anyone have an > >opinion..... It seems like the factory discontinued the counterbalances..... > >for a reason? > ________________________________________________________________________________
Date: Jul 26, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Heavy Ailerons
I brought that question up last year. Dennis Souder said ixnay. The tip vortex flows up and around the tip, and screws it up. (sounds like they already tried it, seemed pretty firm...) Richard Pike MKIII N420P (42OldPoops) > >I have Mk III kit # 274, and received the aileron counterbalance on request, >at no charge. If they're not available any more, I could easily measure >mine and send them to you. They'd be very simple to build. On the spade >question, here's another question. Since the counterbalance already ties >into the outer end of the aileron, and points forward, it should almost act >as a spade as it is. How about fastening a small tab to the front of it to >give more leverage ?? By slowly making the tab larger - in small steps - >couldn't you tailor the aileron effort to your own taste ?? Thanks for >bringing this up, I would really like an answer from some of the engineer >types out there. > Big Lar. ________________________________________________________________________________
Date: Jul 26, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Heavy Ailerons
I was going to do that, but if that adds more weight to the trailing edge of the ailerons, (and it will!) then you better for sure plan on counterbalances. I think spades will be the simplest and least likely to screw up. Dennis said that if you use spades, they work best at the center of the aileron. Richard Pike MKIII N420P (42OldPoops) > >Has anyone tried servo tabs on their ailerons? Im thinking of going this >route sometime this winter. Should work well if done right. > >Maurice ________________________________________________________________________________
From: Lrb1476(at)aol.com
Date: Jul 26, 1999
Subject: Re: Heavy Ailerons/ Cross Country trip
<< Don't think the aileron counterbalances will solve the problem. Counterbalances are to prevent aileron flutter, and would not affect the heaviness of the ailerons. I agree that the ailerons are very heavy, especially compared to the very light rudder and elevator. I suspect that the best solution would be spades >> Thanks for the input...I have two buddies down here in Miami with the Rans S-12. Their planes have heavy controls like the Kolb. They like the heavy controls, because they train (BFI's) in their planes, and claim they like that kind of control for the students. I'll see if they have plans etc... I went on my first cross country with fellow LAFA (EAA Chapter 103)
http://www.lafa.com/ Home Page members this weekend. There were two Rans S-12's with 503's and a Buc 11 with a 582. We flew from Miami due north over the Everglades and over Lake Okeechobee to three Airparks. Home sites were for sale, the area is east of Sebring, (home of Lockwood Aviation). Total flight about 280 miles round trip. I've lived in Florida just about my whole life, but have never seen it from the ultra-light slow and low perspective. I was totally amazed at the sights. I was in sensory overload when I got home, was dead tired, but couldn't sleep. I spent the next day, Sunday, walking around in a stupor, like a drug addict coming off a high. Like the old Harley Davidson saying goes...If I have to explain, you won't understand... Rich Bragassa Mk lll Miami, Fl. ________________________________________________________________________________
Date: Jul 26, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re:GPS Alert
>Subject: GPS Alert Date: Mon, 26 Jul 1999 Just passing this on from our Club...... End-of-Week Rollover for GPS- August 22, 1999 The GPS EOW rollover happens every 1,024 weeks -- about once every 20 years. The GPS system calculates time by counting the number of weeks since January 6, 1980 -- up to a maximum of 1,023 weeks. At midnight between August 21-22, 1999, the GPS week "counter" will roll back to zero weeks. DOD says this will not create problems for the GPS satellites or DOD's GPS ground control center, but it could be a problem for consumers who use GPS receivers and related applications. That's because after August 21, 1999, receivers could process satellite data incorrectly and display inaccurate information. GPS and Y2K As for the Year 2000 date change, DOD has determined that the GPS satellites and its ground control center will operate properly after December 31, 1999. But if consumer GPS receivers and applications are not Y2K ready, they could process satellite data incorrectly. Consumers who depend on GPS for geographic locations at sea, on land or in the air, may experience serious safety hazards. Specifically, consumers may experience one of the following problems with their receiver: * It will be unable to locate the satellites, resulting in the receiver not working at all. * It will take more time than usual to locate the satellites. * It will appear to be working but display inaccurate positions, times or dates. What Should You Do? If you use GPS, check with your receiver manufacturer to find out if your receiver and applications are EOW rollover- and Y2K-compliant. You may want to check the Coast Guard Navigation Center's web site <
http://www.navcen.uscg.mil/gps/geninfo/y2k/default.htm>where the Department of Transportation has posted a list of receiver manufacturers and contacts. You also can call the free Y2K consumer hotline (1-888-USA-4-Y2K) to get manufacturer contact information. You will need to tell the manufacturer your receiver's model, serial number, and the firmware version or release date that is displayed on the startup screen. ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: Heavy Ailerons
Date: Jul 27, 1999
Oh well ........................! ! ! Frustrated Lar. ----- Original Message ----- From: Richard Pike <rpike(at)preferred.com> Sent: Monday, July 26, 1999 4:53 PM Subject: Re: Kolb-List: Heavy Ailerons > > I brought that question up last year. > Dennis Souder said ixnay. > The tip vortex flows up and around the tip, > and screws it up. (sounds like they already > tried it, seemed pretty firm...) > Richard Pike > MKIII N420P (42OldPoops) > > > > > >I have Mk III kit # 274, and received the aileron counterbalance on request, > >at no charge. If they're not available any more, I could easily measure > >mine and send them to you. They'd be very simple to build. On the spade > >question, here's another question. Since the counterbalance already ties > >into the outer end of the aileron, and points forward, it should almost act > >as a spade as it is. How about fastening a small tab to the front of it to > >give more leverage ?? By slowly making the tab larger - in small steps - > >couldn't you tailor the aileron effort to your own taste ?? Thanks for > >bringing this up, I would really like an answer from some of the engineer > >types out there. > > Big Lar. > > ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Aileron Spades
Date: Jul 27, 1999
Okay sports fans, now that I've stopped pouting, how about those aileron spades ?? I haven't started covering yet, so could easily work them in. I think. Has it been done ?? Are there plans ?? I've got just 1 hr. in a Citabria, 2 yrs ago, and the ailerons were very heavy. If I have an alternative, I'd just as soon not fight something like that in my own plane. I'm known to be a sucker for punishment, but there ARE limits. Lazy Lar. ________________________________________________________________________________
From: DRMusgrove(at)aol.com
Date: Jul 27, 1999
Subject: Re: MkIII Tailwheel
> ...The only problem I have found prior to installing it is > the that the hole is .745 instead of .750 so I will have to take it to a > machine shop and get it enlarged a bit. > ... > Bill George > Mk-3 582 Powerfin Hey Bill - I'm certainly against anything that sounds like 'half-assing', but in this case, why not chuck a strip of emery in a split rod and take out that .005 to fit. Take your time (but not much time) with a hand drill and you'll get a perfect fit. Would save you a trip to the machini$t and the results should be better! FWIW David M. ________________________________________________________________________________
From: Lrb1476(at)aol.com
Date: Jul 27, 1999
Subject: Re: Aileron Spades
In a message dated 7/27/99 4:15:11 AM Eastern Daylight Time, larrybiglar(at)earthlink.net writes: << Okay sports fans, now that I've stopped pouting, how about those aileron spades ?? I haven't started covering yet, so could easily work them in. >> Kolbers, Since I started this aileron discussion, I was wondering WHY they are so heavy, opposed to other ultra-light aircraft? I hope the answer is not that their ALL heavy. Rich Bragassa ________________________________________________________________________________
From: "Michael Highsmith" <michael.highsmith(at)worldnet.att.net>
Subject: Re: Heavy Ailerons servo tabs
Date: Jul 27, 1999
Yes, and it is a lot of work for what you get. It was built into the original Ferguson ailerons. They could be adjusted from inside the cockpit. They did work but it was not worth all the effort to get the right effect. My suggestion is if you want to take out some of the heaviness make your ailerons smaller and your flaps larger. There are a lot of airplanes out there with a lot smaller ailerons that work just fine. At slow speeds the ailerons are not that heavy so it has to do with the amount of air traveling over the surfaces. The faster you go the heavier they get. Another thing is you might want to put a little negative reflex in the ailerons to get then up out of the air stream a little for straight and level flight. I know this will improve your top speed. Then shallow turns takes more of a thought than moving the stick. Just thinking again and passing it along. Michael -----Original Message----- From: Maurice Shettel <mshettel(at)mindspring.com> Date: Monday, July 26, 1999 5:50 PM Subject: Re: Kolb-List: Heavy Ailerons > >Has anyone tried servo tabs on their ailerons? Im thinking of going this >route sometime this winter. Should work well if done right. > >Maurice > > >Richard Pike wrote: > >> >> Don't think the aileron counterbalances will solve the problem. >> Counterbalances are to prevent aileron flutter, and would >> not affect the heaviness of the ailerons. >> I agree that the ailerons are very heavy, especially >> compared to the very light rudder and elevator. >> I suspect that the best solution would be spades >> mounted on the bottom of the ailerons, >> about in the middle of each one. >> But that will be a good project for this winter, when I can't fly. >> Right now it is better to fly a good airplane with heavy ailerons. >> >> P.S. Some of the early Rans S-12 Airailes had ailerons that >> were heavy as sin, and the company came out with a spade kit. >> Anybody know someone that has/had such a beast, >> and might have plans, pictures, etc. of those spades? >> Hate re-inventing the wheel. >> (Maybe I should just call Rans?) >> Richard Pike >> MKIII N420P (42OldPoops) >> >> > >> >Fellow Kolbers, >> >> >My kit is #289, and doesn't have aileron counterbalances like some of the >> >older Mk lll's. My ailerons are quite heavy, and I would like to lighten them >> >up (a little). I remember this discussion in the past, but never came to a >> >clear cut conclusion. >> > >> >Does the factory still make them or were they in the older blue prints? I >> >realize they would have to be added after the fact. Does anyone have an >> >opinion..... It seems like the factory discontinued the counterbalances..... >> >for a reason? >> > > ________________________________________________________________________________
From: STAECS(at)aol.com
Date: Jul 27, 1999
Subject: (no subject)
Please remove me from the list. Steve Anderson staecs(at)aol.com ________________________________________________________________________________
Date: Jul 27, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re: MkIII Tailwheel
> > >In a message dated 7/27/99 2:18:34 AM, DRMusgrove(at)aol.com writes: >> ...The only problem I have found prior to installing it is > the that the hole is .745 instead of .750 so I will have to take it to a > machine shop and get it enlarged a bit. ><< , why not chuck a strip of emery in a split rod and take out that .005 to >fit. Take your time (but not much time) with a hand drill and you'll get a >perfect fit. Would save you a trip to the machini$t and the results should >be better! >> We found it easier to buy a .750 inch stone for your drill bit and run it through the inside of the bearing so it will slip on, if that's what your having trouble with. That way the little axel will still fit in the bracket. Those things are really made to be pressed on any way, but that won't work for you. ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Jul 27, 1999
Subject: Re: Aileron Spades
I have been flying a Kolb MK 3 a friend bought. He had no ultra-light time or tailgear time and had not flown in a while so I did the honors of test flying it for several hours. I put it through it paces quite a bit. This was a second hand airplane with about 50 hours on it. I then flew him several hours of t&g and stalls and turns etc and now he is getting his flight review and tailgear endorsement in it--about 5 hours from a local flight instructor. Anyway, those ailerons are heavy. I was somewhat displeased with them being so. I have a Kitfox 4 and they are finger light compared to the Kolbs and so much more responsive and roll rate is much higher than for the Kolb. I think the idea of spades might be a good one. I think refexing them up just a tad might also help. I am building an RV4 and have the full swivel RV conversion in my shop back home. I think it would be a big improvement over that plastic thing Kolb gives you. I landed on a paved runway and the little bugger provided very little steering or stability.Better stick to grasss untill something is done about it-- me and my friend. JR--new Kolb pilot for a bit longer ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Jul 27, 1999
Subject: Intercom noise--help!!!!
What intercom set up you guys use. I have been using my Flight tech and my friend bought a similar unit--neither will work at all in the Kolb cockpit due to being overwelmed by ambient noise. We have Lightspeed and David Clarks and Softcom headset and none work. Set squelch low enough and no work and set it high and are overwhemed by noise--loud enough to damage ears. He has doors but the rear section is open behind your heads. What do we need to do to get rid of the engine prop noise so we can speak over the intercom. Both units work great in the Fox. Help?????/!!!!!!!!!! ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Jul 27, 1999
Subject: Re: MkIII Tailwheel-reamer
Maybe try a chucking reamer of .75 or .749 etc. Lube well and turn by hand or CareFully in a press or drill. That size will probably need a drill press or at least Arnold arms. JR ________________________________________________________________________________
Date: Jul 27, 1999
From: Paul VonLindern <paulv(at)digisys.net>
Subject: Re: Welding
Larry, The covering process is long, but not tough. It's actually kinda fun (in a sick way). My web address is http://www.digisys.net/users/paulv/kolb.htm Stay outa da heat PaulV Larry Bourne wrote: > > Good to hear from you, Paul. I've lost your web-site address somewhere > along the line. Thought I was better organized than that. > Sounds like the covering process is a long and tough one. You've been at it > quite a while now. I'll look forward to seeing some pics. Please re-send > your web address. Lar. ________________________________________________________________________________
From: BICUM(at)aol.com
Date: Jul 27, 1999
Subject: Help with drilling wheel axles?
Need help from the list, I have reached a point where I need to drill the two 3/16" holes in each wheel axle. This is not the alignment hole but the two holes in each axle. I have used three bits and have made very little dent in this thing. I was wondering if anyone has had a similar problem and any offerings of possible solutions. The axles are tagged "Heat treated, do not weld". The only thing I can come up is get to the drill press and slow it down ,take my time and drill away. I'm looking for some better bits in the meantime. I checked the archives and my search didn't turn up anything specific on this problem. any help appreciated, John (not at Oskosh) Bickham St. Francisville, LA Mark III N308JB (assigned) ________________________________________________________________________________
From: BKlebon(at)aol.com
Date: Jul 27, 1999
Subject: Re: Help with drilling wheel axles?
I had great success with Black & Decker "Bullet" drill bits I purchased at Lowe's. You can find them anywhere. I recently saw that Walmart even carries them. Good luck! ________________________________________________________________________________
From: "Michael Highsmith" <michael.highsmith(at)worldnet.att.net>
Subject: Re: Intercom noise--help!!!!
Date: Jul 27, 1999
Kolb Gang, Get a 3 blade IVO or equivalent, close in the back with lexan, make sure that you have all the fabric around the back section of the cockpit attached to the formers with double side stick foam tape to stop the drumming and shield the plug wires from the base of the plugs to the base of the coils. If your are still picking up radio noise a lot, which you can do through your intercom, one or more of a plug wire end may be deteriorating so you may want to pull them off and check them. I had one that had burned itself off up into the insulation 1/2 ''. over a period of time it made so much noise in the radio I couldn't squelch it out. That's when I knew I had a problem. I cut it back to the good wire core and reinstalled it. The noise has not returned. I also get much better tx on the radio without having to tx the noise. My wingman immediately noticed the clarity of the tx. Make sure all of your intercom wires are shielded, But do one thing at a time. These all help but there may be one thing that is causing most of your problem. I continually get compliment on how quit my plane is in the air and in the cockpit but that's because Ive done all these things over time. It was real noisy when I first started flying it too. Let use know what you do to solve the problem you may find something we can use. Michael ________________________________________________________________________________
From: "Lindy" <lindy(at)snowhill.com>
"Ted Cowan" , "Scott Sharon Wilcox" , "Sam Cox" , "Rutledge Fuller" , "Paul Spadin" , "Michael Highsmith" , "Kolb Builders" , "Glenn Rinck" , "Fly Ultralights" , "Dave Thomas" , "Danny Day" , "Buddy Carilse" , "Bob Moorehead" , "Bob Cooper" , "Ben Cole" , "ASC2"
Subject: Fw: GREAT!
Date: Jul 27, 1999
----- Original Message ----- From: greg moloney <gregmol(at)ihug.com.au> Sent: Tuesday, July 27, 1999 4:52 AM Subject: Fw: GREAT! > > > >>Subject: GPS Alert > >Date: Mon, 26 Jul 1999 > > > >Just passing this on from our Club...... > > > >End-of-Week Rollover for GPS- August 22, 1999 > >The GPS EOW rollover happens every 1,024 weeks -- about once every 20 > years. > >The GPS system calculates time by counting the number of weeks since > January > >6, 1980 -- up to a maximum of 1,023 weeks. At midnight between August > 21-22, > >1999, the GPS week "counter" will roll back to zero weeks. DOD says this > >will not create problems for the GPS satellites or DOD's GPS ground control > >center, but it could be a problem for consumers who use GPS receivers and > >related applications. That's because after August 21, 1999, receivers could > >process satellite data incorrectly and display inaccurate information. > >GPS and Y2K > >As for the Year 2000 date change, DOD has determined that the GPS > satellites > >and its ground control center will operate properly after December 31, > 1999. > > > >But if consumer GPS receivers and applications are not Y2K ready, they > could > >process satellite data incorrectly. Consumers who depend on GPS for > >geographic locations at sea, on land or in the air, may experience serious > >safety hazards. Specifically, consumers may experience one of the following > >problems with their receiver: > >* It will be unable to locate the satellites, resulting in the > >receiver not working at all. > >* It will take more time than usual to locate the satellites. > >* It will appear to be working but display inaccurate positions, > >times > >or dates. > >What Should You Do? > >If you use GPS, check with your receiver manufacturer to find out if your > >receiver and applications are EOW rollover- and Y2K-compliant. You may want > >to check the Coast Guard Navigation Center's web site > ><http://www.navcen.uscg.mil/gps/geninfo/y2k/default.htm>where the > Department > >of Transportation has posted a list of receiver manufacturers and contacts. > >You also can call the free Y2K consumer hotline (1-888-USA-4-Y2K) to get > >manufacturer contact information. You will need to tell the manufacturer > >your receiver's model, serial number, and the firmware version or release > >date that is displayed on the startup screen. > > > > > > > ________________________________________________________________________________
Date: Jul 27, 1999
From: Terry Swartz <tswartz(at)desupernet.net>
Subject: Re: Heavy Ailerons
I asked Dennis Souder the same question and he said don't do it and was quite convinced. Terry Richard Pike wrote: > > I brought that question up last year. > Dennis Souder said ixnay. > The tip vortex flows up and around the tip, > and screws it up. (sounds like they already > tried it, seemed pretty firm...) > Richard Pike > MKIII N420P (42OldPoops) > > > > >I have Mk III kit # 274, and received the aileron counterbalance on request, > >at no charge. If they're not available any more, I could easily measure > >mine and send them to you. They'd be very simple to build. On the spade > >question, here's another question. Since the counterbalance already ties > >into the outer end of the aileron, and points forward, it should almost act > >as a spade as it is. How about fastening a small tab to the front of it to > >give more leverage ?? By slowly making the tab larger - in small steps - > >couldn't you tailor the aileron effort to your own taste ?? Thanks for > >bringing this up, I would really like an answer from some of the engineer > >types out there. > > Big Lar. > ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: Aileron Spades
Date: Jul 27, 1999
OK, OK, I'm convinced ! ! ! I'm familiar with tip vortices, so that makes sense, so now all I need is some kind of plan for spades. How big, what material, what shape, where and how to attach ???? I'm real sure I don't like heavy anything in my controls, so I think it sounds like a worthwhile addition. Big Lar. ----- Original Message ----- From: <JRWillJR(at)aol.com> Sent: Tuesday, July 27, 1999 10:32 AM Subject: Re: Kolb-List: Aileron Spades > > I have been flying a Kolb MK 3 a friend bought. He had no ultra-light time or > tailgear time and had not flown in a while so I did the honors of test flying > it for several hours. I put it through it paces quite a bit. This was a > second hand airplane with about 50 hours on it. I then flew him several hours > of t&g and stalls and turns etc and now he is getting his flight review and > tailgear endorsement in it--about 5 hours from a local flight instructor. > Anyway, those ailerons are heavy. I was somewhat displeased with them being > so. I have a Kitfox 4 and they are finger light compared to the Kolbs and so > much more responsive and roll rate is much higher than for the Kolb. I think > the idea of spades might be a good one. I think refexing them up just a tad > ________________________________________________________________________________
Date: Jul 27, 1999
From: Terry Swartz <tswartz(at)desupernet.net>
Subject: Re: Help with drilling wheel axles?
I used Cobalt bits with a handheld drill without a problem as someone suggested several years ago. Terry BICUM(at)aol.com wrote: > > Need help from the list, > > I have reached a point where I need to drill the two 3/16" holes in each > wheel axle. This is not the alignment hole but the two holes in each axle. > I have used three bits and have made very little dent in this thing. I was > wondering if anyone has had a similar problem and any offerings of possible > solutions. The axles are tagged "Heat treated, do not weld". The only thing > I can come up is get to the drill press and slow it down ,take my time and > drill away. I'm looking for some better bits in the meantime. > > I checked the archives and my search didn't turn up anything specific on this > problem. > > any help appreciated, > > John (not at Oskosh) Bickham > St. Francisville, LA > Mark III > N308JB (assigned) > ________________________________________________________________________________
Date: Jul 27, 1999
From: Terry Swartz <tswartz(at)desupernet.net>
Subject: Re: Intercom noise--help!!!!
I used a Hush-A-Com, which is no longer made, with good success for a year and a half. However, on long flights the noise still got old. I then got a set custom made which work great. They are 27 db passive noise reduction and I am using the sigtronics SPO-22N intercom which is made for high noise. BTY The Hush-A-Com is for sale 200.00 for two headsets and intercom. Terry JRWillJR(at)aol.com wrote: > > What intercom set up you guys use. I have been using my Flight tech and my > friend bought a similar unit--neither will work at all in the Kolb cockpit > due to being overwelmed by ambient noise. We have Lightspeed and David Clarks > and Softcom headset and none work. Set squelch low enough and no work and set > it high and are overwhemed by noise--loud enough to damage ears. He has doors > but the rear section is open behind your heads. What do we need to do to get > rid of the engine prop noise so we can speak over the intercom. Both units > work great in the Fox. Help?????/!!!!!!!!!! > ________________________________________________________________________________
Date: Jul 27, 1999
From: Richard <swidersk(at)digital.net>
Subject: Re: Help with drilling wheel axles?
John, You got the right idea with using the drill press @ the slowest setting. Use a Cobalt drill bit & cool it continuously with a very light light oil (diesel fuel will even work). Push it only hard enough to keep it cutting. If you don't let it overheat & take your time, it will be a piece of cake. Richard S BICUM(at)aol.com wrote: > > Need help from the list, > > I have reached a point where I need to drill the two 3/16" holes in each > wheel axle. This is not the alignment hole but the two holes in each axle. > I have used three bits and have made very little dent in this thing. I was > wondering if anyone has had a similar problem and any offerings of possible > solutions. The axles are tagged "Heat treated, do not weld". The only thing > I can come up is get to the drill press and slow it down ,take my time and > drill away. I'm looking for some better bits in the meantime. > > I checked the archives and my search didn't turn up anything specific on this > problem. > > any help appreciated, > > John (not at Oskosh) Bickham > St. Francisville, LA > Mark III > N308JB (assigned) > ________________________________________________________________________________
From: Lrb1476(at)aol.com
Date: Jul 27, 1999
Subject: Re: Heavy Ailerons? /a good answer....finally
Kolbers, I finally made contact with a man who lives in Florida who has built 26....., yes thats twenty six Kolb aircraft in the last twenty five or so years. He is responsible for alot of major design changes and options for the Kolb factory. Anyway he is a walking Bible on the entire Kolb line. He is kind of private so I wont use his name on the list (bummer)... unless he advises otherwise. I'm probable the only idiot that doesn't know him anyway. He advises that the heavy ailerons is a simple fix, and if you do it right the plane flys like it has power steering. First ajust your ailerons about 3/8" up from the bottom of the wing. Some guys have already figured this out. Fly the plane and see if theres a difference. Next install the counter-balances. He says it makes all the difference in the world when both of these have been done. Any way I'm going to try the ajustment part this weekend and see if It makes a difference. Good Luck, Rich Bragassa ________________________________________________________________________________
From: JON CROKE <joncroke(at)itol.com>
Subject: New web site: UltralightPilot.com
Date: Jul 27, 1999
Fellow Kolbers: I would like to announce a new website I have deployed. www.UltralightPilot.com The purpose of this site is to register and list ultralight pilots in a national directory that is available freely to all. The intended benefits of this mission is to be able someday to allow you to 'search' or find other pilots in YOUR neighborhood with similar aircraft, interests, etc. I feel that there is a real need to have a 'white pages' directory to help us find each other and share our interests and expertise in this hobby? just like this list does for Kolb builders. This idea may 'take off and fly' or may die if there is no interest. However, I have a webserver available to me, the expertise to build databases (do it for a living) and NO financial interest or incentive of any kind. I simply cannot believe there is currently not a place to go to find 'others' (ultralight enthusiasts) in my geographical area that are experienced/interested in this sport. (this includes providing outlets for students and instructors to connect) You are invited to register yourself in the database?. Give it a try! (You can always delete yourself later). Live dangerously! See what happens! I expect to do some campaigning at Osh Kosh. Your feedback in this matter is welcome (probably best offline, this isnt Kolb related material!) after you visit the site. Thanks Jon near Greenbay FS I ________________________________________________________________________________
From: BILLBEAM(at)aol.com
Date: Jul 27, 1999
Subject: Re: New web site: UltralightPilot.com
In a message dated 7/27/99 11:09:04 PM Eastern Daylight Time, joncroke(at)itol.com writes: << www.UltralightPilot.com >> Jon, Is there some trick to getting to your new website? I keep getting knocked off. Bill ________________________________________________________________________________
Date: Jul 28, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re: HEY GUYS!
Just finished my new plane - want to see some pictures? <http://www.mindspring.com/~possums/> ________________________________________________________________________________
Date: Jul 28, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re: MkIII Tailwheel
> >Yo Possum: > >Thanks for the info. Perhaps I wasn't clear on the .745 thing. The clearance >I was talking about was for the strut, not the wheel axle. This is for the >new assembly which is totally different from original. It has a steerable >feature which switches to full swivel after a set limit is reached. I'm still >going to take it down to the machine shop and get it fit nicely. It will add >about 3 pounds over the original tailwheel so the CG will be at the aft edge. Mines Aft edge too - about 36%. But flys great & turns on a dime. ________________________________________________________________________________
From: "Larry & Karen Cottrel" <lcottrel(at)kfalls.net>
Subject: Re: MkIII Tailwheel
Date: Jul 27, 1999
---------- > From: Possum <possums(at)mindspring.com> > To: kolb-list(at)matronics.com > Subject: Re: Kolb-List: Re: MkIII Tailwheel > Date: Tuesday, July 27, 1999 10:48 PM > Say Possum- where did you get the model for the jacket or what ever that was? I;m from the east where they have a lot of possums and that don't look like any that I ever saw while I was there. Perhaps they elvolved into something that looks like a fox while I've been gone. The plane looked good though. Larry ________________________________________________________________________________
Date: Jul 28, 1999
From: Terry Swartz <tswartz(at)desupernet.net>
Subject: Re: HEY GUYS!
Plane looks great. Paint appears to have a high gloss. What paint did you use? Terry Possum wrote: > > Just finished my new plane - want to see some pictures? > <http://www.mindspring.com/~possums/> > ________________________________________________________________________________
Date: Jul 28, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re: HEY GUYS!
> > Paint appears to have a high gloss. What paint did you use? Aerothane - from Aircraft Spruce. ________________________________________________________________________________
From: "Howard Ping" <hping(at)hyperaction.net>
Date: Jul 28, 1999
Subject: pucker patch
Kolbers I just set up a home page.The grass strip is located 12 mi. west of TNK.check it out. Howard http://www.hyperaction.net/hping ________________________________________________________________________________
Date: Jul 28, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: pucker patch
> >Kolbers >I just set up a home page.The grass strip is located 12 mi. west >of TNK.check it out. >Howard >http://www.hyperaction.net/hping Excellent! Appreciate a man giving the Lord thanks for the blessing of flight. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
From: WGeorge737(at)aol.com
Date: Jul 28, 1999
Subject: Oshkosh 99 on TV
Hi Gang: Perhaps the rest of the planet already knows this but the Discovery Wings channel will start airing AirVenture 99 tomorrow July 29. It runs for four days I think. Bill George Mk-3 582 Powerfin ________________________________________________________________________________
From: Tim.Hrib(at)carefirst.com
Date: Jul 29, 1999
Subject: GPS update
--0__=gY5TrJuK9E6TtUCKSfJBHmI9UCpSWanXaZLe4YMRDMprguUfKV6IMHPP .......... to whom it may concern ......... Magellan Corporation Year 2000 (Y2K) and GPS End-of Week Rollover (EOW) Information For some time, Magellan Corporation has had a company-wide project underway to evaluate our operations and products to ensure their readiness for the Year 2000 and GPS End-of-Week Rollover events. Recognizing its importance to our customers and business partners, we have made the project a high priority within the company. As a result of this ongoing, rigorous testing program and in keeping with the standards described later in this document, we have determined that the following products currently being sold by Magellan are compliant with both the Y2K and GPS EOW events: --0__=gY5TrJuK9E6TtUCKSfJBHmI9UCpSWanXaZLe4YMRDMprguUfKV6IMHPP =B7 GPS 300 =B7 GPS 315 =B7 GPS 315A =B7 GPS 320 =B7 GPS Blazer12 =B7 GPS 2000XL =B7 GPS Tracker =B7 GPS Color Track =B7 NAV 6000 =B7 MAP 410 =B7 GSC 100 =B7 SkyStar PLUS =B7 EC-20X =B7 AIV-10 =B7 AIV-10SI =B7 ProMARK X =B7 ProMARK X-CP =B7 ProMARK X-CM The company is also testing products that are no longer in production, with the most recently produced products tested first. The results of those tests will be released as the individual tests are completed, and well in advance of either the EOW or Y2K event. As of May 4, 1999, we have determined the following Magellan products to be Y2K and EOW compliant: =B7 NAV 5000 =B7 NAV 5000D =B7 NAV 5000DX =B7 NAV 5000DLX =B7 NAV 5200 =B7 NAV 5200D =B7 NAV 5200DX =B7 NAV 5000A =B7 MAP 7000 =B7 SkyNAV 5000 =B7 NAV 5000 PRO =B7 FieldNAV =B7 ProMARK V =B7 ProMARK V-CM =B7 OEM 5000 =B7 NAV 1000M5 =B7 The HAWK =B7 FieldPRO V =B7 Meridian =B7 Trailblazer =B7 Meridian XL =B7 Trailblazer XL =B7 NAV 1200 =B7 NAV 1200XL =B7 SkyBlazer =B7 SkyBlazer XL =B7 SkyBlazer LT =B7 SkyStar =B7 Patriot =B7 GPS 2000 =B7 GPS 3000 =B7 GPS 4000 =B7 GPS 3000XL =B7 GPS 4000XL =B7 GPS Pioneer =B7 NAV DLX-10 =B7 Chartmate If your Magellan product is not yet listed, please continue to look to this location for updated information on Magellan's Y2K and GPS EOW Compliance Program. Magellan Year 2000 and GPS End-of-Week Rollover Compliance Program Magellan's Y2K and EOW Program tests our products' compliance with the Y2K and EOW standards described below. The compliance testing process evaluates each model of GPS receiver and communications product that the company has sold since the company's inception, beginning with the most recently released products. Customers should check the evaluation list for information about their particular model product. For each product that we identify which does not meet the following standards, the company will determine whether to fix or modify the product to make it compliant. We will keep customers and business partners informed of this program through the www.magellangps.com and www.ashtech.com websites. This information also is available by calling the company's customer service and technical support departments and through the email addresses Y2K(at)mgln.com and Y2K(at)ashtech.com . The Year 2000 Issue The Y2K issue arises from computer software written to use only the last two digits of a year to recognize and correctly process date data. When the date changes from December 31, 1999 to January 1, 2000, this software and any product in which it is used may recognize the year "00" as "1900" rather than "2000", causing product failure, malfunction or data corruption. In response to this concern, Magellan Corporation is evaluating its products using the following Y2K standard: Definition: "Year 2000 conformity shall mean that neither performance nor functionality is affected by dates prior to, during and after the Year 2000. This means 1) No value for the current date will cause any interruption in operation; 2) Date-based functionality must behave consistently for dates prior to, during and after the Year 2000; 3) In all interfaces and data storage, the century in any date must be specified either explicitly or by unambiguous algorithms or inferencing rules; and 4) The Year 2000 must be recognized as a leap year." GPS End-of-Week Rollover Issue In addition to evaluating its products for compliance with the Y2K, Magellan is also evaluating its products for compliance with the EOW event, which is similar to the date rollover at the end of the century, but unique to Global Positioning System technology. GPS time is based on a "GPS week number" ranging from "0" to "1023". Week 1023 will end at midnight (UTC time) on August 21, 1999, at which time the week number will "roll over" or re-set to week 0 beginning on August 22, 1999. If a receiver has not been prepared to handle this week rollover event, the receiver may calculate inaccurate position fixes, generate erroneous dates or have difficulty acquiring satellite signals. Magellan is evaluating its products for compliance with this event using the following EOW standard: Definition: "GPS End-of-Week compliance shall mean that neither performance nor functionality is affected by dates prior to, during and after the GPS system time rollover. This means: 1) No value of the GPS week will cause any interruption in operation of the hardware or software in the GPS product. Rollover between all time demarcations will be performed correctly. 2) The product must behave consistently for dates prior to, during and after the GPS week 1023. 3) For all interfaces and data storage, any date must be specified either explicitly or by unambiguous algorithms or inferencing rules from the value entered. Y2K and EOW Compliance Testing Procedure Magellan is currently evaluating its products for compliance with the Y2K and EOW events using a GPS simulator programmed to provide signals similar to what experts believe will be received from the GPS satellites at the time of such events. We have designed our tests using simulated dates prior to and after the EOW and Y2K events to consider various possibilities of product turn-on and use. In addition, we have used the U.S. Air Force GPS Week Number Rollover and Y2K test plan in designing our tests and believe the resulting Magellan Testing Program to be more extensive than the Air Force requirements. Compliance Results: Magellan's Y2K and EOW Program is well underway and will be completed in time to make a smooth transition before the EOW and the new millennium. With over 100 different models of GPS and communications products manufactured since 1989, and over one million products sold, the task is an enormous and an important one. As our Program advances, we will release product evaluation test results. The results will be released on our Internet websites listed above. The company has also established email addresses at Y2K(at)mgln.com (consumer products) and Y2K(at)ashtech.com (precision products) to receive and respond to specific inquiries for the latest information about our compliance Program. Important Legal Information and Disclaimer Magellan has provided the foregoing solely to disseminate information to our customers regarding product compliance with the Y2K and EOW standards set forth herein. While we have been careful in our planning, testing, and reporting of the results, we are necessarily dependent upon information and equipment received from others and used in our Program. Accordingly, the accuracy of our results is dependent upon the accuracy and performance of such third party information, and Magellan makes no representation or warranty of any kind with respect to such third party information. THE INFORMATION CONTAINED IN THIS DOCUMENT IS PROVIDED TO CUSTOMERS FOR THE SOLE PURPOSE OF ASSISTING IN PLANNING FOR THE Y2K AND EOW EVENTS, AND DOES NOT CONSTITUTE AN EXPRESS OR IMPLIED WARRANTY OR REPRESENTATION OF ANY KIND WITH RESPECT TO ANY MAGELLAN PRODUCT. THIS DOCUMENT CONTAINS THE INFORMATION CURRENTLY AVAILABLE REGARDING THE COMPLIANCE OF MAGELLAN'S PRODUCTS TO THE STANDARDS SET FORTH HEREIN AND IS PROVIDED "AS IS". SALE AND WARRANTY OF MAGELLAN PRODUCTS ARE GOVERNED EXCLUSIVELY BY THE TERMS AND CONDITIONS UNDER WHICH SUCH PRODUCTS ARE SOLD AND THE WARRANTIES CONTAINED THEREIN. THIS DOCUMENT SHALL NOT MODIFY ANY TERM OR CONDITION OF SUCH SALES CONTRACT OR PRODUCT WARRANTY. MAGELLAN DISCLAIMS ALL WARRANTIES, EITHER EXPRESS OR IMPLIED, INCLUDING THE WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE. IN NO EVENT SHALL MAGELLAN CORPORATION OR ITS SUPPLIERS BE LIABLE FOR ANY DAMAGES WHATSOEVER INCLUDING DIRECT, INDIRECT, CONSEQUENTIAL, LOSS OF BUSINESS PROFITS, PUNITIVE OR SPECIAL DAMAGES, EVEN IF MAGELLAN CORPORATION OR ITS SUPPLIERS HAVE BEEN ADVISED OF THE POSSIBILITY OF SUCH DAMAGES. = --0__=gY5TrJuK9E6TtUCKSfJBHmI9UCpSWanXaZLe4YMRDMprguUfKV6IMHPP-- ________________________________________________________________________________
Date: Jul 28, 1999
From: Dennis & Diane Kirby <kirbyd(at)flash.net>
Subject: RE: Drilling Wheel Axles
I had the same problem drilling those hardened-steel axles for my Mark-3. Went thru at least four 3/16 drill bits with little progress. Even a Titanium bit didn't do much. Then I bought a Cobalt bit (used for drilling stainless steel) which finally worked. Did fine using a hand drill (that's all I've used for or this whole project). Give it a try. Dennis Kirby s/n 300 Cedar Crest, New Mexico ________________________________________________________________________________
Date: Jul 29, 1999
From: Jerry Bidle <jbidle(at)airmail.net>
Subject: Re: RE: Drilling Wheel Axles
Secret is low speed 500-600 RPM max., slower is better, LOTS of "pressure", and some oil. If you go light on the pressure or go fast (RPM) you just work harden the material and then it's a real bitch to drill. Learned from drilling RV gear legs and steel axles on the Kolb. Run the drill slow, get on it, and use oil. Tapping oil works great. Jerryb > >I had the same problem drilling those hardened-steel axles for my >Mark-3. Went thru at least four 3/16 drill bits with little progress. >Even a Titanium bit didn't do much. Then I bought a Cobalt bit (used >for drilling stainless steel) which finally worked. Did fine using a >hand drill (that's all I've used for or this whole project). Give it a >try. >Dennis Kirby >s/n 300 >Cedar Crest, New Mexico > > ________________________________________________________________________________
From: "David Bruner" <brunerd(at)hvi.net>
Subject: Re: 178 seconds
Date: Jul 29, 1999
Eam, here's that message i told you bout yesterday. Hope you make out well with Jane maybe I'll have already heard when you get this tho. Talk to you soon, or already. Definitely always. love, dad -----Original Message----- From: Ralph H Burlingame <ul15rhb(at)juno.com> Date: Wednesday, July 21, 1999 11:35 PM Subject: Kolb-List: 178 seconds > > >178 Seconds to Live > >How long can a pilot who has little or no instrument training expect to >live after he flies into bad weather and loses visual contact? > >Researchers at the University of Illinois did some tests and came up >with some very interesting data. Twenty student "guinea pigs" flew into >simulated instrument weather, and all went into graveyard spirals or >roller coasters [attribute to the U of I flight training program??]. The >outcome differed in only one respect - the time required till control was >lost. The interval ranged from 480 seconds to 20 seconds. The average >time was 178 seconds -- two seconds short of three minutes. > >Here's the fatal scenario. . . . . . . >The sky is overcast and the visibility is poor. That reported five mile >visibility looks more like two, and you can't judge the height of the >overcast. Your altimeter tells you that you are at 1500 feet but your map >tells >you that there's local terrain as high as 1200 feet. There might be a >tower nearby because you're not sure how far off course you are. But >you've flown into worse weather than this, so press on. >You find yourself unconsciously easing back just a bit on the >controls to clear those towers. With no warning, you're in the soup. >You peer so hard into the milky white mist that your eyes hurt. You fight > >the feeling in your stomach. You try to swallow, only to find your mouth >dry. Now you realize you should have waited for better weather. The >appointment was important, but not all that important. >Somewhere a voice is saying, "You've had it -- it's all over!" >You now have 178 seconds to live. >Your aircraft feels on even keel but your compass turns slowly. You >push a little rudder and add a little pressure on the controls to stop >the turn but this feels unnatural and you return the controls to their >original position. This feels better but now your compass is turning a >little faster and your airspeed is increasing slightly. >You scan your instruments for help but what you see looks somewhat >unfamiliar. You're sure that this is just a bad spot. You'll break out in >a few minutes. > >(But you don't have a few minutes left. . .) > >You now have 100 seconds to live. >You glance at your altimeter and you are shocked to see it unwinding. >You're already down to 1200 feet. Instinctively, you pull back on the >controls but the altimeter still unwinds. The engine is into the red and >the airspeed, nearly so. You have 45 seconds to live. >Now you're sweating and shaking. There must be something wrong with the >controls; pulling back only moves the airspeed indicator further into >the red. You can hear the wind tearing at the aircraft. You are about to >meet your Maker; you have 10 seconds to live. Suddenly you see the >ground. The trees rush up at you. You can see the horizon if you turn >your head far enough but it's at a weird angle -- > >you're almost inverted. You open your mouth to scream but. . . . . .. >you just ran our of seconds. > >Think about it before you press on into marginal weather > >Lucian Bartosik > > ________________________________________________________________________________
From: "Howard Ping" <hping(at)hyperaction.net>
Date: Jul 29, 1999
Subject: Re: pucker patch
Bill Yea! i'm still at 3704-8427 or until I-66 covers up my runway and barn. Glad to hear your a Kolb flyer now,after your first flight what do you think of their climb.All in all I think their hard to beat.The Kolb factory 's cordinates are 3709-8420,it's easy to find,it runs parallel to Ky 80 and is about 1.5 mi. E. of the Rockcastle River bridge. You'll like Oshkosh,their Warbird displays are second to none.but i'm a ultralighter and prefer Sun & Fun .It get's the year started off right. I went up a while last night ,climbed to about 1500' and looked down,fog had started rising up from a rain, every hollow was white,I pulled the power back and landed.My shortest flight ever. Have fun at the world's biggest air show. later Howard ________________________________________________________________________________
Date: Jul 29, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re: MkIII Tailwheel
> > >In a message dated 7/27/99 7:45:49 PM, possums(at)mindspring.com writes: > ><< Mines Aft edge too - about 36%. But flys great & turns on a dime. >> > >What does your manual say for aft limit? It's the same as a regular Firestar as close as I can tell, same wing cord. About 37% back max. Don't really have a manual for this one. ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Jul 29, 1999
Subject: Landing help--how?
What approach and landing style works best for you guys with Mark 3 aircraft. I have been flying it on at about 55 doing wheel landings. Attempts to land the bugger like I would do a Fox or a Cub or an RV as in a normal power off flare into a three point leaves me flopping on to the ground like a wounded duck. There is surely something I am missing here though I have tried several methods to get a nice full stall landing. Wheelies are good but I would like to three-point. Off subject but what does a possum have to do with flying Kolbs--I always preferred Armadillos anyway. Armadillos kick possum tail. As you said -- no respect at all. Just kidding. Thanks. JR ________________________________________________________________________________
From: "George Thompson" <eagle1(at)futureone.com>
Subject: Re: New web site: UltralightPilot.com
Date: Jul 29, 1999
-----Original Message----- From: JON CROKE <joncroke(at)itol.com> Date: Tuesday, July 27, 1999 8:14 PM Subject: Kolb-List: New web site: UltralightPilot.com > >Fellow Kolbers: > >I would like to announce a new website I have deployed. > www.UltralightPilot.com > >The purpose of this site is to register and list ultralight pilots in a >national directory that is available freely to all. >The intended benefits of this mission is to be able someday to allow you to >'search' or find other pilots in YOUR neighborhood with similar aircraft, >interests, etc. I feel that there is a real need to have a 'white pages' >directory to help us find each other and share our interests and expertise >in this hobby? just like this list does for Kolb builders. > >This idea may 'take off and fly' or may die if there is no interest. > However, I have a webserver available to me, the expertise to build >databases (do it for a living) and NO financial interest or incentive of >any kind. I simply cannot believe there is currently not a place to go to >find 'others' (ultralight enthusiasts) in my geographical area that are >experienced/interested in this sport. (this includes providing outlets for >students and instructors to connect) > >You are invited to register yourself in the database?. Give it a try! (You >can always delete yourself later). Live dangerously! See what happens! I >expect to do some campaigning at Osh Kosh. > >Your feedback in this matter is welcome (probably best offline, this isnt >Kolb related material!) after you visit the site. > >Thanks > >Jon near Greenbay >FS I > > >Put me down. Started in ultrilights in 1984. Have built a Hi Max and Firestar KXP. Am just finishing up a Firestar II. eagle1(at)futureone.com > > ________________________________________________________________________________
Date: Jul 29, 1999
From: Billy Jones <bjones8103(at)yahoo.com>
Subject: Re: MkIII Tailwheel
37% is what the factory quoted me for my FirestarII. Sounds a long way back to me. BJones in Houston --- Possum wrote: > > > > > > > >In a message dated 7/27/99 7:45:49 PM, > possums(at)mindspring.com writes: > > > ><< Mines Aft edge too - about 36%. But flys great > & turns on a dime. >> > > > >What does your manual say for aft limit? > > It's the same as a regular Firestar as close as I > can tell, same wing cord. > About 37% back max. Don't really have a manual for > this one. > > > > > > The Kolb-List is sponsored by Matronics, makers > of fine Aircraft > Avionics, and by the generous Contributions of > List members. > > > Matronics: > http://www.matronics.com > Kolb-List: > http://www.matronics.com/kolb-list > Archive Search Engine: > http://www.matronics.com/search > Archive Browsing: > http://www.matronics.com/archives > Other Email Lists: > http://www.matronics.com/other > > > > > Free instant messaging and more at http://messenger.yahoo.com ________________________________________________________________________________
From: "Jeremy Casey" <jrcasey(at)mindspring.com>
Subject: Kolb Fly-in at TNK
Date: Jul 29, 1999
I wanted to see if we could get a collective head count as to how many listers are going to make an appearance at the Fly-In that TNK is planning for late Sept. I live in Alabama and am thinking about driving up with the camper for a couple of days of Kolb building inspiration (boy there's a lot of parts...) I was wondering if we can get a head count here. Question to TNK: Will camping be allowed??? Would there be any chance of a A/C hook-up at the air field??? I promise not to be rowdy!!! It sure would be nice to get 30-40 Kolb's together for some nice formation photo's heh??? Anyway respond to me privately if you want and I'll tally a list for those interested... Jeremy Casey jrcasey(at)mindspring.com Kolb parts owner.. P.S. To the possum...Great web page , especially the last 2 pics...heheheheh P.P.S. to the gentleman who questioned what a possum looks like...Had one climb up on a firewood pile and look in my den window one time. When I went and looked out the window at him , he openned his mouth , showed me his teeth , and hissed. Let's just say this...he could make a mess of your leg if he got a hold of it...And the possums jacket is very accurate as to their looks. Well I've not personally seen one with a leather pilot's helmet and little gomer goggles buuuuuut ...they are in Louisiana....hehehehe ________________________________________________________________________________
Date: Jul 29, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Landing help--how?
Keep the speed up to 60 until just before touchdown, keep a little power on too. Chop the power and hold it off, it'll three point. Richard Pike MKIII N420P (42OldPoops) > >What approach and landing style works best for you guys with Mark 3 aircraft. >I have been flying it on at about 55 doing wheel landings. Attempts to land >the bugger like I would do a Fox or a Cub or an RV as in a normal power off >flare into a three point leaves me flopping on to the ground like a wounded >duck. There is surely something I am missing here though I have tried several >methods to get a nice full stall landing. Wheelies are good but I would like >to three-point. Off subject but what does a possum have to do with flying >Kolbs--I always preferred Armadillos anyway. Armadillos kick possum tail. As >you said -- no respect at all. Just kidding. Thanks. JR ________________________________________________________________________________
From: "Bruce Fletcher" <bwf(at)emailmn.com>
Subject: Re: New web site: Accident report
Date: Jul 29, 1999
The first on your new list: ----- Original Message ----- From: George Thompson <eagle1(at)futureone.com> Sent: Thursday, July 29, 1999 2:02 PM Subject: Re: Kolb-List: New web site: UltralightPilot.com > > > -----Original Message----- > From: JON CROKE <joncroke(at)itol.com> > To: 'kolb-list(at)matronics.com' > Date: Tuesday, July 27, 1999 8:14 PM > Subject: Kolb-List: New web site: UltralightPilot.com > > > > > >Fellow Kolbers: > > > >I would like to announce a new website I have deployed. > > www.UltralightPilot.com > > Gentlemen My Kolb lll www.metroflorida.com/plane amphibian is now an organ donator. After my accident I don't have the money to rebuild. So I am selling it in pieces. This weekend I will be making notes on what's usable. Tomorrow I hope to find what problems I'll be having with my back. To all who had asked about me thanks for your concerns. The morning after the accident the FAA rep stopped in to see me. His first glance at the plane that morning he couldn't see what caused it. So I told him what I thought. I was climbing out and at about 200' 165 mph something snapped in the rudder system. So for 200' I had, I tried to turn away from the swimming beach I was heading for. I landed out side the ropes and altitude. This plane like most planes don't fly very well with out rudder control. About 1 hour later the FAA insp. Called back and told my wife it was not pilot error. He found that one of the pulleys used in rudder the system had frozen to the shaft and after time ( 6 mos. to? ) the cable had sawed trough the pulley and put about 4" of slack in the cable. This is something not easily checked on the preflight in my plane. A yearly check should catch this. Or maybe a good spot for an inspection window. This was a Florida plane for the last 3 years. Anyone interested in parts send me your E-Mail address and when I compile a list I send it to you. Bruce Fletcher bwf(at)emailmn.com ________________________________________________________________________________
From: "Duncan McBride" <duncan.mcbride(at)worldnet.att.net>
Subject: Re: Help with drilling wheel axles?
Date: Jul 30, 1999
Cobalt bits, new and fresh. I burned up two or three regular bullet bits, then had no problem with the cobalt guys. No problem. Good luck. -----Original Message----- From: BICUM(at)aol.com <BICUM(at)aol.com> Date: Tuesday, July 27, 1999 3:50 PM Subject: Kolb-List: Help with drilling wheel axles? > >Need help from the list, > >I have reached a point where I need to drill the two 3/16" holes in each >wheel axle. This is not the alignment hole but the two holes in each axle. >I have used three bits and have made very little dent in this thing. I was >wondering if anyone has had a similar problem and any offerings of possible >solutions. The axles are tagged "Heat treated, do not weld". The only thing >I can come up is get to the drill press and slow it down ,take my time and >drill away. I'm looking for some better bits in the meantime. > >I checked the archives and my search didn't turn up anything specific on this >problem. > > >any help appreciated, > >John (not at Oskosh) Bickham >St. Francisville, LA >Mark III >N308JB (assigned) > > ________________________________________________________________________________
From: gerken(at)us.ibm.com
Date: Jul 30, 1999
Subject: Re: Landing the MKiii
>From: JRWillJR(at)aol.com >Subject: Kolb-List: Landing help--how? > > >What approach and landing style works best for you guys with Mark 3 aircraft. >I have been flying it on at about 55 doing wheel landings. Attempts to land >the bugger like I would do a Fox or a Cub or an RV as in a normal power off >flare into a three point leaves me flopping on to the ground like a wounded >duck. I'll second that! I was making perfect wheel landings all season until I decided I should be making three-pt instead, and started to flare more. For two weeks I kept trying until one new gear leg was in order. Now I am back to making perfect wheel landings. I think with the tail dragger it makes more sense to perform wheel landings anyway. It is kind of nice to have the tail flying last since the rudder gives great control compared to the tailwheel. The longer I keep the tailwheel in the air, the smoother and straighter I seem to land. That's my experience anyway. As for landing with power, that's OK, unless you don't have any. I practice all idle-engine landings everytime (no power after 600'AGL), in preparation for the day it happens that my engine quits. I lower the nose, use half flaps, keep airspeed at 60. If cross-wind, I use no flaps. If passenger with experience, I use full flaps. Once over the runway, speed drops to 50 and I quit watching it. Happy "Wheelies", Jim G ________________________________________________________________________________
From: "Brian Hale" <AccessToData(at)email.msn.com>
Subject: Re: : Kolb-List:Whatever Goes Up ...
Date: Jul 30, 1999
Here is different kind of accident that I thought the list might find interesting. I don't think the pilot would mind if I share this, but just in case, I won't mention any names. I think something can be learned from this. "...when we were ready to leave, I had a problem...I had let a kid sit in my plane while I ate breakfast, and he messed with the controls...no problem usually, but as the guys were ready to leave with their engines running, I started up my Carrera like usual, but didn't check the throttle position B4 starting it from behind, and when it started, it was at FULL THROTTLE! Since I was behind the plane, I grabbed the wire that goes from the wing to the tail, and was able to hold it as it went in a circle, dragging me...There were alot of people there to help me, but they couldn't get in there to grab the plane, as it was circling too fast...a couple of guys tossed sweaters and other clothing at the prop, but the new Sportprop was too tough, and just shredded them. After about 30-40 circles in Jim's field, the wire began cutting my skin on my hand, and I couldn't hold on any longer. When the plane was pointed away from his house/people/planes, I finally let go, aiming it at some shrubs and a tree. I had been working it towards that tree on purpose, hoping it would stop it, but my fingers were bleeding at this point, and the pain became unbearable. When I finally let go, the Carrera headed towards that tree, just brushing it. Then it went into the open field, accelerating till it began to fly by itself. It climbed out, clearing the trees that lined the field, trimmed perfectly at first (and the fuel tanks were full at this point too. I had visions of it flying till it finally would run outta gas, probably over the ocean somewhere... Well, when it got to about 100-200 feet up, it began to turn right, circling and losing altitude till it hit a fir tree, stopping it. It fell down into the lower branches, still at full throttle, till a branch hit the prop, stopping the motor. My new Sportprop was ruined, now only about half the original diam. The left wing is totaled, but the fuselage and right wing are OK, and my motor seems ok too. The tail has only one slightly bent tube also. Definately repairable, but it will take a while. I do hope to have it fixed in time for the Alvord fly-in. I thought for sure it would have been totaled, but got lucky." Brian Hale Firestar I # 439 Sacramento, CA PS: The guy I bought my Firestar from hit his throttle while climbing in. With one leg in and one out he managed to stay with the plane and kill the throttle. ________________________________________________________________________________
From: Lrb1476(at)aol.com
Date: Jul 30, 1999
Subject: Re: ailerons
Dell, That's real good news. I'm going to try the fix tomorrow. I don't know about more adjustment. I guess the info was good.....the counterbalances probably will help a little too. Maybe a few other Kolbers will try the fix, then we can come up with a resolution !!!! Rich Bragassa ________________________________________________________________________________
Date: Jul 30, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: ailerons
Have reflexed my ailerons up about 1/4", but have not had the wind/ bad weather ease up enough for a flight test. But maybe this will do the job. If it does, then I will need a trim tab on the elevator to keep the nose down when flying solo. Richard Pike MKIII N420P (42OldPoops) > >Dell, > >That's real good news. I'm going to try the fix tomorrow. I don't know about >more adjustment. I guess the info was good.....the counterbalances probably >will help a little too. Maybe a few other Kolbers will try the fix, then we >can come up with a resolution !!!! > >Rich Bragassa > > ________________________________________________________________________________
Date: Jul 30, 1999
From: Skip Staub <skips(at)bhip.infi.net>
Subject: Re: Landing the MKiii
Gents, >>a normal power off flare into >>a three point leaves me flopping on to the ground like a wounded duck. Just a thought... Not being able to make decent 3 point landings in a particular aircraft, while you are able to do so in other aircraft, sounds to me as if you might have a forward CG problem. In any case, that's usually the problem when people tell me that they are having trouble 3 pointing their Swift. >I think with the tail dragger it makes more >sense to perform wheel landings anyway. FWIW... It usually takes a bit more skill to consistantly make good 3 point landings as opposed to wheeling the plane on. But... As I see it, 3 pointers allow you to land at a slower speed thus saving wear and tear on the airplane as well as markedly shortening your landing roll. Save the wheel landings for the times when they might be advantageous such as in extreme crosswinds. Regards, Skip Ellenton, FL 1984 Kolb UltraStar 1946 Globe Swift Ellenton, FL ________________________________________________________________________________
Date: Jul 30, 1999
From: Richard Bluhm <irena(at)ccis.com>
Subject: Re: Landing the MKiii
gerken(at)us.ibm.com wrote: > > >From: JRWillJR(at)aol.com > >Subject: Kolb-List: Landing help--how? > > > > > >What approach and landing style works best for you guys with Mark 3 > aircraft. > >I have been flying it on at about 55 doing wheel landings. Attempts > to land > >the bugger like I would do a Fox or a Cub or an RV as in a normal > power off > >flare into a three point leaves me flopping on to the ground like a > wounded > >duck. > > I'll second that! I was making perfect wheel landings all season > until I > decided I should be making three-pt instead, and started to flare > more. For two > weeks I kept trying until one new gear leg was in order. Now I am > back to > making perfect wheel landings. > The longer I keep the tailwheel in the air, the smoother and > straighter I seem to > land. That's my experience anyway. > keep airspeed at 60. If cross-wind, I use no flaps. If passenger > with experience, I > use full flaps. Once over the runway, speed drops to 50 and I quit > watching it. > > Happy "Wheelies", > Jim G Hello guy's; Here's my 2 cents worth: Rather than tell you what my ASI reads, I'll just say that my landing approach is 5 mph faster than my take-off (actual lift-off) speed. Whenever I fly solo, my main wheels usually land first. (I have made 3 point landings, but these aren't due to any attempt.) Then my tail wheel settles down. Whenever I have a passenger, (due to my trim) my tail wheel "always" touches down first. I can feel the tail wheel hit just prior to my mains touching down... The secret here is to determine your actual lift-off speed as indicated by your own ASI, add 5 mph and that will be a good landing approach speed. I have some power added for these approaches, but with an engine out, my approace would have a greater angle to maintain this speed. (just happens my ASI reads 55 for my approaches) I have also noticed the MKIII, with dead-stick, is hard to get over 60 in a descent... Have you guys noticed this?? Well, this is just another one of those opinions that may be of assistance. I find I can land just about anywhere in most winds using this method. Mistakes may cause for an abort, as there isn't enough speed left to try and correct without adding throttle. The slowness of your approach will give you plenty of time to see an oncoming problem. Regards Doc ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Jul 30, 1999
Subject: Re: Landing the MKiii?
The airplane quits flying as soon as I come back on the stick to round off into a flare. I was using 50 over the fence slowing to about 45 or so as I began the flare--it just stops flying--flops to the ground. Using a 1.3 X stall with stall seeming to be at 37 MPH then a proper approach should be flown power off at 48 to 50 MPH. This works in every other airplane I have flown--example, Pitts, Midget mustang, Cub, Super Cub, RV4-6, Kitfox, Aeronca, Luscombe, Decatholon and quiet a few others until now. Something is amiss. Still wondering if flying on in a wheelie at 60 MPH power on to about 4500 RPM is the only way to land the Kolb--what is wrong? JR-sure would hate to hit a possum at 60--might ding the gear ________________________________________________________________________________
From: WGeorge737(at)aol.com
Date: Jul 30, 1999
Subject: Re: Landing the MKiii?
In a message dated 7/30/99 5:50:41 AM, JRWillJR(at)aol.com writes: << The airplane quits flying as soon as I come back on the stick to round off into a flare. I was using 50 over the fence slowing to about 45 or so as I began the flare--it just stops flying--flops to the ground. Using a 1.3 X stall with stall seeming to be at 37 MPH then a proper approach should be flown power off at 48 to 50 MPH. This works in every other airplane I have flown--example, Pitts, Midget mustang, Cub, Super Cub, RV4-6, Kitfox, Aeronca, Luscombe, Decatholon and quiet a few others until now >> Not being an expert in Kolb technique I offer this. The 1.3 Vso works in other airplanes because they have a certain amount of float in them. Due to the fact that speed bleeds off rapidly in very light craft I expect that 1.5 Vso is more appropriate. Add 1/2 the steady wind and all of the gust and you have a speed that is provides a more comfortable round out. Just an opinion. Bill George Mk-3 582 Powerfin ________________________________________________________________________________
Date: Jul 30, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Landing the MKiii?
> >The airplane quits flying as soon as I come back on the stick to round off >into a flare. I was using 50 over the fence slowing to about 45 or so as I >began the flare--it just stops flying--flops to the ground. Using a 1.3 X >stall with stall seeming to be at 37 MPH then a proper approach should be >flown power off at 48 to 50 MPH. This works in every other airplane I have >flown--example, Pitts, Midget mustang, Cub, Super Cub, RV4-6, Kitfox, >Aeronca, Luscombe, Decatholon and quiet a few others until now. Something is >amiss. All the airplanes you list have more mass and/or less drag, and will carry more inertia through the flare. The Kolb has more drag and less inertia, and gives off it's energy much faster. Use more speed over the fence, and don't start to give up any speed until you are closer to the ground. Kolbs fly more like traditional airplanes, but they still land more like traditional ultralights in their ability to dissipate inertia. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
From: "Michael Highsmith" <michael.highsmith(at)worldnet.att.net>
Subject: Re: Landing the MKiii ;Three pionters
Date: Jul 30, 1999
Just my opinion. I believe that wheel landings in the MK3 and other UL aircraft of its' type is the safe and proper way to land in almost all cases. In a Ga aircraft you will have considerably more weight and kinetic energy to carry you through the round out and the landing. Our planes have a way of dropping airspeed quickly because of the lack of kinetic energy and weight once you have cut the power and pulled the nose up to flare. The time for us to make a good three point landing is considerably shorter than the heavier GA plane. It is also considerably more likely to be effected by any change in the direction and speed of the relative wind at landing because of the narrow critical angle of attack in which we have to attain in order to threepoint successfully without bouncing. I have over 2000 logged landings in these type aircraft and I have been able to land three point many times with great success but the only time I have ever bent the gear was when I was trying to three point on an unfamiliar field that I thought I should land as short as possible. As it turned out the field had a slight upgrade on the end that I was attempting to land and I did not has the air speed or the attitude to abort the landing. I landed in a perfect three point with the terrain rising to meet me in the upgrade. That was all it took to bend the gear legs. A wheel landing would have been the right choice at that time and I have since made many landings there on the mains without any problems with that short field. I currently land on 900' with trees at both ends along with the banner plane pilots who land as short as I do consistently some 300-400'. They too land many times on the mains and have a lot more control on roll out which for them it is usually 500-700'. For me it isn't worth the potential damage to my airplane to do three point landings when I can land with a lot more control and stop in as short a distance using little brakes by wheel landing. I'm not advocating wheel landings only and I believe we should practice three pointers but on the average I believe the potential is there to damage the airplane more times with threepoints than it is with a wheel landing. Sometimes we get stuck on the belief that there is only one way to skin a cat. There are lots of options open to our kind of flying. Take advantage of them all. Some may fit your particular style of flying better than others. Safety is what we are after here so we don't have to read about those "Ops" as often as we do. Again, just my opinion. Michael ________________________________________________________________________________
Date: Jul 30, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: 2-stroke reliability
> > >I know nothing about 2-stroke engines, so my question is. Why are the CHT >and EGT so critical when a 2-stroke is used as an airplane engine? With my >weed-eater, lawnmower, etc, it's just crank and go. Never have to worry >about it. I think they will run forever. > Thanks, Ron Take your 2-stroke weedeater and go to full throttle, and start richening up the high speed needle. It runs slower and slower. Now start to lean it out, and it speeds up. 2-strokes are sort of mixture driven, in terms of efficiency and horsepower, much more than 4-strokes. The weedeater and lawnmower are so de-tuned that they are somewhat "idiot proof". An efficient and powerful 2-stroke engine is not, and can be leaned to the point that it will "good itself to death", so it is necessary to know how close to the peak you are operating, without going so far as to compromise reliability. Temperature monitoring is a reliable way to do that. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
From: Dirk4315(at)aol.com
Date: Jul 30, 1999
Subject: Kolb Mark III for sale in Ca.
Late model Mark III for sale in Ca. with aluminum amphibious floats powered by a 912 Rotax with 45 hours total time. 90% of the construction was done by a United aircraft mechanic. It has a Warp Drive tapered tip prop, BRS chute, 15.5 gallon Kolb factory aluminum fuel tank, advanced EIS engine monitor system, strobes, electrical system, hydraulic brakes, and much more, a very nice aircraft flies great, I have photos to e-mail. Large investment. Asking 27,000 My name is Dirk Davis, if you have any question call me at 925-516-4875 or Dirk4315(at)aol.com ________________________________________________________________________________
From: "Clarence R. Perry Jr." <perryr(at)123.net>
Subject: For Sale: Kolb Ultrastar
Date: Jul 30, 1999
For Sale: 1984 Kolb Ultrastar 100 Hours TTE/A Flew great until aborted take-off/crash in June 1999. Serious fuselage/landing gear damage (Cromoly steel) Some holes in wing covering from prop turning into toothpicks. Cuyuna UL/II Engine still runs great. I have all original build plans and revisions plus original builders notes/sales receipts. Comes with fully enclosed trailer. Helmet. Great project for someone who knows how to weld and has the time. Asking $2000.00 for all or trade for PPG. Located in Michigan. For Crash pics, see: http://mula.perrydice.com/ultrasta.htm For what it look like before/and trailer, see: http://mula.perrydice.com/robsnew.htm Thanks for your time, Rob Perry rob.perry(at)perrydice.com ________________________________________________________________________________
Date: Jul 30, 1999
From: Dell Vinal <zoper(at)mint.net>
Subject: landings
On the wheelie vs stall landing. If your airplane doesn't sit on the ground at least at the stall angle, you're going to hit tail first every stall landing and then drop in.This puts a good shock to the plane twice every landing. The wheel landing is hard to learn, but then easy as flying.because that's what you do ,fly it onto the ground without much shock at all. A navy study proved that you can wheel it on fast, and while you have speed and elevator you can brake hard and stop at least as short as a stall landing because while the stall landing is flaring the wheelie is on the ground under heavy braking. However, if you are using a tailhook,you should always follow the POH. I'm going to try another couple turns on the aileron rods next time I fly.Keep tuned. . I thank every one for their landing insights. I am going to use this stuff the next time I fly. ________________________________________________________________________________
From: BILLBEAM(at)aol.com
Date: Jul 30, 1999
Subject: Re: landings
For my 2 cents worth on landings (bad ones). 1. Use full seat belt and two strap shoulder harness. Not a GM car belt. 2. Wear an approved full sided helmet. 3. If battery is used, install it in a secure, enclosed box. Battery acid spills will destroy skin and clothing. 4. Install vent tubes on the fuel tanks that terminate below the thanks. They will be above the tank(s) if you flip over. Don't wait to learn these the hard way. Enough said. Thanks for listening. Bill FS438 ________________________________________________________________________________
From: "Dean Halstead" <deanbo(at)calweb.com>
Subject: Re: : Kolb-List:Whatever Goes Up ...
Date: Jul 30, 1999
It seems like a lot of these recent accident descriptions bear the signs of poor pre-flight inspections. I'm not perfect and I've made a couple misses of my own but as a GA pilot of thirty years, I never get in a plane without giving it the once over. I don't even trust fellow pilots when I ride co-pilot with them. I do my own secondary pre-flights. ________________________________________________________________________________
Date: Jul 31, 1999
From: Gary Thacker <gthacker(at)mciu.org>
Subject: Re: Lubs and probes
Just a couple of quick questions. I know in the past there has been thoughts about lubs for hinges, cables, and pulleys etc. What is the preferred lube for these things. I have heard, in the past that some of the lubes attract dirt and can have a negative effect. What are you guy's usin? One other thing. I had to replace my CHT probes yesterday. Just wonderin. Should the probes contact the head directly or should they go between the compression ring and spark plug. Common sense would say the head but ya never know. I would think they would "fit" better between the the compession ring on the plug and the plug face. I don't know if that little change would make that much difference. Gary Souderton,Pa. gthacker(at)mciu.org | ____F i r e S t a r____ ___(+)___ (_) \ / ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: Lubs and probes
Date: Jul 31, 1999
This'll be interesting. My understanding is that you're supposed to take the factory ring off the plug, and just use the CHT sender. Let's see what comments you generate. Big Lar. ----- Original Message ----- From: Gary Thacker <gthacker(at)mciu.org> Sent: Saturday, July 31, 1999 7:00 AM Subject: Kolb-List: Re: Lubs and probes > > > One other thing. I had to replace my CHT probes yesterday. Just > wonderin. Should the probes contact the head directly or should they go > between the compression ring and spark plug. Common sense would say the > head but ya never know. I would think they would "fit" better between > the the compession ring on the plug and the plug face. I don't know if > that little change would make that much difference. > > > Gary > Souderton,Pa. > gthacker(at)mciu.org > > | > ____F i r e S t a r____ > ___(+)___ > (_) > \ / > > ________________________________________________________________________________
From: "Larry Davis" <ldavis(at)gatem02.netusa1.net>
Date: Jul 31, 1999
Subject: Re: Lubs and probes
I found I had a much better seal if I first removed the sparkplug gasket, put the CHT sender on the sparkplug threads, and then re- installed the gasket on the sparkplug threads. It also makes threading the sparkplugs back into the head easier. IMHO This'll be interesting. My understanding is that you're supposed to take the factory ring off the plug, and just use the CHT sender. Let's see what comments you generate. Big Lar. ----- Original Message ----- From: Gary Thacker <gthacker(at)mciu.org> Sent: Saturday, July 31, 1999 7:00 AM Subject: Kolb-List: Re: Lubs and probes > > > One other thing. I had to replace my CHT probes yesterday. Just > wonderin. Should the probes contact the head directly or should they go > between the compression ring and spark plug. Common sense would say the > head but ya never know. I would think they would "fit" better between > the the compession ring on the plug and the plug face. I don't know if > that little change would make that much difference. > > > Gary > Souderton,Pa. > gthacker(at)mciu.org > > | > ____F i r e S t a r____ > ___(+)___ > (_) > \ / > > -- Larry Davis Marion, Indiana Challenger 1 CW http://www.netusa1.net/~ldavis/airplane.html ________________________________________________________________________________
Date: Jul 31, 1999
From: "Alan I. Goldman" <goldman(at)ameslab.gov>
Subject: bent landing gear
My partner and I just had the (apparently common) experience of bending a gear leg during a rough landing. We need to replace the leg on a 1986 Kolb Twinstar MKII, and are tempted to get a rod of Al and have it tapered here in town. Problem is, that we are not sure which aluminum grade, species, etc... to use. Any help here would be greatly appreciated. thanks in advance alan Alan I. Goldman Professor and Chair, Department of Physics and Astronomy Senior Physicist, Ames Laboratory USDOE Director, Midwest Universities Collaborative Access Team A501 Physics Addition Iowa State University Ames, IA 50011 phone: 515-294-3585, 515-294-5442 fax: 515-294-6027, 515-294-7129 email: goldman(at)ameslab.gov homepage: http://www.public.iastate.edu/~cmpexp/groups/goldman/homepage.html ________________________________________________________________________________
From: "merle hargis" <merlepilar(at)worldnet.att.net>
Subject: Re: Heavy Ailerons/ Cross Country trip
Date: Jul 31, 1999
You don't have to explain. I live in Orlando and fly all over central Fl. I try to fly at least once a week and get my "fix" for the week. Merle Hargis (Twinstar) from Orlando > I went on my first cross country with fellow LAFA (EAA Chapter 103) > http://www.lafa.com/ > Home Page members this weekend. There > were two Rans S-12's with 503's and a Buc 11 with a 582. We flew from Miami > due north over the Everglades and over Lake Okeechobee to three Airparks. > Home sites were for sale, the area is east of Sebring, (home of Lockwood > Aviation). Total flight about 280 miles round trip. I've lived in Florida > just about my whole life, but have never seen it from the ultra-light slow > and low perspective. I was totally amazed at the sights. I was in sensory > overload when I got home, was dead tired, but couldn't sleep. I spent the > next day, Sunday, walking around in a stupor, like a drug addict coming off a > high. > > Like the old Harley Davidson saying goes...If I have to explain, you won't > understand... > > Rich Bragassa > Mk lll > Miami, Fl. ________________________________________________________________________________
Date: Jul 31, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: MKIII ailerons/elevator trim
Today I had a chance to try out the ailerons in a reflexed condition to see if they felt any lighter. Since I knew from previous experience that reflexing the ailerons makes the MKIII fly as if it were tailheavy, I went ahead and added trim tabs to the elevators to give it a little more of a nose down tendency. Since I had previously modified the stainless steel "L" brackets at the front of the horizontal stab, raising the front of the horizontal stab to also help get rid of the tendency to nose up, I found that I had created some really weird trim conditions. The trim tabs on the elevators are 16" long, and started out 2" wide (not counting the part that is rivited to the elevator). The are on the top, and slant up at about a 20 degree angle. That was too big, and combined with the raised front stabilizer brackets, they create two different unsatisfactory trim situations. At higher speeds and higher power settings, (70 MPH, 5800 RPM) it required most of the available up elevator trim to stabilize level flight. At lower power settings and speeds (50 MPH, 4800 RPM) the airplane would once again try to nose up and slow down some more at the same elevator trim setting. More disturbing, I got the distinct impression that the combination of down elevator trim tabs and the raised front edge of the stabilizer created an unstable situation, the airplane no longer felt like it would behave itself properly in all situations. Pitch unstable at certain speeds. Also felt that adding or reducing power further destabilized the situation. Ailerons had been reflexed up 4 turns of the end fitting from the way they normally are, no apparent improvement. Removed the shims from the front of the stabilizer and tried it again. Now it was stable, but different speeds affected how effective the elevator trim tabs were. Too effective at high speeds, not enough at low speeds. Landed and trimmed 1/2" off the back edge of the trim tabs. Much more consistent at all speeds, still needed a little more up elevator trim than It seemed like it should. Reflexed the ailerons up 4 turns more, and things were better all around. The balance between the elevator tabs and the ailerons was very good, only needed a little up elevator trim from the stock lever, and and trim was close to constant at all speeds. Ailerons were lighter, especially at slower speeds, still a bit too heavy at higher speeds. The improvement in the ailerons was good enough that adding spades or servo tabs is no longer likely an option for me, will wait until I fly two up to see if maybe I can reflex them up a bit more and see how that works. Right now the apparent reflex is such that in flight, the ailerons look to be up about three degrees from parallel to the bottom of the wing. Trimmed another 1/8" off the rear of one of the elevator trim tabs, now it seems just about right. Handling qualities now are better than ever, and that was always good. Realize this has been pretty long, but maybe it will help some one else work their way through the same situation. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
From: "Michael Highsmith" <michael.highsmith(at)worldnet.att.net>
Subject: Re: Lubs and probes
Date: Jul 31, 1999
Kolbers and non Kolbers, Any lubrication on the hinges is better than none. There was a test done on moving metal parts years ago. What was found is that metal wears 300 time faster without lubrication than it does with lubrication. It was done on motorcycle chains back in the 70s. I found out through my on experimentation that I could make a moto cross bike chain last some 10 times as long with a continuous supply of oil running to the chain from a reserve that I had built into the frame. I proved the test results myself this way. I could run a whole day of racing without so much as having to adjust the chain while my racing buddies were constantly having the adjust and replace their chains and sprockets. I use the used gearbox oil to lube my hinges and all the metal pivot points on the whole airframe. Anything that moves or even vibrates needs some oil. I take a cable tie and dip it in a small container that holds an oz. or two of the gear oil. This way I can control how much oil I want to use and see where it is going. After I apply I wipe all excess. The small amount that gets to the point of pivot is all that is needed to make all your moving metal parts last a good portion of the life of the airframe. Although a smooth running engine and prop has a lot to do with wear on the airframe and after 750 hours on mine I believe now it will at lest take another 750 hours before I even think of replacing hinges. So far there is no appreciable wear on the hinges and there want be any dirt on them either as long as I wipe them off while I do my walk around. Now that I know you know how to make your moving parts last let me tell you how I keep my plugs from ever leaking oil around their base. I use an anti seize stick I get from Advanced Auto that looks like a Crayola crayon with the paper wrapped around it. I learned this from the old A&P that works at our field. As often as we should change and check our plugs we should always use it to keep the threads in the heads from getting worn out. The best thing is it will keep the oil from seeping out around the base of the plugs. After I tighten new plugs down to compress the ring gasket I pull it out and put the thermo couple on the bottom next to the head with anti seize on the threads. A little anti seize goes a long way. It works well for me and they don't leak. The CHT gauge doesn't seem to know the difference. I got to fly 3.6 hours today and landed at 3 different places with two of wingmen. Hope y'all had as happy a day also. I had so much fun I think I'll do it again tomorrow. We're "sky hole pok'rs" down here in the panhandle. Negative reflex does help in a lot of ways, especially in hands off flying. Michael ________________________________________________________________________________
From: "Beauford Tuton" <beaufordw(at)worldnet.att.net>
Subject: Re: bent landing gear
Date: Jul 31, 1999
Alan: For whatever it's worth... the legs on the Firefly are 7075-T651... rpt 7075-T651... good luck Bill Tuton Building at FF 076 Brandon, Fl. -----Original Message----- From: Alan I. Goldman <goldman(at)ameslab.gov> Date: Saturday, July 31, 1999 2:20 PM Subject: Kolb-List: bent landing gear > >My partner and I just had the (apparently common) experience of bending a >gear leg during a rough landing. We need to replace the leg on a 1986 Kolb >Twinstar MKII, and are tempted to get a rod of Al and have it tapered here >in town. Problem is, that we are not sure which aluminum grade, species, >etc... to use. Any help here would be greatly appreciated. > >thanks in advance > >alan > > >Alan I. Goldman > >Professor and Chair, Department of Physics and Astronomy >Senior Physicist, Ames Laboratory USDOE >Director, Midwest Universities Collaborative Access Team > >A501 Physics Addition >Iowa State University >Ames, IA 50011 > >phone: 515-294-3585, 515-294-5442 >fax: 515-294-6027, 515-294-7129 >email: goldman(at)ameslab.gov >homepage:
http://www.public.iastate.edu/~cmpexp/groups/goldman/homepage.html > > ________________________________________________________________________________
Date: Jul 31, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: landings
> I'm glad to hear that 4 more turns are gonna make even better >results.I weigh 210, Old Poops, what do you go?I was suprised to hear >about trim concerns . I weigh 190, and my Kolb always acted tail heavy solo, unless I drooped the ailerons a tiny bit. Not any more. Flew this afternoon, took a passenger, very nice, and the ailerons are a bit better. (4 more turns out since this morning) Ailerons look to be about 4 degrees higher than parallel to the wing lower surface while in flight. > I looked at an Air Command gyro today. Built in 92-93 from a 91 >kit. 582,prerotator, stock-never flown. It seems they have an annoying >tendency to tip over when a certian situation arrises. This one had new >draggon rotor blades and seemed in good shape.Somebody tell me some >reasons why I shouldn't buy this thing, Please.5 thou. The wife of our former chapter president is a widow. Snowbird two seater. A bolt tucked into a control system cluster behind the second seat was not visible/accessable during preflight. Closed casket funeral. He was a scrupulous perfectionist, and a flight instructor, but it got him and his student anyway. I am a firm believer in staying away from anything where all the crucial stuff that keeps you aloft, or can decapitate you, is in unstable motion. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: Kolb-List - First flight
Date: Jul 31, 1999
Too bad you're just lurking. Sounds like you're really up and doing it - - - the right way. Congratulations, and good luck. Keep us posted. Big Lar. ----- Original Message ----- From: John Cooley <johnc(at)datasync.com> Sent: Saturday, July 31, 1999 7:41 PM Subject: Kolb-List: Re: Kolb-List - First flight > > Hello Gang: > Well I finally got in the air today. Here's a quick recap of my plane as > I'm sure most of you don't remember. I purchased a 1988 model Twinstar MK 11 ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: landings
Date: Jul 31, 1999
I think I'd be real wary of anything that has a tendency to "tip over." I've got a real hard head, but the rest of me is real fragile. I'm thoroughly enjoying this input on aileron reflexing. Keep it up, and thanks. Sensitive Lar. ----- Original Message ----- From: Richard Pike <rpike(at)preferred.com> Sent: Saturday, July 31, 1999 8:49 PM Subject: Re: Kolb-List: landings > > > > I looked at an Air Command gyro today. Built in 92-93 from a 91 > >kit. 582,prerotator, stock-never flown. It seems they have an annoying > >tendency to tip over when a certian situation arrises. This one had new > >draggon rotor blades and seemed in good shape.Somebody tell me some > >reasons why I shouldn't buy this thing, Please.5 thou. > > ________________________________________________________________________________
Date: Aug 01, 1999
From: wood <duesouth(at)iname.com>
Subject: Re: bent landing gear
> >My partner and I just had the (apparently common) experience of bending a >gear leg during a rough landing. We need to replace the leg on a 1986 Kolb >Twinstar MKII, and are tempted to get a rod of Al and have it tapered here >in town. Problem is, that we are not sure which aluminum grade, species, >etc... to use. Any help here would be greatly appreciated. > >thanks in advance > >alan > > I think it is 7075. It is a common grade. Some of the guys on the list are using 4130 steel for the legs. Woody ________________________________________________________________________________
From: HShack(at)aol.com
Date: Aug 01, 1999
Subject: Re: Reflexed Ailerons
I,too noticed rather heavy ailerons on my Firestar I; I think this is probably not a bad thing as the less "yank & bank" you do the more likely you are to stay out of trouble. However..... On Friday, I reflexed my ailerons up four turns & did indeed find them lighter & more responsive without any noticeable change in climb performance or any pitch change. My CG is dead in the middle of the recommended range. I do have counterbalances but don't believe they have much effect on 'heaviness'. Howard Shackleford FS I SC ________________________________________________________________________________
Date: Aug 01, 1999
From: "Alan I. Goldman" <goldman(at)ameslab.gov>
Subject: twinstar MKII
Hi all, Thanks for the response on the gear rod material. A couple more questions if anyone can answer. We just purchased a Twinstar MKII (serial #4)with a Rotax 582. Apparently the plane was sent back to the factory to beef up the support for the engine. What we don't know are the relevent numbers for typical empty weigt, gross weight, c.g. range (with respect to, say, the leading edge of the wing) and various speeds for safe operation. The owners manual was not with the mound of paper we received. The plane was orignally on a set of full lotus floats, that we have since removed, and the tail wheel support was extended down to account for the added height of the tube above the floats. Now we need to shorten that tube to bring the planed back to its original configuration. What angle should the tube be with respect to the horizontal ( that will tell me how much shorter the tailwheel support has to be). In addition, there is a steel wire strung between the two mains that has snapped (in an unfortunate landing). Does anyone know what the tension in that cable should be? All information about the twinstar would be appreciated. We would be especially grateful if anyone can supply us with a copy of a manual for a 1986 Twinstar MKII. thanks in advance alan ________________________________________________________________________________
Date: Aug 01, 1999
From: Skip Staub <skips(at)bhip.infi.net>
Subject: Missing Man @ Wimauma
Hi Beauford, Another Sunday's flying is in the log books (so to speak). Ann and I went out to Wimauma International about 8:00 am and unfolded the UltraStar.and I flew it for about 45 minutes. There were three trikes on the field and two of them flew. The 3rd one was just bought by a gent that lives up near Lake City and has his own strip and a Cessna 150. He bought the trike and now needs to learn to fly it. Unfortunately, he had been travelling most of the night and didn't feel up to the challenge of learning something new today. A friend of one of the trike owners ("James A Barone" ) seems rather interested in Kolb aircraft. I don't know if he has any flight experience or not, but he enjoys riding in the trikes. When I told him that there was a man in Brandon building a Kolb Firefly he seemed VERY interested in seeing how one was built. He is a professional mechanic so I doubt if the project would be beyond his capabilities. In any case, I gave him your e-mail address and you might hear from him as I'm sure he has some questions. (I too would like to see your project:) In a previous message to me you said something to the effect that you brought your boat back to MacDill. Are you retired from the military? I was both an enlisted man and an officer in both the Air Force and the Navy. Retired in 1979. 20 years ago---- damn I'm getting old! Regards, Skip ________________________________________________________________________________
From: Lrb1476(at)aol.com
Date: Aug 01, 1999
Subject: Re: MKIII ailerons...another cross country
<< Reflexed the ailerons up 4 turns more, and things were better all around. >> Richard, Looks like my friends info was some what accurate...I tried 3 turns this weekend, with a very slight improvement in stick pressure. My adjustment is approx. 3/8". If I understand your info you went 4 turns and then another 4? What would that be in inch measurement from the trailing edge of the aileron, and the bottom of the wing? Since we all build a little different our "turns" will have other values. I would like to "crank" in some more turns. I went on another cross country this weekend. My buddy and I flew from Miami due west across the Everglades to the west coast to Everglades City (a fishing community). Great trip, one hour fifteen minutes with a five mph tail wind. The Airport is small, but probable the most modern and nicest in the State. The Airport manager, John treated us like Royality. We ate lunch, at a local joint and watched the weather building up in the NW, probably an hour or two away. I called our buddies on the phone at our club field in Homestead. They said the weather was clear there, so we halled butt back to Miami. The elephants were walking in front of that rain at 500 to 1,000 feet, so we climed to 5,000. It was real smooth, but cold as hell...no doors...tee shirts and shorts...... We were cruising at 75 indicated with a 10 mph tail wind. Got back in 50 minutes. Sure enough 4 hours later in the afternoon the rain came in, but I was in my Lazy-Boy dreaming about next weekend....... Rich Bragassa Mk lll ________________________________________________________________________________
From: GeoR38(at)aol.com
Date: Aug 01, 1999
Subject: Re: pucker patch
In a message dated 7/28/99 9:56:58 AM Eastern Daylight Time, hping(at)hyperaction.net writes: << http://www.hyperaction.net/hping >> Howard, you are a talented guy and have created a bit of heaven on earth...it is quite easy to see......keep it up buddy!!...........GeoR38 ________________________________________________________________________________
From: "plane" <plane(at)atomic.net>
Subject: Re: For Sale: Kolb Ultrastar
Date: Aug 01, 1999
-----Original Message----- From: Clarence R. Perry Jr. <perryr(at)123.net> Date: Friday, July 30, 1999 7:06 PM Subject: Kolb-List: For Sale: Kolb Ultrastar > >For Sale: >1984 Kolb Ultrastar >100 Hours TTE/A >Flew great until aborted take-off/crash in June 1999. >Serious fuselage/landing gear damage (Cromoly steel) >Some holes in wing covering from prop turning into toothpicks. >Cuyuna UL/II Engine still runs great. >I have all original build plans and revisions plus original builders >notes/sales receipts. >Comes with fully enclosed trailer. Helmet. > >Great project for someone who knows how to weld and has the time. > >Asking $2000.00 for all or trade for PPG. > >Located in Michigan. > >For Crash pics, see: >http://mula.perrydice.com/ultrasta.htm > >For what it look like before/and trailer, see: >http://mula.perrydice.com/robsnew.htm > >Thanks for your time, >Rob Perry >rob.perry(at)perrydice.com > > ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Density Altitude
Date: Aug 01, 1999
Seems like every time I go for a taildragger lesson, something more comes of it than I expect. This Fri., the 30th, it was back to APV for another shot at the Champ. My share-expense passenger couldn't make it till 9:00 AM, so we were an hour later getting up there. After pre-flighting the student (me) and then the plane, we didn't commence to Aviate till after 11:00 AM. Bad Mistake. This is High Desert, folks, getting up toward Doc's neck of the woods. Hot and windy. APV is at 3059' msl, and by the time we started we had a 10-12 mph crosswind - 90 to runway 18. Let's just say that the 1st takeoff was.................interesting. I could hear John suck in air in the back seat, even over the engine noise. Nuffa that !!! Events 2, 3, and 4 we did off rwy 26, and it was much better, except that by takeoff # 4, the temp was up to 103. Aircraft is a Champ with just 75 hp, and 380 lb. of student and instructor. Terrain west of 26 rises toward a small mountain about a mile or so away. Our pitiful rate of climb was just barely greater than the rising ground. We managed a normal pattern, and called it a day. Density Altitude in Action. Surprising thing was that t.o. # 3 was fine. Climb in the Champ isn't anything to brag about at the best of times, but it was sufficient. In the time it took to do the pattern, make a full stop, taxi back, and go for # 4, there was a great difference. Lest you think we're completely insane, our out was descending ground to the north, but would have required a right turn, and blown the pattern. Still, it was there if we needed it. A side note is that our planned lunch at Big Bear, (L35) was out of the question. Would have taken all day to climb up there in the 172. Fun, fun, fun, in the warm California sun. Except that I guess everybody has had that blistering sun this past week. Not much fun is it ?? Big Lar. ________________________________________________________________________________
Date: Aug 01, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: MKIII ailerons...another cross country
>Looks like my friends info was some what accurate...I tried 3 turns this >weekend, with a very slight improvement in stick pressure. My adjustment is >approx. 3/8". If I understand your info you went 4 turns and then another 4? >What would that be in inch measurement from the trailing edge of the aileron, >and the bottom of the wing? Since we all build a little different our >"turns" will have other values. I would like to "crank" in some more turns. Really don't know how much in inches. Just looking at the end of the wing, and where the aileron used to go straight back, now it looks like it goes up about 3/8" in flight. Now that I think about it, I dont know if I turned the end fitting eight half turns (4 full turns) or twelve (six full turns). I just kept turning and test flying until they reflexed up a little as you look at it in flight. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
Date: Aug 02, 1999
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Antennas and Portland Seminar questions
>Have been reading your comments on GlaStarNet with interest. I have a couple >of questions that perhaps you could help me with. > >1. I purchased and ACK ELT for installation in the GlaStar. In the >installation instructions, it states that the antenna should be installed a >minimum of 5 ft. from any com antenna. > >It does not state why, nor does it state the consequences if the above >"should" is violated. The only two things I can think of is that if the ELT >were activated, it could overload the rf into the com receiver. >Alternatively, is it possible the com signal could overload the ELT >transmitter, active or inactive? Do you have any knowledge of why the >instruction is included? Like software designers who believe their work is the most important program on your computer and loads up your quick start icons with a half dozen links to THEIR program, hardware designers constantly dream about the ideal install of their equipment in your computer -OR- airplane. In the real world, there are few performance issues with respect to antennas that ever get idealized on airplanes . . . especially the lower frequency devices (VHF) . . . gee, when I got started in electronics, 100 MHz was the edge of no-man's land . . . guys who could make things work at 2-meters (144 MHz) were revered for their technical accumen that was rumored to include special blessings and perhaps a bit of black-magic. Nowadays, we're all wishing that 50 year old VHF "junk" would just go away. Transponders, GPS and Cell-phone antennas (900 MHz and up) are about as close to ideal installs as you can get in any vehicle. 100 MHz has become the new "low" frequency service with its huge, bulky antenna and quirky idealized requirments that are hard to achieve on anything smaller than a DC-9 . . . If your ELT were really, Really, REALLY close to the com transmit antenna, there might be some risk of the com transmitter popping somethign in the ELT but were talking inches of separation. Given that the output stages of the ELT are another TRANSMITTER designed to handle considerable power comparted to the sensitive amplifiers in the front end of a RECEIVER, it's unlikely that the ELT can be damaged by proximity coupled energy from another light plane transmitter (airlines use 25 watt transmitters and are potentially more dangerous to other on-board systems). Bottom line is install things were they (1) fit, (2) look best or (3) work best . . . according to most builders choices (1) and (2) are handily accomodated by installing all antennas inside the tailcone . . . keeps of the bugs, rain, and make the airplane look really sharp. Given that you've probably spent $K$ on your electro-goodies, it would be nice that they also work . . . My best advice is to look over installations other builders have been flying and if they're happy with the way things work, your chances of a similar result are good. >2. I am thinking (and dealing with time conflict) of attending your seminar >in Portland (possibly another preson as well). What is the sign-up deadline? > Can we sign-up/pay at the seminar? The Portland gig was postponed for lack of interest. We're in the re-organization mode. Watch the seminar webpage. We'll also announce new dates and places on the various lists. To other list-servers . . . I've been out of town a lot over the past month and have a couple of trips (weekend only) yet this month . . . this is why I've been so quiet lately on the lists. I've been able to teach my laptop how to dial using a calling card so I was able to keep up with most e-mail while Dee and I were on an extended trip earlier last month. Right now, I'm sitting at a folding table in our new office here at the house. No furniture in it yet but I do have the copy machine installed. Spent most of the weekend installing all the telephone and networking cables in the walls . . . carpenter things are not my favorite pastimes! Got all the phone system up and running about 1 a.m. this morning. When all the office furniture is out of the shop, we'll be adding about 200 square feet of new shelving and plan to greatly expand our electro-goodies inventory. I've got a guy working on a new website with a shopping cart catalog. The goal by the end of the year is to become a truely one-stop-shopping source for all your electrical system needs. It's going to take several more days to get the office back together so I may continue to be more "distant" than usual . . . but I'll be back! Bob . . . //// (o o) ===========o00o=(_)=o00o========= < Independence Kansas: the > < Jurassic Park of aviation. > < Your source for brand new > < 40 year old airplanes. > ================================= http://www.aeroelectric.com ________________________________________________________________________________
From: gerken(at)us.ibm.com
Date: Aug 02, 1999
Subject: RE: Flaps reflex...
The flaps replex discussion has been interesting. A recent post: >Dell, > >That's real good news. I'm going to try the fix tomorrow. I don't know about >more adjustment. I guess the info was good.....the counterbalances probably >will help a little too. Maybe a few other Kolbers will try the fix, then we >can come up with a resolution !!!! > >Rich Bragassa I have always had the counterbalances on (the mkiii). This weekend I tried the reflex ideas too. I assumed that you guys were adjusting BOTH the ailerons AND flaps, right??? That's what I did, adjusted all four surfaces up about 1/2", as measured at the rear tip of the surfaces. This took a couple turns of each end of each linkage. After adjustment, the surfaces appeared to be slightly higher than parrallel with the bottom of the wing, when in flight. They may have been too low before. Flight results: no detectable change in trim bias, no detactable change in stall or top speed, no detectable change in control force to move ailerons. Since I have not yet affected the trim bias, should I go further? Jim Gerken ________________________________________________________________________________
From: Timandjan(at)aol.com
Date: Aug 01, 1999
Subject: BACK FROM OSHKOSH
Just got back from Oshkosh. The new owners are real nice. They have a new Mark 3 (actually his) and a new slingshot with a 912 that they were flying. They are also plavving a flyin in Kentucky in September, near the end (forgot the date). I live in the Virginia Washington DC area if anybody ion the area wants to go maybe we can go together. (trailer to the place) tim ________________________________________________________________________________
Date: Aug 02, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: RE: Flaps reflex...
> >I have always had the counterbalances on (the mkiii). This weekend I tried the >reflex ideas too. I assumed that you guys were adjusting BOTH the ailerons AND >flaps, right??? I had previously modified the flap control handle so that I can adjust the flaps up and down in small increments to affect trim, so: yes. That's what I did, adjusted all four surfaces up about >1/2", as >measured at the rear tip of the surfaces. This took a couple turns of each end >of each linkage. After adjustment, the surfaces appeared to be slightly >higher >than parrallel with the bottom of the wing, when in flight. They may have been >too low before. Flight results: no detectable change in trim bias, no >detactable change in stall or top speed, no detectable change in control force >to move ailerons. > Jim Gerken Interesting. On my MKIII, any change in aileron or flap raising/drooping immediately raises or lowers the nose quite a bit. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
From: "Michael Highsmith" <michael.highsmith(at)worldnet.att.net>
Subject: Flaps and Aileron reflex:
Date: Aug 02, 1999
Think about this+ADs- If you leave the flaps set straight in line with the bottom of the wing and the ailerons were set up from the bottom about 4-5 degrees would not this give you a positive control in a stall? This would make the inside of the wing next to the wing root stall first but the outside of the wing next to the tip would still be flying being you have effectively reduced the angle of attack by turning up the ailerons, therefore you would be given a small advantage in time and control as the wing is approaching and during the stall. The Lazair ultralight has a slightly washed out wing for this purpose. With no flaps a pilot could put the Lazair in a complete stall at very slow speed but as the whole wing dropped the ailerons were still effective to somewhat because they had not stalled nor did the wing tip. It could be stalled for long descents with a good portion of control. Based on experimentation in my opinion there is an advantage to turning up the flaps and ailerons for cruise but if they is turned up to much and I do mean a lot your stall speed will increase and there is a point that it can add drag. There is a balance though that works very well for cruise and stalls. This is where you might want to look. It's like fine tuning your aircraft to perform to its' optimum. Every wing is a little different so the exact thing that works for one may or may not work for another. I'm just trying to give something to think about while you are flying along wondering how to improve a good design. It will also give you something else to do next weekend. Michael ________________________________________________________________________________
Date: Aug 02, 1999
Subject: Re: RE: Flaps reflex...
From: Ray L Baker <rbaker2(at)juno.com>
Jim/Richard, How do your CG's compare?????? L. Ray Baker Lake Butler, Fl Building Mark III, SN 312 writes: >>detactable change in stall or top speed, no detectable change in >control force >>to move ailerons. >> Jim Gerken > >Interesting. On my MKIII, any change in aileron or flap >raising/drooping >immediately >raises or lowers the nose quite a bit. >Richard Pike >MKIII N420P (42OldPoops) ________________________________________________________________________________
Date: Aug 02, 1999
From: Erich Weaver 805-683-0200 <sbaew(at)dames.com>
Subject: Re: RE: CG calculations
Im getting ready for test flight in Mark III with a 912 and did some center of gravity calculations. Perhaps a few of the old hands out there could look over my shoulder and see if anything looks funny to you? Not having built the plane myself, Im going off of what I as able to get old Kolb to send to me, Ben Ransoms Firestar web site, and Kolb list postings. I expected the plane to be tail heavy with the 912, but was a little surprised that I had to put 52 lbs in the nose of the plane to reach mid-range of what is recommended. Check it out: CENTER OF GRAVITY CALCULATION (Sorry if the formatting of this post gets messed up through the e-mail system.) The basics: Empty weight=510 lbs (plane, parachute, no gas, no pilot or passenger Plane attitude at 9 degrees pitch upward, as measured along bottom surface of wing with 4-foot level and ruler set at 7.5 inches. Measuring points for weight: R wheel, L wheel, T wheel Datum for CG calculation: leading edge of wing Avg. Wing chord = 66 in. (leading edge to trailing edge of wing, including flap) Distances between measuring points and datum: R wheel: 7" L wheel: 7" T wheel: 207" (all measurements aft of datum; i.e they will have positive moments) Formula: Total Moment = Weight x Distance Case: Plane + 9.5 gallons gas + me (188 lbs) with radio and helmet + 52 lbs nose weight (Nose weight center of mass approximately 49" in front of datum) Measured wt Distance Moment (lbs) (inches) (inch-lbs) R wheel 349 7 2,443 L wheel 409 7 2,863 T wheel 53 207 10,971 Total Wt. 811 Total Moment 16,277 Resultant Distance = Total Moment / Total Weight = 16,277 / 811 = 20.1 % chord = Resultant Distance / Avg Wing Chord = 20.1 / 66 = 30.4% (acceptable range: 25-35%) Conclusions: optimum balance achieved for case of me as pilot, full tank of gas, and added nose weight Does everything look hunky-dory here? Did a theoretical calculation to consider same circumstances but with a low fuel tank (~3 gal gas). CG was still very near optimum. Appears that with the 52 lbs nose weight in place, amount of fuel in tank affects CG very little. I guess thats a good thing...... Did a for-real CG check with full tank, passenger (168 lbs) and no nose weight added; CG was right in middle of acceptable range. That should make it easy: add full nose weight when by myself; remove all nose weight when have passenger of average build. Thanks in advance for any critiques of my methods and results. Plan on using a test pilot who weighs a little less than me, so will be looking at the affect of a lighter pilot as well... Erich Weaver ________________________________________________________________________________
Date: Aug 02, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Flaps and Aileron reflex:
> > >Think about this+ADs- > If you leave the flaps set straight in line with the bottom of the wing >and the ailerons were set up from the bottom about 4-5 degrees would not >this give you a positive control in a stall? This would make the inside of >the wing next to the wing root stall first but the outside of the wing next >to the tip would still be flying being you have effectively reduced the >angle of attack by turning up the ailerons, therefore you would be given a >small advantage in time and control as the wing is approaching and during >the stall. Agree. It would be better to have the ailerons a little higher. >Based on experimentation in my opinion there is an advantage to turning up >the flaps and ailerons for cruise but if they is turned up to much and I do >mean a lot your stall speed will increase and there is a point that it can >add drag. There is a balance though that works very well for cruise and >stalls. This is where you might want to look. It's like fine tuning your >aircraft to perform to its' optimum. Agree again. So far my solo rate of climb is staying right at 1000' FPM and dual the other day, 180 lb. passenger, 83 degrees was 600-700 FPM. Cruise is the same or better than before, dual or solo. Stall no change. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
Date: Aug 02, 1999
From: Randy Appleton <randy(at)euclid.acs.NMU.EDU>
Subject: Re: Kolb-List Digest: 07/26/99
I was talking to the ultralight instructor who lives nearest my house. Unfortunately, he lives 4 hours away by car. Anyway, he was telling me that ultralight activity is down both locally (Northern Michigan) and nationally. He seemed rather depressed about it, but not unreasonably so. My question is: How is the state of ultralight activity? Increasing, decreasing? -Much Thanks -Randy ======================================================================== || Randy Appleton, Professor of Computer Science at Northern Michigan || || University. And a big fan of Linux! || ================= mailto:randy(at)euclid.nmu.edu ========================== ________________________________________________________________________________
Date: Aug 02, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: RE: Flaps reflex...
Solo, I am diet limited. Right now I weigh 190. If I get down below 165, I need to add a passenger, or wear heavier shoes. So I am somewhat near the rear CG solo. ( I could go out and dig the paperwork out, and give you specific numbers, but you get the idea.) Richard Pike MKIII N420P (42OldPoops) > >Jim/Richard, > >How do your CG's compare?????? > >L. Ray Baker >Lake Butler, Fl >Building Mark III, SN 312 > > >>no detectable change in stall or top speed, no detectable change in >>control force >>>to move ailerons. >>> Jim Gerken >> >>Interesting. On my MKIII, any change in aileron or flap >>raising/drooping >>immediately >>raises or lowers the nose quite a bit. >>Richard Pike >>MKIII N420P (42OldPoops) ________________________________________________________________________________
Date: Aug 02, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re: RE: CG calculations
> >Im getting ready for test flight in Mark III with a 912 and did some >center of gravity calculations. Perhaps a few of the old hands out there >could look over my shoulder and see if anything looks funny to you? Not >having built the plane myself, Im going off of what I as able to get old >Kolb to send to me, Ben Ransoms Firestar web site, and Kolb list >postings. I expected the plane to be tail heavy with the 912, but was a >little surprised that I had to put 52 lbs in the nose of the plane to >reach mid-range of what is recommended. Check it out: You don't have to hit the "Middle" just stay within bounds would be O.K. I,m at 36% and flys great. But on the other hand you can always take weight out, of the nose after you fly it for a while. They turn better a "little" Tail heavy it seems to me-so far. ________________________________________________________________________________
From: Mhqqqqq(at)aol.com
Date: Aug 02, 1999
Subject: Re: Lubs and probes
has anyone used chain wax? ________________________________________________________________________________
From: WEBEFLYRS(at)aol.com
Date: Aug 02, 1999
Subject: Re: Lubs and probes
WHATS IT FOR ________________________________________________________________________________
Date: Aug 02, 1999
From: bob n <ronoy(at)shentel.net>
Subject: Re: Lubs and probes
Waxes yer chain. ________________________________________________________________________________
From: JL1339(at)aol.com
Date: Aug 02, 1999
Subject: Re: : Kolb-List:Unscribe
Please remove me from your mailing list, Thank You very much. JL1339(at)aol.com ________________________________________________________________________________
From: JL1339(at)aol.com
Date: Aug 02, 1999
Subject: Re: Unsubscribe
Please remove me from your mailing list, Thank You very much. JL1339(at)aol.com ________________________________________________________________________________
Date: Aug 02, 1999
From: Skip Staub <skips(at)bhip.infi.net>
Subject: Re: Lubs and probes
>has anyone used chain wax? I find chain wax to be a superior lubricant for motorcycle chains, but I'm not certain that it would be the best thing for aircraft hinges. To be effective on a motorcycle, the chain must be warmed up by riding for awhile before application. I doubt that physically moving an aileron or elevator back and forth would generate the heat necessary. :) Maybe warming the hinge with a heat gun prior to application would work? I can only guess that chain wax would be a little cleaner than oil. Personally, I just use a little engine oil (in a squirt can) and then wipe off the excess. ________________________________________________________________________________
From: "John Cooley" <johnc(at)datasync.com>
Subject: Re: Kolb-List Digest: 07/26/99
Date: Aug 02, 1999
----- Original Message ----- From: Randy Appleton <randy(at)euclid.acs.NMU.EDU> Sent: Monday, August 02, 1999 1:40 PM Subject: Kolb-List: Re: Kolb-List Digest: 07/26/99 Anyway, he was telling me > that ultralight activity is down both locally (Northern Michigan) and > nationally Hi All: Seems to be increasing in here in South Ms. Hearing reports at work of lots of Ultralight sightings over the weekend. Still high from first flight in my plane! Hope to get another fix Wednesday morning. Later, John Cooley ________________________________________________________________________________
From: Lrb1476(at)aol.com
Date: Aug 02, 1999
Subject: Re: RE: Flaps reflex...
I have always had the counterbalances on (the mkiii). This weekend I tried the reflex ideas too. I assumed that you guys were adjusting BOTH the ailerons AND flaps, right??? That's what I did, adjusted all four surfaces up about 1/2", as measured at the rear tip of the surfaces. This took a couple turns of each end of each linkage. Jim, My info was to raise only the ailerons, I think raising both would defeat the purpose. I'm going to try a little more next weekend to see if theres a noticable difference. Richard Pike got some good results so far.....lets see..... Rich Bragassa Mklll Miami, Fl ________________________________________________________________________________
From: JFHan44(at)aol.com
Date: Aug 02, 1999
Subject: Re: Official Usage Guideline [Please Read] [Monthly
Posting] unsubcribe ________________________________________________________________________________
From: gerken(at)us.ibm.com
Date: Aug 03, 1999
Subject: flaps, trim, CG, etc...
I am afraid that I don't have the info handy either, but here's my rough figures: I have placarded it "Minimum solo pilot 150 lbs." If I remember correctly, that is 37% CG. I weigh 190. I will go to the airport and check this out on the paperwork, and report back again if it is different than reported here. >From: Richard Pike <rpike(at)preferred.com> >Subject: Re: Kolb-List: RE: Flaps reflex... >. > > >Solo, I am diet limited. Right now I weigh 190. If I get down below 165, I need >to add a passenger, or wear heavier shoes. So I am somewhat near the >rear CG solo. ( I could go out and dig the paperwork out, and give you >specific numbers, but you get the idea.) >Richard Pike >MKIII N420P (42OldPoops) >> > >> >>Jim/Richard, >> >>How do your CG's compare?????? >> >>L. Ray Baker >>Lake Butler, Fl >>Building Mark III, SN 312 >> >> >>>no detectable change in stall or top speed, no detectable change in >>>control force >.>>to move ailerons. >>>> Jim Gerken >.> >>>Interesting. On my MKIII, any change in aileron or flap >>.raising/drooping >.>>immediately >>>raises or lowers the nose quite a bit. >>>Richard Pike >>>MKIII N420P (42OldPoops) Jim G ________________________________________________________________________________
From: "Ron C Reece" <rcreec(at)ftw.rsc.raytheon.com>
Date: Aug 04, 1999
Subject: OOPS!
Gang As much as I'd like to say that things are going great with construction of my FSII, things aren't. I just realized that after finishing both horizontal stabilizers and most of the verticals, I realized that I used the 3/8s tubing for bracing instead of the 5/16 stuff. #@&$@*#!!!! Is this a problem? Do I need to change it out? I know I have to reorder same, but I really don't want to rip things apart so soon. Any thoughts folks? Signed ashamed Ron Reece ________________________________________________________________________________
Date: Aug 04, 1999
From: "Douglas G. Murray" <dgmurray(at)telusplanet.net>
Subject: Re: OOPS!
Ron C Reece wrote: > Gang > > As much as I'd like to say that things are going great with construction of my > FSII, things aren't. I just realized that after finishing both horizontal > stabilizers and most of the verticals, I realized that I used the 3/8s tubing > for bracing instead of the 5/16 stuff. #@&$@*#!!!! Is this a problem? Do I > need to change it out? I know I have to reorder same, but I really don't want > to rip things apart so soon. Any thoughts folks? > > Signed > ashamed > > Ron Reece Ron - you will probably make many more mistakes as you build your aircraft. Don't feel ashamed over mistakes 'cause that's how we learn. Since you are just starting your project you will be on a steep learning curve and will make more mistakes now than later. It is better for you to step back from your project and reorder the new tubing for your stabilator now, than to make a choice to compromise your project and be happy with mistakes. Remember - it will be your life on the line when you are up in the sky flying. Do you really want to be in an aircraft that you _know_ that you could have built better? Have fun building and do it right. Doug Murray FireStar 1 flying since 1990 Southern Alberta ________________________________________________________________________________
From: "Michael Highsmith" <michael.highsmith(at)worldnet.att.net>
Subject: Re: OOPS!
Date: Aug 04, 1999
It want hurt to use a little larger tubing in the tail feather bracing. It will add a tad more weight. It shouldn't change the CG. I for one would not take it out and I would go ahead and order to replace that that I had used you need it later. Do think about it and take your time. You'll make a lot more mistakes before you are through. The trick is to keep them at a minimum. One mistake I made was not getting out all the little metal shavings out of the wing and tail before I covered. You just can't be vigilant enough on getting out every little speck before you cover. They'll show up just about the time you get ready to paint. Michael ________________________________________________________________________________
Date: Aug 04, 1999
From: wood <duesouth(at)iname.com>
Subject: Re: OOPS!
> > >Gang > >As much as I'd like to say that things are going great with construction of my >FSII, things aren't. I just realized that after finishing both horizontal >stabilizers and most of the verticals, I realized that I used the 3/8s tubing >for bracing instead of the 5/16 stuff. #@&$@*#!!!! Is this a problem? Do I >need to change it out? I know I have to reorder same, but I really don't want >to rip things apart so soon. Any thoughts folks? > >Signed >ashamed Gosh no oone on this list has ever screwed up before. I am not sure which tubes you are refering to but if it is the ones I am thinking about I would leave them in and order more 3/8 tube to replace what you accidentally used up. I doubt if it added that much extra weight to the tail. If you used 5/16 instead of 3/8 I would be worried Woody ________________________________________________________________________________
From: WillU(at)aol.com
Date: Aug 04, 1999
Subject: Re: OOPS!
Ron, been there done that. I use the 3/8" tube only on the vertical stabilizer. Dennis Souder said it was no problem, he also sent me replacement tubing at no charge. I'm not use to mentally converting fractions to decimal or vice versa. The plans shows the dimension in fractions and the tube's dimensions are printed in decimal. I think the plans should show the dimension in fractions as well as in decimals. Nowadays to double check I'm using the right tube size is by side an open end wrench, http://member.aol.com/fs2kolb/pictures/19.jpg I also printed a fraction to decimal conversion chart and pasted it on the wall. Don't get discourage, It's all part of the learning experience. Will Uribe http://member.aol.com/WillU/index.html > > > > Gang > > As much as I'd like to say that things are going great with construction of > my > FSII, things aren't. I just realized that after finishing both horizontal > stabilizers and most of the verticals, I realized that I used the 3/8s > tubing > for bracing instead of the 5/16 stuff. #@&$@*#!!!! Is this a problem? Do > I > need to change it out? I know I have to reorder same, but I really don't > want > to rip things apart so soon. Any thoughts folks? ________________________________________________________________________________
From: WGeorge737(at)aol.com
Date: Aug 04, 1999
Subject: Prop pitch & EGTs
HI Gang: This subject has received a lot of coverage on the list. John Hauk has put out some valuable info and John, if you have recovered from Oshkosh, I'd appreciate you jumping in here. Background. Engine is 582 with "C" box at 3:1 ratio. Operating from an airport at 2700 MSL and density altitude of 3900 ft. Engine starts quick, runs smooth and idles well. I purchased a Powerfin "F" model 68 inch three blade and when winds permit I have been trying to dial in the proper pitch. The Ivo three 67 1/2 blade that was previously installed loaded the engine to the extent that RPM never exceeded 6000. EGTs were always around 1000 and below for all throttle openings. The thing ran so cool that I never got specific numbers. Temps were always in the low side of the green arc. Started the Powerfin pitch setting at the factory recommended 10.5 degrees tip angle, which was way too little, and have been increasing pitch from there. Once in the range that the static RPM was around 6100-6200 I began flight testing. I am now to 12.5 degrees pitch. Performance is good. WOT in level flight is redline. Full throttle climb temps are 1000. However, as soon as throttle was reduced from max power the temps went up to 1200. Idle was OK below 1000. Since I BELIEVED the prop is pitched close I then raised the needles to the bottom clip (one notch) and the mid range temps now seem only slightly above the full throttle temps. But it seemed that at cruise power the engine was not quite as smooth. This was hard to determine because by late morning there was lots of wind and thermal activity. I do understand the relationships of loading and EGT on two strokes. But, I am wondering if I should have increased pitch another half degree before going to the needles? This, particularly since the old installation had good temps. I'd appreciated numbers from those with similar installation on the following: 1) RPM and EGT for full throttle climb. 2) EGT at cruise RPM 3) EGT at partial power descent (3500 to 4000 RPM) 4) Blade angle at tip Thanks for your input. Bill George MK-3 582 Powerfin ________________________________________________________________________________
Date: Aug 04, 1999
From: Dennis & Diane Kirby <kirbyd(at)flash.net>
Subject: Cutting Instrument Panel Holes
Hey, Gang - I'm stuck, and need some advice. (Be kind, all - this is the first human-carrying airplane I've ever built.) I am ready to begin cutting out instrument panel holes, and want to go about it properly. (My instrument panel is .063 alum sheet, same size & shape as the stock fiberglas panel on the nosecone, only offset 6 inches aft from the nosecone. It's supported by an alum framework and hinges at the bottom for fold-down easy access to instruments. Also, the alum panel is shock-mounted to its support structure ... good news for the instruments. Top glare shield (.025 Al sheet) finishes appearance nicely. Thanks again, Cliff, for the excellent idea!) Earlier this year, when I asked the List about instrument holes, the advice was generally that one could use door-hole saws - the kind used for wood or aluminum doors. I've seen these at the hardware store, 3 inches diam. Hole size requirement is 3 and an eighth. (Actually, a wee bit more, to allow a bit of play for easy installing.) Is the accepted practice to drill the 3-inch hole, then hog out the rest using a good-quality rounded file? (Seems like I heard that somewhere.) What's the right kind of file to use for this? Is there a better/easier method? Thanks for the help - Dennis Kirby (wishing I could be at OSH instead) Mark-III, s/n 300 80% finished in New Mexico ________________________________________________________________________________
From: "Michael Highsmith" <michael.highsmith(at)worldnet.att.net>
Subject: Prop pitch and EGT for 582
Date: Aug 04, 1999
With 755 hours of flight, 582, 3/1 Ebox , 70+ACI- IVO, pitch at tip is 11.5 degrees Max climb out RPM is 6400 Water temp is always between 145-170 and at cruise it hangs at around 150-160 EGT on climb out is 950-1000 ( Normal per rotax is 930- 1150) CHT is 190-225 ( Normal per Rotax is 230-270) mine has always read low? Cruise EGT is 1000-1050 Cruise CHT is 200-225 Here is the clincher---My normal fuel burn for 5000-5200 rpm is 3-3.2 gals/ hr My normal fuel burn for 5800-6000 rpm at an AS of 80 -85 mph( my preferred cruise / John Hauck) is only 3.4-3.6 gals/ hr I have checked it many times and it always comes out the same. I for one am not going to change it or complain about it. It burns the same or less than most 503s I fly with. I do have a little exhaust deflector I have fabricated on the stinger pipe to keep the hot gas and oil off the prop. It does a good job for what I designed it for but when I installed it I had to drop the main jet down to +ACM-150 in order to get these temps. I also dropped to a +ACM-45 idle jet to keep it idling smooth. The engine runs smooth in all ranges and it has the power I need. Go figure? One comment here. I did find out that these gauges are notoriously off a lot of the time. I had a new Rotax Tach that would read off everytime it got hot ( cockpit temperature hot) Sometimes by as much as 1000 RPM. Another thing I have found out through experience with my 582, is that if you let the K+ACY-N filter go to long without cleaning it or if you fly through through to much rain and not service it, it will wake you up one day on climb out with a series of skips and misses. Then the wrong thing to do is clean it with gas because its' all you got. It will cost you a cool +ACQ-50 for that little mistake. Been there done that. Michael ________________________________________________________________________________
From: BILLBEAM(at)aol.com
Date: Aug 04, 1999
Subject: Re: Cutting Instrument Panel Holes
Dennis, I have similar question about instrument installation. The previous owner or builder installed all the gages from the rear of the panel. Can you see some logical reason for this? I'm going to make a new panel on piano hinge like yours and thought about putting the instruments in from the front. This will hide the rough edges made by the extra 1/8 inch. Any thoughts? Bill Beams FS348 Wilmore, Ky ________________________________________________________________________________
Date: Aug 04, 1999
From: Paul VonLindern <paulv(at)digisys.net>
Subject: Re: Cutting Instrument Panel Holes
Dennis I just cut the holes for my panel and I used a circle cutter. I purchased it at Western Building Center ( Ace Hardware ) and cost about $12.00. It cuts a very nice clean hole, especially if you use a cutting fluid ( I used a product called "Tap magic" ). After the hole was cut no filing was necessary. It must be used in a drill press and I would suggest drilling some sample holes in a piece of scrap material to get the hole size adjusted correctly. PaulV ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: Cutting Instrument Panel Holes
Date: Aug 04, 1999
I used a Milwaukee Hole Saw, pn 49-56-3120, of 3 1/8" diameter for the large holes. A friend loaned me a machinists 2 1/4" hole hog for the small ones, but it made them a little too tight. Very tedious opening them up. Finally tried one of those rotary sandpaper "flapper" things in my drill, and it did a pretty good job, and kept the holes round. I'm sure Milwaukee makes a 2 1/4". If you like, I can email you a picture of the panel. I agree with Paul - use a drill press - you can't hold a hand drill steady enough for nice results. Never tried Paul's circle cutter, but it sounds like it did a nice job, and you only need to buy one, for all the holes. The biggest hair puller I ran into on the panel, was getting all the mounting screw holes lined up nice and neat. A possible reason someone installed the gauges from the back of Bill's panel may be that they used aircraft instruments, which are designed that way. Automotive instruments are slightly smaller, and are designed to slip in from the front of the panel. BTW, I used all aircraft instruments; I too used .063 aluminum, and faced it with wood grain formica. I know the formica may add 8 or 10 ounces, but boy, it sure looks good, and is 0 maintenance. I thought of using some kind of fancy veneer, but then thought of trying to refinish it in the future - no way - uh-uh. Big Lar. ----- Original Message ----- From: Dennis & Diane Kirby <kirbyd(at)flash.net> Sent: Wednesday, August 04, 1999 12:45 PM Subject: Kolb-List: Cutting Instrument Panel Holes > > Hey, Gang - > I'm stuck, and need some advice. (Be kind, all - this is the first > human-carrying airplane I've ever built.) > I am ready to begin cutting out instrument panel holes, and want to go > about it properly. > > (My instrument panel is .063 alum sheet, same size & shape as the stock > fiberglas panel on the nosecone, only offset 6 inches aft from the > nosecone. It's supported by an alum framework and hinges at the bottom > for fold-down easy access to instruments. Also, the alum panel is > shock-mounted to its support structure ... good news for the > instruments. Top glare shield (.025 Al sheet) finishes appearance > nicely. Thanks again, Cliff, for the excellent idea!) ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Seats and Plastic
Date: Aug 04, 1999
For those of you I promised pictures of my bucket seats and mounts, I've finally got some photos of them back, and will get them on their way to you. Now, I have a question. To connect the intake runners to the throttle body, I need tubing of 1 1 /4" I.D. Local NAPA store has radiator tubing that will fit and probably last forever, but I seem to keep getting more and more carried away with this thing. I'd really like to find some blue urethane, or similar tubing that would look better. I'll be painting the intake system, and the cooling shrouds a medium metallic blue, and will be using blue anodized braided hoses for fuel and oil lines. A local plastics supplier can get me all I want, of any color I choose, as long as I start with a minimum 50' order. I need 10". Help ! ! ! Where would I logically (or otherwise) look to find such a thing ?? ..............................You know, I was just about to hit "send", and had the idea - if all else fails, maybe blue heat shrink tubing over the radiator hose ?? Where would I look for some of that in about 1 1/2" diameter ?? Big Lar. ________________________________________________________________________________
From: WGeorge737(at)aol.com
Date: Aug 04, 1999
Subject: Re: Prop pitch and EGT for 582
Thanks for the response. I will print this one out. One question. What is your field elevation and what sort of OATs in your area? Bill ________________________________________________________________________________
Date: Aug 04, 1999
From: Erich Weaver 805-683-0200 <sbaew(at)dames.com>
Subject: Re: Seats and Plastic
Big Lar: Talk to MSC Industrial Supply, and get a free catelog while you're at it. Phone: 800-645-7270. If they dont have what you want, it most likely doesnt exist. There are thousands of pages of stuff I never knew I needed before in their catelog. Easy index when you know what you want. Great toilet reading when you're just looking for something to want. Let me know how you make out. Erich ________________________________________________________________________________
Date: Aug 04, 1999
From: "Douglas G. Murray" <dgmurray(at)telusplanet.net>
Subject: Re: Cutting Instrument Panel Holes
Dennis & Diane Kirby wrote: > --Hey, Gang - > I'm stuck, and need some advice. (Be kind, all - this is the first > human-carrying airplane I've ever built.) > I am ready to begin cutting out instrument panel holes, and want to go > about it properly. > > (My instrument panel is .063 alum sheet, same size & shape as the stock > fiberglas panel on the nosecone, only offset 6 inches aft from the > nosecone. It's supported by an alum framework and hinges at the bottom > for fold-down easy access to instruments. Also, the alum panel is > shock-mounted to its support structure ... good news for the > instruments. Top glare shield (.025 Al sheet) finishes appearance > nicely. Thanks again, Cliff, for the excellent idea!) > > Earlier this year, when I asked the List about instrument holes, the > advice was generally that one could use door-hole saws - the kind used > for wood or aluminum doors. I've seen these at the hardware store, 3 > inches diam. Hole size requirement is 3 and an eighth. (Actually, a > wee bit more, to allow a bit of play for easy installing.) > > Is the accepted practice to drill the 3-inch hole, then hog out the > rest using a good-quality rounded file? (Seems like I heard that > somewhere.) What's the right kind of file to use for this? Is there a > better/easier method? > > Thanks for the help - > Dennis Kirby (wishing I could be at OSH instead) > Mark-III, s/n 300 > 80% finished in New Mexico Dennis - There are two accepted methods to cut instrument holes in you IP. The first is to use a flycutter and cut the holes real carefully. The second is to use a 'GreenLee' punch and punch out the hole. The punch has the tendency to leave ragged edges and a slightly deformed panel but is accurate it size and quick. the punch is rather expensive. The flycutter can be adjusted for any size and leaves a real nice hole that needs only a light deburr to clean it up. If you really want a super and expensive job you could always graph out an IP on your CAD and have it laser cut. Hope this helps Doug Murray FireStar 1 flying since 1990 Southern Alberta ________________________________________________________________________________
From: "Frank & Winnie Hodson" <fwhodson(at)bigfoot.com>
Subject: OOPS!
Date: Aug 04, 1999
> -----Original Message----- I just realized that after finishing both > horizontal > stabilizers and most of the verticals, I realized that I used the > 3/8s tubing > for bracing instead of the 5/16 stuff. #@&$@*#!!!! Is this a > problem? Do I > need to change it out? I know I have to reorder same, but I > really don't want > to rip things apart so soon. Dear Ron: You have now become a seasoned builder who made a slight 'modification" in the interest of increased strength! Seriously you have made a boo-boo in the best direction and place...It will increase the bracing capability beyond what was needed without changing the basic design/function. All of the empanage bracing hides inside the shapes of larger structural tubing and will not show through to the final finish. The weight penalty will total less than 1/2# in a project that will eventually weigh between 300 and 400 pounds. If this is the only time you become confused or make a mistake you make during your project...You will become the winner of the KOLB CRAFTSMAN award! This Project is absolutely riveting! FRANK HODSON, OXFORD ME (FSII N6399J) ________________________________________________________________________________
From: Timandjan(at)aol.com
Date: Aug 05, 1999
Subject: pane;
> > (My instrument panel is .063 alum sheet, same size & shape as the stock > fiberglas panel on the nosecone, only offset 6 inches aft from the > nosecone. It's supported by an alum framework and hinges at the bottom > for fold-down easy access to instruments. Also, the alum panel is > shock-mounted to its support structure ... good news for the > instruments. Top glare shield (.025 Al sheet) finishes appearance > nicely. Thanks again, Cliff, for the excellent idea!) > > Earlier this year, when I asked the List about instrument holes, the > advice was generally that one could use door-hole saws - the kind used > for wood or aluminum doors. I've seen these at the hardware store, 3 > inches diam. Hole size requirement is 3 and an eighth. (Actually, a > wee bit more, to allow a bit of play for easy installing.) > > Is the accepted practice to drill the 3-inch hole, then hog out the > rest using a good-quality rounded file? (Seems like I heard that > somewhere.) What's the right kind of file to use for this? Is there a > better/ My Ideas???? The 3 1/8 hole saws are available but pricy. The rounding out method with a file works but gives an umpefect round hole which I have never been happy with. Another method, they sell these adjustable hole saws, the cutting blades are sharpened 1/8 inch steel rods, the are designed for wood, however, I have cut a many holes in the aluminum and if you cut slowld thay work fine. I think they sell for around 10 dollars. I have seen them at Home Depot as one place. tim ________________________________________________________________________________
Date: Aug 05, 1999
From: Tom Barton <barton(at)ameslab.gov>
Why would using stronger tubing for bracing be a problem? The only reason I can imagine would be weight. Tom > >Gang > >As much as I'd like to say that things are going great with construction of my >FSII, things aren't. I just realized that after finishing both horizontal >stabilizers and most of the verticals, I realized that I used the 3/8s tubing >for bracing instead of the 5/16 stuff. #@&$@*#!!!! Is this a problem? Do I >need to change it out? I know I have to reorder same, but I really don't want >to rip things apart so soon. Any thoughts folks? > >Signed >ashamed > >Ron Reece > Tom Barton Director, Ames Laboratory Director, Institute of Physical Research & Technology Distinguished Professor of Chemistry Iowa State University Ames, Iowa 50011 Phone: 515-294-2770 Fax: 515-294-4456 ________________________________________________________________________________
From: gerken(at)us.ibm.com
Date: Aug 05, 1999
Subject: Big Lar's got the blues...
Big Lar wrote: >From: "Larry Bourne" <larrybiglar(at)earthlink.net> >Subject: Kolb-List: Seats and Plastic > For those of you I promised pictures of my bucket seats and mounts, >I've finally got some photos of them back, and will get them on their way to >you. > Now, I have a question. To connect the intake runners to the >throttle body, I need tubing of 1 1 /4" I.D. Local NAPA store has >radiator tubing that will fit and probably last forever, but I seem to keep >getting more and more carried away with this thing. I'd really like to find >some blue urethane, or similar tubing that would look better. I'll be >painting the intake system, and the cooling shrouds a medium metallic blue, >and will be using blue anodized braided hoses for fuel and oil lines. A >local plastics supplier can get me all I want, of any color I choose, as >long as I start with a minimum 50' order. I need 10". Help ! ! ! Where >would I logically (or otherwise) look to find such a thing ?? >..............................You know, I was just about to hit "send", and >had the idea - if all else fails, maybe blue heat shrink tubing over the >radiator hose ?? Where would I look for some of that in about 1 1/2" >diameter ?? Big Lar. Larry, I also started off making everything color-neat and mostly one color. This looks less home-made when you get done but there is a drawback to keeping all the plumbing one color: Inspection efficiency. I have found that, once it is all plumbed and complicated-looking, it is kind of nice to have a few different colors of hoses for the various functions, to make tracing and inspecting easier. Think of it this way: how would you like to do all your electrical wiring with the same color? big mess, Big Lar! Just my two cents..., use some black hoses mixed in with your blue, and save yourself some headaches and cash. If this doesn't suit you, then you should know that HPC of Kansas offers high-temp coatings for exhaust systems in about ten different colors, including BLUE! Jim G ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Aug 05, 1999
Subject: HPC coatings--???
Please elaborate on HPC coating of Kansas. I am interested please. Thanks. JR of Kansas ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Aug 05, 1999
Subject: Cutting instrument holes
For cutting your instrument holes a quality hole saw works great--oneintended for metal. I used a tool known as a flycutter. The flycutter is an adjustable diameter cutting tool on a rod for varying the diameter with a set screw. Operate at lowest RPM on a floor type drill press. Be careful--a flycutter will grb your arms, hands, fangles, clothing. Another tool available from Avery and Cleveland tool is a reversible 3 1/8 and 2 1/4 hole punch at about 80$ for the tool that will neatly and professionally cut your instrument holes. A template is available from Aircraft spruce for laying out your screw holes and cutouts for altimeter or make your own. JR ________________________________________________________________________________
Date: Aug 05, 1999
From: Wally Hofmann <wally(at)foxfibre.com>
Subject: Cutting Instrument Panel Holes
I just finished drilling the holes in the fiberglass panel for my FireFly. It may not be the same in aluminum but an adjustable 'fly cutter' worked great. I got it adjusted just right by drilling scrap material. It left a very clean edge. The biggest problem was building a jig to hold the nose cone under the drill press. I think the most important thing is to go slow. I didn't try the hole saw but would be afraid it might chip up the edge of the hole. I also discovered that a coping saw with a very fine blade worked really well for cutting the rectangular hole for the EIS unit. Wally Hofmann Wickenburg, AZ ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: Cutting instrument holes
Date: Aug 05, 1999
Yah, I got that metal template from A/C Spruce, and it works - sorta. The holes in it don't .........quite..........match up with the holes in the instruments. Takes a little work with a 1/8" round file. It helps a lot, but care must still be taken to get the holes all lined up. I found it to be pretty tedious, but the finished result looks very good. Big Lar. ----- Original Message ----- From: <JRWillJR(at)aol.com> Sent: Thursday, August 05, 1999 10:06 AM Subject: Kolb-List: Cutting instrument holes > > For cutting your instrument holes a quality hole saw works great--oneintended > for metal. I used a tool known as a flycutter. The flycutter is an adjustable > diameter cutting tool on a rod for varying the diameter with a set screw. > Operate at lowest RPM on a floor type drill press. Be careful--a flycutter > will grb your arms, hands, fangles, clothing. Another tool available from > Avery and Cleveland tool is a reversible 3 1/8 and 2 1/4 hole punch at about > 80$ for the tool that will neatly and professionally cut your instrument > holes. A template is available from Aircraft spruce for laying out your screw > holes and cutouts for altimeter or make your own. JR > > ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: Big Lar's got the blues...
Date: Aug 05, 1999
Thanks Jim. Your point is well taken, and I'll have to sit and chew on that for a while. I do want - definitely - to keep everything in light colors, both to reduce heat absorption here in the desert, and also to make leaks and cracks easier to spot. Blue Lar. ----- Original Message ----- From: <gerken(at)us.ibm.com> Sent: Thursday, August 05, 1999 9:41 AM Subject: Kolb-List: Big Lar's got the blues... > > Larry, I also started off making everything color-neat and mostly one color. > This looks less home-made when you get done but there is a drawback to keeping > all the plumbing one color: Inspection efficiency. I have found that, once it > is all plumbed and complicated-looking, it is kind of nice to have a few > different colors of hoses for the various functions, to make tracing and > inspecting easier. Think of it this way: how would you like to do all your > electrical wiring with the same color? big mess, Big Lar! > > Just my two cents..., use some black hoses mixed in with your blue, and save > yourself some headaches and cash. If this doesn't suit you, then you should > know that HPC of Kansas offers high-temp coatings for exhaust systems in about > ten different colors, including BLUE! > > Jim G > > ________________________________________________________________________________
From: "John Cooley" <johnc(at)datasync.com>
Subject: MK II VNE
Date: Aug 05, 1999
Hello Folks: Just got thru with my second lesson in my Twinstar MK II. Practiced coordinated turns for about 1 hour and then practiced flying in the pattern and pretty much landed the plane myself on the third pass. Of course the instructor kept a light feel on the stick just in case. Had a blast and just want to get back in the air real soon. I would like some info if anyone could help please. When I bought the plane it didn't have any paperwork with it and I need to know the published VNE, stall speed, roc (single and double) and any other pertinent info. Oh yea! Even though the instructor is a "M-Squared man" he commented on how well the Kolb fly's and lands. Of course having 3500 ft of runway does help. Our indicated airspeed on landings was about 50-55 mph. I have no idea how accurate or inaccurate my indicator is. I did use one of Ben Ransom's idea's ( I'll give him credit since I saw it on one of his post) by venting the static port to both sides of the front pod. Airspeed at 5800 rpm was approx. 55 mph if I remember correctly. I know I'm rambling too much so I'll quit. Thanks, John Cooley ________________________________________________________________________________
From: WillU(at)aol.com
Date: Aug 05, 1999
Subject: Re: Cutting Instrument Panel Holes
A picture so you can get an idea on cutting the instrument panel holes. http://member.aol.com/n8754k/page/ssdc170.jpg In a message dated 8/5/99 3:07:26 PM Mountain Daylight Time, Wally Hofmann writes: > I got it adjusted just right by drilling scrap > material. It left a very clean edge. The biggest problem was building a > jig to hold the nose cone under the drill press. ________________________________________________________________________________
From: "Jon Croke" <joncroke(at)itol.com>
Subject: Re: back home
Date: Aug 05, 1999
> > Hi Guys, > > My trip to Oshkosh was very nice. It was about a 600 mile round trip from > Minneapolis and back. About the only discouraging thing that happened was > that I was grounded from flying during the event by Jamie Kee for > crossing over the active runway without permission. I was camped on the > west side which made it necessary to taxi around or across. He made Ralph, Congrats on making that long trip! Sorry I missed you, but did run into Kent, my 'neighbor' to the north and we swapped some stories, etc. I wanted to find you, but I couldnt stay long enough. Im curious, how many stops did you make in each direction? Any wind problems, etc. Im alsways amazed at those making that long of a trip in these planes..... I still never leave a 20 mile circle around my house! Chicken! As for Osh Kosh... maybe its just me, but I see evidence every year of more 'lack of consideration' for the ultralight sport. It starts with the fact that I had to spend over $40 just to set foot in the place. At Sun n Fun its $10. When I want to see UL planes fly at Osh... they cant. Its always either 'air show time' or too windy or too wet. None of this happens at Sun n Fun quite the way it does at Osh. So I am not surprised at how they handled you there.... I share your anger and frustration. I did talk to a PR rep with EAA and asked about the huge cost diff between the two shows, expressing my concerns about the 'average' guy with average funds participating in the UL sport. He said that Sun n Fun is sponsored by EAA MEMBERS, and Osh Kosh is sponsored by the EAA CONVENTION. So that explains it???? Sory about my soap box, but Ralph I give you credit for flying that distance which is a feet in itself -- demonstrating the utmost in skill and spirit of UL flying... and then to get treated like that. You can be sure I tore up my mandatory 3 month EAA membership card... (which is not needed at Sun n Fun). My hat off to all those voulunteers and vendors and pilots that made the UL event fun... we'll have to live with the 'organization' in the mean time. Just blowing off steam! Jon ________________________________________________________________________________
Date: Aug 04, 1999
Subject: Re: Cutting Instrument Panel Holes
From: Robert L Doebler <bobdoebler(at)juno.com>
--------- Begin forwarded message ---------- From: BILLBEAM(at)aol.com Subject: Re: Kolb-List: Cutting Instrument Panel Holes Date: Wed, 4 Aug 1999 16:07:52 EDT Dennis, I have similar question about instrument installation. The previous owner or builder installed all the gages from the rear of the panel. Can you see some logical reason for this? I'm going to make a new panel on piano hinge like yours and thought about putting the instruments in from the front. This will hide the rough edges made by the extra 1/8 inch. Any thoughts? Bill Beams FS348 Wilmore, Ky it will work just fine. Just a slightly different look is all. Bob Doebler --------- End forwarded message ---------- ________________________________________________________________________________
From: "Christopher John Armstrong" <Tophera(at)centuryinter.net>
Subject: Re: RE: Flaps reflex...
Date: Aug 05, 1999
While at oshkosh I was looking over the factory slingshot... it uses flaperons like the firefly and my firestar II. THey had put an aileron control stop on the end of the wing pivot bolt, which stoped the aileron from over deflecting with 0 degrees flaperon setting. This stop location also stoped the aileron from deflecting AT ALL when the flaperons were set to full. I repeat it would not allow any left aileron at full flaperon!!!!! If you are adjusting your ailerons to try out relex make sure you check your motion and any stops you have installed before flight after each adjustment. If you are putting in flaperons keep this in mind. I thought this was way dangerous. Topher ________________________________________________________________________________
From: "Frank & Winnie Hodson" <fwhodson(at)bigfoot.com>
Subject: HPC coatings--???
Date: Aug 05, 1999
> -----Original Message----- > Please elaborate on HPC coating of Kansas. I am interested > please. Thanks. JR > of Kansas Dear JR: I had my entire exhaust system coated silver by HPC, including the springs. It was a quality job. I have run the 503 about 3 hours total time breaking it in and trying to work out some electrical gremlins...so far not even a hint of discoloration. Without digging through drawers full of receipts and invoices my best recall is that it cost me about $140 total including the shipping. It looks so good, I'd do it again in a minute. FRANK HODSON, OXFORD ME ________________________________________________________________________________
From: "Lindy" <lindy(at)snowhill.com>
"Sam Cox" , "Rutledge Fuller" , "Paul Spadin" , "Michael Highsmith" , "Kolb Builders" , "John Hauck" , "Greg Moloney" , "Glenn Rinck" , "Danny Day" , "Buddy Carilse" , "Bob Moorehead" , "Ben Cole" , "ASC2"
Subject: Fw: RegReps re USUA Topics
Date: Aug 05, 1999
----- Original Message ----- From: <Johnusua(at)aol.com> ; ; ; ; ; ; Sent: Thursday, August 05, 1999 3:06 PM Subject: RegReps re USUA Topics > August 5, 1999 > > > Dear Directors and Regional Representatives > > AT LAST, > USUA has 3rd Party Liability Insurance Coverage FOR USUA MEMBERS > > Pre-Announcement: Not for distribution yet. > > The final tweaks to the application and information brochure are being > accomplished right now. But we want you to be first to know that this > coverage is available and to know the basics of what the insurance plan is > and how it affects you and other ultralighters in the United States. You > first heard about this program from Andy Kain at the 1999 Annual Meeting. > > This type of insurance pays your cost of defense and penalties if through > your flying activity you injure someone or damage their property. The plan > provides up to $1,000,000 (One Million Dollars) each accident (combined > aggregate of bodily injury and property damage). > > The insurance program is open to all USUA members who operate > "Fat-ultralight" airplanes, trikes and hang gliders and have pilot and > vehicle/aircraft registration through FAA or any FAA recognized ultralight > safety program. > > The policy will cover all vehicles/aircraft having a stall speed not > exceeding 35 knots (40 mph) Calibrated Air Speed and with a gross weight of > not more than 992 U.S. pounds. > > The policy costs only $154.50 ($150 plus 3% surplus lines tax). > > The coverage is intended for private owners and instructors. It is not > intended for those involved in commercial flying such as towing of banners & > gliders; aerial seeding, aerial spraying or dusting or other for-hire > operations except instruction. > > You will want this coverage to assure others that if you injure them or > damage their property you are financially able to pay for the damage you > accidentally did to them. Also, many state and municipal facilities employ > financial responsibility laws and require such coverage. Without this type > of coverage, the cost of defense alone could significantly impact your > financial future. There is great value in knowing you have protection in case > of an unplanned event. Besides, the coverage is easy to obtain and only costs > a fraction of your aircraft and yearly operating expenses. > > Pilots: > IF FLYING A SINGLE-SEATER- > A person must be at least 16 years old and a registered ultralight pilot or > instructor with the appropriate category/class privileges in any FAA > recognized ultralight airman competency program. > > IF FLYING A TWO-SEATER- > One of the following: > 1) A USUA registered instructor need do nothing extra. > 2) Instructors in other FAA recognized programs must simply include a > photocopy of their ultralight instructor registration. > 3) FAA private pilot certificate or better with ultralight pilot > registration in any FAA recognized program. > > More than one pilot may be named on the policy. The standard policy allows > two pilots to be named for no extra fee. An unlimited additional number of > pilots may be named on the same policy with an additional premium of $25.75 > ($25 plus 3% surplus lines tax) per pilot. > > I will forward "sanitized" brochure language for wide distribution within a > few business days. At that time applications will be available from USUA HQ. > > This is real. I have already purchased coverage and have received a personal > certificate of insurance from the underwriters. It is big news which I am > delighted to present to you. > > John Ballantyne, President > UNITED STATES ULTRALIGHT ASSOCIATION > ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: Cutting Instrument Panel Holes
Date: Aug 06, 1999
What a job ! ! ! I AM Impressed ! ! ! Humble Lar. ----- Original Message ----- From: <WillU(at)aol.com> Sent: Thursday, August 05, 1999 2:12 PM Subject: Re: Kolb-List: Cutting Instrument Panel Holes > > A picture so you can get an idea on cutting the instrument panel holes. > http://member.aol.com/n8754k/page/ssdc170.jpg > > In a message dated 8/5/99 3:07:26 PM Mountain Daylight Time, Wally Hofmann > writes: > > > I got it adjusted just right by drilling scrap > > material. It left a very clean edge. The biggest problem was building a > > jig to hold the nose cone under the drill press. > > ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: RE: Flaps reflex...
Date: Aug 06, 1999
I wonder what the reasoning is ?? There must be a purpose in it somewhere. Any one ?? Seems to me that a friends' Firefly has flaperons. Any Firefly owners notice this ?? Puzzled Lar. ----- Original Message ----- From: Christopher John Armstrong <Tophera(at)centuryinter.net> Sent: Thursday, August 05, 1999 6:42 PM Subject: Re: Kolb-List: RE: Flaps reflex... > > While at oshkosh I was looking over the factory slingshot... it uses > flaperons like the firefly and my firestar II. THey had put an aileron > control stop on the end of the wing pivot bolt, which stoped the aileron > from over deflecting with 0 degrees flaperon setting. This stop location > also stoped the aileron from deflecting AT ALL when the flaperons were set > to full. I repeat it would not allow any left aileron at full flaperon!!!!! > If you are adjusting your ailerons to try out relex make sure you check your > motion and any stops you have installed before flight after each adjustment. > If you are putting in flaperons keep this in mind. I thought this was way > dangerous. > > Topher > > ________________________________________________________________________________
From: "David Bruner" <brunerd(at)hvi.net>
Subject: Re: MK II VNE
Date: Aug 05, 1999
> >Hello Folks: > > I would like some info if anyone could help please. When I bought the >plane it didn't have any paperwork with it and I need to know the published >VNE, stall speed, roc (single and double) and any other pertinent info. John, You're slightly ahead of me in air time - I got about 2 sec a few weeks ago from a gust doing moderate taxiing. After refurbishing, it was test flown recently and now I'm getting close! I've got an original spec sheet for the Twinstar and a copy of a FAX on the Twinstar Mk II I'd be happy to copy and mail to you. Not too descriptive, more like advertising. Until then: Empty 320# Gross 750# ROC at gross with 47hp Rotax - 700fpm Vne = 80 Max cruise = 73 Stall = 30 TO at gross wt on grass = 300' These are straight from the sheet, "your values may vary". I've also got the 2 booklets and next week will get a set of blueprints to copy. Might as well do 2 copies if you want one. Also, just found out from John Yates today how to set the Mk II up for CG calculations - I was using 4-5 degrees and without 2 people I was aft of CG! David Bruner Mk II #M2-202 Kingston, NY ________________________________________________________________________________
From: gerken(at)us.ibm.com
Date: Aug 06, 1999
Subject: lead in your tail, and HPC coatings
>Why would using stronger tubing for bracing be a problem? >The only reason I can imagine would be weight. >Tom Most Kolbs I have heard of experience weight and balance figures near the back of the allowable CG range, adding weight at the tail makes for problems later, keep it to a minimum. I don't think I am exagerating when I say: One pound at the tail makes it possible you'll have to add ten or fifteen pounds in the nose later for balance. If I was going to add weight to the tail, it would be for compression springs instead of extension springs for the tailwheel steering (comp springs can't fall off!), and maybe a wider tailwheel that wouldn't cut into the soft grass so badly. -------------------------------------------------------------------------------------------------------------------------------------------------------- > >Please elaborate on HPC coating of Kansas. I am interested please. Thanks. >JR >of Kansas HPC (and similar products like Jet Hot) are GOOD STUFF! I have tried many kinds of paints on 2-stroke exhaust tuners over the years and never found anything that'd stay on. Now I have and it is HPC. My 582 Rotax exhaust with HPC "CHROME" has 78 hours on it so far and looks as good as the day I opened the box. They coated the inside and outside of the "Y" pipe and elbow, and the outside only of the muffler, and the band clamps for about $105, plus shipping. I should have sent them the springs too. It has not blued at all, even in the "Y" pipe, which is amazing. Here is the web address, check it out and then give them a call. Tell them you have a SNOWMOBILE EXHAUST SYSTEM, or they may get nervous about liability. Best results will be attained using brand-new exhaust components. Tell them they may bead blast but plug the muffler to keep the inside clean. Send them the clamps too, and the brackets if you wish. I think they can even do bolts and springs. By the way, if you have a new Rotax exhaust, and think the black paint that came on it looks good, kiss it goodbye because in three hours' running time your new muffler will be rusting and ugly. http://www.hpcoatings.com/ Jim G ________________________________________________________________________________
Date: Aug 06, 1999
From: bob n <ronoy(at)shentel.net>
Subject: Re: RE: Flaps reflex...
Yes, my FF has flaperons, at least last time I ckd. ________________________________________________________________________________
Date: Aug 06, 1999
From: Ben Ransom <bransom(at)ucdavis.edu>
Subject: Re: ailerons
> > Back to the heavy ailerons- I'm thinking about extending the stick >upward. this alone should give a reduction in effort equal to the >percentage of length increase. This is in a mk3. Thoughts? On my FS, I cut the stick a little shorter after 2nd year. The primary need for me to do this was to avoid the stick hitting the left side of the 3/4 enclosure I made. However, I also appreciated the shorter stick in flying, cuz the rubber grip is now right at my knees for hands-free stuff (lunch, photos, maps). Also, when I get to playing with yankin the plane around some, I found I like gripping the top of the stick (hand facing down). Maybe this was just my getting used to a way to deal with the heavier force, but I liked it. I even put my PTT button on the front of the stick grip, about 5" down so that it wouldn't be pushed when I was in Snoopy mode with hand on top, yankin and bankin. Geez, I see that I'm writing in past tense here -- shame on me -- I better go rebuild that thing. Still not free quite yet. -Ben ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Aug 06, 1999
Subject: Re: RE: Flaps reflex...
With deployment of flaperons you would want considerably more up aileron movement (down control) on the inside wing and little additional down aileron movement (up control) on the outside wing due to severe adverse yaw. JR ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Aug 06, 1999
Subject: Rod ends and washers
I noticed this on my friends Kolb 3 that the control rod ends did not have a large area washer capturing them positively. This is basic stuff and is something that should be done wherever a rod end is not trapped. The other thing I noticed is that apparently Kolb supplied fiber locking nuts for the elevator clevis at four places. At least as set up on this airplane it should be a castellated nut and cotter key. Wherever a bolt is used as a bearing or subject to rotation fiber lock nuts are not acceptable. Saw this mentioned in another Kolb list post and I second it. Refer to AC 43-13 and other references like AC 65 and Tony Bingellis books. JR, A&P ________________________________________________________________________________
Date: Aug 06, 1999
From: Wally Hofmann <wally(at)foxfibre.com>
Subject: Re: Cutting Instrument Panel Holes
> From: WillU(at)aol.com > Subject: Re: Kolb-List: Cutting Instrument Panel Holes > A picture so you can get an idea on cutting the instrument panel > holes. > http://member.aol.com/n8754k/page/ssdc170.jpg After seeing how Will drilled his panel holes (http://member.aol.com/n8754k/page/ssdc170.jpg) all I can say is I certainly did it the hard way. I wish I had taken a picture of the Rube Goldburg contraption I built to hold the nose under the drill press. Wally Hofmann Wickenburg, AZ ________________________________________________________________________________
From: RLCPTL(at)aol.com
Date: Aug 06, 1999
Subject: Re: Aileron Spades
Hey Lar: I talked to Dennis about spades a couple of years ago and he said "NO-NO". Today, I cannot remember the technical reason for his strong negative reaction. You might talk to the NEW KOLB AIRCRAFT people. They are very accommodating, of course. Ron Christensen MKIII1/2 ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: Aileron Spades
Date: Aug 06, 1999
Welcome back, Ron. How was OSH ?? 'Scuse me - AirVenture 99 ?? Envious Lar. ----- Original Message ----- From: <RLCPTL(at)aol.com> Sent: Friday, August 06, 1999 8:52 PM Subject: Re: Kolb-List: Aileron Spades > > Hey Lar: > I talked to Dennis about spades a couple of years ago and he said "NO-NO". > Today, I cannot remember the technical reason for his strong negative > reaction. You might talk to the NEW KOLB AIRCRAFT people. They are very > accommodating, of course. > Ron Christensen > MKIII1/2 > > ________________________________________________________________________________
Date: Aug 07, 1999
From: Richard <swidersk(at)digital.net>
Subject: Re: Aileron Spades
Ron & Lar, I talked with Dennis about spades a couple years ago also & can't clearly remember the reason for his concern. But I think it has to do with the limited strength of the leading edge aileron tube. They were designed to handle the amount of torque applied by the stick control stick. Adding spades also adds more torque & depending on the spade setup it could be alot more toque. This makes sense to me, but if is incorrect logic, please don't attribute it to Dennis. Also, it seems we are adding a powerful unknown (to me) variable into the flutter equation. Are there any compensations that need to be made besides static balance? The length of the spades moment arm, the angle of the moment arm, the angle of the spade on the moment arm, and the area of the spade-- all would seem to be critical design factors that could determine the strength of the added torque & whether it is applied gradually or (worst case scenario) if it kicks in suddenly & then amplifies itself. These are some considerations that have been bouncing around in my head. The technology exists & it works well. We just have to figure out how to do it right! ...Richard S RLCPTL(at)aol.com wrote: > > Hey Lar: > I talked to Dennis about spades a couple of years ago and he said "NO-NO". > Today, I cannot remember the technical reason for his strong negative > reaction. You might talk to the NEW KOLB AIRCRAFT people. They are very > accommodating, of course. > Ron Christensen > MKIII1/2 > ________________________________________________________________________________
From: DBindl(at)cs.com
Date: Aug 07, 1999
Subject: Re: RE: Flaps reflex...
If a flaperon is allowed to deflect tooooo far it becomes all drag and is no longer contributing lift for the wing banking effort. Daniel Bindl ________________________________________________________________________________
From: "David Bruner" <brunerd(at)hvi.net>
Subject: Re: MK II VNE
Date: Aug 07, 1999
> Hello and thanks for the info! Yes I would like the spec. sheet and blue >print. How about checking the center of gravity. What's involved to check >the CG. Could you describe the procedure if it's not to much trouble. > Let me know if you need some reimbursement for the sheet and plans and >once again thank you very much. John, Sure, send me your address and I'll put together a care package. The blueprints are big and might cost a bit to copy - I'll let you know. Everything else I can do at work. The CG procedure is described in 2 sheets, which now (Thank You John Y!) has the crucial detail that establishes the datum from which all measurements are taken. Do you have the 2 booklets? One is the construction book and the other is the Photo Assembly book. Also, there are at least 2 ADs that were sent by Kolb to builders. After I got my new-to-me Mk II, I called Kolb and they sent me a waiver to sign so I can get technical support, parts and any future ADs that might be required. Call 'em. In May, I automatically received one that reinforces the aileron bell crank and the other one I know of is a bracket to reinforce the tab on the wings that attach to the universal joint. It had already been done on mine. David Bruner Mk II, Kingston NY ________________________________________________________________________________
From: WillU(at)aol.com
Date: Aug 07, 1999
Subject: Re: Cutting Instrument Panel Holes
Hi Wally I can't take credit for the instrument holes cutting setup. The picture was taken by Rusty when he was building his SlingShot. http://members.aol.com/n8754k/page/index.htm Will Uribe El Paso, TX Will's FireStar II > > > From: WillU(at)aol.com > > Subject: Re: Kolb-List: Cutting Instrument Panel Holes > > > > A picture so you can get an idea on cutting the instrument panel > > holes. > > http://member.aol.com/n8754k/page/ssdc170.jpg > > After seeing how Will drilled his panel holes > (http://member.aol.com/n8754k/page/ssdc170.jpg) all I can say is I > certainly did it the hard way. > > I wish I had taken a picture of the Rube Goldburg contraption I built to > hold the nose under the drill press. ________________________________________________________________________________
Date: Aug 07, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Aileron Spades
I think you have a valid concern. We had a fly-in at VJI airport today, and one of the guys brought in his Citabria with spades added to the ailerons. The attach brackets are about as beefy as the wing spar attach brackets on the MKIII! After looking them over carefully, I decided that maybe spades would be exploring too much unknown territory. A couple of us got talking about reducing aileron force, and the attention turned to the bellcrank that comes out of the middle of the rear fuselage. What about drilling another hole about 1" closer to the pivot, making up longer aileron pushrod tubes, and trying that out? Stick force would be less, and leverage would be better. You would have less total aileron throw, but watching my ailerons move in flight while coming back home today, most of the time the ailerons only move an inch or two anyway. May or may not work, but probably much less risky than playing with unknown aerodynamic forces pulling on spades. Just checked in the garage, I already have enough .035 x 1/2" chromoly and will order the AN490 threaded rod ends Monday, will let you know how it works, probably by next weekend. Richard Pike MKIII N420P (42OldPoops) > >Ron & Lar, > > I talked with Dennis about spades a couple years ago also & can't clearly >remember the reason for his concern. But I think it has to do with the >limited >strength of the leading edge aileron tube. They were designed to handle the >amount of torque applied by the stick control stick. Adding spades also adds >more torque & depending on the spade setup it could be alot more toque. This >makes sense to me, but if is incorrect logic, please don't attribute it to >Dennis. Also, it seems we are adding a powerful unknown (to me) variable into >the flutter equation. Are there any compensations that need to be made besides >static balance? The length of the spades moment arm, the angle of the moment >arm, the angle of the spade on the moment arm, and the area of the spade-- all >would seem to be critical design factors that could determine the strength of >the added torque & whether it is applied gradually or (worst case scenario) if >it kicks in suddenly & then amplifies itself. These are some considerations >that have been bouncing around in my head. The technology exists & it works >well. We just have to figure out how to do it right! ...Richard S > >RLCPTL(at)aol.com wrote: > >> >> Hey Lar: >> I talked to Dennis about spades a couple of years ago and he said "NO-NO". >> Today, I cannot remember the technical reason for his strong negative >> reaction. You might talk to the NEW KOLB AIRCRAFT people. They are very >> accommodating, of course. >> Ron Christensen >> MKIII1/2 ________________________________________________________________________________
From: "Peter Zutrauen" <peterz(at)zutrasoft.com>
Subject: Jabiru?
Date: Aug 07, 1999
Hi folks, I'm thinking of building a Slingshot.... but am discouraged about it's apparent performance with the 912 (and the engine's cost). I understand the Jabiru 4-stroke is 80 horsepower (5 min), direct-drive and light (120 fully rigged). How would this compare to the 2-stroke 582? What is the 582's weight fully rigged (starter, reduction, exhaust etc.)? Why aren't there more Jabiru users? Thanks, Pete Z. ________________________________________________________________________________
Date: Aug 07, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re: Aileron Spades/bell crank
>Subject: Re: what does 2" of throw in the bell crank do. I have the old style "bell crank" off my old plane (Firestar). They used to mount them behind your head. Rewelded the bottom bar and moved the holes "out" 1 inch on each side for the aileron control bars. My new ailerons are 2 inches "narrower" than a regular Firestar-all the way down. It helps with that "heavy stick control", so I could afford to move them a little faster and a little more, without getting into trouble (they're stops on the stick lever to keep from moving them too far} and counter weights like a slingshot. Firestars really have a "lot" of aileron anyway, may a little too much I don't know about MIII. See at <http://www.mindspring.com/~possums/> ________________________________________________________________________________
Date: Aug 07, 1999
From: wood <duesouth(at)iname.com>
Subject: another bird in the sky
Good day today. After 4 yrs (3 of which were in limbo) Andy's MK3 got some air under its tires. All went well, the wheels come unstuck at 40 mph and dropped back on at 40 mph. Made 3 flights to dial in the prop and almost have it now. The Hirth ran smoothly but after the final pitch change started running about 500* cht. on climb out. Allmost tempted to turn the darn thing off and coast in. Hot enough to melt the heart of a rotax boy but Ok on a Hirth for short periods. We may not have enough adjustment on the needle so perhaps a jet change is in order. Did not do any performance checks but I sure like that ESI gizmo on the dash. Soon as a peremiter was exceeded it flashed a warning light and then the object of concern displayed. Perhaps we can get Andy to tell us his version of the story of the first flight of the MK 3. It sure felt good from the pilot seat. Woody ________________________________________________________________________________
From: "Christopher John Armstrong" <Tophera(at)centuryinter.net>
Subject: Re: Jabiru?
Date: Aug 07, 1999
>Why aren't there more Jabiru users? I heard rumers at oshkosh from several manufacturers who had tried the Jabiru that it was not putting out the power claimed. I really like them, though they are to big for my FSII. Just rumers but something to look into Topher ________________________________________________________________________________
From: "Christopher John Armstrong" <Tophera(at)centuryinter.net>
Subject: Re: Aileron Spades
Date: Aug 07, 1999
Spades are area balances, the aerodynamic equivilent of mass balances, and will reduce any tendency to flutter. (unless you do them wrong!) As far as forces go, they are set to provide no force at center stick and to replace some of the stick force as you go off center. so there will be no additional total force in the system for a given amount of deflection. Where you get into trouble is that it is now really easy to deflect your ailerons, so you deflect them much more, and now they load up and cause very high roll rates and that will cause more forces in the system. If you want to try them start small and make them bigger till they reduce the forces the amount you want. size the structure according to the amount of load that that size piece of flat plate can generate at VNE when 90 degrees to the airflow. That will be overkill. THen dont yank them around just because you now can, cause that will put high forces throughout the aircraft, and maybe get you a snaped wing with your snaproll. ANother option is a servo tab. this is a trim tab that changes angle with deflection so as to assist in the deflection. An ANtiservotab changes its angle with deflection to hinder deflection. Topher ________________________________________________________________________________
Date: Aug 08, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Aileron Spades
Very Good, thanks. Question; given your analysis of spades and forces exerted, would it be easier on the structure (assuming normal flight inputs, no aerobatics) to have spades on or about the center of the aileron span to reduce the torque twisting input to the tube caused by the normal control system, or would it be better to change the leverage at the bellcrank, and rely on better leverage to twist the aileron tube with stick inputs, and with out "spade aid"? Richard Pike MKIII N420P (42OldPoops) > > >Spades are area balances, the aerodynamic equivilent of mass balances, and >will reduce any tendency to flutter. (unless you do them wrong!) As far as >forces go, they are set to provide no force at center stick and to replace >some of the stick force as you go off center. so there will be no >additional total force in the system for a given amount of deflection. >Where you get into trouble is that it is now really easy to deflect your >ailerons, so you deflect them much more, and now they load up and cause very >high roll rates and that will cause more forces in the system. If you want >to try them start small and make them bigger till they reduce the forces the >amount you want. size the structure according to the amount of load that >that size piece of flat plate can generate at VNE when 90 degrees to the >airflow. That will be overkill. THen dont yank them around just because >you now can, cause that will put high forces throughout the aircraft, and >maybe get you a snaped wing with your snaproll. > >ANother option is a servo tab. this is a trim tab that changes angle with >deflection so as to assist in the deflection. An ANtiservotab changes its >angle with deflection to hinder deflection. > >Topher ________________________________________________________________________________
Date: Aug 08, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Aileron Reflex
Flew several times the last three days, solo and two up, and it appears there is a certain eficiency limit that is quickly reached by reflexing. Some reflex is good, lightens up the ailerons and allows about 5 mph extra cruise speed at a given throttle setting. More than that does not appear to do any good for improving speed or reducing stick force. Optimum all around was when the ailerons appeared to be just above straight back looking along the bottom of the lower surface, probably about 1/4" to 3/8" reflexed. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
Date: Aug 08, 1999
From: Norman Labhart <njlabhart(at)kih.net>
Subject: Oshkosh 99 photos on The New Kolb Aircraft website
Hi Gang, I have posted photos from Oshkosh '99 on the New Kolb Aircraft website. There is a link on the Homepage to them: http://www.tnkolbaircraft.com/index.html It was a real pleasure meeting some of you in person. Seems like Kolb people are as nice in person as they are online. I hope a lot of you get to come to the Kolb Flyin at the factory September 25th. As per many of your requests I have added directions to the factory on the Contacts page: http://www.tnkolbaircraft.com/contact.htm In the next day or so I will post the Flyin webpage on the site. It will have details on the Flyin. Norm Labhart Webmaster for The New Kolb Aircraft Co. njlabhart(at)kih.net 1956 Cessna 172 7453A Graham Lee Nieuport 11 replica Serial Number 1080, On the Gear! http://www.users.kih.net/~njlabhart/nieuport.htm ________________________________________________________________________________
From: WGeorge737(at)aol.com
Date: Aug 08, 1999
Subject: Re: Aileron Reflex
In a message dated 8/8/99 9:00:13 AM, rpike(at)preferred.com writes: << Flew several times the last three days, solo and two up, and it appears there is a certain efficiency limit that is quickly reached by reflexing. Some reflex is good, lightens up the ailerons and allows about 5 mph extra cruise speed at a given throttle setting. More than that does not appear to do any good for improving speed or reducing stick force. Optimum all around was when the ailerons appeared to be just above straight back looking along the bottom of the lower surface, probably about 1/4" to 3/8" reflexed.>> Hi Richard: I have been following the very interesting "reflex" thread and have a comment/question for you and others who have reflexed. IMHO the lightening of control forces probably comes from the fact that when an aileron is deflected upward it is in a lower pressure position and when deflected downward it is moving into a higher pressure airstream creating induced drag (thus adverse yaw.) Reflexing then would increase the amount of deflection into the "lighter" airstream and reduce the deflection into the "heavier" lower stream. It would seem to me that the overall effectiveness of lateral control, or roll rate per unit of stick deflection, would be reduced. Result: lighter feel but less roll rate. Do you think you have lost some roll rate or is about the same? Thanks Bill George Mk-3 582 Powerfin ________________________________________________________________________________
From: "Jeremy Casey" <jrcasey(at)mindspring.com>
Subject: Glider tug
Date: Aug 08, 1999
I just looked at the pictures of the glider tug on the TNK web site , Oshkosh pictures. Did anyone notice that the center wing section was painted different and also resembles (exactly) the center wing section that is on the original Mark 3 prototype that is on all the brochures??? I remember noticing in my info kit way back when , that the early M3 pictures showed a cloth center wing section while the later ultralight flying write up showed a plexiglass center section... Just call me Columbo... Jeremy Casey jrcasey(at)mindspring.com ________________________________________________________________________________
From: HShack(at)aol.com
Date: Aug 08, 1999
Subject: Re: Aileron Reflex
In a message dated 8/8/99 4:14:13 PM Eastern Daylight Time, WGeorge737(at)aol.com writes: << Reflexing then would increase the amount of deflection into the "lighter" airstream and reduce the deflection into the "heavier" lower stream. It would seem to me that the overall effectiveness of lateral control, or roll rate per unit of stick deflection, would be reduced. Result: lighter feel but less roll rate. Do you think you have lost some roll rate or is about the same? >> I posted earlier that I had reflexed up my ailerons from 'level' with wing bottom t o about 3/8" up and that ailerons were not as "heavy" with no apparent pitch change. After putting on about 3 hours I found that I did indeed have more aileron authority with less "heaviness" but I did have to hold some forward stick-too much for comfort. I took out about half of the reflex I put in and am calling it a good compromise. Howard Shackleford FS I SC ________________________________________________________________________________
From: BICUM(at)aol.com
Date: Aug 08, 1999
Subject: Tire leaks on Matco rims???
Hello group, I am having trouble with the leak on one of my Matco rims. I have taken this rim apart twice and checked the O-ring with no success. I was wondering how many of you had a similar problem and just went on to an inner tube. Thanks for any and all help, John Bickham St. Francisville, LA Mark III (N308JB assigned) ________________________________________________________________________________
From: HShack(at)aol.com
Date: Aug 08, 1999
Subject: Re: Tire leaks on Matco rims???
In a message dated 8/8/99 7:02:43 PM Eastern Daylight Time, BICUM(at)aol.com writes: << I was wondering how many of you had a similar problem and just went on to an inner tube. >> Our field has lots of sand spurs so almost everyone here installs tubes. I also went to a four-ply tire. Howard Shackleford FS I SC ________________________________________________________________________________
From: KHe1144783(at)aol.com
Date: Aug 08, 1999
Subject: Re: Jabiru?
I have a Jabiru engine and understand the differance between it and the 912. The 912 has a reduction drive that increases the torque over the Jabiru and increases the effeciancy of the propeller and allowing one to use a three blade prop. The Jabiru weighs about 40 to 50 lbs. less than the 912 (depending who you talk to) all up weight because it is air cooled and no redrive is used. What it boils down to by looking at the power/ Torque curve is that to match the performance of the 912 you need to (1) Use a 2-blade wood prop from the best company possible, Prince or Props. Inc. The best choice depends on your particular application, eg. cruise speed, climb speed, top speed, total drag etc. (2) You need to run the engine at higher rpm to benifit from the design. About 3000 to 3150 cruise rpm. which is max. continuous. Its O.K. just differant. If the prop choice was good, the combination will click and you can match the 912 performance (your a good 40 lbs. lighter remember with no radiator out in the slipstream to slow you down, no water hoses to leak and you saved a couple of grand to boot. Early engines had "bugs' but have been addressed. Its a proud company now with great factory support. 3-Wire Palm Springs ________________________________________________________________________________
From: N51SK(at)aol.com
Date: Aug 08, 1999
Subject: Re: Kolb-List Digest: 08/06/99
In a message dated 8/7/99 1:58:02 AM Central Daylight Time, kolb-list-digest(at)matronics.com writes: > Until then: > Empty 320# > Gross 750# > ROC at gross with 47hp Rotax - 700fpm > Vne = 80 > Max cruise = 73 > Stall = 30 > TO at gross wt on grass = 300' > > These are straight from the sheet, "your values may vary". > I'd just like to add that all of these stats have turned out to be correct on my mk2 with the exception of empty weight. Mine came in at 380# with chute, brakes, dual gas tanks, and all the little AD type mods the factory made along the way (main wing pin reinforcement, reinforced outer wing ribs, heavy duty landing gear. My guess is that without all these additional add-ons and with a little less paint, I would probably have been very close to the 320#. Steve Kroll ________________________________________________________________________________
From: "Christopher John Armstrong" <Tophera(at)centuryinter.net>
Subject: Re: Aileron Spades
Date: Aug 08, 1999
>or would it be better to change the leverage at the bellcrank, and rely on >better >leverage to twist the aileron tube with stick inputs, and with out "spade aid"? This will not change the forces on any part of the system except the bellcrank itself. To get the same amount of aileron deflection you will have to move the stick more, and after you move the stick more the forces will be the same, except on the bell crank where they will be changed relative to the amount you moved the lever arm. As far as where to put spades I would put them center span cause the flow will be the most consistent there. For structure see a structures guy, but I would think that you can handle the loads since they are currently being generated by the stick, and would just be devided between the stick and spade now. Topher ________________________________________________________________________________
Date: Aug 08, 1999
From: Richard Bluhm <irena(at)ccis.com>
Subject: Re: Tire leaks on Matco rims???
BICUM(at)aol.com wrote: > Hello group, > > I am having trouble with the leak on one of my Matco rims. I have > taken this > rim apart twice and checked the O-ring with no success. I was > wondering how > many of you had a similar problem and just went on to an inner tube. > Thanks for any and all help, > John Bickham > St. Francisville, LA > Mark III (N308JB assigned) Hello there John, There is a couple things you might checkout... First,you might check to see if the two rims fit flush together. ( I was told to check this and thought the idea crazy, but after a check I found they weren't flush.)Every now and then, after a rough landing, a mild wave might develope in the entire rim causing a misfit. This is easy to straighten and may be your problem, but then there is another possibility.. I have been putting vasolene petrolium jelly on the "O" ring to insure the seal in the line between the rims.. If these two possibilities have already been addressed by you,, you may just need the tubes. I even tried that self sealing tire compound that you spray into the tire to seal leaks...I don't recomend this proceedure as a cure. Good Luck Regards Doc ________________________________________________________________________________
Date: Aug 08, 1999
From: Bill Weber <bweber2(at)earthlink.net>
Subject: Safety wire & Kill switch
I am finally finishing up my Firestar and have a few loose ends. The last 10% seems to take 90% of the time. 1. The turnbuckles for the elevator controls need to be safety wired. How is the saftety wire routed? 2. I haven't decided which way I want the kill switch to move to kill the engine. Pulling up to kill seems easiest if I need to do it in a hurry. On the other hand, pulling up also seems like it could happen by accident more easily. Any experiences that have pointed to one way or the other? -- *********************************************** * Bill Weber * Keep * * Voiceboard Corp * the shiny * * Simi Valley, CA * side up * *********************************************** ________________________________________________________________________________
Date: Aug 09, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Aileron Reflex
Roll rate seems about the same. Minor aileron inputs seem to take a little less pressure. Big inputs seem about the same, and roll response also seems about the same, but that's pretty subjective. No hard data. Richard Pike MKIII N420P (42OldPoops) >I have been following the very interesting "reflex" thread and have a >comment/question for you and others who have reflexed. It would seem to me that the overall effectiveness of lateral >control, or roll rate per unit of stick deflection, would be reduced. Result: >lighter feel but less roll rate. > >Do you think you have lost some roll rate or is about the same? > >Thanks > >Bill George >Mk-3 582 Powerfin > > ________________________________________________________________________________
From: "Frank & Winnie Hodson" <fwhodson(at)bigfoot.com>
Subject: Rectifier replacement
Date: Aug 09, 1999
Dear John: Thanks for the advice to swap out the rectifier, You were right in your assessment. Even though the first rectifier was supplied new by the original Kolb factory, it never made more than an average 8 volts. The replacement unit has been installed and is operating the EIS perfectly and registers in at approximately 14 volts. As always technical advice continues to be an important factor in building this project. Respectfully: FRANK HODSON, OXFORD ME ( FS II, N6399J) fwhodson@megalink.net http://www.megalink.net/~fwhodson ________________________________________________________________________________
From: "Frank & Winnie Hodson" <fwhodson(at)bigfoot.com>
Subject: Safety wire & Kill switch
Date: Aug 09, 1999
> > I am finally finishing up my Firestar and have a few loose ends. The > last 10% seems to take 90% of the time. > > 1. The turnbuckles for the elevator controls need to be safety wired. > How is the safety wire routed? > > 2. I haven't decided which way I want the kill switch to move to kill > the engine. Pulling up to kill seems easiest if I need to do it in a > hurry. On the other hand, pulling up also seems like it could happen by > accident more easily. Any experiences that have pointed to one way or > the other? Dear Bill: 1. If you have an AIRCRAFT SPRUCE catalogue, look in the turnbuckle section for diagrams of the acceptable safety wire alternatives. If you don't have a catalogue, send for one (I believe you'll find it to be the best $5 spent on your project). 2. The kill switch(s) position is entirely preferential. I have a switch box for the EIS and strobe unit on the left side of the cockpit. On is to the left / off to the right. To make it easier on the simple pilot who plans to fly it I made oriented the kill switches the same way in the interest of uniformity (could avoid confusion under stress). GOOD LUCK: FRANK HODSON, OXFORD ME (FS II, N6399J) ________________________________________________________________________________
Date: Aug 08, 1999
From: "Douglas G. Murray" <dgmurray(at)telusplanet.net>
Subject: Re: Safety wire & Kill switch
Bill Weber wrote: > > I am finally finishing up my Firestar and have a few loose ends. The > last 10% seems to take 90% of the time. > > 1. The turnbuckles for the elevator controls need to be safety wired. > How is the saftety wire routed? > > 2. I haven't decided which way I want the kill switch to move to kill > the engine. Pulling up to kill seems easiest if I need to do it in a > hurry. On the other hand, pulling up also seems like it could happen by > accident more easily. Any experiences that have pointed to one way or > the other? > Bill - Congratulations on your progress. It won't be long now before you are having fun in the air. The safety wires can be installed in two or three methods. I would suggest that you look in AC43 - 1B & 2B Accepted Aircraft Building Practices or any of Tony Bingelus' books. Both demonstrate pictorially the methods used to safety a turnbuckle. It is kind of hard to describe it in words but you want to stop the barrel from rotating and changing the setting you need. I usually start by cutting a piece of .032" stainless wire about ten inches long. Fold it in half and put one leg of the wire though one end of the turnbuckle yoke/clevis. Wrap each end of the wire two turns around the yoke/ clevis end in opposite directions and then insert each end of the wire through the center barrel hole - again in opposite directions. Wrap the wire ends two times around the yoke/ clevis on the other end of the turnbuckle from your starting point and then put one of the wire ends through the end of the yoke/clevis and then tie off the two ends of the safety wire. It is a lot easier to see in a picture or in real life than to explain but I hope this helps. On your second question - Switches are always ON when FORWARD or UP. OFF when REARWARD or DOWN. You may need to change the cover plate that comes with your kit so it is labled correctly. If you cut off the little locator tab on the inside of the hole, the cover label plate can be rotated around so that your switch movement and operation are correct. Have a safe first flight. Doug Murray Firestar 1 flying since 1990 Southern Alberta ________________________________________________________________________________
From: djwatson(at)olg.com
Date: Aug 09, 1999
User-Agent: IMP/PHP3 Imap webMail Program 2.0.10
Subject: Re: Kolb in St. Mary's County MD.
Hi All Club 109 had there meeting last night and two of our members reported seeing a yellow and red Kolb in the area. One of the guys said he flew formation with the Kolb for a while. Does anyone know who this might have been?? I would like to get together with him and invite him to join our club. Shoot,I'll even pay his dues for a year. Dennis (Ridge,MD.) ________________________________________________________________________________
From: gerken(at)us.ibm.com
Date: Aug 09, 1999
Subject: Re: Reflex, last post I'll need to make
>In a message dated 8/8/99 9:00:13 AM, rpike(at)preferred.com writes: ><< Flew several times the last three days, solo and two up, >and it appears there is a certain efficiency limit that is >quickly reached by reflexing. Some reflex is good, lightens up >the ailerons and allows about 5 mph extra cruise speed at a >given throttle setting. More than that does not appear to do >any good for improving speed or reducing stick force. >Optimum all around was when the ailerons appeared to >be just above straight back looking along the bottom of the >lower surface, probably about 1/4" to 3/8" reflexed.>>> Richard, my experience agrees with most of what you said here. There is a limit, and your description is about where I would put it. On my mkiii, you may recall I have adjusted flaps and Ailerons twice, once to about flat with wing bottom, and found no flight differences, and again to about 5/8" high on the ailerons and flaps just 1/8" high, with the following conclusions: I do beleive that the minimal progress that was made in lowering the stick pressure was at the expense of aileron effectiveness. After flight tests, I have concluded that the stick pressure was decreased for small movements, but the aileron effectiveness was decreased in this range also. I did not pick up any more top speed at all. I MAY have increased efficiency at lower power settings/speeds, but these numbers are hard to nail down exactly. And I lost climb rate BIG TIME! Two-up it climbed like one blade had fallen off the prop. And surprisingly, no solo trim bias was detectable. I will be going back to a near-flat setting. Then Bill George wrote: >Hi Richard: >I have been following the very interesting "reflex" thread and have a >comment/question for you and others who have reflexed. IMHO the lightening of >control forces probably comes from the fact that when an aileron is deflected >upward it is in a lower pressure position and when deflected downward it is >moving into a higher pressure airstream creating induced drag (thus adverse >yaw.) Reflexing then would increase the amount of deflection into the >"lighter" airstream and reduce the deflection into the "heavier" lower >stream. It would seem to me that the overall effectiveness of lateral >control, or roll rate per unit of stick deflection, would be reduced. Result: >lighter feel but less roll rate. >Do you think you have lost some roll rate or is about the same? >. >Thanks >Bill George Bill, yes, I agree. Some small reduction was made in stick force, for a small movement because the control surface was not out in the airstream, it was tucked into the top-side air. When the stick was moved further, the same old high forces came back. Roll rate for the same (small) stick deflection was slower. CG: Someone last week asked about CG. My minimum placarded pilot is 139 lbs. I was wrong last week I said 150lbs, that was last year's data. So I guess that my empty CG is further forward than Richards. Does this explain any of these differences in our planes? Jim G ________________________________________________________________________________
Date: Aug 09, 1999
From: John Jung <jrjung(at)execpc.com>
Subject: Re: Glider tug
Jeremy, It doesn't just resemble the center wing section, it "is" the center wing section from the first Mark III that was used in the promotions. It is the same plane with different wings. It was built different than other Mark III's and was purchased from Kolb specifically for the tug operation a year ago or so. It flys out of a local airport and I have known the owner for 11 years. John Jung Jeremy Casey wrote: > > I just looked at the pictures of the glider tug on the TNK web site , > Oshkosh pictures. Did anyone notice that the center wing section was > painted different and also resembles (exactly) the center wing section that > is on the original Mark 3 prototype that is on all the brochures??? I > remember noticing in my info kit way back when , that the early M3 pictures > showed a cloth center wing section while the later ultralight flying write > up showed a plexiglass center section... > > Just call me Columbo... > Jeremy Casey jrcasey(at)mindspring.com ________________________________________________________________________________
From: MitchMnD(at)aol.com
Date: Aug 09, 1999
Subject: FireStar ll for sale
All of us in the Tallahassee area mourn the loss of everybody's friend Leon Friedman. He died 7/30 of cancer. I have been asked by the family to sell his plane. It is a beautiful FireStar ll modified to carry a big pilot (no jump-seat). Rotax 503, dual carbs, dual ignition,BRS canister parachute,100 Hours on plane and engine, built graduate engineer, always hangared and ready to fly. Price $ 15,500. Call Duane Mitchell (850), 878-9047, 7AM 'till ________________________________________________________________________________
Date: Aug 09, 1999
From: Kim Steiner <steiner(at)spreda.sk.ca>
Subject: Re: Safety wire & Kill switch
"Bill Weber wrote: > > > > > I am finally finishing up my Firestar and have a few loose ends. The > > last 10% seems to take 90% of the time. > > > > 1. The turnbuckles for the elevator controls need to be safety wired. > > How is the saftety wire routed? > > Safety wire methods for turnbuckles can be found in the Aircraft Space & Specialty Co. catalogue on page 134 (1999 - 2000 edition) I picked up my catalogue about a week ago in Oshkosh. I asked the Kolb company if they had a Kolb owners quest book. It would have been interesting too see how many list members were at Oshkosh. Kim Steiner (1990 Mark 111) Saskatchewan, Canada ________________________________________________________________________________
From: TCowan1917(at)aol.com
Date: Aug 09, 1999
Subject: Re: Off/On switches
I would like to comment on the off/on switch for your kolb. I have mine installed inside of a plastic cap that comes with fuel jugs for RC airplane engines - Glow Fuel. It has a a little bevel in it and it is perfect and is also red. Makes it easy to see and use and you wont accidentally turn it off. You can visit your local RC club (they seem to be everywhere) and bum one off the jugs there. Hope this helps. Thanks G'day Ted ________________________________________________________________________________
Date: Aug 09, 1999
From: AUDREY LEWIS <audreylewis(at)planters.net>
Subject: Fire Fly Brakes
I have six inch wheels and mechanical individual heel brakes. The slightest pressure on the pedal causes the brakes to grab and release. It appears the drum is out of round from it's action. Can't adjust the brakes properly for fear of ground looping! Anybody had this problem or has a solution. Thanks. Audrey Jr. ________________________________________________________________________________
Date: Aug 09, 1999
From: Richard <swidersk(at)digital.net>
Subject: Re: Aileron Spades
Kolbers: As I followed this thread, I noticed a couple inferences that spades do not add additional forces to the aileron structure. The bottom line is that what ever input you supply with your arm through the stick, the spade also adds more input on its own, therefore the total potential or available force will always be greater. The total force can be the same or less if the pilot uses discretion & applies less force in a gradual manner, in order to achieve a given role rate. But if you are attempting maximum role rate, then the possibility of over stressing the stock system is not unthinkable. ...Richard S ________________________________________________________________________________
Date: Aug 09, 1999
From: Richard <swidersk(at)digital.net>
Subject: Re: Tire leaks on Matco rims???
Richard B: Not wanting to add the extra weight of inner tubes, I lightly coated all the mating surfaces of the wheel (even the O-ring) with RTV silicone sealant. I even coated the rim and tire bead where they contact each other. It never leaked again, even when I ran less than 10psi. ...Richard S Richard Bluhm wrote: > > BICUM(at)aol.com wrote: > > > Hello group, > > > > I am having trouble with the leak on one of my Matco rims. I have > > taken this > > rim apart twice and checked the O-ring with no success. I was > > wondering how > > many of you had a similar problem and just went on to an inner tube. > > Thanks for any and all help, > > John Bickham > > St. Francisville, LA > > Mark III (N308JB assigned) > > Hello there John, > There is a couple things you might checkout... First,you might check to > see if the two rims fit flush together. ( I was told to check this and > thought the idea crazy, but after a check I found they weren't > flush.)Every now and then, after a rough landing, a mild wave might > develope in the entire rim causing a misfit. This is easy to straighten > and may be your problem, but then there is another possibility.. I have > been putting vasolene petrolium jelly on the "O" ring to insure the seal > in the line between the rims.. If these two possibilities have already > been addressed by you,, you may just need the tubes. I even tried that > self sealing tire compound that you spray into the tire to seal > leaks...I don't recomend this proceedure as a cure. > Good Luck > Regards > Doc > ________________________________________________________________________________
Date: Aug 09, 1999
From: Norman Labhart <njlabhart(at)kih.net>
Subject: Re: Safety wire & Kill switch
Hi Kim, A guest book would have been a good idea. There was a sign-up sheet for list members at the Kolb site. There was an informal gathering at 7:00 each night. There was about 15 names on the list last time I looked. Don't know how many actually got together. Norm Webmaster for the New Kolb Aircraft > >I asked the Kolb company if they had a Kolb owners quest book. It would have been >interesting too see how many list members were at Oshkosh. > >Kim Steiner (1990 Mark 111) > >Saskatchewan, Canada njlabhart(at)kih.net 1956 Cessna 172 7453A Graham Lee Nieuport 11 replica Serial Number 1080, On the Gear! http://www.users.kih.net/~njlabhart/nieuport.htm ________________________________________________________________________________
Subject: Re: Safety wire & Kill switch
From: Ralph H Burlingame <ul15rhb(at)juno.com>
Date: Aug 09, 1999
Bill and others, I would like to make a comment on the kill switch. I forgot how it is positioned on the new FireStars, but on the Original FS it can be installed with the toggle position right side up. You may think this is OK for easy access, but on my second flight out, I was reaching under the seat for my camera and inadvertently hit the kill switch with my jacket sleeve. All I knew at the time was the engine quit and I made my first deadstick landing. When I tried to start the engine, I realized what had happened. From that time on, I simply turned the toggle switch upside down which made it inaccessible for this type of situation. Ralph Burlingame Original FireStar, 447 powered writes: >2. I haven't decided which way I want the kill switch to move to kill >the engine. Pulling up to kill seems easiest if I need to do it in a >hurry. On the other hand, pulling up also seems like it could happen >by >accident more easily. Any experiences that have pointed to one way or ________________________________________________________________________________
From: "Frank & Winnie Hodson" <fwhodson(at)bigfoot.com>
Subject: Fire Fly Brakes
Date: Aug 09, 1999
> -----Original Message----- > > I have six inch wheels and mechanical individual heel brakes. The > slightest pressure on the pedal causes the brakes to grab and release. It > appears the drum is out of round from it's action. Can't adjust > the brakes > properly for fear of ground looping! Anybody had this problem or has a > solution. Thanks. Dear Audrey: I had a similar problem when I first installed the same brake setup. The cure for me was to take the brake baking plate off where it bolts to the axle. I then drilled the four bolt holes oversize to allow the brake shoe assembly to move slightly to center themselves to the brake drums. I also used slightly longer bolts so they would not have to be as tight and still show some threads past the stopnuts. This does not affect how the wheel is attached to the axle but does take out the grab and release stuttering scenario. Good luck: FRANK HODSON, OXFORD ME (FSII N6399J) ________________________________________________________________________________
From: HShack(at)aol.com
Date: Aug 09, 1999
Subject: Geo/Suzuki Engine with Raven Redrive
Am intrigued by this Raven Redrive on Geo combination. Has anyone tried it on a Firestar I/II? I own a FS I with 503DCDI. Specs. show the 503 with "C" Box to weigh 98.7 pounds [50 HP]. One of the Raven combinations yields 60 HP at 118 pounds [probably doesn't include radiator, hoses, or coolant]. Is a 503 the biggest rated engine for the Firestar? Found nothing on this in the Archives. Howard Shackleford FS I SC ________________________________________________________________________________
Date: Aug 09, 1999
From: Jerry Bidle <jbidle(at)airmail.net>
Subject: Re: Fire Fly Brakes
Couple things. First have you changed the wheel bearings to the better quality ones, if not just do it. They will cost you about $5 bearing. See the archives for part number. If you can't find it email me direct and I'll locate it for you. This will make the wheel track straight and not wobble, it also reduced the tendency for the brake to grab when you go to apply the brakes. We got about 100 hours on our FireFly now and it made a lot of difference. It allowed us to adjust the brakes up where they need to be to obtain the proper braking effect. Next, when you installed the drum to the wheel, did you get it well centered. If not it will appear to be out of round, not the brake drum them selves are not perfect but usually there good enough. I used the washers placed inside the drum to align the drum to the wheels bearing. I also found while being tedious, drilling one hole at a time and disassembling putting in the bolt for that hole and then reassembling, drilling disassembling, reassemble, and drill the next one to product the truest alignment. (Got a spare wheel.) Also check to make sure the wheel itself is true. That's part of the reason why we have the spare, we had one that would wobble bad on it own just spinning on the axle. The drum worst. Jerryb FireFly > >I have six inch wheels and mechanical individual heel brakes. The >slightest pressure on the pedal causes the brakes to grab and release. It >appears the drum is out of round from it's action. Can't adjust the brakes >properly for fear of ground looping! Anybody had this problem or has a >solution. Thanks. > >Audrey Jr. > > ________________________________________________________________________________
From: "Christopher John Armstrong" <Tophera(at)centuryinter.net>
Subject: Re: Aileron Spades
Date: Aug 09, 1999
The bottom line is that what >ever input you supply with your arm through the stick, the spade also adds more >input on its own, therefore the total potential or available force will always >be greater. The total force can be the same or less if the pilot uses >discretion & applies less force in a gradual manner, in order to achieve a given >role rate. But if you are attempting maximum role rate, then the possibility of >over stressing the stock system is not unthinkable. ...Richard S The aileron provides the forces via the air that is acting over it. the pilot provides the deflection. That is why there is no force required to deflect the aileron when you are not moving through the air. The spade carries some of the force that the pilot would otherwise have to exert to get a given amount of difflection. It becomes easier for the pilot to deflect the stick and get bigger difflections but the forces on the aileron for a given diflection are the same, cause they still come from the air flow over them. to the aileron and the hinges and the wing structure nothing has changed. If the aileron could withstand full deflections before it can withstand them after spades are installed. the question is could the aileron withstand full deflections before, or were full deflections not possible cause of the limits of the pilots strength. if so then the max difflection is greater and the loads would go up. Topher ________________________________________________________________________________
Date: Aug 09, 1999
From: Jerry Bidle <jbidle(at)airmail.net>
Subject: Fire Fly Brakes
In my previous post I didn't mention this but true, centering the brake pad plate to the drum is part of the installation operation. We loosened our bolts slightly and allow the plate to find its own stable location while spinning the wheel. The tighten it down. I from the old school if you leave it floating loose, it will cause wear on the mounting holes those believe you should tighten the bolts back up once you feel you have it centered. Again I stress that much of our grabbing problem went away after swapping out the wheel bearing with better quality units. Try the centering trick first, if it doesn't help, then change the bearings. Regarding the bearing. Ours and a number of others reported cases were shot by time we approached 20 hours on the airplane. Their wheel barrow wheels and bearings they come with are not designed to handle the speed and stress there being placed under. Jerryb > > >> -----Original Message----- >> >> I have six inch wheels and mechanical individual heel brakes. The >> slightest pressure on the pedal causes the brakes to grab and release. It >> appears the drum is out of round from it's action. Can't adjust >> the brakes >> properly for fear of ground looping! Anybody had this problem or has a >> solution. Thanks. > >Dear Audrey: > I had a similar problem when I first installed the same brake setup. The >cure for me was to take the brake baking plate off where it bolts to the >axle. I then drilled the four bolt holes oversize to allow the brake shoe >assembly to move slightly to center themselves to the brake drums. I also >used slightly longer bolts so they would not have to be as tight and still >show some threads past the stopnuts. > This does not affect how the wheel is attached to the axle but does take >out the grab and release stuttering scenario. > >Good luck: FRANK HODSON, OXFORD ME (FSII N6399J) > > ________________________________________________________________________________
Date: Aug 10, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Fire Fly Brakes
>Regarding the bearing. Ours and a number of others reported cases were >shot by time we approached 20 hours on the airplane. Their wheel barrow >wheels and bearings they come with are not designed to handle the speed and >stress there being placed under. > >Jerryb We have a Northern Equipment store locally, and I tried some of their #13808 bearings in my MKIII wheels. They look slightly different, instead of having a flange around one edge, they have a groove milled in them, and a snap ring. This caused them to fit very slightly differently into the wheel, and I had to make up an internal spacer a little longer than the old internal spacer. ( I believe that having a spacer inside the wheels to absorb the squeeze loads imposed by tightening the axle nuts will cut down on bearing wear.) Anyway, they cost $3.29 each locally and so far are doing better than various others I have tried. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
Date: Aug 10, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: MKIII Enclosure
For those who wanted drawings and data of the MKIII enclosure, Mustek FINALLY sent me a new power supply for my scanner, and I can send out copies. Whoever wants that, let me know and when I think I have got a full list, I will send out the drawings as .jpg files. It will be a fairly big down load, so don't freak. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
From: "Vince Nicely" <vincenicely(at)intermediatn.net>
Subject: Re: Aileron Spades
Date: Aug 10, 1999
Hi Gang, I believe that I understand the argument below, but think there is another angle to the effect of spades on the Kolb depending on where they are placed. The forces on the wing and aileron could be increased considerably, I believe. The reason is as follows. At least on my Firestar II, the aileron spar twists as the stick is moved sidewise. As the speed increases, the aileron deflection becomes less for a given stick motion because of the twist in the spar. If a spade is placed in the area of the aileron's working surface, then the deflection will be aided by a force applied at the aileron rather than on the remote end of a rather limp tube. The aileron will likely deflect more as well as more easily, and the forces on everything will go up. This thinking has kept me from exploring spades, and if it is wrong would like to hear why. Vince > The aileron provides the forces via the air that is acting over it. the > pilot provides the deflection. That is why there is no force required to > deflect the aileron when you are not moving through the air. The spade > carries some of the force that the pilot would otherwise have to exert to > get a given amount of difflection. It becomes easier for the pilot to > deflect the stick and get bigger difflections but the forces on the aileron > for a given diflection are the same, cause they still come from the air flow > over them. to the aileron and the hinges and the wing structure nothing has > changed. If the aileron could withstand full deflections before it can > withstand them after spades are installed. the question is could the > aileron withstand full deflections before, or were full deflections not > possible cause of the limits of the pilots strength. if so then the max > difflection is greater and the loads would go up. > > Topher > > ________________________________________________________________________________
Date: Aug 10, 1999
From: "Bill Johnston Jr." <wingmen(at)hotbot.com>
Subject: (No Subject)
Hi to all you Kolbers out there! I've taken the plunge and ordered the new Mark III and have the Blueprints in hand and waiting on the arrival of Kit #1. Was wondering if there is any other printed material on the construction of this plane out there, just want all the info I can get my hands on before the materials arrive! Lets here from all you Mark III drivers out there! Thanks in advance Bill (aka WingMan) HotBot - Search smarter. http://www.hotbot.com ________________________________________________________________________________
From: "Larry Bourne" <larrybiglar(at)earthlink.net>
Subject: Re: MKIII Enclosure
Date: Aug 10, 1999
Please put me on your list. Thanks. Lar. ----- Original Message ----- From: Richard Pike <rpike(at)preferred.com> Sent: Tuesday, August 10, 1999 8:03 AM Subject: Kolb-List: MKIII Enclosure > > For those who wanted drawings and data of the MKIII enclosure, Mustek > FINALLY sent me a new power supply for my scanner, and I can send out > copies. Whoever wants that, let me know and when I think I have got a full > list, I will send out the drawings as .jpg files. It will be a fairly big > down load, so don't freak. > Richard Pike > MKIII N420P (42OldPoops) > > ________________________________________________________________________________
Date: Aug 10, 1999
From: Paul VonLindern <paulv(at)digisys.net>
Subject: Re: MKIII Enclosure
Add me to. Paulv Richard Pike wrote: > > For those who wanted drawings and data of the MKIII enclosure, Mustek > FINALLY sent me a new power supply for my scanner, and I can send out > copies. Whoever wants that, let me know and when I think I have got a full > list, I will send out the drawings as .jpg files. It will be a fairly big > down load, so don't freak. > Richard Pike > MKIII N420P (42OldPoops) > ________________________________________________________________________________
From: "Jeremy Casey" <jrcasey(at)mindspring.com>
Subject: Richard's Plans
Date: Aug 10, 1999
Richard Pike, I have been meaning to suggest this the last few times someone has had something to send a bunch of people. Why don't you send it to Matt Dralle and get him to put it in the misc. stuff section of the Kolb-List web page for a while. You want have to send it 400 times and keep up with all the people to send it to in the first place. He offered to do that one time I remember when someone whined about not being able to send attachments to the entire list. If he is too busy to do it then send it to me and I will upload it to a web page and just post the URL to the list for everybody to go get it thereselves... Just thought I'd mention it... Jeremy Casey jrcasey(at)mindspring.com P.S. It would be good to get Matt to do it so this kind of "tips and tricks" stuff can be archived for future builders... ________________________________________________________________________________
From: "AWIA" <awia(at)vcn.com>
Subject: Re: Kolb-List Digest: 08/09/99
Date: Aug 10, 1999
I have made several instrument panels for follow flyers using 1/8 inch plywood purchased from local hobby shop. It comes in sheets of 12" by 24" which is ideal for the Firestar. Look in the R/C airplane department. The advantage of the plywood is that it is light and strong and is very easy to work using ordinary wood working tools. One of my panels survived a crash without any damage. I shock mount the panels with rubber grommets. The plywood does not seem to "drum" with vibration like some aluminum panels. I know that many Firestar builders extent their panels and plywood works great for this. ________________________________________________________________________________
From: JRWillJR(at)aol.com
Date: Aug 10, 1999
Subject: Re: MKIII Enclosure
If you could add me to your list for the enclosure drawing that would be helpful. Thanks. JR ________________________________________________________________________________
From: "Mike Gallar" <MikeG(at)ij.net>
Subject: MKIII Enclosure
Date: Aug 10, 1999
Richard I would like a set Thanks Mike Gallar MikeG(at)ij.net > -----Original Message----- > From: owner-kolb-list-server(at)matronics.com > [mailto:owner-kolb-list-server(at)matronics.com]On Behalf Of Richard Pike > Sent: Tuesday, August 10, 1999 11:03 AM > To: kolb-list(at)matronics.com > Subject: Kolb-List: MKIII Enclosure > > > For those who wanted drawings and data of the MKIII enclosure, Mustek > FINALLY sent me a new power supply for my scanner, and I can send out > copies. Whoever wants that, let me know and when I think I have got a full > list, I will send out the drawings as .jpg files. It will be a fairly big > down load, so don't freak. > Richard Pike > MKIII N420P (42OldPoops) > > > --------- > > --------- > > --------- > > ________________________________________________________________________________
From: BICUM(at)aol.com
Date: Aug 10, 1999
Subject: Wing Alignment and Grinding Metal ????
John, Group, and Support, I've hit a big snag with my wing alignment. My head hurts from thinking about this so much and trying to figure it out. This one is a litttle hard to describe accurately with the written word so please bear with me. I called TNK and John Yates is on vacation (everyone deserves one). My basic problem is the interference (pieces butt together) between the wing main spar tang and the 1" square tubing of the cage. I have the wings up on H-sections, level both directions, in line spanwise, and within 1/4" tip to tail both wings. To accomplish this the drag strut horns are sticking out ~1 1/4" vs. the specified 7/8". With the main spar tang butted up against the square tubing of the cage, I'm pretty sure there is going to be a problem with lifting the wing for diehdral and lowering the wing after strut removal for folding. Plus I don't like the idea of the metal fatigue and torque that could cause a catastrophic failure and hitting the ground hard at an abrupt angle. Another problem is that right now the inboard steel tubes are more than 36" apart and I'll have to make the gap seal greater than the 36" specified in the plans to cover this up. I'd like to get closer to the drag horn sticking out 7/8" to minimze the distance between the bottom steel tube of the inboard ribs and the tube of the cage that runs along side of it. I looked a few Kolbs over pretty closely at a couple of Sun-N-Fun's and don't remember the gaps on the bottom of the wing being as much as mine is right now. The only way I can see to achieve this is to remove ~3/8" from each of the main spar tangs with a grinder. The main spar tangs on my inboard steel ribs stick out 1 3/8" from the vertical square tubing of the inboard rib. The plans (Section U-U) are drawn to scale and measure 1" for this dimension. I was wondering if some of you with older kits have the same 1 3/8" here or smaller. That 3/8" seems to be the problems to me. Has anyone else had this problem???? tang touching | | square tubing | | | | \/ | | | | |-------------------- | | | | Inboard Steel | | | Rib Vertical Square Tubing ________--------------- | | | | | | Square Tubing of cage | | | | ________| | | | --------------- | | |_____________| | | | O Sorry for the long note. Many of you have been a great help in the past when Ive asked for help from the group during these moments of "air turbelance". Much appreciation for that help past and future. Thanks again, John Bickham St. Francisville, LA Mark III (N308JB assigned) ________________________________________________________________________________
From: "Bruce Fletcher" <bwf(at)emailmn.com>
Subject: Re: Parts for sale
Date: Aug 10, 1999
Anyone out there needing parts to finish there kolb lll I have inst, inercom, headsets, elect trim, elect gear, chute, 912 (200 hrs) and more. Bruce Minneapolis MN bwf(at)emailmn.com 612 545-8722 ________________________________________________________________________________
From: "Jeremy Casey" <jrcasey(at)mindspring.com>
Subject: Re: Parts for sale
Date: Aug 10, 1999
> >Anyone out there needing parts to finish there kolb lll > >I have inst, inercom, headsets, elect trim, elect gear, chute, 912 (200 >hrs) and more. > >Bruce >Minneapolis MN >bwf(at)emailmn.com >612 545-8722 I emailed you earlier before I spoke to you on the phone so you should have another message from me as well. I am dropping this note to remind you that we spoke. I am interested in possibly buying your parts. You told me that you wanted about $8000 for the whole lot. I am going to see what I can work out and will get back to you in a few days. Jeremy Casey jrcasey(at)mindspring.com ________________________________________________________________________________
Date: Aug 10, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: Wing Alignment and Grinding Metal ????
> >John, Group, and Support, > >I've hit a big snag with my wing alignment. My head hurts from thinking >about this so much and trying to figure it out. The only way I can see to >achieve this is to remove ~3/8" from each of the main spar tangs with a >grinder. > >The main spar tangs on my inboard steel ribs stick out 1 3/8" from the >vertical square tubing of the inboard rib. The plans (Section U-U) are drawn >to scale and measure 1" for this dimension. I was wondering if some of you >with older kits have the same 1 3/8" here or smaller. That 3/8" seems to be >the problems to me. Has anyone else had this problem???? If you can grind off the metal inside of where the clevis pin would go through the spar tang, and still have at least 5/16" of thickness left over after you are done, you should be all right. The spar applies most of it's loading in compression, and much less in tension at that point, so if you presently have about 1/2" too much ( if I understand your situation correctly), you should be able to grind some off. Do you have an EAA technical counselor near by that you can call? This is a good situation to get an "Old Hand" to come and look your situation over. Call your nearest EAA chapter, and see if they can help you out. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
From: "Frank & Winnie Hodson" <fwhodson(at)bigfoot.com>
Subject: 503 OIL RESEVOIR VOLUME
Date: Aug 10, 1999
Dear Kolbers: I am making my weight and balance sheet. I started with empty weight first, I then fueled it with gas and oil for the engine break-in. ALAS, I know that gas is 6# per gallon and I have 10 gallons total but I have no Idea how much oil the pump reservoir holds. Anybody out there know the volume so I can avoid draining the tank to measure it? I know it is not a big thing to do but I thought I could possibly avoid the mess and having to purge the line again. THANKS IN ADVANCE: FRANK HODSON, OXFORD ME (503 ROTAX DCDI) fwhodson@megalink.net http://www.megalink.net/~fwhodson ________________________________________________________________________________
Date: Aug 10, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re: Instrument panels
> >I have made several instrument panels for follow flyers using 1/8 inch >plywood purchased from local hobby shop. It comes in sheets of 12" by 24" >which is ideal for the Firestar. Look in the R/C airplane department. Just a note to those of you who haven't made or painted you intrument panels yet. "Flat black" is better. Anything that is left white, or "chrome" anywhere near the panel or directly below it will show up on your windshield like a "heads up" display. Not a big problem, but gets old after a while,on a firestar anyway. Even the white numbers on the instruments show up when the sun hits them. ________________________________________________________________________________
Date: Aug 10, 1999
From: Richard Bluhm <irena(at)ccis.com>
Subject: Re: Wing Alignment and Grinding Metal ????
BICUM(at)aol.com wrote: > > John, Group, and Support, > > I've hit a big snag with my wing alignment. My head hurts from > thinking > about this so much and trying to figure it out. This one is a litttle > hard > to describe accurately with the written word so please bear with me. > I > called TNK and John Yates is on vacation (everyone deserves one). Hey John, I think I know what you are talking about. I went and ordered extra long drag-strut horns, but when I re-installed them, I noticed the original length horns would have worked. Here's what I would suggest: Push the horns in to the recomended distance of 7/8", then make sure the trailing edges are in line. ( You can sight-line this). This will back off the closeness of the tangs in the front. If it doesn't work,, redo it again... Sight line the trailing edge again. It should line up okay without grinding any metal off. I know the feeling you are having as I had a hard time explaining the situation to Dennis Sauder. My horns are extra long, but you couldn't tell as they are inside the drag strut. I didn't know what happened to get them in line that second time, but I assume (the a word) it had something to do with lining up the trailing edge. Hope this helps Regards Doc ________________________________________________________________________________
Date: Aug 10, 1999
From: Bill Weber <bweber2(at)earthlink.net>
Subject: Re: Safety wire & Kill switch
Thanks for posting the method for safety wire on turnbuckles. Someone also sent me an illustration. Between the two, it should be a piece of cake. "Douglas G. Murray" wrote: > > > Bill Weber wrote: > > > > > I am finally finishing up my Firestar and have a few loose ends. The > > last 10% seems to take 90% of the time. > > > > 1. The turnbuckles for the elevator controls need to be safety wired. > > How is the saftety wire routed? > > > > 2. I haven't decided which way I want the kill switch to move to kill > > the engine. Pulling up to kill seems easiest if I need to do it in a > > hurry. On the other hand, pulling up also seems like it could happen by > > accident more easily. Any experiences that have pointed to one way or > > the other? > > > > Bill - Congratulations on your progress. It won't be long now before you are > having fun in the air. The safety wires can be installed in two or three > methods. I would suggest that you look in AC43 - 1B & 2B Accepted Aircraft > Building Practices or any of Tony Bingelus' books. Both demonstrate pictorially > the methods used to safety a turnbuckle. It is kind of hard to describe it in > words but you want to stop the barrel from rotating and changing the setting you > need. I usually start by cutting a piece of .032" stainless wire about ten > inches long. Fold it in half and put one leg of the wire though one end of the > turnbuckle yoke/clevis. Wrap each end of the wire two turns around the yoke/ > clevis end in opposite directions and then insert each end of the wire through > the center barrel hole - again in opposite directions. Wrap the wire ends two > times around the yoke/ clevis on the other end of the turnbuckle from your > starting point and then put one of the wire ends through the end of the > yoke/clevis and then tie off the two ends of the safety wire. It is a lot > easier to see in a picture or in real life than to explain but I hope this > helps. > > On your second question - Switches are always ON when FORWARD or UP. OFF > when REARWARD or DOWN. You may need to change the cover plate that comes with > your kit so it is labled correctly. If you cut off the little locator tab on the > inside of the hole, the cover label plate can be rotated around so that your > switch movement and operation are correct. > > Have a safe first flight. > > Doug Murray Firestar 1 flying since 1990 > Southern Alberta > -- *********************************************** * Bill Weber * Keep * * Voiceboard Corp * the shiny * * Simi Valley, CA * side up * *********************************************** ________________________________________________________________________________
From: "Lindy" <lindy(at)snowhill.com>
"Tom Ferguson" , "Ted Cowan" , "Scott Sharon Wilcox" , "Sam Cox" , "Paul Spadin" , "Michael Highsmith" , "Kolb Builders" , "John Hauck" , "Greg Moloney" , "Glenn Rinck" , "Frank Kahn" , "Dave Thomas" , "Danny Day" , "Buddy Carilse" , "Bob Moorehead" , "Ben Cole" , "ASC2"
Subject: Fw: Fw: Flying
Date: Aug 11, 1999
----- Original Message ----- From: Aniceto I Bagley <aibagley(at)juno.com> Sent: Tuesday, August 10, 1999 9:52 PM Subject: Fw: Fw: Flying > > Aniceto I. Bagley > 6013 Rickwood Dr., NW > Huntsville, AL 35810-2569 > Tel: (256) 852-7973 > e-mail: aibagley(at)juno.com > > --------- Forwarded message ---------- > From: Ray Weinberg <raykw(at)juno.com> > To: Oimon4(at)AOL.COM, IRVnLAKE(at)AOL.COM, aibagley(at)juno.com, > desiree.weinberg(at)mcclellan.af.mil > Date: Tue, 10 Aug 1999 08:56:50 -0500 > Subject: Fw: Flying > Message-ID: <19990810.101904.-83377.26.RAYKW(at)juno.com> > > > > - > Aviation 101 > > Takeoffs are optional. Landings are mandatory. > > If you push the stick forward, the houses get bigger, if you > pull the stick back they get smaller. Unless you keep > pulling the stick back then they get bigger again. > > Flying is not dangerous; crashing is dangerous. > > The propeller is just a big fan in the front of the plane to > keep the pilot cool. Want proof? Make it stop; then watch > the pilot break out into a sweat. > > The only time you have too much fuel is when you're on fire. > > Every one already knows the definition of a 'good' landing > is one from which you can walk away. But very few know the > definition of a 'great landing.' It's one after which you > can use the airplane another time. > > The probability of survival is equal to the angle of > arrival. > > A helicopter is a collection of rotating parts going round > and round and reciprocating parts going up and down -- all > of them trying to become random in motion. Helicopters > can't really fly -- they're just so ugly that the earth > immediately repels them. > > Learn from the mistakes of others. You won't live long > enough to make all of them yourself. > > There are three simple rules for making a smooth landing: > Unfortunately, no one knows what they are. > > The only thing worse than a captain who never flew as > copilot is a copilot who once was a captain. > > It's easy to make a small fortune in aviation. You start > with a large fortune. > > A male pilot is a confused soul who talks about women when > he's flying, and about flying when he's with a woman. > > Try to keep the number of your landings equal to the number > of your takeoffs. > > Asking what a pilot thinks about the FAA is like asking a > fire hydrant what it thinks about dogs. > > ****************************** > If you're not livin' on the edge, > You're takin' up too much space! > ****************************** > > ___________________________________________________________________ > Get the Internet just the way you want it. > Free software, free e-mail, and free Internet access for a month! > Try Juno Web: http://dl.www.juno.com/dynoget/tagj. ________________________________________________________________________________
From: Tusky(at)aol.com
Date: Aug 11, 1999
Subject: Re: Kolb-List Digest: 08/10/99
Hey, K-listers: I have a nice FireStar KXP, DCDI, BRS VLS750 for sale. Fair price. E-mail me at Tusky(at)aol.com. (Charlotte, NC) ________________________________________________________________________________
Date: Aug 11, 1999
From: wood <duesouth(at)iname.com>
Subject: Re: Wing Alignment and Grinding Metal ????
> >John, Group, and Support, > >I've hit a big snag with my wing alignment. My head hurts from thinking >about this so much and trying to figure it out. This one is a litttle hard >to describe accurately with the written word so please bear with me. I >called TNK and John Yates is on vacation (everyone deserves one). > >My basic problem is the interference (pieces butt together) between the wing >main spar tang and the 1" square tubing of the cage. I have the wings up on >H-sections, level both directions, in line spanwise, and within 1/4" tip to >tail both wings. To accomplish this the drag strut horns are sticking out ~1 >1/4" vs. the specified 7/8". Have you drilled the holes in the tang yet? If not then put a spacer on the end of the tang with duct tape and realign the wings. This will push the front tang out and the drag strut in. Other than that if you have the holes drilled your idea of grinding may be the only way. Woody ________________________________________________________________________________
Date: Aug 11, 1999
From: Ron Hoyt <Ronald.R.Hoyt@gd-is.com>
Subject: Re: Batteries
Lar Yuasa also has a web site showing their suit of batteries. I passed through it in finding the Power Sonics. Ron > > >Thanks Ron: I went to their web-site, and found the batteries to be a >little awkward. My old one was about 2 1/2 x 3 x 4, and was a perfect fit >with the intercom in my fanny pack. Power Sonics 3 amp is too long, and >their 5 amp is too deep and heavy. Seems to me the old one was a Yuasa, and >I'm trying to find a dealer now. Thanks very much for your help. >Lar. > ________________________________________________________________________________
From: HShack(at)aol.com
Date: Aug 11, 1999
Subject: Re: Batteries
In a message dated 8/11/99 3:38:57 PM Eastern Daylight Time, larrybiglar(at)earthlink.net writes: << My old one was about 2 1/2 x 3 x 4, and was a perfect fit with the intercom in my fanny pack. >> Larry, I am in the burglar alarm business and have accessto lots of different size batteries. Let me know if you still need one & I'll send you one at my cost plus UPS; you can then just send me a check. I have a cheap backpack strapped where the rear seat used to hang with a 4 Amp-hour battery in it for GPS & Radio. Howard Shackleford FS I SC ________________________________________________________________________________
Date: Aug 11, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re: Batteries
Just a thought- Seems to help a lot if you "ground" the battery-back to the engine or the engine mount and "not" to the aircraft "frame". I know I get a "lot" more kick that way on a smaller Amp Hour battery. I even used a jumper cable because the battery cables I found were too large, and it still works great. ________________________________________________________________________________
From: GeoR38(at)aol.com
Date: Aug 11, 1999
Subject: Re: Safety wire & Kill switch
In a message dated 8/9/99 1:03:27 PM Eastern Daylight Time, steiner(at)spreda.sk.ca writes: << I asked the Kolb company if they had a Kolb owners quest book. It would have been interesting too see how many list members were at Oshkosh. Kim Steiner (1990 Mark 111) Saskatchewan, Canada >> Kim, I was the first one (except for John Hauck), to be at the kolb tent on Wed.and talked to Bruce about organizing something for this newsgroup and he gave me a piece of paper for me to sign, which I did and he pronounced me in charge of the newsgroup list!!....I was honored ...indeed....except by 7pm, I was still the only one on the list!!...I talked to JH for a half hour and had to leave...completely!! When I left, I was still the only one of this newsgroup with my name on the yellow piece of paper at the Kolb tent....surprised me! ... Iwas hoping to meet some of you folks.................GeoR38 In charge! :-) ________________________________________________________________________________
From: GeoR38(at)aol.com
Date: Aug 11, 1999
Subject: Re: Off/On switches
In a message dated 8/9/99 3:35:58 PM Eastern Daylight Time, TCowan1917(at)aol.com writes: << I would like to comment on the off/on switch for your kolb. I have mine installed inside of a plastic cap that comes with fuel jugs for RC airplane engines - Glow Fuel. It has a a little bevel in it and it is perfect and is also red. Makes it easy to see and use and you wont accidentally turn it off. >> I did the same thing, Ted, but only after the horse left the barn, unfortunately, namely I let a CFI fly my Firestar one day and he accidently bumped the ignition toggle with his plump littly knee,and found himself surrounded by trees on his downwind approach and......silence! He did ok on this his first flight in an ultralight, but only after taking a few years off his life from sheer terror! I got a cap off a spray paint can and surrounded the toggle bat with that.....and bought 2 more gear legs...one had broke off completely and the other looked like a huge piece of someones curly hair! The CFI was chalky white and had a pretty sore leg for a day or two.....no real damage though.....happened a coupla years ago. GeoR38 ________________________________________________________________________________
From: "Frank & Winnie Hodson" <fwhodson(at)bigfoot.com>
Subject: Geo/Suzuki Engine with Raven Redrive
Date: Aug 12, 1999
> > Am intrigued by this Raven Redrive on Geo combination. Has > anyone tried it > on a Firestar I/II? I own a FS I with 503DCDI. Specs. show the > 503 with "C" > Box to weigh 98.7 pounds [50 HP]. One of the Raven combinations > yields 60 HP > at 118 pounds > [probably doesn't include radiator, hoses, or coolant]. Is a 503 > the biggest > rated engine for the Firestar? Found nothing on this in the Archives. > > Howard Shackleford > FS I > SC Dear Howard: I found this message in the archives: (Good luck, FRANK HODSON/OXFORD ME) Match: #205 Message: #6620 From: DLSOUDER(at)aol.com Date: Sep 10, 1998 Subject: 4 Cylinder FireStar Recived a call from the FAA about a FireStar crash, pilot was doing high speed taxi testing and he wound up in a tree. FAA wanted to know if it was an UL or experimental. Our records showed that he purchased the kit, but no engine. We said we really didn't know because we don't know what engine he may have used. The FAA investigator said he didn't know either, but he did know that it had 4 cylinders! In case you don't know - you shouldn't do that! Please don't do that! A FireStar does not need more than 2 cylinders - 4 is way too many cylinders. Please count your cylinders before installing ... remember 4 is too many. Dennis (another sleepless night) Souder Pres Kolb Aircraft ________________________________________________________________________________
From: BKlebon(at)aol.com
Date: Aug 12, 1999
Subject: Re: Kolb in St. Mary's County MD.
I have a Firestar that is painted international orange with yellow stripes. I live in Salisbury and fly up and down the eastern shore. Have never flown across the "big pond" so I doubt it was me. I you ever get to this side of the bay, please call as I have found no other Kolbs here. Rick Klebon 410-749-9495. ________________________________________________________________________________
Date: Aug 12, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: MKIII Enclosure
To all that have asked about the MKIII enclosure: Matt has offered to put it up in the archives as a bitmap file, so that it will be available to anybody anytime. The drawings are copyrighted, and as soon as we get permission, will be able to get it done. Richard Pike MKIII N420P (42OldPoops) ________________________________________________________________________________
From: Richard_Harris(at)albemarle.com
Date: Aug 12, 1999
Subject: MK3
Hi gang Am new to the list. got a question about MK3 & 912 angle of mount. I am getting some tail shake about 80 mph . don't know where its coming from, but the 912 is mounted with the front about 1/2 in higher as per kolb. Just thinking someone might something to do. thanks RH ________________________________________________________________________________
Date: Aug 12, 1999
Subject: f/s engine
From: Robert L Doebler <bobdoebler(at)juno.com>
I was told when I bought my Firestar II that the largest engine I could use was the 503 DCDI, and I had to install the heavier duty wing( larger rib count) think its 7 rib versus 5. Bob Doebler ________________________________________________________________________________
Date: Aug 12, 1999
From: Richard Pike <rpike(at)preferred.com>
Subject: Re: MK3
Had a shaking problem caused by too much weight on the trailing edge of the rudder. Had a friend in another Kolb follow me up one day and watch and discovered it was rudder flutter. One giveaway of rudder flutter is that the rudder pedals move rapidly back and forth, and it quits when you hold both feet tight against the pedals. A word of caution: it didn't seem too bad from the cockpit, but the pilot watching said it looked very radical and alarming from behind and above, (said the 6" fuselage boom tube apeared to be in a sine wave!?!?) so I would think any flutter or shake might be worse than you can accurately evaluate from the cockpit, and therefore unacceptable for more than a few seconds at a time. Be careful. Richard Pike MKIII N420P (42OldPoops) > >Hi gang > > Am new to the list. got a question about MK3 & 912 angle of >mount. I am getting some tail shake about 80 mph . don't know where its >coming from, but the 912 is mounted with the front about 1/2 in higher as >per kolb. Just thinking someone might something to do. >thanks > > > RH > > ________________________________________________________________________________
From: HShack(at)aol.com
Date: Aug 12, 1999
Subject: Re: Geo/Suzuki Engine with Raven Redrive
In a message dated 8/12/99 12:12:25 AM Eastern Daylight Time, fwhodson(at)bigfoot.com writes: << I found this message in the archives: (Good luck, FRANK HODSON/OXFORD ME) Match: #205 Message: #6620 From: DLSOUDER(at)aol.com Date: Sep 10, 1998 Subject: 4 Cylinder FireStar >> Thanks, Frank. I remember reading that message when Dennis wrote it. The Geo engine I,m thinking about using is about 150LBS all up weight-about 30 pounds heavier than my 503 w/ "C" Box, so I am mostly concerned with the CG. Right now I am right in the middle at 28%. The power is approx. 60 HP; not too worried about that. I understand FS II's & Twinstars have been flying for years with 532's & 582's & they use the same wing that that I have. Comments? Howard Shackleford FS I SC ________________________________________________________________________________
From: B708408(at)aol.com
Date: Aug 12, 1999
Subject: Hinge Pins
Reference: Piano hinges, instructions say to cut the hinge pin 1/2" shorter and crimp the hinge to retain the pin. I wonder if any one has a less permanent idea. I would like to retain the option of removing the pins to separate the hinges and the movable serfaces. I can't believe I'm the only one who would like to keep that option open. John Mallet Working on a FS II in Sulphur, La. ________________________________________________________________________________
Date: Aug 12, 1999
From: Possum <possums(at)mindspring.com>
Subject: Re: Hinge Pins
> > Reference: Piano hinges, instructions say to cut the hinge pin 1/2" shorter >and crimp the hinge to retain the pin. I wonder if any one has a less >permanent idea. I would like to retain the option of removing the pins to >separate the hinges and the movable serfaces. I can't believe I'm the only >one who would like to keep that option open. > >John Mallet >Working on a FS II in Yes, I have had the pins actually drill themselves out, even after you have "crimped" the hinges. It always happens on the hinges nearest the engine and has happened more than once to me, and on other planes besides mine. I suppose it has something to do with the vibration of the engine. This time I drilled small holes in the ends of the hinges and put in small "stainless steel" cotter pins. It was a lot easier than I thought. P.S. It is a good idea to "oil" the hinges like Mike Highsmith says. ________________________________________________________________________________
Subject: rudder oscillation
From: Ralph H Burlingame <ul15rhb(at)juno.com>
Date: Aug 12, 1999
Hi Guys, While on this subject of rudder flutter, I too have experienced a type of rudder flutter, but I prefer to call it an oscillation induced by manmade thermal activity. I was flying one day with my feet off the pedals and on the floor when I flew over a smokestack from a power plant. Immediately, the plane went into a slow back and forth yawing action where the long fuse tube was swaying and the wings were yawing. Putting my feet on the rudder pedals would not stop it, so I pulled up hard to stall the plane and when the speed dropped off, the yawing action also stopped. If this had continued, I'm sure the cage would have suffered structural failure due to the twisting from the yaw. This happened over 10 years ago and I have flown regularly since but with both feet on the pedals. I believe this was a very freak incident where the combination of initial slack in the rudder system (from not having my feet on the pedals) and the shock of the thermal hit the rudder just right to initiate this action. If it ever happens again, I know what to do. Ralph Burlingame Original FireStar, 447 powered writes: > >Had a shaking problem caused by too much weight on the trailing edge >of the >rudder. Had a friend in another Kolb follow me up one day and watch >and >discovered it was rudder flutter. One giveaway of rudder flutter is >that >the rudder pedals move rapidly back and forth, and it quits when you >hold >both feet tight against the pedals. A word of caution: it didn't seem >too >bad from the cockpit, but the pilot watching said it looked very >radical >and alarming from behind and above, (said the 6" fuselage boom tube >apeared >to be in a sine wave!?!?) so I would think any flutter or shake might >be >worse than you can accurately evaluate from the cockpit, and therefore >unacceptable for more than a few seconds at a time. Be careful. >Richard Pike >MKIII N420P (42OldPoops) ________________________________________________________________________________
From: Timandjan(at)aol.com
Date: Aug 12, 1999
Subject: Re: Hinge Pins
I drilled small holes in each end and ran a loop of safety wire through the holes to keep the hinge pin in. This way each year when I do my inspection, I can remove each piano hinge pin, clean it, and re lube each hinge. I also noticed on the new kolb Slingsjot at Oshkosh this year they have done the same thing. tim ________________________________________________________________________________
From: aquila33(at)webtv.net (dann mann)
Date: Aug 12, 1999
Subject: Re: Hinge Pins
On the MINIMAX plans it says to cut the pins short, drill a small hole and insert a cotter pin. This would prevent the long pin from coming out. Dan ________________________________________________________________________________
From: HShack(at)aol.com
Date: Aug 12, 1999
Subject: Re: Hinge Pins
In a message dated 8/12/99 7:59:50 PM Eastern Daylight Time, B708408(at)aol.com writes: << I would like to retain the option of removing the pins to separate the hinges and the movable serfaces. I can't believe I'm the only one who would like to keep that option open. >> Cut the pins 1/2" shorter than the hinge, drill the hinge on both ends & install little cotter pins. Howard Shackleford FS I SC ________________________________________________________________________________
From: "Christopher John Armstrong" <Tophera(at)centuryinter.net>
Subject: Re: Hinge Pins
Date: Aug 12, 1999
>Yes, I have had the pins actually drill themselves out, even after you have >"crimped" the hinges. It always happens on the hinges nearest the engine >and has happened more than once to me, and on other planes besides mine. I >suppose it has something to do with the vibration of the engine. This time >I drilled small holes in the ends of the hinges and put in small "stainless >steel" cotter pins. It was a lot easier than I thought. THe big GA planes and homebuilts that use piano hinges to hold cowlings together often make the hinge pins long, not short, turn a loop in the extra length and put a screw through the loop into the hinge material or some nearby metal. I think this is the direction I will go, as the twisted end of the hing forms a spring that should withstand the vibratiions that tend to drill through the crimped end of the hing or even a cotter pin. very easy to remove too. Topher ________________________________________________________________________________
From: "Frank & Winnie Hodson" <fwhodson(at)bigfoot.com>
Subject: Geo/Suzuki Engine with Raven Redrive
Date: Aug 12, 1999
> -----Original Message----- > The > Geo engine I,m thinking about using is about 150LBS all up > weight-about 30 > pounds heavier than my 503 w/ "C" Box, so I am mostly concerned > with the CG. Dear Howard: You can calculate the new C.G. by measuring the arm to the center of your present engine and multiplying it by the extra 30# to find the moment. Add this to your present weight and balance to find if it will be within an acceptable range ( this figure will not be totally accurate but will come pretty close as long as you haven't underestimated the actual weight of the Geo set-up). Good Luck: FRANK HODSON, OXFORD ME P.S.: Do you have any idea as to the volume of the 503's oil reservoir? ________________________________________________________________________________
From: "Lindy" <lindy(at)snowhill.com>
"Charles Waller" , "Dan Dantzer" , "Danny Day" , "Dave Thomas" , "Glenn Rinck" , "Greg Moloney" , "John Hauck" , "Kolb Builders" , "Michael Highsmith" , "Paul Spadin" , "Rutledge Fuller" , "Sam Cox"
Subject: Fw: RegReps re USUA Topics
Date: Aug 12, 1999
----- Original Message ----- From: <USUAHQ(at)aol.com> ; ; ; ; ; ; Sent: Thursday, August 12, 1999 9:58 AM Subject: RegReps re USUA Topics > August 12, 1999 > > Dear Directors and Regional Representatives: > > My last e-mail to you was confidential, this one is not. Interestingly that > confidential mail showed up on the KOLB chat group and, I presume, spread > from there so it doesn't seem to matter how they are marked. > > This contains a number of topics which relate to the upcoming September issue > of Ultralight Flying! Magazine. It is being sent to you so you will have > advance knowledge of the issues. Editorial comments are in italics. > > There will also be an insurance plan announcement. However, I will send it > to you in a separate e-mail along with detailed program specifics so you can > better answer member questions. You may want to contact the clubs in your > region with this information as affordable third-party liability insurance > has been desired by many for a long time. > > John Ballantyne, USUA President > > -------------------------------------------------- > Ultralight Flying! magazine has raised USUA subscription prices by over 16%. > This is not tolerable at current membership rates, and requires that we raise > dues as discussed by Directors in Knoxville. Here is the magazine blurb > associated the dues increase: > > MEMBERSHIP DUES/MAGAZINE PRICES INCREASED > USUA annual membership dues were raised a total of $7.00 when Ultralight > Flying! magazine subscriptions increased $5.00 as of September 1st. Members > not receiving the magazine with membership saw a $2.00 increase. [Ed note-UF! > wants to delete USUA references to their subscription rate increase.] > > USUA dues have not increased during the 1990s. > > "USUA has done a spectacular job of keeping costs down while increasing > services. But after a full decade with no dues increase it has finally caught > up with us," said USUA President John Ballantyne. "Averaging 3 percent > inflation for each of the 10 years since USUA last increased dues would > indicate the need for $53.69 in dues to simply stay even. However, USUA has > become more efficient and has developed non-dues revenue sources to offset > the need for higher member dues increases. Members expect USUA to be > financially sound and this step assures we stay in line with that plan." > > The new member dues still represent a significant bargain considering what a > member receives in return. On average, USUA members receive $76.00 in > products, benefits and services for their annual $46.95 dues, including: > > -Ultralight Flying!, Ultralight Aviation's largest magazine > > -Merchandise Discount Coupon worth up to $25 off selected products > > -access to free technical advisors on USUA's Pilot and Owner Assistance > Hotline > > -the USUA On-line system offering the latest news, club and instructor and > Hall of Celebrities listings, and free aviation weather via personal computer > > -access to internationally recognized achievement awards and flying programs > > Also available are a myriad of special programs including the USUA Ultralight > Airmen & Vehicle Registration Program, Insurance and financing programs, > discounts on rental cars and, for instructors, the USUA Student Rebate and > training material discount programs. > > -------------------------------------------------- > > -------------------------------------------- > > Editorial for the September Ultralight Flying! magazine > by John Ballantyne > > FAA Administrator-Public Meetings > I would like to compliment FAA Administrator, Jane Garvey, for her stage > presence and first-hand knowledge of FAA's activities at a recent, public > meeting during which she answered many audience questions. She is obviously > paying attention and is aware of many issues of concern to FAA. > > FAA ARAC Rule Project > However, it was disappointing to hear her answer a question about the > progress of the FAA Aviation Rulemaking Advisory Committee (ARAC) "Sport > Pilot" project. Without hesitation she responded that FAA was considering a > reduced medical certificate and, while she could not promise anything, FAA > was trying real hard. The disappointing part was that she stopped there. Her > briefings have apparently been limited to medical issues as being the > significant topic in the ARAC project. > > You may recall that he advisory group of representatives from many > associations had drafted a request to FAA for a shell of standards under > which new pilot certificate programs could be administratively created and > modified. The medical requirement for pilots is one of many issues associated > with the draft request. As USUA has reported many times, the exclusive focus > on medicals came after large aviation groups began to participate in the last > few working groups meetings. Now it seems that the FAA Administrator is not > hearing much about anything thing else. > > EAA/ASC petitions to FAA? > Meanwhile sources report that FAA is working to create a new FAA category > specifically for trikes outside the FAA Sport Pilot ARAC project. Reports > also indicate that FAA has recently received input from EAA and ASC as well. > Apparently ASC has submitted a petition although ASC has not responded to my > telephone message about their request. EAA is drafting a petition to FAA for > some form of commercial use with some experimental aircraft including trikes. > > There has been no cooperation between the associations even though I > personally telephoned EAA and ASC with an invitation/suggestion to work > together with petitions to FAA. While both groups verbally agreed to share > information, ASC then petitioned FAA in secret and EAA now says they will > provide a copy their petition only after submitting it to FAA. > > I wonder if this is a good way for an industry to do business? There are > serious implications to ultralighting in these exemption requests by EAA/ASC. > Have the members of those groups been consulted or even been told how they > are being represented to FAA? > > FAA Internal Activity > What is FAA doing and why do they appear to be ignoring the ARAC Sport Pilot > working group are additional questions which need answering. FAA created the > Sport Pilot ARAC working group to resolve such things. > > While the Sport Pilot ARAC working group awaits response from FAA legal and > FAA economists, there has been no expectation that FAA would take unilateral > action. USUA will continue to uncover these matters and report in upcoming > issues of Ultralight Flying! magazine. > > WOW - USUA Insurance program like never before! > USUA sets a new standard for affordable insurance with the announcement of > one million dollar third party liability insurance for only $150.00 per year. > It covers pilots/instructors of "Fat" single-seaters and two place > ultralights as well. I want to personally thank Willis Corroon vice-president > Andrew Kain who has devoted a huge amount of time to the creation of this > program. Refer to the separate information on this program in this issue of > Ultralight Flying! magazine. Please participate. > > Highest Membership Ever > Finally, I want to thank each USUA member for your membership and support of > USUA. This month the current, annual membership of USUA is higher than ever > before. While we are still a relatively small organization in the broad view, > our constant direction and business-like methods are effective. > > USUA is the only association in the world which is entirely dedicated to > American ultralight aviation and is solidly connected all the way from the > local club network to the member-elected regional representatives, to the > full-time national headquarters near Washington DC, to the FAI international > microlight commission in Lausanne, Switzerland. > > USUA is a not-for-profit corporation which receives no advertising money and > is in debt to no one. No other organization controls or directs its > activities. Every USUA Director is an active ultralight pilot/instructor and > cares very much about the health and direction of our air sport. > > Obviously more and more people are recognizing the value of this association. > We appreciate your increasing support and promise to squeeze every dollar as > much as possible to promote, protect and represent your interests in > ultralight aviation. > > ps: > When I use the word "ultralighting," I refer to the act of aviating by > pilots of single and two-place craft that fly slowly and are primarily for > recreation. "Ultralight" and "Microlight" are international terms which are > sometimes interchanged. Refer to FAR Part 103 for vehicle definitions and > operating rules. Some flight operations are regulated by FARs 61 and 91. Be > sure you know the difference. > ---------------------END-------------------------- > > ________________________________________________________________________________
From: RLCPTL(at)aol.com
Date: Aug 13, 1999
Subject: Re: Hinge Pins
Hi John: You asked - - quote - - Piano hinges, instructions say to cut the hinge pin 1/2" shorter and crimp the hinge to retain the pin. I wonder if any one has a less permanent idea. - unquote. I drilled a very small hole in each end of the hinge and inserted a small cotter pin. Of course, the hinge pin is about 1/2" shorter than the hinge. This way, the hinge can be disassembled very easily. Works for me! Ron Christensen MKIII1/2 ________________________________________________________________________________
From: "Lindy" <lindy(at)snowhill.com>
"Rutledge Fuller" , "Paul Spadin" , "Michael Highsmith" , "Kolb Builders" , "John Hauck" , "Greg Moloney" , "Glenn Rinck" , "Frank Kahn" , "Dave Thomas" , "Danny Day" , "Charles Waller" , "Dan Dantzer" , "Buddy Carilse" , "Bob Moorehead" , "ASC2"
Subject: Fw: RegReps re USUA Topics
Date: Aug 12, 1999
----- Original Message ----- From: <USUAHQ(at)aol.com> ; ; ; ; ; ; Sent: Thursday, August 12, 1999 9:59 AM Subject: RegReps re USUA Topics > August 12, 1999 > > Dear Directors and Regional Representatives: > > > This information about the new USUA Insurance program is for general > distribution. The following text comes from two sources: USUA Headquarters > News portion of the upcoming issue of Ultralight Flying! Magazine, and a > brochure available from USUA HQ. > > You may want to contact the clubs in your region with this information as > affordable third-party liability insurance has been desired by many for a > long time. > > John Ballantyne, USUA President > > ------------------------------------------------ > > Text from upcoming Ultralight Flying! magazine: > > USUA INSURANCE PLAN > INSURANCE FINALLY AVAILABLE > > Individual third party liability insurance coverage for single and two seat > "ultralight" operations is now available exclusively to USUA members. This > type of insurance covers your cost of defense and penalties, if through your > flying activity, you injure someone or damage someone's property but not a > student or passenger or someone associated with the operation of the > vehicle/aircraft. The plan provides a USUA member in good standing coverage > up to $1 million combined per accident. This breaks down to a maximum of > $100,000 each person for bodily injury and $1,000,000 for property damage. > > USUA recently concluded the last details to put the program in motion. "The > long process to set up a program to provide members with their own personal > liability insurance plan is over," said USUA President John Ballantyne. "A > special thanks to the Willis Company and specifically to Andy Kain, > Vice-president, for seeing the value of this service to our community and > partnering with USUA to develop this plan that has led ultralighting into the > new millennium." > > The insurance program is open to all who operate "ultralight" airplanes, > trikes and hang gliders and have pilot and vehicle/aircraft registration > through FAA or any FAA recognized ultralight safety program. The policy will > cover all vehicles/aircraft having a stall speed not exceeding 35 knots (40 > mph) Calibrated Air Speed and with a gross weight of not more than 992 U.S. > pounds. The policy costs only $154.50 per year ($150 plus 3% surplus lines > tax). > > "USUA is pleased to offer this insurance coverage to many of our members," > Ballantyne commented. "This is the beginning. As the policy base grows and > the underwriters can see how well we perform, the plan can be expanded to > include more members such as those operating powered parachutes." > > The coverage is intended for private owners and instructors. It is not > intended for those involved in commercial flying such as towing of banners & > gliders; aerial seeding, aerial spraying or dusting or other for-hire > operations except instruction. > > To receive USUA Insurance Plan details and an application, visit the USUA > Website or directly contact USUA Tel: (301) 695-9100, Fax: (301) 695-0763. > > --------------------------------------------------- > > The following text is from a tri-fold handout which is available from USUA. > > Enjoy Peace of Mind, > > Financial Protection for Your Family and Your Future. > > > With a USUA 3rd Party Insurance Policy In Hand > > > USUA: PROTECTING YOUR > PRIVILEGE TO FLY FOR FUN! > > > USUA INSURANCE PLAN > 3rd Party Liability Coverage For Pilots of Ultralights: Trike, Airplane and > Hang Glider > > > AT LAST, > 3rd Party Liability Insurance Coverage FOR USUA MEMBERS > > 8 $1 Million Per Accident > > 8 Open to "Fat Ultralights" > - airplanes, trikes and hang gliders > > - stall speed not exceeding 35 knots (40 mph) Calibrated Air Speed > > - Gross weight of not more than 992 U.S. pounds > > 8 Registration through FAA or any FAA recognized ultralight safety program. > > 8 Only Costs $154.50 > ($150 per year plus 3% surplus lines tax) > > The coverage is intended for private owners and instructors. It is not > intended for those involved in commercial flying such as towing of banners & > gliders; aerial seeding, aerial spraying or dusting or other for-hire > operations except instruction. > > ALL APPLICATIONS ARE SUBJECT TO APPROVAL BY WILLIS. > > The USUA Airmen Registration Program is the oldest and most widely known and > accepted program in the United States. It has been imitated by subsequent > programs and has been used as a model for similar ultralight training > programs worldwide. Program costs are recovered through participation. > > No USUA member dues are taken from other programs to subsidize this program. > > > ANSWERS TO COMMON QUESTIONS > > HOW MUCH COVERAGE DO I GET? > Coverage subject to a deductible of $50 in respect of property damage each > accident > Bodily injury any one person any one accident-$100,000 USD: > Property damage any one accident-$1,000,000 USD: > Overall Combined Bodily injury and property damage shall not exceed any one > accident-$1,000,000 USD > > > WHY DO I WANT THIS INSURANCE COVERAGE? > This is the way you assure others that if you injure them or damage their > property you are financially able to pay for the damage you accidentally did > to them. Also, many state and municipal facilities employ financial > responsibility laws and require such coverage. > > Without this type of coverage, the cost of defense alone could significantly > impact your financial future. There is great value in knowing you have > protection in case of an unplanned event. Besides, the coverage is easy to > obtain and only costs a fraction of your vehicle/aircraft and yearly > operating expenses. > > > WHAT DOES THIRD PARTY LIABILITY MEAN? > When, through your flying activity, you injure someone or damage someone's > property but not a student or passenger or someone associated with the > operation of the vehicle/aircraft. > > > WHAT ARE THE REQUIREMENTS FOR MY VEHICLE/AIRCRAFT? > DEFINITION > Fixed or flexible wing, engine powered vehicle/aircraft [airplane or trike > configuration] of not more than 450 kilograms (992 U.S. pounds), which has a > power-off stall speed of not more than 35 knots calibrated airspeed (40 miles > per hour) at maximum gross weight including hang gliders but excluding > gliders. > > REGISTRATION AND MARKING > The Vehicle/Aircraft must be registered in any FAA recognized ultralight > vehicle registration program or registered with FAA. (Photocopy required if > not registered with USUA) > > > WHAT ARE THE REQUIREMENTS FOR ME? > IF FLYING A SINGLE-SEATER- > A person must be at least 16 years old and a registered ultralight pilot or > instructor with the appropriate category/class privileges in any FAA > recognized ultralight airman competency program. > > IF FLYING A TWO-SEATER- > One of the following: > 1) A USUA registered instructor need do nothing extra. > 2) Instructors in other FAA recognized programs must simply include a > photocopy of their ultralight instructor registration. > 3) FAA private pilot certificate or better with ultralight pilot > registration in any FAA recognized program. > > > CAN MORE THAN ONE PILOT BE NAMED ON A POLICY? > Yes. The standard policy allows two pilots to be named at no additional cost. > An unlimited additional number of pilots may be named on the same policy with > an additional premium of $25.75 ($25 plus 3% surplus lines tax) per pilot. > > > ARE INSTRUCTIONAL FLIGHTS COVERED? > Yes. > > > DOES THIS POLICY COVER DAMAGE TO MY VEHICLE/ AIRCRAFT OR INJURY TO MY STUDENT > OR PASSENGER? > No. The coverage only applies to people and property not associated with the > operation of the vehicle/aircraft. > > > HOW ABOUT STUDENT SOLO? > No. Solo flight by a student is not covered under this program. > > > I AM NOT A USUA MEMBER. CAN I GET THIS INSURANCE? > Yes, by joining USUA. Annual dues are a required portion of the insurance > application. In the case where a member asks and has a membership which is > valid beyond the insurance period, the requirement for renewal may be waived. > > > HOW MUCH DOES IT COST? > Only $154.50 per year ($150 plus 3% surplus lines tax). > > FOR AN APPLICATION CONTACT: > United States Ultralight Association > PO Box 667, Frederick, MD 21705 > Tel: (301) 695-9100, Fax: (301) 695-0763


July 22, 1999 - August 13, 1999

Kolb-Archive.digest.vol-bo